Service Information: Alexander Schleicher
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Publication Indexes • Service Bulletins • Service Information
Maintenance Instructions: All AS 33 Series AS 34Me ASG 29 (ASW 27-18) Series ASG 32 ASH 25 Series ASH 26 Series ASH 30Mi ASH 31Mi ASK 21 Series ASK 23 Series ASW 15 ASW 19 ASW 20 ASW 22 Series ASW 24 Series ASW 27 ASW 28 Series
Technical Notes: All AS 33Es AS 33Me AS 34Me AS-Propellers ASG 29 (ASW 27-18) ASG 29E (ASW 27-18E) ASG 32 ASH 25 ASH 25E/M/Mi ASH 26 ASH 26E ASH 30Mi ASH 31Mi ASK 13 ASK 14 ASK 16 ASK 18 ASK 21 ASK 21B ASK 21Mi ASK 23 Series ASW 12 ASW 15 ASW 17 ASW 19 ASW 20 ASW 22/B/BL ASW 22BE/BLE ASW 24 ASW 24E ASW 24TOP ASW 27 ASW 28-18E ASW 28/28-18 ASW 28B K10 K11 K7 K8 K9 Ka2/Ka2b Ka4 / Rhönlerche II Ka6
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI | en | Paint Cracks on Fiber Composite Gliders | 06/26/1989 | |
MI | en | Installation of Equipment Not Listed in Equipment List of AMM | 01/16/2008 | |
MI | en | Complete Dumping of Integrated (Wet) Water Ballast Tanks Inside Wings | 05/06/2002 | |
MI | de | Assembly and Dismantling Water Ballast Valves | 07/25/1994 | |
MI | en | Installation and Inspection Instruction for Flexible Fuel Tanks (Working Instruction No. 32) | 08/31/2017 | |
MI | de | Installation and Inspection Instruction for Flexible Fuel Tanks (Working Instruction No. 32) | 08/31/2017 | |
MI | de | Paint Cracks on Fiber Composite Gliders | 06/26/1989 | |
MI | en | Removal of Play between Lift Pins and Bushings at Fuselage-Wing-Junction | 06/19/1986 | |
MI | en | To Vent Oil Pump | 03/25/1997 | |
MI | de | To Vent Oil Pump | 03/25/1997 | |
MI | en | Assembly and Dismantling Water Ballast Valves | 07/25/1994 | |
MI | en | Adjusting Drive Belt | 08/27/2007 | |
MI | Iss 2 | de | Fuel Types | 11/01/2001 |
MI | Iss 2 | en | Removal of Play between Lift Pins and Bushings at Fuselage-Wing-Junction | 11/02/2020 |
MI | Iss 2 | de | Removal of Play between Lift Pins and Bushings at Fuselage-Wing-Junction | 11/02/2020 |
MI | Iss 2 | de | Installation of Equipment Not Listed in Equipment List of AMM | 04/25/2016 |
MI | Iss 2 | en | Fuel Types | 11/01/2001 |
MI | Iss 2 | en | Installation of Equipment Not Listed in Equipment List of AMM | 04/25/2016 |
MI | Iss 3 | en | Fire Protection Paint in Engine Compartment | 07/07/2022 |
MI | Iss 3 | de | Fire Protection Paint in Engine Compartment | 07/07/2022 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI A | en | Replacing Elastic Fairing Tape at Control Surface Gaps and at Gaps of Engine Compartment Doors. Installing and Replacing Turbulators on Wings and Vertical Tail | 08/25/2020 | |
MI A | Iss 2 | en | Replacing Elastic Fairing Tape at Control Surface Gaps and at Gaps of Engine Compartment Doors. Installing and Replacing Turbulators on Wings and Vertical Tail | 09/16/2021 |
MI A | Iss 2 | de | Replacing Elastic Fairing Tape at Control Surface Gaps and at Gaps of Engine Compartment Doors. Installing and Replacing Turbulators on Wings and Vertical Tail | 09/16/2021 |
MI B | en | Repair Instruction if Overlap Joint of Fuselage in Cockpit Area has been Damaged because of Landings with Retracted Landing Gear | 08/25/2020 | |
MI B | de | Repair Instruction if Overlap Joint of Fuselage in Cockpit Area has been Damaged because of Landings with Retracted Landing Gear | 08/25/2020 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI A | en | Replacing Elastic Fairing Tape at Control Surface Gaps and at Gaps of Engine Compartment Doors. Installing and Replacing Turbulators on Wings and Vertical Tail | 02/04/2022 | |
MI A | de | Replacing Elastic Fairing Tape at Control Surface Gaps and at Gaps of Engine Compartment Doors. Installing and Replacing Turbulators on Wings and Vertical Tail | 02/04/2022 | |
MI B | en | Repair Instruction if Overlap Joint of Fuselage in Cockpit Area has been Damaged because of Landings with Retracted Landing Gear | 02/04/2022 | |
MI B | de | Repair Instruction if Overlap Joint of Fuselage in Cockpit Area has been Damaged because of Landings with Retracted Landing Gear | 02/04/2022 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI | en | Alternative Rim for Main Wheel | 06/01/2011 | |
MI | de | Alternative Rim for Main Wheel | 06/01/2011 | |
MI 389 | de | Damage of Fuselage in Overlap Joint Area Because of Belly Landings with Retracted Landing Gear | 12/17/2001 | |
MI 389 | en | Damage of Fuselage in Overlap Joint Area Because of Belly Landings with Retracted Landing Gear | 12/17/2001 | |
MI A | en | Replacing of Elastic Fairing Tapes (Elastic Lip Seal) at Control Surface Gaps of Aileron, Horizontal and Vertical Tail | 09/19/2007 | |
MI A | de | Replacing of Elastic Fairing Tapes (Elastic Lip Seal) at Control Surface Gaps of Aileron, Horizontal and Vertical Tail | 09/19/2007 | |
MI B | en | Turbulators (Zig-Zag-Tapes) for Wings, Winglets, Horizontal and Vertical Tail Planes | 09/19/2007 | |
MI B | Iss 2 | de | Turbulators (Zig-Zag-Tapes) for Wings, Winglets, Horizontal and Vertical Tail Planes | 11/20/2015 |
MI C | en | Adjustment of Actuation System for Water Ballast Valves | 09/19/2007 | |
MI C | de | Adjustment of Actuation System for Water Ballast Valves | 09/19/2007 | |
MI D | de | Repair of Tailcone by Scarfing | 09/19/2007 | |
MI D | en | Repair of Tailcone by Scarfing | 09/19/2007 | |
MI D | en | Adjustment of Air Brakes | 03/12/2002 | |
MI D | de | Adjustment of Air Brakes | 03/12/2002 | |
MI E | en | ASW27-18E Only: Replacement of Gas Spring or Spindle in Engine Bay | 09/01/2009 | |
MI E | de | ASW27-18E Only: Replacement of Gas Spring or Spindle in Engine Bay | 09/01/2009 | |
MI F | en | Performing an Engine Test Run on Ground | 09/03/2015 | |
MI F | de | Performing an Engine Test Run on Ground | 09/03/2015 | |
MI G | en | Dis- and Re-Assembling of Starter Motor; Adjusting Reference Position | 09/03/2015 | |
MI G | de | Dis- and Re-Assembling of Starter Motor; Adjusting Reference Position | 09/03/2015 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI | en | Equipped with Inspection Holes at Fuselage Underside; these will Allow Exchange of Spark Plugs with Power-Plant Still Mounted | 12/18/2015 | |
MI | de | Equipped with Inspection Holes at Fuselage Underside; these will Allow Exchange of Spark Plugs with Power-Plant Still Mounted | 12/18/2015 | |
MI | en | ASG 32 Mi Only: Exchange of Spark Plugs | 12/18/2015 | |
MI | de | ASG 32 Mi Only: Exchange of Spark Plugs | 12/18/2015 | |
MI | Iss 2 | de | Coloured Painting | 05/16/2018 |
MI | Iss 2 | en | Coloured Painting | 05/16/2018 |
MI | Iss 3 | de | Coloured Painting | 10/24/2023 |
MI | Iss 3 | en | Coloured Painting | 10/24/2023 |
MI A | Iss 4 | de | Replacing Elastic Fairing Tapes at Control Surface Gaps and on Engine Compartment Doors and Main Wheel Doors. Fixing and Replacing Turbulators on Wing, Winglets, Horizontal and Vertical Tail | 09/04/2018 |
MI A | Iss 4 | en | Replacing Elastic Fairing Tapes at Control Surface Gaps and on Engine Compartment Doors and Main Wheel Doors. Fixing and Replacing Turbulators on Wing, Winglets, Horizontal and Vertical Tail | 09/04/2018 |
MI B | de | Repair Instruction for Cockpit Area | 01/15/2016 | |
MI B | en | Repair Instruction for Cockpit Area | 01/15/2016 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI | de | ASH 25 Mi Only: Spark Plug Replacement with Engine Installed | 11/01/2001 | |
MI | de | ASH 25 Mi Only: Replacement of Spark Plugs | 03/01/2005 | |
MI | Iss 2 | en | ASH 25 Mi Only: Fuel Types | 11/01/2001 |
MI | Iss 2 | de | ASH 25 Mi Only: Fuel Types | 11/01/2001 |
MI 858 | en | ASH 25 E Only: Fire Protection Paint in Engine Compartment | 10/20/1988 | |
MI 858 | de | ASH 25 E Only: Fire Protection Paint in Engine Compartment | 10/20/1988 | |
MI A | Iss 2 | en | Fixing for First Time or Replacing Plastic Fairing Tape (Elastic Lip Seal) at Control Surface Gaps at Wing (Upper and Lower Surfaces), at Horizontal Tailplane (Upper Surface) and Vertical Tailplane (Left & Right) | 02/28/1990 |
MI A | Iss 3 | de | Fixing for First Time or Replacing Plastic Fairing Tape (Elastic Lip Seal) at Control Surface Gaps at Wing (Upper and Lower Surfaces), at Horizontal Tailplane (Upper Surface) and Vertical Tailplane (Left & Right) | 11/01/2001 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI | de | Alternative Rim for Main Wheel | 06/01/2011 | |
MI | en | Alternative Rim for Main Wheel | 06/01/2011 | |
MI | de | ASH 26E Only: Replacement of Spark Plugs | 03/01/2005 | |
MI | Iss 2 | en | ASH 26E Only: Fuel Types | 11/01/2001 |
MI | Iss 2 | de | ASH 26E Only: Fuel Types | 11/01/2001 |
MI A | en | Replacing Plastic Fairing Tape (Elastic Lipseal) at Control Surface Gaps of Aileron, Horizontal & Vertical Tail and Flaps | 07/31/1995 | |
MI A | Iss 3 | en | Replacing Plastic Fairing Tape (Elastic Lipseal) at Control Surface Gaps of Aileron, Horizontal & Vertical Tail and Flaps | 06/26/2003 |
MI A | Iss 3 | de | Replacing Plastic Fairing Tape (Elastic Lipseal) at Control Surface Gaps of Aileron, Horizontal & Vertical Tail and Flaps | 06/26/2003 |
MI B | Iss 2 | en | ASH 26E Only: New Adjustment of Fuel Contents Indication of ILEC Engine Control Unit | 05/22/2005 |
MI B | Iss 2 | en | ASH 26E Only: New Adjustment of Fuel Contents Indication of ILEC Engine Control Unit | 05/22/2005 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI | en | Exchange of Spark Plugs | 12/18/2015 | |
MI | de | Exchange of Spark Plugs | 12/18/2015 | |
MI A | en | Replacing Elastic Fairing Tapes at Control Surface Gaps & at Gaps of Engine Compartment Doors. Replacing Turbulators on Winglets, Wingtips, Horizontal & Vertical Tail | 12/18/2015 | |
MI A | de | Replacing Elastic Fairing Tapes at Control Surface Gaps & at Gaps of Engine Compartment Doors. Replacing Turbulators on Winglets, Wingtips, Horizontal & Vertical Tail | 12/18/2015 | |
MI B | de | Repair Instruction for Cockpit Area | 12/18/2015 | |
MI B | en | Repair Instruction for Cockpit Area | 12/18/2015 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI | de | Exchange of Spark Plugs | 10/01/2011 | |
MI | en | Exchange of Spark Plugs | 10/01/2011 | |
MI A | Iss 2 | de | Replacing Elastic Fairing Tape at Control Surface Gaps of Vertical & Horizontal Tail, Aileron, Flaps & at Gaps of Engine Bay Doors. Position of Turbulators on Wing, Horizontal & Vertical Tail & Wing-Lets | 03/16/2015 |
MI A | Iss 2 | en | Replacing Elastic Fairing Tape at Control Surface Gaps of Vertical & Horizontal Tail, Aileron, Flaps & at Gaps of Engine Bay Doors. Position of Turbulators on Wing, Horizontal & Vertical Tail & Wing-Lets | 03/16/2015 |
MI B | en | Repair Instruction for Cockpit Area | 10/01/2011 | |
MI B | de | Repair Instruction for Cockpit Area | 10/01/2011 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI | de | ASK 21Mi Only: Spark Plug Replacement with Engine Installed | 12/01/2007 | |
MI | de | Locking of Canopy Emergency Jettison Lever (Front Cockpit) | 12/20/2018 | |
MI | de | Alternative Rim for Main Wheel | 06/01/2010 | |
MI | en | Alternative Rim for Main Wheel | 06/01/2010 | |
MI | en | Locking of Canopy Emergency Jettison Lever (Front Cockpit) | 12/20/2018 | |
MI A | en | ASK 21B Only: Re-Adjusting Airbrakes | 06/15/2018 | |
MI A | de | ASK 21B Only: Re-Adjusting Airbrakes | 06/15/2018 | |
MI A | en | Re-Adjusting Airbrakes | 03/23/1987 | |
MI A | de | Re-Adjusting Airbrakes | 03/23/1987 | |
MI A | de | ASK 21Mi Only: Installing or Renewing Elastic Covers on Engine Compartment Lids | 12/01/2007 | |
MI B | en | ASK 21B Only: Installation of Oversize Drag Pins on Rear Wing Connection | 06/15/2018 | |
MI B | en | Installation of Oversize Drag Pins on Rear Wing Connection | 07/04/1990 | |
MI B | Iss 2 | en | Installation of Oversize Drag Pins on Rear Wing Connection | 09/17/2018 |
MI B | Iss 3 | en | ASK 21B Only: Installation of Oversize Drag Pins on Rear Wing Connection | 01/07/2021 |
MI B | Iss 3 | de | ASK 21B Only: Installation of Oversize Drag Pins on Rear Wing Connection | 01/07/2021 |
MI B | Iss 3 | en | Installation of Oversize Drag Pins on Rear Wing Connection | 01/07/2021 |
MI B | Iss 3 | de | Installation of Oversize Drag Pins on Rear Wing Connection | 01/07/2021 |
MI C | en | Installing or Replacing Elastic Fairing Tape at Control Surface Gaps of Aileron and Elevator and Optional on Rudder | 05/07/1992 | |
MI C | de | Installing or Replacing Elastic Fairing Tape at Control Surface Gaps of Aileron and Elevator and Optional on Rudder | 05/07/1992 | |
MI C | Iss 2 | en | ASK 21B Only: Installing or Replacing Elastic Fairing Tape at Control Surface Gaps of Aileron and Elevator and Optional on Rudder | 09/14/2020 |
MI C | Iss 2 | de | ASK 21B Only: Installing or Replacing Elastic Fairing Tape at Control Surface Gaps of Aileron and Elevator and Optional on Rudder | 09/14/2020 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI A | en | Adjusting Ailerons | 12/11/1985 | |
MI A | de | Adjusting Ailerons | 12/11/1985 | |
MI B | en | Repair of Main Bulkhead II | 01/17/1990 | |
MI B | de | Repair of Main Bulkhead II | 01/17/1990 | |
MI C | de | Inspection, Removal & Reinstallation of Bumper III of Height Control | 02/20/2003 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI B | en | Skin - Spar Delamination at Port Wing Root | 10/29/1974 | |
MI B | de | Skin - Spar Delamination at Port Wing Root | 10/29/1974 | |
MI C | en | Installation of Aileron-Control-Crank in Fuselage Not Symmetric | 08/22/1973 | |
MI C | de | Installation of Aileron-Control-Crank in Fuselage Not Symmetric | 08/22/1973 | |
MI D | en | Installation of Aileron Control Bellcrank in Fuselage Non-Symmetric | 09/16/1974 | |
MI D | de | Installation of Aileron Control Bellcrank in Fuselage Non-Symmetric | 09/16/1974 | |
MI E | en | Elimination of Stiffness in Aileron Control Circuit Nylon Guides | 12/17/1974 | |
MI E | de | Elimination of Stiffness in Aileron Control Circuit Nylon Guides | 12/17/1974 | |
MI F | de | Replacing of Actuating Pins at Pendulum Tailplane | 02/12/1977 | |
MI G | en | Inspection of Root Ribs at Wings for Damages | 06/28/2021 | |
MI G | de | Inspection of Root Ribs at Wings for Damages | 06/28/2021 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI A | de | Maintenance & Improvement of Wheel Brake | 01/17/1978 | |
MI A | en | Maintenance & Improvement of Wheel Brake | 01/17/1978 | |
MI B | de | Correction of Lateral Stability | 03/01/1978 | |
MI B | en | Correction of Lateral Stability | 03/01/1978 | |
MI C | en | Adjustment of Airbrake | 02/15/1979 | |
MI C | de | Adjustment of Airbrake | 02/15/1979 | |
MI E | de | Adaptation of Cockpit to Extreme Pilot Sizes | 06/28/1979 | |
MI F | en | Replacement of a Wing | 07/15/1980 | |
MI G | de | Installation of Turnpoint Camera | 01/13/1981 | |
MI G | en | Installation of Turnpoint Camera | 01/13/1981 | |
MI H | en | Adjusting Towhook After an Unintentional Release | 08/30/1981 | |
MI H | de | Adjusting Towhook After an Unintentional Release | 08/30/1981 | |
MI I | de | Exchange of Fourth Elevator Pushrod in Fuselage | 01/26/1990 | |
MI I | en | Exchange of Fourth Elevator Pushrod in Fuselage | 01/26/1990 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI A | de | Maintenance & Improvement of Wheel Brake | 01/17/1978 | |
MI A | en | Maintenance & Improvement of Wheel Brake | 01/17/1978 | |
MI C | en | Adjustment of Airbrake | 02/15/1979 | |
MI C | de | Adjustment of Airbrake | 02/15/1979 | |
MI E | de | Adaptation of Cockpit to Extreme Pilot Sizes | 06/28/1979 | |
MI F | en | Replacement of a Wing | 07/15/1980 | |
MI G | en | Installation of Turnpoint Camera | 01/13/1981 | |
MI G | de | Installation of Turnpoint Camera | 01/13/1981 | |
MI H | en | Adjusting Towhook After an Unintentional Release | 08/30/1981 | |
MI H | de | Adjusting Towhook After an Unintentional Release | 08/30/1981 | |
MI L | de | Exchange of Fourth Elevator Pushrod in Fuselage | 01/26/1990 | |
MI L | en | Exchange of Fourth Elevator Pushrod in Fuselage | 01/26/1990 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI 834 | de | ASW 22BE Only: Fire Protection Paint in Engine Compartment | 10/20/1988 | |
MI 834 | en | ASW 22BE Only: Fire Protection Paint in Engine Compartment | 10/20/1988 | |
MI A | Iss 2 | de | Fixing for First Time or Replacing Plastic Fairing Tape (Elastic Lip Seal) at Control Surface Gaps at Wing (Upper and Lower Surfaces), at Horizontal Tailplane (Upper Surface) and Vertical Tailplane (Left & Right). Positions of Zig-Zag Tapes and Blow Turbulators | 02/28/1990 |
MI A | Iss 2 | en | Fixing for First Time or Replacing Plastic Fairing Tape (Elastic Lip Seal) at Control Surface Gaps at Wing (Upper and Lower Surfaces), at Horizontal Tailplane (Upper Surface) and Vertical Tailplane (Left & Right). Positions of Zig-Zag Tapes and Blow Turbulators | 02/28/1990 |
MI A | Iss 3 | de | Fixing for First Time or Replacing Plastic Fairing Tape (Elastic Lip Seal) at Control Surface Gaps at Wing (Upper and Lower Surfaces), at Horizontal Tailplane (Upper Surface) and Vertical Tailplane (Left & Right). Positions of Zig-Zag Tapes and Blow Turbulators | 01/15/2002 |
MI A | Iss 3 | en | Fixing for First Time or Replacing Plastic Fairing Tape (Elastic Lip Seal) at Control Surface Gaps at Wing (Upper and Lower Surfaces), at Horizontal Tailplane (Upper Surface) and Vertical Tailplane (Left & Right). Positions of Zig-Zag Tapes and Blow Turbulators | 01/15/2002 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI | en | Alternative Rim for Main Wheel | 06/01/2011 | |
MI | de | Alternative Rim for Main Wheel | 06/01/2011 | |
MI 859 | en | ASW 24E Only: Fire Protection Paint in Engine Compartment | 10/20/1988 | |
MI 859 | de | ASW 24E Only: Fire Protection Paint in Engine Compartment | 10/20/1988 | |
MI A | en | Replacing Plastic Fairing Tape (Elastic Lipseal) at Control Surface Gaps of Aileron and Horizontal and Vertical Tail | 02/05/1990 | |
MI A | de | Replacing Plastic Fairing Tape (Elastic Lipseal) at Control Surface Gaps of Aileron and Horizontal and Vertical Tail | 02/05/1990 | |
MI B | de | Fixing or Replacing Turbulators on Wing, Horizontal and Vertical Tail | 02/07/1990 | |
MI B | en | Fixing or Replacing Turbulators on Wing, Horizontal and Vertical Tail | 02/07/1990 | |
MI C | en | Repair of Landing Gear Box | 04/26/1990 | |
MI C | de | Repair of Landing Gear Box | 04/26/1990 | |
MI D | de | Installation of Airbrake and Aileron Quadrant Bellcranks Including FRP Basis Plate into Wing Root Rib | 12/02/1992 | |
MI D | en | Installation of Airbrake and Aileron Quadrant Bellcranks Including FRP Basis Plate into Wing Root Rib | 12/02/1992 | |
MI E | de | Repair of Fuselage by Scarfing | 03/28/1996 | |
MI E | en | Repair of Fuselage by Scarfing | 03/28/1996 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI | de | Alternative Rim for Main Wheel | 06/01/2011 | |
MI | en | Alternative Rim for Main Wheel | 06/01/2011 | |
MI 290.99.0002 | Iss 2 | en | Adjustment of Actuation System for Water Ballast Valves | 10/25/2023 |
MI 290.99.0002 | Iss 2 | de | Adjustment of Actuation System for Water Ballast Valves | 10/25/2023 |
MI 389 | de | Damage of Fuselage in Overlap Joint Area Because of Belly Landings with Retracted Landing Gear | 12/17/2001 | |
MI 389 | en | Damage of Fuselage in Overlap Joint Area Because of Belly Landings with Retracted Landing Gear | 12/17/2001 | |
MI A | de | Replacing of Elastic Fairing Tapes (Elastic Lipseal) at Control Surface Gaps of Aileron, Horizontal and Vertical Tail, and Flaps as Well as of ZZ-Turbulator Tapes | 01/20/1997 | |
MI A | en | Replacing of Elastic Fairing Tapes (Elastic Lipseal) at Control Surface Gaps of Aileron, Horizontal and Vertical Tail, and Flaps as Well as of ZZ-Turbulator Tapes | 01/20/1997 | |
MI B | Iss 2 | de | Adjustment of Water Ballast Actuation Inside Fuselage | 05/04/1999 |
MI B | Iss 2 | en | Adjustment of Water Ballast Actuation Inside Fuselage | 05/04/1999 |
MI C | en | Repair of Fuselage by Scarfing | 04/07/1997 | |
MI C | de | Repair of Fuselage by Scarfing | 04/07/1997 | |
MI D | en | Adjustment of Air Brakes | 03/12/2002 | |
MI D | de | Adjustment of Air Brakes | 03/12/2002 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
MI | de | Complete Dumping of Integrated (Wet) Water Ballast Tanks Inside Wings | 05/06/2002 | |
MI | en | Alternative Rim for Main Wheel | 06/01/2011 | |
MI | en | Complete Dumping of Integrated (Wet) Water Ballast Tanks Inside Wings | 05/06/2002 | |
MI | de | Alternative Rim for Main Wheel | 06/01/2011 | |
MI 423 | en | Check of Safety of Aileron Hinge Pins | 09/05/2001 | |
MI 423 | de | Check of Safety of Aileron Hinge Pins | 09/05/2001 | |
MI 423 | en | Damage of Fuselage in Overlap Joint Area Because of Belly Landings with Retracted Landing Gear | 12/17/2001 | |
MI 423 | de | Damage of Fuselage in Overlap Joint Area Because of Belly Landings with Retracted Landing Gear | 12/17/2001 | |
MI A | en | ASW 28B Only: Replacing Elastic Fairing Tapes at Control Surface Gaps. Installing & Replacing Turbulators on Wings, Horizontal & Vertical Tail | 02/01/2022 | |
MI A | de | ASW 28B Only: Replacing Elastic Fairing Tapes at Control Surface Gaps. Installing & Replacing Turbulators on Wings, Horizontal & Vertical Tail | 02/01/2022 | |
MI A | de | ASW 28-18 Only: Replacing of Elastic Fairing Tapes (Elastic Lip Seal) at Control Surface Gaps of Aileron, Horizontal and Vertical Tail | 05/14/2004 | |
MI A | en | ASW 28-18 Only: Replacing of Elastic Fairing Tapes (Elastic Lip Seal) at Control Surface Gaps of Aileron, Horizontal and Vertical Tail | 05/14/2004 | |
MI A | de | Replacing of Elastic Fairing Tapes (Elastic Lip Seal) at Control Surface Gaps of Aileron, Horizontal and Vertical Tail | 07/02/2001 | |
MI A | en | Replacing of Elastic Fairing Tapes (Elastic Lip Seal) at Control Surface Gaps of Aileron, Horizontal and Vertical Tail | 07/02/2001 | |
MI B | de | Turbulators (Zig-Zag-Tapes) for Winglets, Horizontal and Vertical Tail Planes | 07/02/2001 | |
MI B | en | Turbulators (Zig-Zag-Tapes) for Winglets, Horizontal and Vertical Tail Planes | 07/02/2001 | |
MI B | en | ASW 28-18 Only: Turbulators (Zig-Zag-Tapes) for Winglets, Horizontal and Vertical Tail Planes | 05/14/2004 | |
MI B | de | ASW 28-18 Only: Turbulators (Zig-Zag-Tapes) for Winglets, Horizontal and Vertical Tail Planes | 05/14/2004 | |
MI B | en | ASW 28B Only: Repair Instruction if Overlap Joint of Fuselage in Cockpit Area has been Damaged because of Landings with Retracted Landing Gear | 02/01/2022 | |
MI B | de | ASW 28B Only: Repair Instruction if Overlap Joint of Fuselage in Cockpit Area has been Damaged because of Landings with Retracted Landing Gear | 02/01/2022 | |
MI C | de | Adjustment of Water Ballast Actuation Inside Fuselage | 07/02/2001 | |
MI C | en | Adjustment of Water Ballast Actuation Inside Fuselage | 07/02/2001 | |
MI D | en | Tail Wheel Fairing | 05/07/2002 | |
MI D | de | Tail Wheel Fairing | 05/07/2002 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
PL 320.99.0001 | en | ASG 32 / ASG 32Mi / ASG 32El | ||
PL 335.99.0001 | en | AS 33Me | ||
PL 336.99.0001 | en | AS 33Es | ||
PL 340.99.0001 | Iss 2 | en | AS 34Me | |
PL ASG29 | de | ASG 29 (ASW 27-18) | 04/01/2011 | |
PL ASG29 | de | ASG 29E (ASW 27-18E) | 09/01/2014 | |
PL ASG29 | en | ASG 29E (ASW 27-18E) | 09/01/2014 | |
PL ASH25 | en | ASH 25E, ASH 25M | 05/01/2005 | |
PL ASH25 | de | ASH 25E, ASH 25M | 05/01/2005 | |
PL ASH25 | en | ASH 25 | 05/01/2005 | |
PL ASH25 | de | ASH 25 | 05/01/2005 | |
PL ASH26 | de | ASH 26E | 05/01/2005 | |
PL ASH26 | en | ASH 26E | 05/01/2005 | |
PL ASH26 | de | ASH 26 | 05/01/2005 | |
PL ASH26 | en | ASH 26 | 05/01/2005 | |
PL ASH30Mi | en | ASH 30Mi | 05/01/2005 | |
PL ASH30Mi | de | ASH 30Mi | 05/01/2005 | |
PL ASH31Mi | de | ASH 31Mi | 05/01/2005 | |
PL ASH31Mi | en | ASH 31Mi | 05/01/2005 | |
PL ASK13 | de | ASK 13 | 03/01/2006 | |
PL ASK13 | en | ASK 13 | 03/01/2006 | |
PL ASK14 | de | ASK 14 | 05/01/2005 | |
PL ASK14 | en | ASK 14 | 05/01/2005 | |
PL ASK16 | en | ASK 16 | 05/01/2005 | |
PL ASK16 | de | ASK 16 | 05/01/2005 | |
PL ASK18 | de | ASK 18 | 05/01/2005 | |
PL ASK18 | en | ASK 18 | 05/01/2005 | |
PL ASK21 | en | ASK 21 | 03/01/2013 | |
PL ASK21 | en | ASK 21Mi | 05/01/2015 | |
PL ASK21 | de | ASK 21Mi | 05/01/2015 | |
PL ASK21B | en | ASK 21B | 05/01/2005 | |
PL ASK21B | de | ASK 21B | 05/01/2005 | |
PL ASK23 | de | ASK 23 | 05/01/2005 | |
PL ASK23 | en | ASK 23 | 05/01/2005 | |
PL ASW12 | de | ASW 12 | 05/01/2005 | |
PL ASW15 | de | ASW 15 | 05/01/2005 | |
PL ASW15 | en | ASW 15 | 05/01/2005 | |
PL ASW17 | en | ASW 17 | 05/01/2005 | |
PL ASW17 | de | ASW 17 | 05/01/2005 | |
PL ASW19 | de | ASW 19 | 05/01/2005 | |
PL ASW19 | en | ASW 19 | 05/01/2005 | |
PL ASW20 | de | ASW 20 | 05/01/2005 | |
PL ASW20 | en | ASW 20 | 05/01/2005 | |
PL ASW22 | de | ASW 22/B/BL | 05/01/2005 | |
PL ASW22 | en | ASW 22/B/BL | 05/01/2005 | |
PL ASW22 | en | ASW 22M/BE/BLE | 05/01/2005 | |
PL ASW22 | de | ASW 22M/BE/BLE | 05/01/2005 | |
PL ASW24 | de | ASW 24TOP | 05/01/2005 | |
PL ASW24 | en | ASW 24E | 04/01/2011 | |
PL ASW24 | de | ASW 24E | 04/01/2011 | |
PL ASW24 | en | ASW 24 | 04/01/2011 | |
PL ASW24 | de | ASW 24 | 04/01/2011 | |
PL ASW27 | en | ASW 27 | 04/01/2011 | |
PL ASW27 | de | ASW 27 | 04/01/2011 | |
PL ASW28 | en | ASW 28B | 05/01/2005 | |
PL ASW28 | de | ASW 28B | 05/01/2005 | |
PL ASW28 | en | ASW 28-18E | 09/01/2014 | |
PL ASW28 | de | ASW 28-18E | 09/01/2014 | |
PL ASW28 | de | ASW 28/28-18 | 04/01/2011 | |
PL K7 | de | K7 | 05/01/2005 | |
PL K8 | en | K8 | 03/01/2006 | |
PL K8 | de | K8 | 03/01/2006 | |
PL K10 | de | K10 | 05/01/2005 | |
PL K11 | de | K11 | ||
PL Ka2 | de | Ka2 / Ka2b | 11/15/2012 | |
PL Ka4 | de | Ka4 - Rhönlerche II | 05/01/2005 | |
PL Ka6 | en | Ka6 | 05/01/2005 | |
PL Ka6 | de | Ka6 | 05/01/2005 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
SB 32.110/25/1 | en | Propeller Blade Airfoil Thickness | 10/29/2001 | |
SB 4603-10 | en | Maintenance of Engine - "SOLO 2 350" | 07/19/2001 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
SI 99-099-0001-00 | en | Additional Engine Oils for Rotary Engine AE50R Series | 10/10/2024 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN | de | Carbon Push Rods Replacing Aluminum Alloy Push Rods in Aileron & Flap Control Circuits Inside Wings | 06/30/1999 | |
TN | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN | en | Carbon Push Rods Replacing Aluminum Alloy Push Rods in Aileron & Flap Control Circuits Inside Wings | 06/30/1999 | |
TN 01-99 | de | New Resin System for Laminating Glass, Carbon and Aramid Fiber Cloth | 03/12/1999 | |
TN 01-99 | en | New Resin System for Laminating Glass, Carbon and Aramid Fiber Cloth | 03/12/1999 | |
TN 01-2002 | de | Installation of Solar Cells (Modules) to Improve Power Supply | 07/12/2002 | |
TN 01-2005 | de | Use of Rigid Foam According to Material Specification 5.1460.2 | 02/24/2005 | |
TN 01-2008 | de | FPM-ECO DIN 73379 - 3E Fuel Hoses Replace Previous Rubber Hoses | 06/30/2008 | |
TN 01-2013 | en | Replacement of Sandwich-Core U-PICAMAT through Lantor LRC Soric | 05/01/2013 | |
TN 01-2013 | de | Replacement of Sandwich-Core U-PICAMAT through Lantor LRC Soric | 05/01/2013 | |
TN 01-2020 | en | Replacement for Polyester Fleece PKM 80, Molton or Flanell 406 | 04/15/2020 | |
TN 01-2020 | Iss 2 | en | Replacement for Polyester Fleece PKM 80, Molton or Flanell 406 | 12/04/2020 |
TN 01-2020 | Iss 2 | de | Replacement for Polyester Fleece PKM 80, Molton or Flanell 406 | 12/04/2020 |
TN 01-2020 | Iss 3 | en | Replacement for Polyester Fleece PKM 80, Molton or Flanell 406 | 02/21/2023 |
TN 01-2020 | Iss 3 | de | Replacement for Polyester Fleece PKM 80, Molton or Flanell 406 | 02/21/2023 |
TN 02-99 | en | New Finish for Glass Fiber Cloth | 03/15/1999 | |
TN 02-99 | Iss 2 | en | New Finish for Glass Fiber Cloth | 06/08/2011 |
TN 02-99 | Iss 3 | de | New Finish for Glass Fiber Cloth | 12/04/2020 |
TN 02-99 | Iss 3 | en | New Finish for Glass Fiber Cloth | 12/04/2020 |
TN 02-99 | Iss 4 | en | New Finish for Glass Fiber Cloth | 02/21/2023 |
TN 02-99 | Iss 4 | de | New Finish for Glass Fiber Cloth | 02/21/2023 |
TN 02-2005 | de | Approved Repair Procedures According to EU-VO 1702/2003, Part 21, Section M | 05/24/2005 | |
TN 02-2005 | en | Approved Repair Procedures According to EU-VO 1702/2003, Part 21, Section M | 05/24/2005 | |
TN 02-2008 | en | Instruction for Installations of Equipment ((MI)) | 01/16/2008 | |
TN 02-2008 | Iss 2 | en | Instruction for Installations of Equipment | 04/25/2016 |
TN 02-2008 | Iss 3 | de | Instruction for Installations of Equipment | 12/04/2020 |
TN 02-2008 | Iss 3 | en | Instruction for Installations of Equipment | 12/04/2020 |
TN 02-2008 | Iss 4 | en | Instruction for Installations of Equipment ((MI II, Annex II)) | 02/21/2023 |
TN 02-2008 | Iss 4 | de | Instruction for Installations of Equipment ((MI II, Annex II)) | 02/21/2023 |
TN 02-2013 | en | Carbon Fibre Cloth with Fibre Type Pyrofil TR30S 3K | 05/01/2013 | |
TN 02-2013 | Iss 2 | en | Carbon Fibre Cloth with Fibre Type Pyrofil TR30S 3K | 12/04/2020 |
TN 02-2013 | Iss 2 | de | Carbon Fibre Cloth with Fibre Type Pyrofil TR30S 3K | 12/04/2020 |
TN 02-2013 | Iss 3 | en | Carbon Fibre Cloth with Fibre Type Pyrofil TR30S 3K | 02/21/2023 |
TN 02-2013 | Iss 3 | de | Carbon Fibre Cloth with Fibre Type Pyrofil TR30S 3K | 02/21/2023 |
TN 02-2020 | en | Installation of AIR Control Display 57 (ACD-57) as Primary Altimeter | 11/19/2020 | |
TN 02-2020 | Iss 2 | en | Installation of AIR Control Display 57 (ACD-57) as Primary Altimeter | 02/21/2023 |
TN 02-2020 | Iss 2 | de | Installation of AIR Control Display 57 (ACD-57) as Primary Altimeter | 02/21/2023 |
TN 03-99 | en | New Material Specifications for Copper-Zinc Alloys (Formerly Brass) | 03/26/1999 | |
TN 03-99 | de | New Material Specifications for Copper-Zinc Alloys (Formerly Brass) | 03/26/1999 | |
TN 03-2008 | en | Fibres of the Type EC9 756 P109 Replace the Fibres Previously Used for Glass Fibre Spar Caps | 02/12/2008 | |
TN 03-2008 | de | Fibres of the Type EC9 756 P109 Replace the Fibres Previously Used for Glass Fibre Spar Caps | 02/12/2008 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | en | Expansion of Flight-Envelope | 03/09/2021 | |
TN 1 | de | Expansion of Flight-Envelope | 03/09/2021 | |
TN 2 | en | Installation of a Fuel Tank Extension | 03/09/2021 | |
TN 2 | de | Installation of a Fuel Tank Extension | 03/09/2021 | |
TN 3 | de | Battery Holder Version 2 in Baggage Compartment ((FM)) | 04/28/2021 | |
TN 3 | en | Battery Holder Version 2 in Baggage Compartment ((FM)) | 04/28/2021 | |
TN 4 | en | 15m Outer Wings | 11/16/2021 | |
TN 4 | Iss 2 | de | 15m Outer Wings ((FM)) | 01/03/2022 |
TN 4 | Iss 2 | en | 15m Outer Wings ((FM)) | 01/03/2022 |
TN 5 | de | Wing Tip Wheels | 03/08/2023 | |
TN 5 | en | Wing Tip Wheels | 03/08/2023 | |
TN 6 | en | Push Rod End Bearings Aileron Control | 02/06/2023 | |
TN 6 | Iss 2 | en | Push Rod End Bearings Aileron Control | 03/08/2023 |
TN 6 | Iss 2 | de | Push Rod End Bearings Aileron Control | 03/08/2023 |
TN 8 | en | Revision of AMM ((MM)) | 08/07/2023 | |
TN 8 | de | Revision of AMM ((MM)) | 08/07/2023 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | en | Alternative Battery Cells for Propulsion Battery | 11/01/2022 | |
TN 1 | de | Alternative Battery Cells for Propulsion Battery | 11/01/2022 | |
TN 2 | de | Revision of AMM ((MM)) | 08/07/2023 | |
TN 2 | en | Revision of AMM ((MM)) | 08/07/2023 | |
TN 3 | de | Approved Software Versions | 11/01/2023 | |
TN 3 | en | Approved Software Versions | 11/01/2023 | |
TN 5 | en | Improved PRS Cooling | 02/07/2025 | |
TN 5 | de | Improved PRS Cooling | 02/07/2025 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Alternative Battery Cells for Propulsion Battery ((FM)) | 10/01/2022 | |
TN 1 | en | Alternative Battery Cells for Propulsion Battery ((FM)) | 10/01/2022 | |
TN 3 | en | Revision of AMM ((MM)) | 08/07/2023 | |
TN 3 | de | Revision of AMM ((MM)) | 08/07/2023 | |
TN 4 | en | Approved Software Versions | 11/01/2023 | |
TN 4 | de | Approved Software Versions | 11/01/2023 | |
TN 6 | en | Installation of Steerable Tailwheel ((FM)) | 10/01/2024 | |
TN 6 | de | Installation of Steerable Tailwheel ((FM)) | 10/01/2024 | |
TN 7 | de | Improved PRS Cooling | 02/07/2025 | |
TN 7 | en | Improved PRS Cooling | 02/07/2025 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Denomination of Propellers | 02/27/2009 | |
TN 2 | Iss 2 | en | General Information about Service Life Limitations | 01/15/2009 |
TN 2 | Iss 3 | en | General Information about Service Life Limitations | 03/13/2020 |
TN 2 | Iss 4 | en | General Information about Service Life Limitations | 03/24/2022 |
TN 2 | Iss 4 | de | General Information about Service Life Limitations | 03/24/2022 |
TN 3 | Iss 2 | de | Modification of Laminating Scheme - Repair in Case of Delamination in Glue Joint Close to Hub According to Modified Laminating Scheme | 09/01/2009 |
TN 6 | en | Product Improvement & Change; Amendments to AFM, AMM & RM | 05/16/2000 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | en | Modification of a Glider ASG 29 According to TCDS EASA A.220 into Powered Sailplane ASG 29E Under Same Data Sheet | 02/28/2008 | |
TN 1 | de | Modification of a Glider ASG 29 According to TCDS EASA A.220 into Powered Sailplane ASG 29E Under Same Data Sheet | 02/28/2008 | |
TN 2 | de | Installation of a PCB-Transponder Antenna in Vertical Tail | 01/30/2009 | |
TN 2 | en | Installation of a PCB-Transponder Antenna in Vertical Tail | 01/30/2009 | |
TN 3 | en | Installation of Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 3 | de | Installation of Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 4 | de | Installation of Cockpit Vent Behind Canopy Frame ((FM)) | 03/01/2011 | |
TN 4 | en | Installation of Cockpit Vent Behind Canopy Frame ((FM)) | 03/01/2011 | |
TN 6 | de | A) Installation of Tail Wheel Cover; B) Installation of Covers on Rudder; C) Replacement of Covers on Aileron & Flap Actuators; D) Modification of Blow Hole System ((MM, MI)) | 11/20/2015 | |
TN 6 | en | A) Installation of Tail Wheel Cover; B) Installation of Covers on Rudder; C) Replacement of Covers on Aileron & Flap Actuators; D) Modification of Blow Hole System, Maintenance Instruction B Iss2 ((MM, MI)) | 11/20/2015 | |
TN 7 | en | Alternative Hydraulic Wheel Brake System TOST | 02/01/2017 | |
TN 7 | de | Alternative Hydraulic Wheel Brake System TOST | 02/01/2017 | |
TN 8 | en | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 8 | de | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 9 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 | |
TN 9 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Installation of Spring, Supporting Power-Plant Extension | 04/29/2008 | |
TN 1 | en | Installation of Spring, Supporting Power-Plant Extension | 04/29/2008 | |
TN 2 | de | Installation of PCB-Transponder Antenna in Vertical Tail | 01/30/2009 | |
TN 2 | en | Installation of PCB-Transponder Antenna in Vertical Tail | 01/30/2009 | |
TN 3 | de | New Type of Propeller-Stopper | 11/06/2008 | |
TN 3 | en | New Type of Propeller-Stopper ((MM)) | 11/06/2008 | |
TN 4 | en | Installation of Propeller AS2F1-3 ((FM)) | 11/06/2008 | |
TN 4 | de | Installation of Propeller AS2F1-3 ((FM)) | 11/06/2008 | |
TN 5 | de | A) Different Cylinder Heads & Engine Bearer; B) Different Cable Routing Along Engine; C) Usage of Stepless Ear Clamps & Lock-Wire with PUR-Fuel Hoses ((MM)) | 02/18/2009 | |
TN 5 | en | A) Different Cylinder Heads & Engine Bearer; B) Different Cable Routing Along Engine; C) Usage of Stepless Ear Clamps & Lock-Wire with PUR-Fuel Hoses ((MM)) | 02/18/2009 | |
TN 6 | de | A) Measures to Prevent Power-Plant from Remaining Retracted; A1) Software Modification of Power-Plant Instrument; A2) Installation of Harder Stop; A3) Modification of Spiral Spring in Engine Compartment; B) Further Modifications in this Respect; B1) Modification of Gas-Spring; B2) Modification of Bushing on Top of Spindle ((MM)) | 09/09/2009 | |
TN 6 | en | A) Measures to Prevent Power-Plant from Remaining Retracted; A1) Software Modification of Power-Plant Instrument; A2) Installation of Harder Stop; A3) Modification of Spiral Spring in Engine Compartment; B) Further Modifications in this Respect; B1) Modification of Gas-Spring; B2) Modification of Bushing on Top of Spindle ((MM, MI)) | 09/09/2009 | |
TN 7 | de | Revision of Electric System of Power-Plant in Fuselage ((FM)) | 10/08/2011 | |
TN 7 | en | Revision of Electric System of Power-Plant in Fuselage ((MM, FM)) | 10/08/2011 | |
TN 8 | de | Installation of Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 8 | en | Installation of Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 10 | de | Two Piece Engine Bearer with Direct Attachment of Bing-Fuel Pump | 07/01/2014 | |
TN 10 | en | Two Piece Engine Bearer with Direct Attachment of Bing-Fuel Pump | 07/01/2014 | |
TN 11 | de | New Type of Fuel Pump According to SOLO Technical Note TM4603-15 | 07/01/2014 | |
TN 11 | en | New Type of Fuel Pump According to SOLO Technical Note TM4603-15 | 07/01/2014 | |
TN 12 | de | Retrofitting a New Type of Fuel Pump According to SOLO Technical Note TM4603-15, instead of Hitherto BING Fuel Pump | 07/01/2014 | |
TN 12 | en | Retrofitting a New Type of Fuel Pump According to SOLO Technical Note TM4603-15, instead of Hitherto BING Fuel Pump | 07/01/2014 | |
TN 13 | en | Change of Engine Controls and Installation of Starter | 09/03/2015 | |
TN 13 | de | Change of Engine Controls and Installation of Starter | 09/03/2015 | |
TN 14 | de | A) Installation of Tail Wheel Cover; B) Installation of Covers on Rudder; C) Replacement of Covers on Aileron & Flap Actuators; D) Modification of Blow Hole System (29Es MM, 29E MM, MI) | 11/20/2015 | |
TN 14 | en | A) Installation of Tail Wheel Cover; B) Installation of Covers on Rudder; C) Replacement of Covers on Aileron & Flap Actuators; D) Modification of Blow Hole System (29Es MM, 29E MM, MI) | 11/20/2015 | |
TN 15 | de | Replacement of Electric Decompression Valve ((MM)) | 07/01/2016 | |
TN 15 | en | Replacement of Electric Decompression Valve ((MM)) | 07/01/2016 | |
TN 16 | en | Alternative Hydraulic Wheel Brake System TOST | 02/01/2017 | |
TN 16 | de | Alternative Hydraulic Wheel Brake System TOST | 02/01/2017 | |
TN 17 | en | Specification Update of Flexible Fuel Tanks ((MM1, MM2)) | 09/15/2017 | |
TN 17 | de | Specification Update of Flexible Fuel Tanks ((MM1, MM2)) | ||
TN 18 | en | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 18 | de | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 19 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 | |
TN 19 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | en | Alternative Hydraulic Wheel Brake System TOST ((MM for 32, 32Mi)) | 07/01/2016 | |
TN 1 | de | Alternative Hydraulic Wheel Brake System TOST ((MM for 32, 32Mi)) | 07/01/2016 | |
TN 2 | de | Specification Update of Flexible Fuel Tanks ((MM)) | 09/15/2017 | |
TN 2 | en | Specification Update of Flexible Fuel Tanks ((MM)) | 09/15/2017 | |
TN 3 | en | Conversion of FAA Experimental C of A into FAA Standard C of A | 10/04/2017 | |
TN 4 | de | Amendment and Corrections of AFM & AMM | 10/31/2017 | |
TN 4 | en | Amendment and Corrections of AFM & AMM | 10/31/2017 | |
TN 5 | en | Improvement of Performance Map of New IAE50R-AA ECU with S/Ns "AE00XXX" which were Installed as Standard from 2014 Onwards | 05/22/2018 | |
TN 5 | de | Improvement of Performance Map of New IAE50R-AA ECU with S/Ns "AE00XXX" which were Installed as Standard from 2014 Onwards | 05/22/2018 | |
TN 6 | de | 1) Improvement of Liquid Cooling Temperature Display of ILEC Power-Plant Control Unit with an Instrument Diameter of 57mm; 2) Improved Assignment of Two Ignition Circuits to Corresponding Fuses | 05/22/2018 | |
TN 6 | en | 1) Improvement of Liquid Cooling Temperature Display of ILEC Power-Plant Control Unit with an Instrument Diameter of 57mm; 2) Improved Assignment of Two Ignition Circuits to Corresponding Fuses | 05/22/2018 | |
TN 7 | de | Zig-Zag Tape on Lower Wing Side Replaces Blow Holes ((MI)) | 09/04/2018 | |
TN 7 | en | Zig-Zag Tape on Lower Wing Side Replaces Blow Holes ((MI)) | 09/04/2018 | |
TN 8 | en | New Propeller AS2F1-5 ((FM)) | 05/15/2019 | |
TN 8 | de | New Propeller AS2F1-5 ((FM)) | 05/15/2019 | |
TN 9 | de | New Suspension Struts for Main Landing Gear | 11/30/2020 | |
TN 9 | en | New Suspension Struts for Main Landing Gear | 11/30/2020 | |
TN 10 | de | Conversion of Sailplane ASG 32 According TC EASA.A.599 to Powered Sailplane ASG 32 El According the Same TC | 01/22/2021 | |
TN 10 | en | Conversion of Sailplane ASG 32 According TC EASA.A.599 to Powered Sailplane ASG 32 El According the Same TC | 01/22/2021 | |
TN 11 | de | Introduction ASG 32 Mi | 08/23/2021 | |
TN 11 | en | Introduction ASG 32 Mi | 08/23/2021 | |
TN 12 | de | Sustainer Assisted Aerotow ((FM)) | 10/30/2021 | |
TN 12 | en | Sustainer Assisted Aerotow ((FM)) | 10/30/2021 | |
TN 13 | en | Bug Fix Power-Plant Instrument | 03/02/2023 | |
TN 13 | de | Bug Fix Power-Plant Instrument | 03/02/2023 | |
TN 14 | de | Revision of AMM (MM for 32, 32Mi, 32Ei) | 08/07/2023 | |
TN 14 | en | Revision of AMM (MM for 32, 32Mi, 32Ei) | 08/07/2023 | |
TN 15 | de | Alternative Rotor Cooling Air Intake Filter ((MM)) | 08/07/2023 | |
TN 15 | en | Alternative Rotor Cooling Air Intake Filter ((MM)) | 08/07/2023 | |
TN 16 | en | Introduction of Alternative Fuel Main Filter Due to End of Production of Existing One ((MM)) | 10/09/2023 | |
TN 16 | de | Introduction of Alternative Fuel Main Filter Due to End of Production of Existing One ((MM)) | 10/09/2023 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | en | Constructional Preparation of Fuselage of ASH25 for a More Simple Subsequent Retrofitting of Engine Unit when Converting Glider to Motorglider Versio | 04/08/1988 | |
TN 1 | de | Constructional Preparation of Fuselage of ASH25 for a More Simple Subsequent Retrofitting of Engine Unit when Converting Glider to Motorglider Version ((FM)) | 04/08/1988 | |
TN 2 | en | Aerodynamical Improvement Mod to Wingtips | 04/25/1989 | |
TN 2 | de | Aerodynamical Improvement Mod to Wingtips | 04/25/1989 | |
TN 3 | en | Constructional Modifications Applying to Factory Series Production | 01/31/1990 | |
TN 3 | de | Constructional Modifications Applying to Factory Series Production | 01/31/1990 | |
TN 4 | en | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 4 | de | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 5 | de | Installation of a Nose Tow Release Coupling ((MM)) | 10/10/1990 | |
TN 5 | en | Installation of a Nose Tow Release Coupling ((MM)) | 10/10/1990 | |
TN 6 | de | Inspecting Elevator Engaging Actuator (on Top of Fin) in Accordance with Instructions Given in Manuals. Revision to Manuals on those Parts Covering C.G. & Mass & Balance. Editorial Corrections in AFM & AMM. Fitting a 25A-Fuse into Battery Cable for Operational Battery in Baggage Compartment in Front of Spar ((MM)) | 02/28/1991 | |
TN 6 | en | Inspecting Elevator Engaging Actuator (on Top of Fin) in Accordance with Instructions Given in Manuals. Revision to Manuals on those Parts Covering C.G. & Mass & Balance. Editorial Corrections in AFM & AMM. Fitting a 25A-Fuse into Battery Cable for Operational Battery in Baggage Compartment in Front of Spar ((MM)) | 02/28/1991 | |
TN 7 | de | Variation in Construction for Export to Netherlands | 01/17/1992 | |
TN 7 | en | Variation in Construction for Export to Netherlands | 01/17/1992 | |
TN 8 | de | Constructional Changes Applying to Factory Series Production. Installation of a Stiffening at Rear L/G Bulkhead | 02/10/1993 | |
TN 8 | en | Constructional Changes Applying to Factory Series Production. Installation of a Stiffening at Rear L/G Bulkhead | 02/10/1993 | |
TN 9 | de | Wing Separation Joint 12.2M; Detachable Wing Tip | 02/11/1993 | |
TN 9 | en | Wing Separation Joint 12.2M; Detachable Wing Tip | 02/11/1993 | |
TN 10 | en | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD "93-001 L'Hotellier" of German Civil Aviation Authority (LBA) | 07/13/1993 | |
TN 10 | de | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD "93-001 L'Hotellier" of German Civil Aviation Authority (LBA) | 07/13/1993 | |
TN 11 | de | Modification for Optional Operation with/without Wingtip Extension to 25.6m Span Including 0.35m High Winglets ((MM)) | 07/10/1995 | |
TN 11 | en | Modification for Optional Operation with/without Wingtip Extension to 25.6m Span Including 0.35m High Winglets ((MM)) | 07/10/1995 | |
TN 12 | de | Modification of Production: a) Removal of Landing Approach Trim; b) Lamination Plan Extension of Individual Fuselage Parts by Means of a Kevlar Version ((MM)) | 09/09/1993 | |
TN 13 | de | Conversion of Sailplane ASH25 (TCDS 364) and Powered Sailplane ASH25E (TCDS 858) into a Powered Sailplane ASH25M According to TCDS 858 | 11/14/1997 | |
TN 13 | en | Conversion of Sailplane ASH25 (TCDS 364) and Powered Sailplane ASH25E (TCDS 858) into a Powered Sailplane ASH25M According to TCDS 858 | 11/14/1997 | |
TN 14 | de | Increase of Service Life of the Airframe from 6000 to 12000 Hours. Inspection of Elevator Control Linkage after Fuselage & Landing Gear Repairs. Additional Safety Device for Landing Gear Rear Bolts; Change to Maintenance Intervals. Insertion of AD-Note 1993-001/3 (Covering Compulsory Use of Safety Devices for L'Hotellier Quick-Release Connectors) into AFM & AMM ((FM)) | 03/27/1998 | |
TN 14 | en | Increase of Service Life of the Airframe from 6000 to 12000 Hours. Inspection of Elevator Control Linkage after Fuselage & Landing Gear Repairs. Additional Safety Device for Landing Gear Rear Bolts; Change to Maintenance Intervals. Insertion of AD-Note 1993-001/3 (Covering Compulsory Use of Safety Devices for L'Hotellier Quick-Release Connectors) into AFM & AMM | 03/27/1998 | |
TN 15 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 15 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 16 | de | Carbon Push Rods Replacing Aluminum Alloy Push Rods in Aileron and Flap Control Circuits Inside Wings | 06/30/1999 | |
TN 16 | en | Carbon Push Rods Replacing Aluminum Alloy Push Rods in Aileron and Flap Control Circuits Inside Wings | 06/30/1999 | |
TN 17 | de | Modification for Optional Operation with/without Wingtip Extension to 26 m incl. 0,53 m High Winglets ((FM)) | 12/08/2000 | |
TN 18 | de | Several Variations in Fabrication | 12/08/2000 | |
TN 18 | en | Several Variations in Fabrication | 12/08/2000 | |
TN 19 | de | Installation of a Power-Plant with Electronic Fuel Injection for New-Built Aircraft, or as Retrofit, Applicable to Sailplanes ASH25 (TCDS 364) or Powered Sailplanes ASH25E (TCDS 858) or Powered Sailplanes ASH25M (TCDS 858) | 11/29/2001 | |
TN 19 | en | Installation of a Power-Plant with Electronic Fuel Injection for New-Built Aircraft, or as Retrofit, Applicable to Sailplanes ASH25 (TCDS 364) or Powered Sailplanes ASH25E (TCDS 858) or Powered Sailplanes ASH25M (TCDS 858) | 11/29/2001 | |
TN 20 | de | Replacing Lever of Flap Control System in Fuselage | 03/07/2008 | |
TN 20 | en | Replacing Lever of Flap Control System in Fuselage | 03/07/2008 | |
TN 21 | de | Installation of Transponder Antenna Behind or Sideways of Landing Gear ((MI)) | 02/22/2010 | |
TN 23 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 | |
TN 23 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Improvement Mod to Spar Caps | 03/06/1990 | |
TN 1 | en | Improvement Mod to Spar Caps | 03/06/1990 | |
TN 2 | de | Increase of RPM for Engine Rotax 275 ((FM)) | 11/30/1990 | |
TN 2 | en | Increase of RPM for Engine Rotax 275 ((FM)) | 11/30/1990 | |
TN 3b | en | Installation of a Second Propeller Type | 06/30/1991 | |
TN 3b | de | Installation of a Second Propeller Type | 06/30/1991 | |
TN 4 | en | 1. Inspecting Elevator Engaging Actuator (on Top of Fin) in Accordance with Instructions Given in Manuals; 2. Editorial Corrections in AFM & AMM; 3. Exchange of EM; 4. Replacement of One Hose Sleeve in Flexible Fuel Tank System in Wing ((MM)) | 02/28/1991 | |
TN 4 | de | 1. Inspecting Elevator Engaging Actuator (on Top of Fin) in Accordance with Instructions Given in Manuals; 2. Editorial Corrections in AFM & AMM; 3. Exchange of EM; 4. Replacement of One Hose Sleeve in Flexible Fuel Tank System in Wing ((MM)) | 02/28/1991 | |
TN 5 | de | 1. Amendment of AFM & AMM because of Approval of ILEC-TAZ-25 Power-Plant Monitoring Unit; 2. Optional Installation of ILEC-TAZ-25 Power-Plant Monitoring Unit ((FM [en])) | 06/30/1991 | |
TN 6 | en | Variation in Construction for Export to Netherlands | 01/17/1992 | |
TN 6 | de | Variation in Construction for Export to Netherlands | 01/17/1992 | |
TN 7 | de | Constructional Changes Applying to Factory Series Production. Installation of Stiffening at Rear L/G Bulkhead | 02/10/1993 | |
TN 7 | en | Constructional Changes Applying to Factory Series Production. Installation of Stiffening at Rear L/G Bulkhead | 02/10/1993 | |
TN 8 | en | Wing Separation Joint 12.2M; Detachable Wing Tip | 02/11/1993 | |
TN 8 | de | Wing Separation Joint 12.2M; Detachable Wing Tip | 02/11/1993 | |
TN 9 | en | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as AD "93-001 L'Hotellier" of German Civil Aviation Authority (LBA) | 07/13/1993 | |
TN 9 | de | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as AD "93-001 L'Hotellier" of German Civil Aviation Authority (LBA) | 07/13/1993 | |
TN 10 | en | Modification for Optional Operation with/without Wingtip Extension to 25.6m Span Including 0.35 m High Winglets | 07/10/1995 | |
TN 10 | de | Modification for Optional Operation with/without Wingtip Extension to 25.6m Span Including 0.35 m High Winglets ((FM)) | ||
TN 11 | de | Conversion of Sailplane ASH 25 (TCDS 364) and Powered Sailplane ASH25E (TCDS 858) into Powered Sailplane ASH 25M According to TCDS 858 | 11/14/1997 | |
TN 11 | en | Conversion of Sailplane ASH 25 (TCDS 364) and Powered Sailplane ASH25E (TCDS 858) into Powered Sailplane ASH 25M According to TCDS 858 | 11/14/1997 | |
TN 12 | de | Increase of Service Life of Airframe from 6000 to 12000 Hours. Inspection of Elevator Control Linkage after Fuselage and Landing Gear Repairs. Additional Safety Device for Landing Gear Rear Bolts; Change to Maintenance Intervals. Insertion of AD-Note 1993-001/3 (Compulsory Use of Safety Devices for L'Hotellier Quick-Release Connectors) into AFM & AMM ((FM)) | 03/27/1998 | |
TN 12 | en | Increase of Service Life of Airframe from 6000 to 12000 Hours. Inspection of Elevator Control Linkage after Fuselage and Landing Gear Repairs. Additional Safety Device for Landing Gear Rear Bolts; Change to Maintenance Intervals. Insertion of AD-Note 1993-001/3 (Compulsory Use of Safety Devices for L'Hotellier Quick-Release Connectors) into AFM & AMM | 03/27/1998 | |
TN 13 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 13 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 14 | de | Carbon Push Rods Replacing Aluminum Alloy Push Rods in Aileron and Flap Control Circuits Inside Wings | 06/30/1999 | |
TN 14 | en | Carbon Push Rods Replacing Aluminum Alloy Push Rods in Aileron and Flap Control Circuits Inside Wings | 06/30/1999 | |
TN 15 | en | Inspection and Exchange of Exhaust Damper of Power-Plant. Amendment and Corrections to Manuals | 09/03/1999 | |
TN 15 | de | Inspection and Exchange of Exhaust Damper of Power-Plant. Amendment and Corrections to Manuals ((FM)) | 09/03/1999 | |
TN 16 | de | New Propeller AS2F1-1/R153-92-N1 for ASH 25 M ((FM)) | 10/19/2000 | |
TN 17 | de | Installation of Fixed Re-Fueling System in Fuselage ((FM)) | 09/05/2000 | |
TN 17 | en | Installation of Fixed Re-Fueling System in Fuselage | 09/05/2000 | |
TN 18 | de | Modification for Optional Operation with/without Wingtip Extension to 26 m incl. 0,53 m High Winglets ((FM for 25E, 25M)) | 12/08/2000 | |
TN 19 | de | Several Variations in Fabrication | 12/08/2000 | |
TN 19 | en | Several Variations in Fabrication | 12/08/2000 | |
TN 20 | en | Installation of a Power-Plant with Electronic Fuel Injection for New-Built Aircraft, or as Retrofit, Applicable to Sailplanes ASH 25 (TCDS 364) or Powered Sailplanes ASH 25 E (TCDS 858) or Powered Sailplanes ASH 25 M (TCDS 858) | 11/29/2001 | |
TN 20 | de | Installation of a Power-Plant with Electronic Fuel Injection for New-Built Aircraft, or as Retrofit, Applicable to Sailplanes ASH 25 (TCDS 364) or Powered Sailplanes ASH 25 E (TCDS 858) or Powered Sailplanes ASH 25 M (TCDS 858) | 11/29/2001 | |
TN 21 | de | Increase of Max. Take-Off Mass and of Mass of Non-Lift Producing Components ((FM)) | 02/21/2003 | |
TN 21 | en | Increase of Max. Take-Off Mass and of Mass of Non-Lift Producing Components | 02/21/2003 | |
TN 22 | en | Inspection and where Necessary Replacement of One Fuel Line | 02/21/2003 | |
TN 22 | de | Inspection and where Necessary Replacement of One Fuel Line | 02/21/2003 | |
TN 23 | de | Different Construction Modifications: 1) New Engine Battery; 2) Additional O2 Installation in Fuselage Tail Cone ((FM for 25M, 25Mi)) | 09/27/2004 | |
TN 24 | de | Alteration of Engine Manufacturer ((FM for 25M, 25Mi)) | 03/31/2003 | |
TN 24 | en | Alteration of Engine Manufacturer ((FM for 25M)) | 03/31/2003 | |
TN 25 | de | New Fuel Lines (PUR), without Fixed Exchange Intervals ((MM for 25M, 25Mi)) | 05/07/2007 | |
TN 25 | en | New Fuel Lines (PUR), without Fixed Exchange Intervals ((MM for 25M)) | 05/07/2007 | |
TN 26 | Iss 2 | de | Installation of Transponder Antenna Behind or Sideways of Landing Gear (MM for 25E, 25M, 25Mi) | 01/31/2008 |
TN 27 | en | Adjusting Drive Belt ((FM for 25M)) | 01/08/2008 | |
TN 27 | de | Adjusting Drive Belt ((FM for 25M, 25Mi)) | 01/08/2008 | |
TN 28 | en | Replacing a Lever of Flap Control System in Fuselage | 03/07/2008 | |
TN 28 | de | Replacing a Lever of Flap Control System in Fuselage | 03/07/2008 | |
TN 29 | en | Replacement of Carburetor Cap, Tightness of Bleeding Screw on Oil Pump | 09/05/2012 | |
TN 29 | de | Replacement of Carburetor Cap, Tightness of Bleeding Screw on Oil Pump | 09/05/2012 | |
TN 30 | en | Troubleshooting of Engine Control Unit (ECU) | 09/19/2014 | |
TN 30 | de | Troubleshooting of Engine Control Unit (ECU) | 09/19/2014 | |
TN 31 | en | New Calibration of Rotor Internal Cooling Temperature Depending on Position of Temperature Sensor | 04/01/2015 | |
TN 31 | de | New Calibration of Rotor Internal Cooling Temperature Depending on Position of Temperature Sensor ((FM)) | 04/01/2015 | |
TN 32 | en | Replacement of Silencer | 01/08/2016 | |
TN 32 | Iss 2 | de | Replacement of Silencer | 07/19/2017 |
TN 32 | Iss 2 | en | Replacement of Silencer | 07/19/2017 |
TN 34 | en | Specification Update of Flexible Fuel Tanks ((MM for 25M)) | 09/15/2017 | |
TN 34 | de | Specification Update of Flexible Fuel Tanks ((MM for 25M, 25Mi)) | 09/15/2017 | |
TN 35 | de | Improvement of Performance Map of New IAE50R-AA ECU with S/Ns "AE00XXX" which were Installed as Standard from 2014 Onwards | 05/22/2018 | |
TN 35 | en | Improvement of Performance Map of New IAE50R-AA ECU with S/Ns "AE00XXX" which were Installed as Standard from 2014 Onwards | 05/22/2018 | |
TN 36 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM for 25E, 25M)) | 04/03/2020 | |
TN 36 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake (MM for 25E, 25M, 25Mi) | 04/03/2020 | |
TN 37 | de | Alternative Rotor Cooling Air Intake Filter ((MM)) | 08/07/2023 | |
TN 37 | en | Alternative Rotor Cooling Air Intake Filter ((MM)) | 08/07/2023 | |
TN 38 | en | Introduction of Alternative Fuel Main Filter Due to End of Production of Existing One | 10/09/2023 | |
TN 38 | de | Introduction of Alternative Fuel Main Filter Due to End of Production of Existing One ((MM)) | 10/09/2023 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Conversion of Sailplane ASH26 (TCDS 383) into a Powered Sailplane ASH26E According to TCDS 883 | 06/26/1997 | |
TN 1 | en | Conversion of Sailplane ASH26 (TCDS 383) into a Powered Sailplane ASH26E According to TCDS 883 | 06/26/1997 | |
TN 2 | de | Improvement of Airbrake Efficiency ((FM)) | 08/28/1997 | |
TN 2 | en | Improvement of Airbrake Efficiency | 08/28/1997 | |
TN 3 | en | Air Inlets for Blast Holes in Flap and Aileron by Means of NACA Ducts | 09/08/1997 | |
TN 3 | de | Air Inlets for Blast Holes in Flap and Aileron by Means of NACA Ducts | 09/08/1997 | |
TN 4 | en | Modification for Optional Operation with 0.45m High Winglets Including a Short Wing Piece which are Fitted at a Wing Separation Joint | 04/09/1999 | |
TN 4 | de | Modification for Optional Operation with 0.45m High Winglets Including a Short Wing Piece which are Fitted at a Wing Separation Joint ((FM)) | 04/09/1999 | |
TN 5 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 5 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 6 | de | Installation of Transponder Antennas ((MI)) | 01/31/2008 | |
TN 9 | en | Alternative Hydraulic Wheel Brake System TOST ((MM)) | 02/01/2017 | |
TN 9 | de | Alternative Hydraulic Wheel Brake System TOST | 02/01/2017 | |
TN 10 | en | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 10 | de | Alternative Rim for Main Wheel | 11/07/2019 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Checking Cooling Air Temperature in Flight. Improvement and Change of Fan of Engine Internal Air Cooling. Exchange of Temperature Sensor of Internal Air Cooling. Inspection of Further Engine Unit Parts ((FM)) | 10/31/1996 | |
TN 1 | en | Checking Cooling Air Temperature in Flight. Improvement and Change of Fan of Engine Internal Air Cooling. Exchange of Temperature Sensor of Internal Air Cooling. Inspection of Further Engine Unit Parts ((FM)) | 10/31/1996 | |
TN 2 | en | Obtaining TC Status as per TCDS 883, Iss 1 | 08/02/1997 | |
TN 2 | de | Obtaining TC Status as per TCDS 883, Iss 1 | 08/02/1997 | |
TN 3 | de | Improvement of Airbrake Efficiency ((FM)) | 08/28/1997 | |
TN 3 | en | Improvement of Airbrake Efficiency ((FM)) | 08/28/1997 | |
TN 4 | en | Air Inlets for Blast Holes in Flap and Aileron by Means of NACA Ducts | 09/08/1997 | |
TN 4 | de | Air Inlets for Blast Holes in Flap and Aileron by Means of NACA Ducts | 09/08/1997 | |
TN 5 | en | Inspection and Exchange of "Rotor Cooling Air Fan According to TN 1", Fitted at Engine AE 50 R Made by Mid-West Engines ((Inst, MM)) | 07/23/1998 | |
TN 5 | de | Inspection and Exchange of "Rotor Cooling Air Fan According to TN 1", Fitted at Engine AE 50 R Made by Mid-West Engines ((MM)) | 07/23/1998 | |
TN 6 | de | Inspection of Engine Compartment and Exhaust Damper Fairing for Escaped or Spilt Engine Oil | 08/10/1998 | |
TN 6 | en | Inspection of Engine Compartment and Exhaust Damper Fairing for Escaped or Spilt Engine Oil | 08/10/1998 | |
TN 7 | en | Modification for Optional Operation with 0.45m High Winglets Including a Short Wing Piece which are Fitted at a Wing Separation Joint ((FM)) | 04/09/1999 | |
TN 7 | de | Modification for Optional Operation with 0.45m High Winglets Including a Short Wing Piece which are Fitted at a Wing Separation Joint ((FM)) | 04/09/1999 | |
TN 8 | en | Inspection and Exchange of Exhaust Damper of Power-Plant. Amendment and Corrections to Manuals ((MM)) | 08/23/1999 | |
TN 8 | de | Inspection and Exchange of Exhaust Damper of Power-Plant. Amendment and Corrections to Manuals ((MM)) | 08/23/1999 | |
TN 9 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 9 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 10 | en | New Propeller AS2F1-1/R153-92-N1 for ASH26E ((FM)) | 10/05/2000 | |
TN 10 | de | New Propeller AS2F1-1/R153-92-N1 for ASH26E ((FM)) | 10/05/2000 | |
TN 11 | de | Installation of a Fixed Re-Fueling System in Fuselage. Return of Wing Tank Ventilation into Fuselage Tank ((FM)) | 09/25/2000 | |
TN 11 | en | Installation of a Fixed Re-Fueling System in Fuselage. Return of Wing Tank Ventilation into Fuselage Tank ((FM)) | 09/25/2000 | |
TN 12 | de | Alteration of Engine Manufacturer ((FM)) | 05/07/2003 | |
TN 12 | en | Alteration of Engine Manufacturer ((FM)) | 05/07/2003 | |
TN 13 | de | Various Constructional Modifications ((MM)) | 02/22/2005 | |
TN 13 | en | Various Constructional Modifications ((MM)) | 02/22/2005 | |
TN 14 | Iss 2 | de | Installation of Transponder Antennas ((MI)) | 01/31/2008 |
TN 15 | en | Adjusting Drive Belt ((FM)) | 01/08/2008 | |
TN 15 | de | Adjusting Drive Belt ((FM)) | 01/08/2008 | |
TN 16 | de | Replacement of Carburetor Cap, Tightness of Bleeding Screw on Oil Pump | 09/05/2012 | |
TN 16 | en | Replacement of Carburetor Cap, Tightness of Bleeding Screw on Oil Pump | 09/05/2012 | |
TN 18 | de | Exchange of Steerable Tailwheel ((FM)) | 04/10/2014 | |
TN 18 | en | Exchange of Steerable Tailwheel ((FM)) | 04/10/2014 | |
TN 19 | en | Replacement of Silencer | 01/08/2016 | |
TN 19 | Iss 2 | de | Replacement of Silencer | 07/19/2017 |
TN 19 | Iss 2 | en | Replacement of Silencer | 07/19/2017 |
TN 20 | en | Optional Installation of Parking Brake and Piggott Hook ((FM)) | 11/23/2016 | |
TN 20 | de | Optional Installation of Parking Brake and Piggott Hook ((FM)) | 11/23/2016 | |
TN 21 | de | Various Modifications on Power-Plant System | 05/27/2021 | |
TN 21 | en | Various Modifications on Power-Plant System | 05/27/2021 | |
TN 22 | de | Alternative Hydraulic Wheel Brake System TOST | 02/01/2017 | |
TN 22 | en | Alternative Hydraulic Wheel Brake System TOST | 02/01/2017 | |
TN 23 | en | Specification Update of Flexible Fuel Tanks ((MM)) | 09/15/2017 | |
TN 23 | de | Specification Update of Flexible Fuel Tanks ((MM)) | 09/15/2017 | |
TN 24 | en | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 24 | de | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 25 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 | |
TN 25 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | en | Alternative Hydraulic Wheel Brake System TOST ((MM)) | 02/01/2017 | |
TN 1 | de | Alternative Hydraulic Wheel Brake System TOST ((MM)) | 02/01/2017 | |
TN 2 | en | Specification Update of Flexible Fuel Tanks ((MM)) | 09/15/2017 | |
TN 2 | de | Specification Update of Flexible Fuel Tanks ((MM)) | 09/15/2017 | |
TN 3 | en | Improvement of Performance Map of New IAE50R-AA ECU with S/Ns "AE00XXX" which were Installed as Standard from 2014 Onwards | 05/22/2018 | |
TN 3 | de | Improvement of Performance Map of New IAE50R-AA ECU with S/Ns "AE00XXX" which were Installed as Standard from 2014 Onwards | 05/22/2018 | |
TN 4 | en | 1) Improvement of Liquid Cooling Temperature Display of ILEC Power-Plant Control Unit with Instrument Diameter of 57mm; 2) Improved Assignment of Two Ignition Circuits to Corresponding Fuses | 05/22/2018 | |
TN 4 | de | 1) Improvement of Liquid Cooling Temperature Display of ILEC Power-Plant Control Unit with Instrument Diameter of 57mm; 2) Improved Assignment of Two Ignition Circuits to Corresponding Fuses | 05/22/2018 | |
TN 5 | de | New Propeller AS2F1-5 ((FM)) | 05/15/2019 | |
TN 5 | en | New Propeller AS2F1-5 ((FM)) | 05/15/2019 | |
TN 6 | de | New Suspension Struts for Main Landing Gear | 11/30/2020 | |
TN 6 | en | New Suspension Struts for Main Landing Gear | 11/30/2020 | |
TN 7 | en | Bug Fix Power-Plant Instrument | 03/02/2023 | |
TN 7 | de | Bug Fix Power-Plant Instrument | 03/02/2023 | |
TN 8 | en | Alternative Rotor Cooling Air Intake Filter ((MM)) | 08/07/2023 | |
TN 8 | de | Alternative Rotor Cooling Air Intake Filter ((MM)) | 08/07/2023 | |
TN 9 | en | Introduction of Alternative Fuel Main Filter Due to End of Production of Existing One ((MM)) | 10/09/2023 | |
TN 9 | de | Introduction of Alternative Fuel Main Filter Due to End of Production of Existing One ((MM)) | 10/09/2023 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 2 | en | Exchange of Steerable Tailwheel ((FM)) | 04/10/2014 | |
TN 2 | de | Exchange of Steerable Tailwheel ((FM)) | 04/10/2014 | |
TN 3 | de | Troubleshooting of Engine Control Unit (ECU) | 09/19/2014 | |
TN 3 | en | Troubleshooting of Engine Control Unit (ECU) | 09/19/2014 | |
TN 4 | de | Installation of Smaller Version of ILEC Instrument (Control Unit) ((FM)) | 03/16/2015 | |
TN 4 | en | Installation of Smaller Version of ILEC Instrument (Control Unit) ((FM)) | 03/16/2015 | |
TN 5 | de | New Calibration of Rotor Cooling Air (RCA) Temperature Depending on Position of Temperature Sensor ((FM)) | 04/20/2015 | |
TN 5 | en | New Calibration of Rotor Cooling Air (RCA) Temperature Depending on Position of Temperature Sensor ((FM)) | 04/20/2015 | |
TN 6 | de | Automatic Shut-Off System for Refuelling ((FM)) | 03/16/2015 | |
TN 6 | en | Automatic Shut-Off System for Refuelling ((FM)) | 03/16/2015 | |
TN 7 | de | Blow Holes, NACA Inlets and Zig-Zag Tape: Drawing Revision ((MM, MI)) | 03/16/2015 | |
TN 7 | en | Blow Holes, NACA Inlets and Zig-Zag Tape: Drawing Revision ((MM, MI)) | 03/16/2015 | |
TN 8 | en | Self-Loosening of a Bolted Assembly Inside Shock Absorbing Struts of Main Landing Gear ((MM)) | 09/26/2016 | |
TN 8 | de | Self-Loosening of a Bolted Assembly Inside Shock Absorbing Struts of Main Landing Gear ((MM)) | 09/26/2016 | |
TN 9 | de | Calibrating Fuel Contents with Small ILEC Engine Control Unit According to TN 04 is Generating an Error Message | 09/26/2016 | |
TN 9 | en | Calibrating Fuel Contents with Small ILEC Engine Control Unit According to TN 04 is Generating an Error Message | 09/26/2016 | |
TN 10 | en | Alternative Hydraulic Wheel Brake System TOST ((MM)) | 02/01/2017 | |
TN 10 | de | Alternative Hydraulic Wheel Brake System TOST ((MM)) | 02/01/2017 | |
TN 11 | de | Specification Update of Flexible Fuel Tanks ((MM)) | 09/15/2017 | |
TN 11 | en | Specification Update of Flexible Fuel Tanks ((MM)) | 09/15/2017 | |
TN 12 | de | Improvement of Performance Map of New IAE50R-AA ECU with S/Ns "AE00XXX" which were Installed as Standard from 2014 Onwards | 05/22/2018 | |
TN 12 | en | Improvement of Performance Map of New IAE50R-AA ECU with S/Ns "AE00XXX" which were Installed as Standard from 2014 Onwards | 05/22/2018 | |
TN 13 | de | 1) Improvement of Liquid Cooling Temperature Display of ILEC Power-Plant Control Unit with an Instrument Diameter of 57mm; 2) Improved Assignment of Two Ignition Circuits to Corresponding Fuses | 05/22/2018 | |
TN 13 | en | 1) Improvement of Liquid Cooling Temperature Display of ILEC Power-Plant Control Unit with an Instrument Diameter of 57mm; 2) Improved Assignment of Two Ignition Circuits to Corresponding Fuses | 05/22/2018 | |
TN 14 | de | Change of Fairings and Screw Connections of Ailerons and Flaps | 10/31/2018 | |
TN 14 | en | Change of Fairings and Screw Connections of Ailerons and Flaps | 10/31/2018 | |
TN 15 | en | Bug Fix Power-Plant Instrument | 03/02/2023 | |
TN 15 | de | Bug Fix Power-Plant Instrument | 03/02/2023 | |
TN 16 | de | Alternative Rotor Cooling Air Intake Filter ((MM)) | 08/07/2023 | |
TN 16 | en | Alternative Rotor Cooling Air Intake Filter ((MM)) | 08/07/2023 | |
TN 17 | en | Introduction of an Alternative Fuel Main Filter Due to End of Production of Existing One ((MM)) | 10/09/2023 | |
TN 17 | de | Introduction of an Alternative Fuel Main Filter Due to End of Production of Existing One ((MM)) | 10/09/2023 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | en | Installation of an Additional Fair Lead in Rudder Cables | 11/09/1967 | |
TN 1 | de | Installation of an Additional Fair Lead in Rudder Cables | 11/09/1967 | |
TN 2 | de | Installation of Additional Fair Lead in Brake Cable to Prevent Slinging of Cable Around the Hook Lever | 05/30/1968 | |
TN 2 | en | Installation of Additional Fair Lead in Brake Cable to Prevent Slinging of Cable Around the Hook Lever | 05/30/1968 | |
TN 3 | de | Installation of Larger Buffer Plates for Rubber Buffer of Landing Gear | 09/04/1968 | |
TN 3 | en | Installation of Larger Buffer Plates for Rubber Buffer of Landing Gear | 09/04/1968 | |
TN 4 | de | Addition to TC for Semiaerobatics ((FM)) | 07/04/1969 | |
TN 4 | en | Addition to TC for Semiaerobatics | 07/04/1969 | |
TN 5 | de | Jettisoning Device for Canopy | 12/17/1970 | |
TN 5 | en | Jettisoning Device for Canopy | 12/17/1970 | |
TN 6 | de | Simplification of Aileron Assembly | 08/27/1973 | |
TN 7 | de | Installation of a Removable Balance Weight ((FM)) | 11/01/1975 | |
TN 7 | en | Installation of a Removable Balance Weight ((FM)) | 11/01/1975 | |
TN 7a | de | Installation of a Removable Balance Weight ((FM)) | 01/21/1987 | |
TN 8 | de | Installation of a Nose Wheel Instead of Skid | 06/24/1985 | |
TN 8a | de | Installation of a Nose Wheel Instead of Skid | 06/24/1985 | |
TN 8a | en | Installation of a Nose Wheel Instead of Skid | 06/24/1985 | |
TN 9 | de | Installation of Pneumatic Tailwheel in Exchange for Tailskid | 02/05/1986 | |
TN 9 | en | Installation of Pneumatic Tailwheel in Exchange for Tailskid | 02/05/1986 | |
TN 10 | de | Installation of Disc Brake Instead of Shoe Brake | 05/26/1986 | |
TN 11 | de | Covering of Fuselage Front Part with a FRP-Fairing. Extension of Nose Wheel FRP-Fairing | 05/26/1986 | |
TN 11a | de | Covering of Fuselage Front Part with a FRP-Fairing. Extension of Nose Wheel FRP-Fairing | 12/29/1988 | |
TN 12 | de | Elevator | 10/04/1989 | |
TN 12 | en | Elevator | 10/04/1989 | |
TN 13 | de | Inspection of Main-Fittings | 12/19/1990 | |
TN 13 | en | Inspection of Main-Fittings | 12/19/1990 | |
TN 14 | de | Inspecting Bearing Brackets and Toggle Force of Airbrake Control Circuit | 09/27/1991 | |
TN 14 | en | Inspecting Bearing Brackets and Toggle Force of Airbrake Control Circuit | 09/27/1991 | |
TN 15 | en | Modification Open Canopy Convertible | 12/20/2005 | |
TN 15 | de | Modification Open Canopy Convertible ((FM)) | 12/20/2005 | |
TN 16 | de | FRP Fairing Fuselage | 02/02/2006 | |
TN 17 | de | Installation of a Transponder Antenna Behind Landing Gear ((MI)) | 05/05/2008 | |
TN 18 | de | Inspection of Central Support of Elevator | 05/25/2010 | |
TN 18 | en | Inspection of Central Support of Elevator | 05/25/2010 | |
TN 19 | en | Inspection of Automatic Elevator Control Connection | 08/30/2012 | |
TN 19 | 1 | en | Inspection of Automatic Elevator Control Connection | 01/08/2013 |
TN 19 | 1 | de | Inspection of Automatic Elevator Control Connection | 01/08/2013 |
TN 20 | de | Inspection of Elevator ((Appendix)) | 07/12/2021 | |
TN 20 | en | Inspection of Elevator ((Appendix)) | 07/12/2021 | |
TN 20 | Iss 2 | de | Inspection of Elevator ((Appendix)) | 11/01/2023 |
TN 20 | Iss 2 | en | Inspection of Elevator ((Appendix)) | 11/01/2023 |
TN 21 | en | Limitation of Operating Envelope ((Appendix)) | 07/12/2021 | |
TN 21 | de | Limitation of Operating Envelope ((Appendix)) | 07/12/2021 | |
TN 22 | en | Inspection of Control Stick Attachment in Rear Cockpit | 06/15/2023 | |
TN 22 | de | Inspection of Control Stick Attachment in Rear Cockpit | 06/15/2023 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Suspension of Thermos Bottles Below Baggage Compartment | 09/10/1968 | |
TN 1 | en | Suspension of Thermos Bottles Below Baggage Compartment | 09/10/1968 | |
TN 1 | Amend 1 | de | Suspension of Thermos Bottles Below Baggage Compartment | 06/18/1969 |
TN 2 | en | Installation of Collar Around Filler Inlet of Fuel Tank to Prevent Pouring Fuel into Luggage Compartment | 03/17/1970 | |
TN 2 | de | Installation of Collar Around Filler Inlet of Fuel Tank to Prevent Pouring Fuel into Luggage Compartment | 03/17/1970 | |
TN 3 | en | Tube Spar of Elevator | 03/17/1970 | |
TN 3 | de | Tube Spar of Elevator | 03/17/1970 | |
TN 4 | de | Installation of an Electric Starter ((FM)) | 02/14/1973 | |
TN 5 | de | Installation of Retractable Wing Supports ((FM)) | 05/27/1975 | |
TN 6 | en | Fuel Tank ((MM)) | 10/30/1970 | |
TN 6 | de | Fuel Tank ((MM)) | 10/30/1970 | |
TN 7 | de | Installation of Transponder Antennas Behind Landing Gear Inside or Outside Fuselage ((MI)) | 05/15/2008 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | en | Installation of a Cabin Heater ((FM)) | 07/08/1974 | |
TN 1 | de | Installation of a Cabin Heater ((FM)) | 07/08/1974 | |
TN 2 | de | Installation of a Parking Brake ((OM)) | 01/15/1975 | |
TN 2 | en | Installation of a Parking Brake | 01/15/1975 | |
TN 3 | de | Increased Maximum Weight of 750 kp (1650 lbs) ((FM)) | 12/02/1975 | |
TN 3 | en | Increased Maximum Weight of 750 kp (1650 lbs) ((FM, FM2)) | 12/02/1975 | |
TN 3a | de | Increased Maximum Weight of 750 kp (1650 lbs) ((FM)) | 11/06/1986 | |
TN 4 | de | Installation of Removable Auxiliary Fuel Tanks ((FM)) | 12/05/1976 | |
TN 4 | en | Installation of Removable Auxiliary Fuel Tanks ((FM)) | 12/05/1976 | |
TN 5 | en | Exchange of Material | 08/17/1976 | |
TN 5 | de | Installation of an Additional Wing Separation Joint | 04/15/1976 | |
TN 5 | de | Exchange of Material | 08/17/1976 | |
TN 6 | de | Adjustable Cowl Cooling Flap ((FM)) | 10/10/1977 | |
TN 6 | en | Adjustable Cowl Cooling Flap ((FM)) | 10/10/1977 | |
TN 7 | de | Installation of Autopilot Edo Aire Mitchell Century I ((FM)) | 10/10/1977 | |
TN 8 | de | Enlarging of Bolts at Wheel Hub | 07/05/1977 | |
TN 8 | en | Enlarging of Bolts at Wheel Hub | 07/05/1977 | |
TN 9 | en | Wheel Brake Improvement - Modification of Mechanical Drum Brake into a Hydraulic Disc Brake System | 06/12/1985 | |
TN 9 | de | Wheel Brake Improvement - Modification of Mechanical Drum Brake into a Hydraulic Disc Brake System ((OM)) | 06/12/1985 | |
TN 10 | en | Fuel Tank ((MM)) | 05/12/1989 | |
TN 10 | de | Fuel Tank ((MM)) | 05/12/1989 | |
TN 11 | en | Installation of Electric Fuel Tank Gauge System for 60 Liters Fuel Tank | 07/10/1997 | |
TN 11 | de | Installation of Electric Fuel Tank Gauge System for 60 Liters Fuel Tank ((OM)) | 07/10/1997 | |
TN 12 | de | Use of Lead-Free Fuel | 07/15/1998 | |
TN 14 | de | Installation of a Transponder Antenna Behind Landing Gear ((WI)) | 04/15/2008 | |
TN 15 | en | Inspection of Central Support of Elevator | 05/25/2010 | |
TN 15 | de | Inspection of Central Support of Elevator | 05/25/2010 | |
TN 16 | en | a) Replacement of Electric Fuel Pump; b) Replacement of Flange for Fuel Tank Sensor | 01/17/2020 | |
TN 16 | Iss 2 | en | a) Replacement of Electric Fuel Pump; b) Replacement of Flange for Fuel Tank Sensor | 07/11/2022 |
TN 16 | Iss 2 | de | a) Replacement of Electric Fuel Pump; b) Replacement of Flange for Fuel Tank Sensor | 07/11/2022 |
TN 17 | de | Inspection of Elevator ((Appendix)) | 07/12/2021 | |
TN 17 | en | Inspection of Elevator ((Appendix)) | 07/12/2021 | |
TN 17 | Iss 2 | en | Inspection of Elevator ((Appendix)) | 11/01/2023 |
TN 17 | Iss 2 | de | Inspection of Elevator ((Appendix)) | 11/01/2023 |
TN 18 | en | Limitation of Operating Envelope ((Appendix)) | 07/12/2021 | |
TN 18 | de | Limitation of Operating Envelope ((Appendix)) | 07/12/2021 | |
TN HO-V62R/L 160 BT | de | Use of Propeller HO-V 62 R/L 160 BT in Connection with Engine Limbach L 2000 EB 1 | 06/22/1984 | |
TN L2000 EB 1 | de | Replacement of Engine Limbach SL 1700 EB 1 for Limbach L 2000 EB 1 ((FM [en])) | 07/23/1981 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Installation of Mass Balance to Aileron | 09/09/1975 | |
TN 2 | en | Installation of Nose Hook | 03/16/1976 | |
TN 2 | de | Installation of Nose Hook | 03/16/1976 | |
TN 3 | en | Enlarging of Center of Gravity Margin ((FM)) | 04/26/1976 | |
TN 3 | de | Enlarging of Center of Gravity Margin ((FM)) | 04/26/1976 | |
TN 4 | en | Modification to Version ASK18B (Shortening Span to 15m) | 07/01/1976 | |
TN 4 | de | Modification to Version ASK18B (Shortening Span to 15m) | 07/01/1976 | |
TN 5 | en | Exchange of Material | 08/17/1976 | |
TN 5 | de | Exchange of Material | 08/17/1976 | |
TN 6 | en | Elevator | 10/04/1989 | |
TN 6 | de | Elevator | 10/04/1989 | |
TN 7 | en | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 7 | de | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 8 | en | Inspection of Central Support of Elevator | 05/25/2010 | |
TN 8 | de | Inspection of Central Support of Elevator | 05/25/2010 | |
TN 9 | en | Inspection of Automatic Elevator Control Connection | 08/30/2012 | |
TN 9 | 1 | en | Inspection of Automatic Elevator Control Connection | 01/08/2013 |
TN 9 | 1 | de | Inspection of Automatic Elevator Control Connection | 01/08/2013 |
TN 10 | de | Inspection of Elevator ((Appendix)) | 07/12/2021 | |
TN 10 | en | Inspection of Elevator ((Appendix)) | 07/12/2021 | |
TN 10 | Iss 2 | de | Inspection of Elevator ((Appendix)) | 11/01/2023 |
TN 10 | Iss 2 | en | Inspection of Elevator ((Appendix)) | 11/01/2023 |
TN 11 | de | Limitation of Operating Envelope ((Appendix)) | 07/12/2021 | |
TN 11 | en | Limitation of Operating Envelope ((Appendix)) | 07/12/2021 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 2 | de | Installation of Inflatable Tail Wheel ((MM)) | 08/26/1980 | |
TN 2 | en | Installation of Inflatable Tail Wheel ((MM)) | 08/26/1980 | |
TN 3 | de | Installation of Weight Trim | 10/27/1980 | |
TN 4 | de | Trim Ballast for Spin Flights (Spin Ballast) ((FM)) | 11/14/1980 | |
TN 4 | en | Trim Ballast for Spin Flights (Spin Ballast) ((FM)) | 11/14/1980 | |
TN 4a | en | Trim Ballast for Spin Flights (Spin Ballast) ((FM)) | 11/25/2004 | |
TN 4a | de | Trim Ballast for Spin Flights (Spin Ballast) ((FM)) | 11/25/2004 | |
TN 4b | de | Trim Ballast for Spin Flights (Spin Ballast) ((FM)) | 12/12/2012 | |
TN 4b (US Reg) |
en | Trim Ballast for Spin Flights (Spin Ballast) ((FM)) | 10/31/2013 | |
TN 4b | en | Trim Ballast for Spin Flights (Spin Ballast) ((FM)) | 12/12/2012 | |
TN 5a | en | Modification of AFM and Cockpit Placard | 03/26/1981 | |
TN 5a | de | Modification of AFM and Cockpit Placard | 03/26/1981 | |
TN 5b | en | Modification of AFM and Cockpit Placard | 03/26/1981 | |
TN 5b | de | Modification of AFM and Cockpit Placard | 03/26/1981 | |
TN 6 | en | Modification of AFM | 03/26/1982 | |
TN 6 | de | Modification of AFM | 03/26/1982 | |
TN 7 | en | Modification of Suspendition of Trim Ballast | 12/15/1982 | |
TN 7 | de | Modification of Suspendition of Trim Ballast ((FM)) | 12/15/1982 | |
TN 8 | de | Modification of AFM | 06/16/1983 | |
TN 8 | en | Modification of AFM | 06/16/1983 | |
TN 9 | en | Procedure to Obtain a Standard Certificate of Airworthiness According to FAR 21.29 for Prematurely Exported Glider ASK21 to United States | 02/24/1983 | |
TN 10 | de | Modification of Release Cable Fairlead ((MM)) | 10/10/1983 | |
TN 10 | en | Modification of Release Cable Fairlead ((MM, ICA)) | 10/10/1983 | |
TN 11 | en | Automatic Elevator Connection ((FM, FM2)) | 12/20/1983 | |
TN 11 | de | Automatic Elevator Connection ((FM)) | 12/20/1983 | |
TN 12 | de | Modification for Certification for Import in France | 01/16/1984 | |
TN 12 | en | Modification for Certification for Import in France | 01/16/1984 | |
TN 13 | de | Modification of AFM ((FM)) | 02/16/1984 | |
TN 13 | en | Modification of AFM | 02/16/1984 | |
TN 13a | en | Modification of AFM ((FM, FM2)) | 06/04/1984 | |
TN 14 | en | Amendment to Manuals in English Language ((FM, FM2)) | 05/16/1984 | |
TN 15 | de | New Canopy Locking System ((FM)) | 05/25/1984 | |
TN 15 | en | New Canopy Locking System ((FM, FM2)) | 05/25/1984 | |
TN 16 | de | Folding Up of Front Cockpit Instrument Panel | 09/12/1984 | |
TN 16 | en | Folding Up of Front Cockpit Instrument Panel | 09/12/1984 | |
TN 17 | en | Inspection of Wheel Box Cutout in Fuselage | 10/01/1984 | |
TN 17 | de | Inspection of Wheel Box Cutout in Fuselage | 10/01/1984 | |
TN 18 | de | Inspecting Trim Indicator and Reinforcing Bowden Cable Flexible Steel Hose | 07/16/1985 | |
TN 18 | en | Inspecting Trim Indicator and Reinforcing Bowden Cable Flexible Steel Hose | 07/16/1985 | |
TN 19 | de | Inspection and Exchange of Rudder Pedal Support Fitting | 10/22/1986 | |
TN 19 | en | Inspection and Exchange of Rudder Pedal Support Fitting | 10/22/1986 | |
TN 20 | de | 1. Inspection of Rudder Pedals; 2. Change/Supplement to AFM & AMM in Order to Provide Owners with New Inspection & Assembly Instructions; 3. Inspection & Exchange of Airbrake Bellcrank in Fuselage; 4. Inspection & Reinforcement of Rear Canopy Binge ((FM)) | 10/16/1987 | |
TN 20 | en | 1. Inspection of Rudder Pedals; 2. Change/Supplement to AFM & AMM in Order to Provide Owners with New Inspection & Assembly Instructions; 3. Inspection & Exchange of Airbrake Bellcrank in Fuselage; 4. Inspection & Reinforcement of Rear Canopy Binge ((FM, FM2)) | 10/16/1987 | |
TN 21 | en | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 21 | en | Inspecting Elevator Pushrod | 07/01/1993 | |
TN 21 | de | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 22 | de | Checking Parallel Rocker (at Elevator Actuator Rod) in Fin. Exchange of this Part and Amendment to AFM ((FM)) | 11/26/1990 | |
TN 22 | en | Checking Parallel Rocker (at Elevator Actuator Rod) in Fin. Exchange of this Part and Amendment to AFM ((FM, FM2)) | 11/26/1990 | |
TN 23 | de | Revision of AFM ((FM)) | 01/29/1991 | |
TN 23 | en | Revision of AFM ((FM, FM2)) | 01/29/1991 | |
TN 24 | de | A. Amendment of AMM; B. Inspection Program to Increase Service Life ((MM)) | 05/04/1992 | |
TN 24 | en | A. Amendment of AMM; B. Inspection Program to Increase Service Life ((MM, ICA)) | 05/04/1992 | |
TN 25 | en | Rudder Actuated by Means of Hand Lever at Left Cockpit Wall in Front Pilot Seat ((FM)) | 02/16/1993 | |
TN 25 | de | Rudder Actuated by Means of Hand Lever at Left Cockpit Wall in Front Pilot Seat ((FM)) | 02/16/1993 | |
TN 26 | en | Inspecting Elevator Pushrod | 07/01/1983 | |
TN 26 | de | Inspecting Elevator Pushrod | 07/01/1983 | |
TN 27 | en | Securing of L'Hotellier Quick-Release Connectors (Ball & Swivel Joints) as per AD 93-001 L'Hotellier of German Civil Aviation Authority (LBA) | 08/04/1993 | |
TN 27 | de | Securing of L'Hotellier Quick-Release Connectors (Ball & Swivel Joints) as per AD 93-001 L'Hotellier of German Civil Aviation Authority (LBA) | 08/04/1993 | |
TN 28 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 28 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 29 | de | Extension of Service Life Beyond 12000 Operation Hours ((MM)) | 07/25/2003 | |
TN 29 | en | Extension of Service Life Beyond 12000 Operation Hours ((ICA, MM)) | 07/25/2003 | |
TN 30 | de | Rudder Control by Hand for Rear Pilot Seat as Amendment to TN 25. (with a Lever at Left Cockpit Wall) Relocation of Towing Cable Release Handle in Front and Rear Seat ((FM)) | 01/22/2007 | |
TN 30 | en | Rudder Control by Hand for Rear Pilot Seat as Amendment to TN 25. (with a Lever at Left Cockpit Wall) Relocation of Towing Cable Release Handle in Front and Rear Seat ((FM)) | 01/22/2007 | |
TN 31 | en | Installation of Transponder Antenna Inside Fuselage Behind Landing Gear ((WI)) | 02/05/2008 | |
TN 31 | de | Installation of Transponder Antenna Inside Fuselage Behind Landing Gear ((WI)) | 02/05/2008 | |
TN 32 | en | Headrest for Front Seat ((FM, FM2)) | 06/01/2010 | |
TN 32 | de | Headrest for Front Seat ((FM)) | 06/01/2010 | |
TN 33 | en | Alternative Rim for Main Wheel ((MI)) | 06/01/2010 | |
TN 33 | de | Alternative Rim for Main Wheel ((MI)) | 06/01/2010 | |
TN 34 | en | A) Main Wheel with Larger Diameter; B) Main Wheel Fairing with more Ground Clearance; C) Wheels at Wing Tips instead of Skids ((FM, ICA)) | 03/01/2012 | |
TN 34 | de | A) Main Wheel with Larger Diameter; B) Main Wheel Fairing with more Ground Clearance; C) Wheels at Wing Tips instead of Skids ((FM)) | 03/01/2012 | |
TN 35 | en | A) Extended Diagram for Mass and C.G. of Empty Glider; B) Seat of Pilot in Command ((FM, FM2)) | 03/01/2012 | |
TN 35 | de | A) Extended Diagram for Mass and C.G. of Empty Glider; B) Seat of Pilot in Command ((FM)) | 03/01/2012 | |
TN 36 | en | Modification of Lever, which Prevents Front Canopy to be Locked, while Rear Canopy is Locked | 03/01/2012 | |
TN 36 | de | Modification of Lever, which Prevents Front Canopy to be Locked, while Rear Canopy is Locked | 03/01/2012 | |
TN 37 | en | Wheel Brake Lever on Stick ((FM)) | 03/29/2016 | |
TN 37 | de | Wheel Brake Lever on Stick ((FM)) | 03/29/2016 | |
TN 38 | en | Inspection of Rudder Control by a Hand Lever ((FM)) | 05/31/2016 | |
TN 38 | de | Inspection of Rudder Control by a Hand Lever ((FM)) | 05/31/2016 | |
TN 39 | en | Modified Brake Fluid Expansion Tank ((MM, ICA)) | 08/01/2017 | |
TN 39 | de | Modified Brake Fluid Expansion Tank ((MM)) | 08/01/2017 | |
TN 40 | de | General Improvements ((FM)) | 09/24/2018 | |
TN 40 | en | General Improvements ((FM, FM2)) | 09/24/2018 | |
TN 41 | en | Cracks in Bonding of Wing Root Rib | 02/04/2019 | |
TN 41 | Iss 2 | de | Cracks in Bonding of Wing Root Rib ((WI)) | 08/07/2023 |
TN 41 | Iss 2 | en | Cracks in Bonding of Wing Root Rib ((WI)) | 08/07/2023 |
TN 42 | Iss 2 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 10/15/2020 |
TN 42 | Iss 2 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((ICA, MM)) | 10/15/2020 |
TN 43 | de | Clevis Pins on Connection Point of Control Cable and Rudder | 11/04/2020 | |
TN 43 | en | Clevis Pins on Connection Point of Control Cable and Rudder | 11/04/2020 | |
TN 44 | de | Towing Cable Release Handle in Front Cockpit Moved Upwards | 11/16/2020 | |
TN 44 | en | Towing Cable Release Handle in Front Cockpit Moved Upwards | 11/16/2020 | |
TN 45 | en | Hand Lever for Rudder Control | 05/05/2022 | |
TN 45 | de | Hand Lever for Rudder Control | 05/05/2022 | |
TN 46 | en | Tost Main Brake Cylinder ((ICA, MM)) | 08/07/2023 | |
TN 46 | de | Tost Main Brake Cylinder ((MM)) | 08/07/2023 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | US Type Certificate | 11/23/2018 | |
TN 1 | en | US Type Certificate | 11/23/2018 | |
TN 2 | de | Checking Free Movement of Front Rudder Pedals | 07/17/2019 | |
TN 2 | en | Checking Free Movement of Front Rudder Pedals | 07/17/2019 | |
TN 3 | en | (A) Hand-Operated Rudder Control in Front Cockpit; (B) Additional Hand-Operated Rudder Control in Rear Cockpit ((FM)) | 09/05/2019 | |
TN 3 | de | (A) Hand-Operated Rudder Control in Front Cockpit; (B) Additional Hand-Operated Rudder Control in Rear Cockpit ((FM)) | 09/05/2019 | |
TN 4 | de | Additional Wheel Brake Lever on Front Stick ((FM)) | 09/05/2019 | |
TN 4 | en | Additional Wheel Brake Lever on Front Stick ((FM)) | 09/05/2019 | |
TN 5 | de | Inspection of Screw Lock at Automatic Connection of Airbrake Control System | 09/04/2020 | |
TN 5 | en | Inspection of Screw Lock at Automatic Connection of Airbrake Control System | 09/04/2020 | |
TN 6 | de | Clevis Pins on Connection Point of Control Cable and Rudder ((MM)) | 11/04/2020 | |
TN 6 | en | Clevis Pins on Connection Point of Control Cable and Rudder ((MM)) | 11/04/2020 | |
TN 7 | de | Towing Cable Release Handle in Front Cockpit Moved Upwards | 11/16/2020 | |
TN 7 | en | Towing Cable Release Handle in Front Cockpit Moved Upwards | 11/16/2020 | |
TN 8 | de | Hand Lever for Rudder Control | 05/05/2022 | |
TN 8 | en | Hand Lever for Rudder Control | 05/05/2022 | |
TN 9 | en | Amendment of Manuals ((FM)) | 06/20/2022 | |
TN 9 | de | Amendment of Manuals ((FM)) | 06/20/2022 | |
TN 10 | de | Revision of AMM ((MM)) | 08/07/2023 | |
TN 10 | en | Revision of AMM ((MM)) | 08/07/2023 | |
TN 11 | en | Cracks in Bonding of Wing Root Rib ((WI)) | 08/07/2023 | |
TN 11 | de | Cracks in Bonding of Wing Root Rib ((WI)) | 08/07/2023 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Additional, Removable Trim Ballast in Fuselage Nose ((FM)) | 01/08/2008 | |
TN 1 | en | Additional, Removable Trim Ballast in Fuselage Nose ((FM)) | 01/08/2008 | |
TN 2 | de | A) Rudder Actuated by Means of Hand Lever at Left Cockpit Wall in Front Pilot Seat; (B) Rudder Actuated by Means of Hand Lever at Left Cockpit Wall in Rear Pilot Seat; (C) Parting Point between Pedals & Rudder Control System; (D) Additional Wheel Brake Lever on Front Control Stick ((FM [en])) | 03/01/2009 | |
TN 3 | de | Replacement of Batteries as Driving Force (Lead Accumulators) by Lifepo4.Cathode ((FM)) | 07/01/2009 | |
TN 4 | de | Modification of Fuel-Supply Line ((FM [en])) | 09/09/2009 | |
TN 5 | en | Alternative Rim for Main Wheel ((MI)) | 06/01/2010 | |
TN 5 | de | Alternative Rim for Main Wheel | 06/01/2010 | |
TN 6 | de | Wheel Brake Lever on Control Stick ((FM)) | 06/01/2010 | |
TN 6 | en | Wheel Brake Lever on Control Stick ((FM)) | 06/01/2010 | |
TN 7 | de | Trim Ballast for Spin Flights (Spin Ballast) ((FM)) | 12/12/2012 | |
TN 7 | en | Trim Ballast for Spin Flights (Spin Ballast) ((FM)) | 12/12/2012 | |
TN 8 | de | Modification of Lever, which Prevents Front Canopy to be Locked, while Rear Canopy is Locked | 03/01/2012 | |
TN 8 | en | Modification of Lever, which Prevents Front Canopy to be Locked, while Rear Canopy is Locked | 03/01/2012 | |
TN 9 | de | Troubleshooting of Engine Control Unit (ECU) | 09/19/2014 | |
TN 9 | en | Troubleshooting of Engine Control Unit (ECU) | 09/19/2014 | |
TN 10 | de | A) New Calibration of Rotor Internal Cooling Temperature Depending on Position of Temperature Sensor; B) Various Corrections of Manuals ((FM)) | 04/01/2015 | |
TN 10 | en | A) New Calibration of Rotor Internal Cooling Temperature Depending on Position of Temperature Sensor; B) Various Corrections of Manuals ((FM)) | 04/01/2015 | |
TN 11 | en | Replacement of Silencer | 01/08/2016 | |
TN 11 | Iss 2 | en | Replacement of Silencer | 07/19/2017 |
TN 11 | Iss 2 | de | Replacement of Silencer | 07/19/2017 |
TN 12 | en | Wheel Brake Lever on Stick ((FM)) | 03/29/2016 | |
TN 12 | de | Wheel Brake Lever on Stick ((FM)) | 03/29/2016 | |
TN 13 | en | Modified Brake Fluid Expansion Tank ((ICA, MM)) | 08/01/2017 | |
TN 13 | de | Modified Brake Fluid Expansion Tank ((MM)) | 08/01/2017 | |
TN 14 | en | Improvement of Performance Map of New IAE50R-AA ECU with S/Ns "AE00XXX" which were Installed as Standard from 2014 Onwards | 05/22/2018 | |
TN 14 | de | Improvement of Performance Map of New IAE50R-AA ECU with S/Ns "AE00XXX" which were Installed as Standard from 2014 Onwards | 05/22/2018 | |
TN 15 | en | Cracks in Bonding of Wing Root Rib | 02/04/2019 | |
TN 15 | Iss 2 | de | Cracks in Bonding of Wing Root Rib ((WI)) | 08/07/2023 |
TN 15 | Iss 2 | en | Cracks in Bonding of Wing Root Rib ((WI)) | 08/07/2023 |
TN 16 | en | General Improvements ((FM)) | 09/24/2018 | |
TN 16 | Iss 2 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 10/15/2020 |
TN 16 | Iss 2 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 10/15/2020 |
TN 17 | de | Clevis Pins on Connection Point of Control Cable and Rudder | 11/04/2020 | |
TN 17 | en | Clevis Pins on Connection Point of Control Cable and Rudder | 11/04/2020 | |
TN 18 | en | Towing Cable Release Handle in Front Cockpit Moved Upwards | 11/16/2020 | |
TN 18 | de | Towing Cable Release Handle in Front Cockpit Moved Upwards | 11/16/2020 | |
TN 19 | en | Hand Lever for Rudder Control | 05/05/2022 | |
TN 19 | de | Hand Lever for Rudder Control | 05/05/2022 | |
TN 20 | Iss 2 | en | Further Product Improvements ((FM)) | 06/28/2023 |
TN 20 | Iss 2 | de | Further Product Improvements ((FM)) | 06/28/2023 |
TN 21 | en | Registration as FAA Standard C of A ((FM)) | 09/21/2022 | |
TN 22 | de | Revision of AMM ((MM)) | 08/07/2023 | |
TN 22 | en | Revision of AMM ((MM)) | 08/07/2023 | |
TN 23 | de | Alternative Rotor Cooling Air Intake Filter ((MM)) | 08/07/2023 | |
TN 23 | en | Alternative Rotor Cooling Air Intake Filter ((MM)) | 08/07/2023 | |
TN 24 | en | Introduction of an Alternative Fuel Main Filter Due to End of Production of Existing One ((MM)) | 10/09/2023 | |
TN 24 | de | Introduction of an Alternative Fuel Main Filter Due to End of Production of Existing One ((MM)) | 10/09/2023 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1a | de | Some Structural Modification are Necessary for Netherlands | 06/20/1986 | |
TN 2 | en | Installation of Additional Bulkhead in Area of Nose Wheel | 09/13/1985 | |
TN 2 | de | Installation of Additional Bulkhead in Area of Nose Wheel | 09/13/1985 | |
TN 3 | de | Modification to ASK23B ((FM)) | 02/02/1986 | |
TN 3 | en | Modification to ASK23B | 02/02/1986 | |
TN 4 | de | Additional Seatpan Rest | 09/29/1986 | |
TN 4 | en | Additional Seatpan Rest | 09/29/1986 | |
TN 5 | en | A. Improvement of Wheel Brake; B. Modification to Control Stick ((MM)) | 09/06/1988 | |
TN 5 | de | A. Improvement of Wheel Brake; B. Modification to Control Stick ((MM)) | 09/06/1988 | |
TN 6 | en | Amendment of AFM & AMM | 05/10/1990 | |
TN 6 | de | Amendment of AFM & AMM ((FM)) | 05/10/1990 | |
TN 7 | en | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 7 | de | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 8 | en | Checking Parallel Rocker (at Elevator Actuator Rod) in Fin. Exchange of this Part and Amendment to AFM ((FM)) | 11/26/1990 | |
TN 8 | de | Checking Parallel Rocker (at Elevator Actuator Rod) in Fin. Exchange of this Part and Amendment to AFM ((FM)) | 11/26/1990 | |
TN 9 | en | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD 93-001 L'Hotellier of German Civil Aviation Authority (LBA) | 08/04/1993 | |
TN 9 | de | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD 93-001 L'Hotellier of German Civil Aviation Authority (LBA) | 08/04/1993 | |
TN 10 | en | Inspection of Main Bulkhead II (Landing Gear Bulkhead) for Damages | 09/14/1993 | |
TN 10 | de | Inspection of Main Bulkhead II (Landing Gear Bulkhead) for Damages | 09/14/1993 | |
TN 11 | de | Product Improvement - New Trim Spring Mod | 10/09/1996 | |
TN 11 | en | Product Improvement - New Trim Spring Mod | 10/09/1996 | |
TN 12 | de | A) Amendment of AMM B) Inspection Program to Increase Service Life ((MM)) | 06/16/1997 | |
TN 12 | en | A) Amendment of AMM; B) Inspection Program to Increase Service Life | 06/16/1997 | |
TN 13 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 13 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 14 | de | Installation of a Transponder Antenna Inside Fuselage Behind Landing Gear ((MI)) | 02/05/2008 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Adjusting Vane on Elevator | 07/28/1968 | |
TN 1 | en | Adjusting Vane on Elevator | 07/28/1968 | |
TN 2 | de | Releasable Brakechute | 08/28/1968 | |
TN 2 | en | Releasable Brakechute | 08/28/1968 | |
TN 3 | de | Inspection of Window for Elevator Connection Fitting | 05/19/1970 | |
TN 3 | en | Inspection of Window for Elevator Connection Fitting | 05/19/1970 | |
TN 4 | de | Inspection and Interior Preservation of Wing Spar | 05/10/1989 | |
TN 4 | en | Inspection and Interior Preservation of Wing Spar ((Annex)) | 05/10/1989 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Horn Mass Balance of Rudder | 03/06/1970 | |
TN 1 | en | Horn Mass Balance of Rudder | 03/06/1970 | |
TN 2 | en | Strengthening of Middle Bulkhead | 02/06/1970 | |
TN 2 | de | Strengthening of Middle Bulkhead | 02/06/1970 | |
TN 3 | de | Inspection and Stiffener of Rudder-Nose | 02/04/1970 | |
TN 3 | en | Inspection and Stiffener of Rudder-Nose | 02/04/1970 | |
TN 4 | de | Ice, Snow and Dirt Freezing on Push-Pull Rods | 04/24/1971 | |
TN 4 | en | Ice, Snow and Dirt Freezing on Push-Pull Rods | 04/24/1971 | |
TN 5 | de | Installation of Forward Towing Hook | 09/01/1971 | |
TN 5 | en | Installation of Forward Towing Hook | 09/01/1971 | |
TN 5a | de | Installation of Forward Towing Hook ((FM)) | 11/11/1971 | |
TN 5a | en | Installation of Forward Towing Hook | 11/11/1971 | |
TN 6 | en | Additional Ventilation of Wing Nose Boxes through Wing Root Rib | 10/20/1971 | |
TN 6 | de | Additional Ventilation of Wing Nose Boxes through Wing Root Rib | 10/20/1971 | |
TN 7ab | en | Ball Bearing Guided Push-Pull Rods for Aileron Movement Inside Wings | 11/11/1971 | |
TN 7ab | de | Ball Bearing Guided Push-Pull Rods for Aileron Movement Inside Wings | 11/11/1971 | |
TN 8 | de | Replacement of ASW 15 Fuselage by an ASW 15B Fuselage | 09/08/1972 | |
TN 8 | en | Replacement of ASW 15 Fuselage by an ASW 15B Fuselage | 09/08/1972 | |
TN 9 | de | Warning Paint According to NfL II-129/69 and NfL II-139/70 | 09/28/1972 | |
TN 10 | de | Inspection and Stiffening of Rudder Nose | 01/30/1973 | |
TN 10 | en | Inspection and Stiffening of Rudder Nose | 01/30/1973 | |
TN 11 | de | Modified Glue Joint of Fuselage Halves | 08/13/1973 | |
TN 11 | en | Modified Glue Joint of Fuselage Halves | 08/13/1973 | |
TN 12 | de | Change of Construction Material, Technological Improvement | 12/19/1973 | |
TN 12 | en | Change of Construction Material, Technological Improvement | 12/19/1973 | |
TN 13abc | de | a) New Rudder Pedals (without Heel Buckets), Simpler Front Towing Hook Fittings for Simpler Installation of Towing Hook, New Aileron Control Bellcrank in Cockpit Area. Modification of Bucket Seat Mold and Milled Plywood Bulkheads in Cockpit; b) Modification of C of G Towing Hook Fittings which Enable Easier Maintenance; c) Modification of Rudder Lower Hinge | 06/28/1974 | |
TN 13abc | en | a) New Rudder Pedals (without Heel Buckets), Simpler Front Towing Hook Fittings for Simpler Installation of Towing Hook, New Aileron Control Bellcrank in Cockpit Area. Modification of Bucket Seat Mold and Milled Plywood Bulkheads in Cockpit; b) Modification of C of G Towing Hook Fittings which Enable Easier Maintenance; c) Modification of Rudder Lower Hinge | 06/28/1974 | |
TN 14 | de | Fitting of All-Flying-Tail on Elevator and Fin | 07/03/1974 | |
TN 14 | en | Fitting of All-Flying-Tail on Elevator and Fin | 07/03/1974 | |
TN 15ab | en | Replacement of Conticell 60 Foam of Rudder Sandwich and of Upper Sandwich of Ailerons by Rocacell 71 Acrylic Foam | 09/12/1974 | |
TN 15ab | de | Replacement of Conticell 60 Foam of Rudder Sandwich and of Upper Sandwich of Ailerons by Rocacell 71 Acrylic Foam | 09/12/1974 | |
TN 16ab | en | Replacement of Control Cables Corresponding DIN 655 (DIN L9) by New Cables According LN 9374 According to AD 74-323 (R2) of LBA | 11/27/1974 | |
TN 16ab | de | Replacement of Control Cables Corresponding DIN 655 (DIN L9) by New Cables According LN 9374 According to AD 74-323 (R2) of LBA | 11/27/1974 | |
TN 17abc | de | Replacement of Older Fiberglass Cloth by Modern Weavings | 12/10/1974 | |
TN 17abc | en | Replacement of Older Fiberglass Cloth by Modern Weavings | 12/10/1974 | |
TN 18 | de | Change of Production Material. Replacement of Tubus-Core of Cellulose-Acetate by such of Poly-Carbonate | 03/05/1975 | |
TN 18 | en | Change of Production Material. Replacement of Tubus-Core of Cellulose-Acetate by such of Poly-Carbonate | 03/05/1975 | |
TN 19 | de | Exchange of Material | 08/17/1976 | |
TN 19 | en | Exchange of Material | 08/17/1976 | |
TN 20 | en | Increase of Service Life ((OM for 15, 15B)) | 03/16/1981 | |
TN 20 | de | Increase of Service Life ((OM for 15, 15B)) | 03/16/1981 | |
TN 21 | en | 1. Inspection of Elevator Actuator Bellcrank; 2. Amendment to OM ((OM for 15, 15B)) | 11/24/1981 | |
TN 21 | de | 1. Inspection of Elevator Actuator Bellcrank; 2. Amendment to OM ((OM for 15, 15B)) | 11/24/1981 | |
TN 22 | en | 1. Reinforcement of Elevator Actuator Bellcrank Inside Fuselage; 2. Correction of OM | 11/01/1982 | |
TN 22 | de | 1. Reinforcement of Elevator Actuator Bellcrank Inside Fuselage; 2. Correction of OM | 11/01/1982 | |
TN 23 | en | Inspection and Interior Preservation of Wing Spar ((OM for 15, 15B)) | 04/21/1988 | |
TN 23 | de | Inspection and Interior Preservation of Wing Spar ((OM for 15, 15B)) | 04/21/1988 | |
TN 23-1 | en | Inspection and Interior Preservation of Wing Spar | 10/18/1988 | |
TN 23-1 | de | Inspection and Interior Preservation of Wing Spar | 10/18/1988 | |
TN 23-2 | en | Inspection and Interior Preservation of Wing Spar | 02/08/1989 | |
TN 24 | en | Installation of a Tailwheel Instead of Plastic Foam Tailskid | 01/14/1991 | |
TN 24 | de | Installation of a Tailwheel Instead of Plastic Foam Tailskid | 01/14/1991 | |
TN 25 | de | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD 93-001 L'Hotellier of German Civil Aviation Authority (LBA) | 01/04/1994 | |
TN 25 | en | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD 93-001 L'Hotellier of German Civil Aviation Authority (LBA) | 01/04/1994 | |
TN 27 | de | Increase of Service Life ((OM for 15, 15B)) | 05/10/2007 | |
TN 27 | en | Increase of Service Life ((OM for 15, 15B)) | 05/10/2007 | |
TN 28 | de | Installation of Transponder Antennas Inside Fuselage Behind Landing Gear ((MI)) | 03/10/2008 | |
TN 29 | en | Inspection of Wing Root Ribs | 06/28/2021 | |
TN 29 | Iss 2 | de | Inspection of Wing Root Ribs (OM for 15, 15B; RI) | 05/04/2022 |
TN 29 | Iss 2 | en | Inspection of Wing Root Ribs (OM for 15, 15B; RI) | 05/04/2022 |
TN 272-26 (26) |
de | Modification of Wing Tip Edge (Winglets) ((FM for 15, 15B)) | 01/30/1999 | |
TN 272-26 (26) |
en | Modification of Wing Tip Edge (Winglets) ((FM for 15, 15B)) | 01/30/1999 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | en | Modification of Metal Fittings of Front Towing Hook and Wooden Parts in this Area | 05/06/1974 | |
TN 1 | de | Modification of Metal Fittings of Front Towing Hook and Wooden Parts in this Area | 05/06/1974 | |
TN 2 | en | Wide Range of Cockpit Load by Detachable Ballast Weights ((FM)) | 11/08/1974 | |
TN 2 | de | Wide Range of Cockpit Load by Detachable Ballast Weights ((FM)) | 11/08/1974 | |
TN 3 | de | Replacement of Control Cables Corresponding DIN 655 (DIN L9) by New Cables According LN 9374 According to AD 74-323 R2 of LBA | 12/11/1974 | |
TN 3 | en | Replacement of Control Cables Corresponding DIN 655 (DIN L9) by New Cables According LN 9374 According to AD 74-323 R2 of LBA | 12/11/1974 | |
TN 4ab | en | a) Construction of Fuselage with Fiberglass and Carbon-Fiber Sandwich; b) Installation of a Drag Chute Behind Landing Gear | 12/11/1975 | |
TN 4ab | de | a) Construction of Fuselage with Fiberglass and Carbon-Fiber Sandwich; b) Installation of a Drag Chute Behind Landing Gear ((FM)) | 12/11/1975 | |
TN 5 | en | Replacement of Tubus-core of Cellulose-Acetate by such of Poly-Carbonate | 03/05/1975 | |
TN 5 | de | Replacement of Tubus-core of Cellulose-Acetate by such of Poly-Carbonate | 03/05/1975 | |
TN 6 | de | Sealing of a Hose Connection of Water Ballast Exhaust | 11/26/1975 | |
TN 6 | en | Sealing of a Hose Connection of Water Ballast Exhaust | 11/26/1975 | |
TN 7 | de | Installation of a Drag Chute Behind Landing Gear ((FM)) | 03/08/1976 | |
TN 7 | en | Installation of a Drag Chute Behind Landing Gear | 03/08/1976 | |
TN 8 | de | Increased Max. All-Up-Weight to 610 kp ((OM)) | 06/03/1976 | |
TN 8 | en | Increased Max. All-Up-Weight to 610 kp ((OM)) | 06/03/1976 | |
TN 9 | de | Exchange of Material | 08/17/1976 | |
TN 9 | en | Exchange of Material | 08/17/1976 | |
TN 10 | de | Antimetric Four Part Harness | 01/10/1977 | |
TN 11 | de | Bigger Forward Opening Canopy ((FM)) | 01/10/1977 | |
TN 12 | en | Inspection and Interior Preservation of Wing Spar ((Annex)) | 05/08/1989 | |
TN 12 | de | Inspection and Interior Preservation of Wing Spar ((Annex)) | 05/08/1989 | |
TN 13 | en | A) Amendment of OM; B) Inspection Program to Increase Service Life | 01/19/1993 | |
TN 13 | de | A) Amendment of OM; B) Inspection Program to Increase Service Life | 01/19/1993 | |
TN 14 | en | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD 93-001 L'Hotellier of the German Civil Aviation Authority (LBA) | 02/25/1994 | |
TN 14 | de | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD 93-001 L'Hotellier of the German Civil Aviation Authority (LBA) | 02/25/1994 | |
TN 15 | en | Installation of Transponder Antenna Inside Fuselage Behind Landing Gear | 01/21/2015 | |
TN 15 | de | Installation of Transponder Antenna Inside Fuselage Behind Landing Gear ((MI)) | 01/21/2015 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Exchange of Material | 08/17/1976 | |
TN 1 | en | Exchange of Material | 08/17/1976 | |
TN 2 | en | Stiffening of Rudder Surface Panels | 09/06/1976 | |
TN 2 | de | Stiffening of Rudder Surface Panels | 09/06/1976 | |
TN 3 | de | Modification of Water Ballast Dumping System | 01/18/1977 | |
TN 3 | en | Modification of Water Ballast Dumping System | 01/18/1977 | |
TN 4ab | de | a) Installation of ASW20 Landing Gear into ASW19; b) Modification of ASW19 Landing Gear such that Landing Gear Doors Open Wider | 01/18/1977 | |
TN 4ab | en | a) Installation of ASW20 Landing Gear into ASW19; b) Modification of ASW19 Landing Gear such that Landing Gear Doors Open Wider | 01/18/1977 | |
TN 5 | de | Needed Modifications for Export to Netherlands | 02/12/1977 | |
TN 5 | en | Needed Modifications for Export to Netherlands | 02/12/1977 | |
TN 6ab | de | a) Higher All Up Weight b) Installation of Friction Trim | 06/12/1978 | |
TN 6ab | en | a) Higher All Up Weight b) Installation of Friction Trim | 06/12/1978 | |
TN 7 | de | Safety Measures for Inspection Hole Cover in Fuselage | 09/11/1978 | |
TN 7 | en | Safety Measures for Inspection Hole Cover in Fuselage | 09/11/1978 | |
TN 8 | de | Reduction of Production Requirement | 09/11/1978 | |
TN 8 | en | Reduction of Production Requirement | 09/11/1978 | |
TN 9 | de | Weight Savings as Product Improvement | 09/11/1978 | |
TN 9 | en | Weight Savings as Product Improvement | 09/11/1978 | |
TN 10 | de | Change of Wing Glass Layer Plan and Modification of Forward Wingroot Tangential Force Reinforcement | 09/12/1978 | |
TN 10 | en | Change of Wing Glass Layer Plan and Modification of Forward Wingroot Tangential Force Reinforcement | 09/12/1978 | |
TN 11 | de | Bigger Airbrake Area (Modified by Dipl.-Ing. G. Stich, Germany) | 07/03/1978 | |
TN 11 | Iss 2 | de | Bigger Airbrake Area (Modified by Dipl.-Ing. G. Stich, Germany) | 12/06/1995 |
TN 11b | en | Series Production of Bigger Airbrake According to TN 11 | 09/12/1979 | |
TN 11b | de | Series Production of Bigger Airbrake According to TN 11 | 09/12/1979 | |
TN 12 | en | Modification of Aileron and Elevator Hinge Fittings (Control Surface Side) | 11/20/1978 | |
TN 12 | de | Modification of Aileron and Elevator Hinge Fittings (Control Surface Side) | 11/20/1978 | |
TN 13 | Iss 2 | de | Improvement of Wheel Brake Operation (FM for 19 [en] 19B [en]) | 10/16/1985 |
TN 14 | en | Conversion of ASW19 from FAI Standard Class Glider into a Club Class Variant and Vice Versa ((FM for 19, 19B)) | 09/12/1979 | |
TN 14 | de | Conversion of ASW19 from FAI Standard Class Glider into a Club Class Variant and Vice Versa ((FM for 19, 19B)) | 09/12/1979 | |
TN 15 | en | Installation of a Tailwheel Instead of Plastic Foam Tailskid] ((OM for 19, 19B)) | 08/03/1983 | |
TN 15 | de | Installation of a Tailwheel Instead of Plastic Foam Tailskid ((OM for 19, 19B)) | 08/03/1983 | |
TN 16 | en | Continued Airworthiness; Amendments to AFM & OM ((OM for 19, 19B)) | 02/01/1984 | |
TN 16 | de | Continued Airworthiness; Amendments to AFM & OM ((OM for 19, 19B)) | 02/01/1984 | |
TN 17 | en | Continued Airworthiness: Precautions Against Elevator Flutter | 03/27/1984 | |
TN 17 | de | Continued Airworthiness: Precautions Against Elevator Flutter | 03/27/1984 | |
TN 18 | en | Possible Incorrect Mounting of Tow Release Cable Guiding Fittings, Resulting in Misfunction | 07/03/1984 | |
TN 18 | de | Possible Incorrect Mounting of Tow Release Cable Guiding Fittings, Resulting in Misfunction | 07/03/1984 | |
TN 19 | de | New Canopy Frame with Folding Up Instrument Panel and Emergency Jettison Device ((FM for 19, 19B)) | 10/19/1984 | |
TN 19 | en | New Canopy Frame with Folding Up Instrument Panel and Emergency Jettison Device ((FM for 19, 19B)) | 10/19/1984 | |
TN 20 | en | Instrument Binnacle Hinging Upwards with Canopy, Additionally, New Canopy Locking Swivel Handles | 01/16/1985 | |
TN 20 | de | Instrument Binnacle Hinging Upwards with Canopy, Additionally, New Canopy Locking Swivel Handles | 01/16/1985 | |
TN 21 | de | Instrument Binnacle Hinging Upwards with the Canopy | 02/17/1986 | |
TN 21 | en | Instrument Binnacle Hinging Upwards with the Canopy | 02/17/1986 | |
TN 22 | en | Automatic Elevator Connection ((OM for 19, 19B)) | 10/08/1986 | |
TN 22 | de | Automatic Elevator Connection ((OM for 19, 19B)) | 10/08/1986 | |
TN 23 | de | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 23 | en | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 24 | en | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD 93-001 L'Hotellier of the German Civil Aviation Authority (LBA) | 11/24/1993 | |
TN 24 | de | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD 93-001 L'Hotellier of the German Civil Aviation Authority (LBA) | 11/24/1993 | |
TN 25 | en | A) Amendment of AMM; B) Inspection Program to Increase Service Life ((OM for 19, 19B)) | 10/21/1996 | |
TN 25 | de | A) Amendment of AMM; B) Inspection Program to Increase Service Life ((OM for 19, 19B)) | 10/21/1996 | |
TN 26 | en | Modification of Wing Tip Edge (Winglets) | 01/30/1999 | |
TN 26 | de | Modification of Wing Tip Edge (Winglets) ((FM for 19, 19B)) | 01/30/1999 | |
TN 27 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 27 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 28 | de | Installation of Transponder Antennas Inside Fuselage Behind Landing Gear ((MI)) | 01/14/2008 | |
TN 29 | en | Retrofit of a Forward Tow Release | 08/21/2018 | |
TN 29 | de | Retrofit of a Forward Tow Release | 08/21/2018 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | en | Reinforcement of Forward Tow Hook Attachment Point | 10/18/1977 | |
TN 1 | de | Reinforcement of Forward Tow Hook Attachment Point | 10/18/1977 | |
TN 2 | de | Modifications for Export to Netherlands | 01/18/1978 | |
TN 2 | en | Modifications for Export to Netherlands | 01/18/1978 | |
TN 2b | de | Modifications for Export to Netherlands | 06/21/1979 | |
TN 2c | de | Modifications for Export to Netherlands | 08/22/1984 | |
TN 2d | de | Modifications for Export to Netherlands | 08/22/1984 | |
TN 3 | de | Glue Joint of Wing Leading Edge between Wing Root Rib and Change of Taper in Midwing Area | 02/08/1978 | |
TN 3 | en | Glue Joint of Wing Leading Edge between Wing Root Rib and Change of Taper in Midwing Area | 02/08/1978 | |
TN 4 | en | Safety Measures for Inspection Hole Cover in Fuselage | 09/11/1978 | |
TN 4 | de | Safety Measures for Inspection Hole Cover in Fuselage | 09/11/1978 | |
TN 5 | en | Front and Rear Wing Attachment Tube Crossing Fuselage. P/N 200.11.0001 and 200.11.0002 | 09/11/1978 | |
TN 5 | de | Front and Rear Wing Attachment Tube Crossing Fuselage. P/N 200.11.0001 and 200.11.0002 | 09/11/1978 | |
TN 6 | en | Weight Saving as Product Improvement | 09/29/1978 | |
TN 6 | de | Weight Saving as Product Improvement | 09/29/1978 | |
TN 7 | en | Modification of Aileron, Elevator and Flap Hinge Fittings (Control Surface Side) | 01/03/1979 | |
TN 7 | de | Modification of Aileron, Elevator and Flap Hinge Fittings (Control Surface Side) | 01/03/1979 | |
TN 8a | en | Detachable Wing Tip | 11/30/1978 | |
TN 8a | de | Detachable Wing Tip | 11/30/1978 | |
TN 8b | en | Increased Wingspan (16,59 m; 54,43 ft) by Attaching Outer Wing Panels | 03/13/1979 | |
TN 8b | de | Increased Wingspan (16,59 m; 54,43 ft) by Attaching Outer Wing Panels | 03/13/1979 | |
TN 9 | en | Wheel Brake Operation | 12/13/1978 | |
TN 9 | de | Wheel Brake Operation | 12/13/1978 | |
TN 10 | en | Changes in German Version of AFM | 12/08/1980 | |
TN 10 | de | Changes in German Version of AFM ((FM)) | 12/08/1980 | |
TN 11 | de | Modification of Laminating Resin System | 12/03/1980 | |
TN 12 | en | Inspection of Aileron Weight and Aileron CG and Inspection of Play (Backlash) in Aileron and Flap Control Circuits to Avoid Flutter Risk | 02/17/1981 | |
TN 12 | de | Inspection of Aileron Weight and Aileron CG and Inspection of Play (Backlash) in Aileron and Flap Control Circuits to Avoid Flutter Risk | 02/17/1981 | |
TN 13 | en | Installation of Tailwheel Instead of Plastic Foam Tailwheel ((OM for 20, 20L)) | 03/03/1983 | |
TN 13 | de | Installation of Tailwheel Instead of Plastic Foam Tailwheel ((OM for 20, 20L)) | 03/03/1983 | |
TN 14 | en | Preliminary AFM & AMM | 06/08/1983 | |
TN 14 | de | Preliminary AFM & AMM | 06/08/1983 | |
TN 15 | en | Product Improvement ((FM)) | 08/30/1983 | |
TN 15 | de | Product Improvement ((FM)) | 08/30/1983 | |
TN 16 | Iss 2 | en | Installation of a Front Towing Hook (FM for 20, 20B, 20BL, 20C, 20CL, 20L) | 06/28/1984 |
TN 16 | Iss 2 | de | Installation of a Front Towing Hook (FM for 20, 20B, 20BL, 20C, 20CL, 20L) | 06/28/1984 |
TN 17 | en | Continued Airworthiness; Amendments to AFM & OM ((FM for 20, 20L)) | 02/13/1984 | |
TN 17 | de | Continued Airworthiness; Amendments to AFM & OM ((FM for 20, 20L)) | 02/13/1984 | |
TN 18 | de | Exchange of ASW 20 Fuselage against that of ASW 20C ((FM for 20, 20L)) | 05/21/1984 | |
TN 19a | en | Detachable Wing Tip | 05/15/1984 | |
TN 19a | de | Detachable Wing Tip | 05/15/1984 | |
TN 19b | en | Increased Span to 16.59 m by Attaching Outer Wing Extensions | 12/12/1984 | |
TN 19b | de | Increased Span to 16.59 m by Attaching Outer Wing Extensions | 12/12/1984 | |
TN 20a | en | Detachable Wing Tip | 05/15/1984 | |
TN 20a | de | Detachable Wing Tip | 05/15/1984 | |
TN 20b | en | Increased Span to 16.59 m by Attaching Outer Wing Extensions | 12/12/1984 | |
TN 20b | de | Increased Span to 16.59 m by Attaching Outer Wing Extensions | 12/12/1984 | |
TN 21 | en | Possible Incorrect Mounting of Tow Release Cable Guiding Fittings, Resulting in Misfunction | 07/03/1984 | |
TN 21 | de | Possible Incorrect Mounting of Tow Release Cable Guiding Fittings, Resulting in Misfunction | 07/03/1984 | |
TN 22 | en | Upward-Folding Instrument Binnacle | 01/16/1985 | |
TN 22 | de | Upward-Folding Instrument Binnacle | 01/16/1985 | |
TN 23 | en | Exchange of Laminate Resin System | 03/22/1985 | |
TN 23 | de | Exchange of Laminate Resin System | 03/22/1985 | |
TN 24 | en | Exchange of Material | 03/22/1985 | |
TN 24 | de | Exchange of Material | 03/22/1985 | |
TN 25 | en | Canopy Frame and Emergency Jettison Device ((FM for 20B)) | 10/24/1985 | |
TN 25 | de | Canopy Frame and Emergency Jettison Device (FM for 20B, 20BL, 20C, 20CL) | 10/24/1985 | |
TN 26 | en | Instrument Binnacle Hinging Upwards with the Canopy | 02/14/1986 | |
TN 26 | de | Instrument Binnacle Hinging Upwards with the Canopy | 02/14/1986 | |
TN 27 | en | Covering Elevator to Stabilizer Gap on Upper Side by Elastic Lip Seal (Steel or Plastic) (FM for 20B, 20BL, 20C, 20CL; OM for 20, 20L) | 08/26/1986 | |
TN 27 | de | Covering Elevator to Stabilizer Gap on Upper Side by Elastic Lip Seal (Steel or Plastic) (FM for 20B, 20BL, 20C, 20CL; OM for 20, 20L) | 08/26/1986 | |
TN 28 | en | Replacement of Wings of ASW20 or 20L Against those of ASW20C Respectively 20CL ((FM for 20, 20L)) | 06/23/1986 | |
TN 28 | de | Replacement of Wings of ASW20 or 20L Against those of ASW20C Respectively 20CL ((FM for 20, 20L)) | 06/23/1986 | |
TN 29 | en | Automatic Elevator Connection ((OM for 20, 20L)) | 11/06/1986 | |
TN 29 | de | Automatic Elevator Connection ((OM for 20, 20L)) | 11/06/1986 | |
TN 30 | en | Preventive Measure Against Unintentional PIO (Pilot Induced Oscillations) ((FM for 20, 20L)) | 04/01/1987 | |
TN 30 | de | Preventive Measure Against Unintentional PIO (Pilot Induced Oscillations) ((FM for 20, 20L)) | 04/01/1987 | |
TN 31 | en | Preventive Measure Against Aileron Flutter (MM for 20B, 20BL, 20C, 20CL; OM for 20, 20L) | 06/24/1987 | |
TN 31 | de | Preventive Measure Against Aileron Flutter (MM for 20B, 20BL, 20C, 20CL; OM for 20, 20L) | 06/24/1987 | |
TN 32 | en | AFM & AMM Amendment (only when Exported to Italy) | 03/02/1988 | |
TN 33 | en | AFM Amendment (Only when Exported to Canada) | 06/02/1989 | |
TN 34 | de | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 34 | en | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 35 | en | Increase of Mass of Non-Lifting Parts by 10 kg ((FM for 20B, 20BL)) | 01/30/1990 | |
TN 35 | de | Increase of Mass of Non-Lifting Parts by 10 kg ((FM for 20B, 20BL)) | 01/30/1990 | |
TN 36 | en | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD 93-001 L'Hotellier of the German Civil Aviation Authority (LBA) | 09/22/1993 | |
TN 36 | de | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD 93-001 L'Hotellier of the German Civil Aviation Authority (LBA) | 09/22/1993 | |
TN 37 | en | Operation of 15m Wing Span Version with Winglets Designed by Messrs Fiberglas-Technik Rudolf Lindner (FM for 20B, 20BL, 20C, 20CL; OM for 20, 20L) | 01/31/1997 | |
TN 37 | de | Operation of 15m Wing Span Version with Winglets Designed by Messrs Fiberglas-Technik Rudolf Lindner (FM for 20B, 20BL, 20C, 20CL; OM for 20, 20L) | 01/31/1997 | |
TN 38 | de | Conversion to Hood that Swings Up to Rear (Designed by Akaflieg Koln, Germany) ((FM)) | 01/07/1997 | |
TN 39 | en | Amendment of AMM. Inspection Program to Increase Service Life | 02/16/1998 | |
TN 39 | de | Amendment of AMM. Inspection Program to Increase Service Life | 02/16/1998 | |
TN 39 | Iss 2 | de | Amendment of AMM. Inspection Program to Increase Service Life (MM for 20B, 20C, 20CL; OM for 20, 20L) | 04/17/1998 |
TN 39 | Iss 2 | en | Amendment of AMM. Inspection Program to Increase Service Life (MM for 20B, 20C, 20CL; OM for 20, 20L) | 04/17/1998 |
TN 40 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 40 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 41 | de | Installation of Transponder Antennas Inside Fuselage Behind Landing Gear ((MI)) | 01/14/2008 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Improvement of Flying Characteristics by Means of Modified Flaperon Mixer in Outboard Wing ((MM)) | 10/28/1983 | |
TN 1 | en | Improvement of Flying Characteristics by Means of Modified Flaperon Mixer in Outboard Wing ((MM)) | 10/28/1983 | |
TN 2 | en | Exchange of Trim Spring | 03/15/1985 | |
TN 2 | de | Exchange of Trim Spring | 03/15/1985 | |
TN 3 | en | Increase of Mass of Non Lift Producing Parts by 10 kg ((FM)) | 03/25/1985 | |
TN 3 | de | Increase of Mass of Non Lift Producing Parts by 10 kg ((FM)) | 03/25/1985 | |
TN 5 | de | Correction of AFM ((FM)) | 09/15/1986 | |
TN 5 | en | Correction of AFM ((FM)) | 09/15/1986 | |
TN 6 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 6 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 6 | en | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 6 | de | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 01/17/1990 | |
TN 7 | de | Inspecting Elevator Engaging Actuator (on Top of Fin) in Accordance with Instructions Given in AFM & AMM ((FM)) | 06/28/1991 | |
TN 7 | en | Inspecting Elevator Engaging Actuator (on Top of Fin) in Accordance with Instructions Given in AFM & AMM ((FM)) | 06/28/1991 | |
TN 8 | de | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD "93-001 L'Hotellier" of German Civil Aviation Authority (LBA) | 07/13/1993 | |
TN 8 | en | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD "93-001 L'Hotellier" of German Civil Aviation Authority (LBA) | 07/13/1993 | |
TN 9 | de | Conversion to ASW 22BL Series | 11/09/1993 | |
TN 10 | de | Air Inlet for Blast Holes in Wing by Means of NACA Ducts | 01/30/1998 | |
TN 10 | en | Air Inlet for Blast Holes in Wing by Means of NACA Ducts | 01/30/1998 | |
TN 11 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 11 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 12 | de | Carbon Push Rods Replacing Aluminum Alloy Push Rods in Aileron and Flap Control Circuits Inside Wings | 06/30/1999 | |
TN 12 | en | Carbon Push Rods Replacing Aluminum Alloy Push Rods in Aileron and Flap Control Circuits Inside Wings | 06/30/1999 | |
TN 13 | en | Amendment of AMM & RM. Inspection Program to Increase Service Life ((MM)) | 01/15/2002 | |
TN 13 | de | Amendment of AMM & RM. Inspection Program to Increase Service Life ((MM)) | 01/15/2002 | |
TN 14 | de | Wingtip Extension with Detachable Darlington - Winglets, 26,58 m ((FM)) | 03/10/2003 | |
TN 15 | en | Conversion of Sailplane ASW 22B and ASW 22BL (LBA No. 351) to Certified Powered Sailplane ASW 22BE and ASW 22BLE | 02/17/2006 | |
TN 15 | de | Conversion of Sailplane ASW 22B and ASW 22BL (LBA No. 351) to Certified Powered Sailplane ASW 22BE and ASW 22BLE | 02/17/2006 | |
TN 16 | en | Replacing a Lever of Flap Control System in Fuselage | 03/07/2008 | |
TN 16 | de | Replacing a Lever of Flap Control System in Fuselage | 03/07/2008 | |
TN 17 | en | Improvement of Elevator Control Stiffness after 3000 Operating Hours or After Repairs | 02/27/2014 | |
TN 17 | de | Improvement of Elevator Control Stiffness after 3000 Operating Hours or After Repairs | 02/27/2014 | |
TN 18 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM for 22)) | 04/03/2020 | |
TN 18 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake (MM for 22, 22B, 22BL) | 04/03/2020 | |
TN 19 | de | Installation of Transponder Antenna Behind or Sideways of Landing Gear ((MI)) | 06/08/2021 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | en | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD "93-001 L'Hotellier" of German Civil Aviation Authority (LBA) | 07/13/1993 | |
TN 1 | de | Securing of L'Hotellier Quick-Release Connectors (Ball and Swivel Joints) as per AD "93-001 L'Hotellier" of German Civil Aviation Authority (LBA) | 07/13/1993 | |
TN 2 | de | Use of Alternative Propeller ((FM)) | 07/16/1993 | |
TN 2 | en | Use of Alternative Propeller ((FM)) | 07/16/1993 | |
TN 3 | de | Conversion to Series ASW 22BLE (Provisional Only in German Issue) | 11/12/1993 | |
TN 4 | de | Air Inlet for Blast Holes in Wing by Means of NACA Ducts | 01/30/1998 | |
TN 4 | en | Air Inlet for Blast Holes in Wing by Means of NACA Ducts | 01/30/1998 | |
TN 5 | de | Powered Sailplane ASW 22BE Including All Variants According to TCDS 351 can be Approved as Sailplane ASW 22B or BL (whatever Variant is Applicable) After Power-Plant Components have been Removed or After Installation of Powerplant Components it can Again be Approved as Powered Sailplane ASW 22BE or One of Variants According to TCDS 834 | 01/20/1999 | |
TN 5 | en | Powered Sailplane ASW 22BE Including All Variants According to TCDS 351 can be Approved as Sailplane ASW 22B or BL (whatever Variant is Applicable) After Power-Plant Components have been Removed or After Installation of Powerplant Components it can Again be Approved as Powered Sailplane ASW 22BE or One of Variants According to TCDS 834 | 01/20/1999 | |
TN 6 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 6 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 7 | de | Carbon Push Rods Replacing Aluminum Alloy Push Rods in Aileron and Flap Control Circuits Inside Wings | 06/30/1999 | |
TN 7 | en | Carbon Push Rods Replacing Aluminum Alloy Push Rods in Aileron and Flap Control Circuits Inside Wings | 06/30/1999 | |
TN 8A | de | Wing Extension with Removable Darlington Winglets, 26.58 m with an Increase in Non-Load-Bearing Parts to 372 kg (Provisional Only in German Issue) | 05/27/2003 | |
TN 8B | de | Wing Extension with Removable Darlington Winglets, 26.58 m with an Increase in Non-Load-Bearing Parts to 372 kg (Provisional Only in German Issue) ((FM)) | 05/27/2003 | |
TN 9 | en | New Propeller AS2F1-1/R153-92-N1 for ASW 22BLE50R | 01/31/2005 | |
TN 9 | de | New Propeller AS2F1-1/R153-92-N1 for ASW 22BLE50R ((FM)) | 01/31/2005 | |
TN 10A,B,C | de | Increase of Maximum Take-Off Mass to 850 kg - Exchange of ASW 22 BLE 50R AFM Page 4.22 (FM for 22BLE, 22BLE50R) | 09/03/2012 | |
TN 11 | de | New Fuel Lines (PUR) without Change at Specified Intervals ((MM)) | 06/05/2007 | |
TN 12 | de | Adjusting Drive Belt ((FM)) | 01/08/2008 | |
TN 12 | en | Adjusting Drive Belt | 01/08/2008 | |
TN 13 | de | Installation of Transponder Antennas Behind or Sideways of Landing Gear (WI for 22BLE, 22BLE50R) | 01/31/2008 | |
TN 14 | de | Replacement of Carburetor Cap, Tightness of Bleeding Screw on Oil Pump | 09/05/2012 | |
TN 14 | en | Replacement of Carburetor Cap, Tightness of Bleeding Screw on Oil Pump | 09/05/2012 | |
TN 15 | de | Inspection of Propeller Bearing Play ((MM for 22BE/BLE, 22M)) | 05/07/2015 | |
TN 15 | en | Inspection of Propeller Bearing Play | 05/07/2015 | |
TN 16 | en | Replacement of Silencer | 01/08/2016 | |
TN 16 | Iss 2 | en | Replacement of Silencer | 07/19/2017 |
TN 16 | Iss 2 | de | Replacement of Silencer | 07/19/2017 |
TN 17 | de | Specification Update of Flexible Fuel Tanks | 09/15/2017 | |
TN 17 | en | Specification Update of Flexible Fuel Tanks | 09/15/2017 | |
TN 18 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake (MM for 22BE, 22BLE, 22BLE50R) | 04/03/2020 | |
TN 18 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake (MM for 22BE, 22BLE, 22BLE50R, 22M) | 04/03/2020 | |
TN 19 | en | Wing Tip Extension 26.9m | 05/25/2020 | |
TN 19 | Iss 2 | de | Wing Tip Extension 26.9m ((FM for 22BLE, 22BLE50R)) | 03/02/2021 |
TN 19 | Iss 2 | en | Wing Tip Extension 26.9m ((FM for 22BLE, 22BLE50R)) | 03/02/2021 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Deviating Construction for Holland | 03/29/1989 | |
TN 2 | en | Increase of Mass of Non-Lifting Parts by 15 kg ((FM)) | 02/08/1990 | |
TN 2 | de | Increase of Mass of Non-Lifting Parts by 15 kg ((FM)) | 02/08/1990 | |
TN 3 | en | Smiley-Waterbags ((MM)) | 04/27/1990 | |
TN 3 | de | Smiley-Waterbags ((MM)) | 04/27/1990 | |
TN 4 | en | AFM Revision ((FM)) | 01/30/1991 | |
TN 5 | en | AFM Revision ((FM)) | 01/30/1992 | |
TN 6 | en | Modification for Optional Operation with/without 0.3m High Winglets ((FM)) | 08/18/1992 | |
TN 6 | de | Modification for Optional Operation with/without 0.3m High Winglets ((FM)) | 08/18/1992 | |
TN 7 | de | Amendment of AFM & AMM ((FM, MM)) | 04/25/1994 | |
TN 7 | en | Amendment of AFM & AMM (FM, MM, MM2) | 04/25/1994 | |
TN 7 | Amend 2 | en | Amendment of AFM & AMM | 02/28/1995 |
TN 7 | Amend 2 | de | Amendment of AFM & AMM | 02/28/1995 |
TN 8 | en | Modification of Contour of Outboard Wing Leading Edge | 06/23/1994 | |
TN 8 | de | Modification of Contour of Outboard Wing Leading Edge | 06/23/1994 | |
TN 9 | en | Modification of Water Ballast System ((FM)) | 06/23/1994 | |
TN 9 | de | Modification of Water Ballast System ((FM)) | 06/23/1994 | |
TN 10 | en | Improvement of Product by Modifications of Fuselage ((MM)) | 06/30/1994 | |
TN 10 | de | Improvement of Product by Modifications of Fuselage ((MM)) | 06/30/1994 | |
TN 11 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 11 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 12 | de | Modification of Landing Gear | 10/18/2006 | |
TN 12 | en | Modification of Landing Gear | 10/18/2006 | |
TN 13 | en | Installation of Winglets ((FM)) | 03/20/2007 | |
TN 13 | de | Installation of Winglets ((FM)) | 03/20/2007 | |
TN 14 | en | Relocation of Aerotow Hook to Fuselage Nose ((MM for 24, 24B)) | 06/26/2007 | |
TN 14 | de | Relocation of Aerotow Hook to Fuselage Nose ((MM for 24, 24B)) | 06/26/2007 | |
TN 15 | en | Increase of Service Life ((MM)) | 12/06/2007 | |
TN 15 | de | Increase of Service Life ((MM)) | 12/06/2007 | |
TN 16 | de | Installation of Transponder Antennas Behind or Sideways of Landing Gear ((MI, MIB)) | 01/31/2008 | |
TN 17 | en | Installation of a Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 17 | de | Installation of a Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 18 | en | Installation of a Cockpit Vent Behind Canopy Frame ((FM)) | 03/01/2011 | |
TN 18 | de | Installation of a Cockpit Vent Behind Canopy Frame ((FM)) | 03/01/2011 | |
TN 21 | en | Retrofit of a Forward Tow Release | 08/22/2018 | |
TN 21 | de | Retrofit of a Forward Tow Release | 08/22/2018 | |
TN 22 | de | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 22 | en | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 23 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 | |
TN 23 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 | |
TN 40 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 40 | de | Nose Bolt with O-Ring | 06/28/1999 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Deviating Construction for Holland | 03/29/1989 | |
TN 2 | de | A) Securing of Screws at Engine Support Bracket; B) Replacement of Lower Support Bracket of Gas Spring Near Screw Jack; C) Supplement to AMM | 11/07/1991 | |
TN 2 | en | A) Securing of Screws at Engine Support Bracket; B) Replacement of Lower Support Bracket of Gas Spring Near Screw Jack; C) Supplement to AMM | 11/07/1991 | |
TN 3 | en | Modification for Optional Operation with/without 0.3m High Winglets | 09/09/1992 | |
TN 3 | en | AFM Revision | 03/03/1992 | |
TN 4 | en | Modification for Optional Operation with/without 0.3m High Winglets ((FM)) | 09/09/1992 | |
TN 4 | de | Modification for Optional Operation with/without 0.3m High Winglets ((FM)) | 09/09/1992 | |
TN 5 | en | Improvement of Product by Modification of Wing Leading Edge Section. Optional Retrofit Mod to Outboard Wing Leading Edge | 01/05/1995 | |
TN 5 | de | Improvement of Product by Modification of Wing Leading Edge Section. Optional Retrofit Mod to Outboard Wing Leading Edge | 01/05/1995 | |
TN 6 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 6 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 7 | en | Modification of Landing Gear | 10/18/2006 | |
TN 7 | de | Modification of Landing Gear | 10/18/2006 | |
TN 8 | en | Installation of Winglets ((FM)) | 03/20/2007 | |
TN 8 | de | Installation of Winglets ((FM)) | 03/20/2007 | |
TN 9 | de | Relocation of Aerotow Hook to Fuselage Nose ((FM)) | 06/26/2007 | |
TN 9 | en | Relocation of Aerotow Hook to Fuselage Nose ((FM)) | 06/26/2007 | |
TN 10 | en | Increase of Service Life ((MM)) | 12/06/2007 | |
TN 10 | de | Increase of Service Life ((MM)) | 12/06/2007 | |
TN 11 | de | Installation of Transponder Antennas Behind or Sideways of Landing Gear ((MI)) | 02/13/2009 | |
TN 12 | en | Installation of a Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 12 | de | Installation of a Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 15 | en | Specification Update of Flexible Fuel Tanks | 09/15/2017 | |
TN 15 | de | Specification Update of Flexible Fuel Tanks | 09/15/2017 | |
TN 16 | en | AFM Revision | 05/02/2019 | |
TN 17 | en | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 17 | de | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 18 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 | |
TN 18 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Deviating Construction for Holland | 03/29/1989 | |
TN 4 | en | Nose Bolt with O-Ring | 06/28/1999 | |
TN 4 | de | Nose Bolt with O-Ring | 06/28/1999 | |
TN 5 | de | Increase of Service Life ((MM)) | 12/06/2007 | |
TN 5 | en | Increase of Service Life | 12/06/2007 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Improvement of Crashworthiness and Weight Reduction of Fuselage | 10/02/1997 | |
TN 1 | en | Improvement of Crashworthiness and Weight Reduction of Fuselage | 10/02/1997 | |
TN 2 | en | Wings with Integrated (Wet Inner Surface) Water Ballast Tanks ((FM)) | 01/11/1999 | |
TN 2 | de | Wings with Integrated (Wet Inner Surface) Water Ballast Tanks ((FM)) | 01/11/1999 | |
TN 3 | de | Recognition of Designs in Austria | 03/01/1999 | |
TN 4 | en | New Winglets ((FM)) | 04/15/1999 | |
TN 4 | de | New Winglets ((FM)) | 04/15/1999 | |
TN 5 | en | Check of Control Circuit Clearance Inside Fuselage Tail Boom to Fin Intersection | 07/16/1999 | |
TN 5 | de | Check of Control Circuit Clearance Inside Fuselage Tail Boom to Fin Intersection | 07/16/1999 | |
TN 6 | en | Product Improvement. Change and Amendments to AFM, AMM & RM ((FM)) | 05/16/2000 | |
TN 6 | de | Product Improvement. Change and Amendments to AFM, AMM & RM ((FM)) | 05/16/2000 | |
TN 7 | en | Installation of a Fin (Tail) Water Ballast Tank | 11/20/2001 | |
TN 7 | de | Installation of a Fin (Tail) Water Ballast Tank ((FM)) | 11/20/2001 | |
TN 8 | en | Electric Power Supply by Solar Cells, Installed on Top of Fuselage Behind Canopy. Gate Valves for Water Ballast in Fuselage Instead of Valves Inside Wings. Use of "Light Weight" Parts in Fuselage. In-Flight Back Rest Position Adjustment is Replaced by Lighter System Adjustable Before Take-Off ((FM)) | 02/11/2002 | |
TN 8 | de | Electric Power Supply by Solar Cells, Installed on Top of Fuselage Behind Canopy. Gate Valves for Water Ballast in Fuselage Instead of Valves Inside Wings. Use of "Light Weight" Parts in Fuselage. In-Flight Back Rest Position Adjustment is Replaced by Lighter System Adjustable Before Take-Off ((FM)) | 02/11/2002 | |
TN 9 | en | Wings with Integrated (Wet Inner Surface) Water Ballast Tanks. Correction of Forward Empty Weight C. G. - Limits ((FM)) | 02/26/2002 | |
TN 9 | de | Wings with Integrated (Wet Inner Surface) Water Ballast Tanks. Correction of Forward Empty Weight C. G. - Limits ((FM)) | 02/26/2002 | |
TN 10 | de | Modification of Landing Gear | 10/18/2006 | |
TN 10 | en | Modification of Landing Gear | 10/18/2006 | |
TN 11 | de | Relocation of Aerotow Hook to Fuselage Nose ((MM)) | 06/26/2007 | |
TN 11 | en | Relocation of Aerotow Hook to Fuselage Nose ((MM)) | 06/26/2007 | |
TN 12 | en | Installation of Transponder Antennas at Fuselage Behind or Lateral to Landing Gear on an Aircraft with CFRP Fuselage | 01/31/2008 | |
TN 12 | de | Installation of Transponder Antennas at Fuselage Behind or Lateral to Landing Gear on an Aircraft with CFRP Fuselage ((MI)) | 01/31/2008 | |
TN 13 | de | Installation of a PCB-Transponder Antenna in Vertical Tail | 01/30/2009 | |
TN 14 | en | Installation of a Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 14 | de | Installation of a Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 15 | en | Installation of Cockpit Vent Behind Canopy Frame ((FM)) | 03/01/2011 | |
TN 15 | de | Installation of Cockpit Vent Behind Canopy Frame ((FM)) | 03/01/2011 | |
TN 17 | en | A) Installation of Tail Wheel Cover; B) Installation of Covers on Rudder; C) Replacement of Covers on Aileron & Flap Actuators; D) Modification of Blow Hole System | 11/20/2015 | |
TN 17 | de | A) Installation of Tail Wheel Cover; B) Installation of Covers on Rudder; C) Replacement of Covers on Aileron & Flap Actuators; D) Modification of Blow Hole System | 11/20/2015 | |
TN 18 | en | Alternative Hydraulic Wheel Brake System TOST | 02/01/2017 | |
TN 18 | de | Alternative Hydraulic Wheel Brake System TOST | 02/01/2017 | |
TN 19 | en | Manual Correction ((MM)) | 11/01/2017 | |
TN 19 | de | Manual Correction ((MM)) | 11/01/2017 | |
TN 20 | en | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 20 | de | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 21 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 | |
TN 21 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | en | Relocation of Aerotow Hook to Fuselage Nose ((MM)) | 07/12/2006 | |
TN 1 | de | Relocation of Aerotow Hook to Fuselage Nose ((MM)) | 07/12/2006 | |
TN 2 | de | Improved Attachment of RPM-Sensor, Improved Attachment of Fuel Pump. Upgrade of Hardware of Power-Plant Instrument. Exchange of Manual Pages ((FM)) | 09/01/2006 | |
TN 2 | en | Improved Attachment of RPM-Sensor, Improved Attachment of Fuel Pump. Upgrade of Hardware of Power-Plant Instrument. Exchange of Manual Pages ((FM)) | 09/01/2006 | |
TN 3 | en | New Software Versions of Power-Plant Instrument. Changes to Mechanical Control Unit & Propeller Stopper. Alternative Threaded End for Decompression Bowden Cable ((FM)) | 08/29/2006 | |
TN 3 | de | New Software Versions of Power-Plant Instrument. Changes to Mechanical Control Unit & Propeller Stopper. Alternative Threaded End for Decompression Bowden Cable ((FM)) | 08/29/2006 | |
TN 4 | de | Modification of Landing Gear | 10/18/2006 | |
TN 4 | en | Modification of Landing Gear | 10/18/2006 | |
TN 5 | de | Installation of Transponder Antennas Behind or Sideways of Landing Gear ((MI)) | 01/31/2008 | |
TN 6 | de | Directive for Fuels ((FM)) | 03/05/2009 | |
TN 6 | en | Directive for Fuels ((FM)) | 03/05/2009 | |
TN 7 | de | Variant of Software of Power-Plant Instrument, which Closes Solenoid Valve, when Engine is Retracted (Identified with an Appendix 'b' to the Version Number) ((FM)) | 03/05/2009 | |
TN 7 | en | Variant of Software of Power-Plant Instrument, which Closes Solenoid Valve, when Engine is Retracted (Identified with an Appendix 'b' to the Version Number) ((FM)) | 03/05/2009 | |
TN 8 | en | New Type of Propeller-Stopper ((MM)) | 11/06/2008 | |
TN 8 | de | New Type of Propeller-Stopper ((MM)) | 11/06/2008 | |
TN 9 | de | Installation of Propeller AS2F1-3 ((FM)) | 11/06/2008 | |
TN 9 | en | Installation of Propeller AS2F1-3 ((FM)) | 11/06/2008 | |
TN 10 | en | A) Different Cylinder Heads & Engine Bearer; B) Different Cable Routing Along Engine; C) Usage of Stepless Ear Clamps & Lock-Wire with PUR-Fuel Hoses ((MM)) | 02/18/2009 | |
TN 10 | de | A) Different Cylinder Heads & Engine Bearer; B) Different Cable Routing Along Engine; C) Usage of Stepless Ear Clamps & Lock-Wire with PUR-Fuel Hoses ((MM)) | 02/18/2009 | |
TN 11 | de | Installation of a PCB-Transponder Antenna in Vertical Tail | 01/30/2009 | |
TN 12 | de | Installation of a Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 12 | en | Installation of a Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 14 | de | Improvement of Power-Plant Control - Use of ASG 29E-System ((FM, MM)) | 02/01/2014 | |
TN 14 | en | Improvement of Power-Plant Control - Use of ASG 29E-System ((FM, MM)) | 02/01/2014 | |
TN 15 | de | Potential Cracks in Left and Right Engine Bearer and Attachment of Fuel Pump ((FM)) | 09/01/2014 | |
TN 15 | en | Potential Cracks in Left and Right Engine Bearer and Attachment of Fuel Pump ((FM)) | 09/01/2014 | |
TN 16 | de | Two Piece Engine Bearer with Direct Attachment of Bing-Fuel Pump | 07/01/2014 | |
TN 16 | en | Two Piece Engine Bearer with Direct Attachment of Bing-Fuel Pump | 07/01/2014 | |
TN 17 | de | New Type of Fuel Pump According to SOLO Technical Note TM4603-15 | 07/01/2014 | |
TN 17 | en | New Type of Fuel Pump According to SOLO Technical Note TM4603-15 | 07/01/2014 | |
TN 18 | en | Retrofitting a New Type of Fuel Pump According to SOLO Technical Note TM4603-15, instead of the Hitherto BING Fuel Pump | 07/01/2014 | |
TN 18 | de | Retrofitting a New Type of Fuel Pump According to SOLO Technical Note TM4603-15, instead of the Hitherto BING Fuel Pump | 07/01/2014 | |
TN 20 | en | Specification Update of Flexible Fuel Tanks ((MM1, MM2)) | 09/15/2017 | |
TN 20 | de | Specification Update of Flexible Fuel Tanks ((MM1, MM2)) | 09/15/2017 | |
TN 21 | en | Manual Correction ((MM)) | 11/01/2017 | |
TN 21 | Iss 2 | en | Manual Correction | 03/12/2018 |
TN 21 | Iss 2 | de | Manual Correction | 03/12/2018 |
TN 22 | de | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 22 | en | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 23 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 | |
TN 23 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM)) | 04/03/2020 | |
TN 24 | de | Installation of Three-Piece Airbrakes with Improved Effectiveness; New Winglets ((FM)) | 03/01/2023 | |
TN 24 | en | Installation of Three-Piece Airbrakes with Improved Effectiveness; New Winglets ((FM)) | 03/01/2023 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Relocation of Aerotow Hook to Fuselage Nose ((MM for 28, 28-18)) | 07/12/2006 | |
TN 1 | en | Relocation of Aerotow Hook to Fuselage Nose ((MM for 28, 28-18)) | 07/12/2006 | |
TN 2 | de | Modification of Landing Gear | 10/18/2006 | |
TN 2 | en | Modification of Landing Gear | 10/18/2006 | |
TN 3 | de | Conversion of Sailplane ASW 28-18 (TC EASA. A.017) into a Powered Sailplane ASW 28-18E According to TC EASA. A.034 | 04/16/2007 | |
TN 4 | de | Installation of Transponder Antennas Behind or Sideways of Landing Gear ((WI for 28, 28-18)) | 01/31/2008 | |
TN 5 | de | Installation of a PCB-Transponder Antenna in Vertical Tail | 01/30/2009 | |
TN 6 | de | Installation of a Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 6 | en | Installation of a Strobe Light in Nose of Vertical Fin | 03/01/2011 | |
TN 7 | de | Installation of a Cockpit Vent Behind Canopy Frame ((FM for 28, 28-18)) | 03/01/2011 | |
TN 7 | en | Installation of a Cockpit Vent Behind Canopy Frame ((FM for 28, 28-18)) | 03/01/2011 | |
TN 10 | en | Manual Correction ((MM for 28, 28-18)) | 11/01/2017 | |
TN 10 | Iss 2 | de | Manual Correction | 03/12/2018 |
TN 10 | Iss 2 | en | Manual Correction | 03/12/2018 |
TN 11 | en | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 11 | de | Alternative Rim for Main Wheel | 11/07/2019 | |
TN 12 | en | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM for 28, 28-18)) | 04/03/2020 | |
TN 12 | de | Specification of Service Life Limitations for Brake Hoses of Hydraulic Wheel Brake ((MM for 28, 28-18)) | 04/03/2020 | |
TN 13 | en | Installation of Three-Piece Airbrakes with Improved Effectiveness; New Winglets ((FM)) | 03/01/2023 | |
TN 13 | de | Installation of Three-Piece Airbrakes with Improved Effectiveness; New Winglets ((FM)) | 03/01/2023 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Revision of AMM ((MM)) | 08/07/2023 | |
TN 1 | en | Revision of AMM ((MM)) | 08/07/2023 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Installation of Tost Universal/53 Kombi 54 Resp. of Modified Tost Universal 53 | 12/14/1965 | |
TN 2 | de | Spar Tube on Pendulum Rudder | 10/30/1970 | |
TN 3 | de | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 04/12/1990 | |
TN 3 | en | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 04/12/1990 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Elevator | 10/04/1989 | |
TN 1 | en | Elevator | 10/04/1989 | |
TN 2 | de | Inspection of Elevator ((FM [en])) | 11/01/2021 | |
TN 3 | de | Limitation of Operating Range ((FM [en])) | 11/01/2021 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Occurrence of Wear. Interchangeable Socket Pins on Rear Fin Suspension | 08/18/1958 | |
TN 2 | en | Strengthening of Plywood Web on Outer Spar at Aileron Bell Crank | 10/25/1963 | |
TN 2 | de | Strengthening of Plywood Web on Outer Spar at Aileron Bell Crank | 10/25/1963 | |
TN 3 | en | Changing of Middle Elevator Bearing Support | 10/25/1963 | |
TN 3 | de | Changing of Middle Elevator Bearing Support | 10/25/1963 | |
TN 4 | en | Strengthening of Steel Tubes of Rear Fuselage | 10/29/1963 | |
TN 4 | de | Strengthening of Steel Tubes of Rear Fuselage | 10/29/1963 | |
TN 5 | de | Installation of a Brake Wheel | 03/01/1961 | |
TN 6 | de | Reinforcement of Tubular Steel Rods of Hull | 03/21/1961 | |
TN 7 | de | Additional Support of Elevator Bumper | 11/23/1961 | |
TN 8 | de | Additional Support of Elevator Push Rod | 11/23/1961 | |
TN 8 | en | Additional Support of Elevator Push Rod | 11/23/1961 | |
TN 9 | de | Double Tab on BK Bumper Fork | 09/12/1962 | |
TN 10 | de | Check of Stick Attachment in Rear Cockpit | 04/16/1963 | |
TN 10 | en | Check of Stick Attachment in Rear Cockpit | 04/16/1963 | |
TN 11 | de | Replacement of Steel Stick Universal Joint Block with One Made of Superlene | 11/26/1964 | |
TN 12 | de | Installation of Pressure Tapping Points for Dynamic Pressure Anemometers | 11/16/1965 | |
TN 13 | de | Installation of Tost Universal / 53-Kombi54 Resp. of Modified Tost Universal 53 | 12/14/1965 | |
TN 13 | en | Installation of Tost Universal / 53-Kombi54 Resp. of Modified Tost Universal 53 | 12/14/1965 | |
TN 14 | de | Installation of Tost Safety Clutch Universal/53 Kombi 54 or Modified Tost Safety Clutch Universal 53 | 12/13/1965 | |
TN 15 | de | Subsequent Installation of ASK 13 Wheel Suspension in K 7 | 01/26/1968 | |
TN 16 | de | Installation of a Removable Balance Weight ((FM, Appendix)) | 11/01/1975 | |
TN 16 | en | Installation of a Removable Balance Weight ((Appendix)) | 11/01/1975 | |
TN 16a | de | Installation of a Removable Balance Weight | 01/29/1990 | |
TN 17 | en | Installation of a Pneumatic Tailwheel in Exchange for Tailskid | 02/05/1986 | |
TN 17 | de | Installation of a Pneumatic Tailwheel in Exchange for Tailskid | 02/05/1986 | |
TN 18 | en | Elevator | 10/04/1989 | |
TN 18 | de | Elevator | 10/04/1989 | |
TN 19 | de | Installation of a Nose Wheel Instead of Skid | 01/29/1990 | |
TN 20 | de | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 04/12/1990 | |
TN 20 | en | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 04/12/1990 | |
TN 21 | de | Extension of Empty Mass Center of Gravity ((Appendix)) | 05/07/1993 | |
TN 22 | en | Inspection of Central Support of Elevator | 05/25/2010 | |
TN 22 | de | Inspection of Central Support of Elevator | 05/25/2010 | |
TN 23 | de | Installation of a Transponder Antenna Behind Landing Gear ((MI)) | 04/19/2010 | |
TN 24 | en | Inspection of Automatic Elevator Control Connection | 08/30/2012 | |
TN 24 | 1 | de | Inspection of Automatic Elevator Control Connection | 01/08/2013 |
TN 24 | 1 | en | Inspection of Automatic Elevator Control Connection | 01/08/2013 |
TN 25 | de | Inspection of Elevator ((Appendix)) | 07/12/2021 | |
TN 25 | en | Inspection of Elevator ((Appendix)) | 07/12/2021 | |
TN 25 | Iss 2 | en | Inspection of Elevator ((Appendix R1)) | 11/01/2023 |
TN 25 | Iss 2 | de | Inspection of Elevator ((Appendix R1)) | 11/01/2023 |
TN 26 | en | Limitation of Operating Envelope ((Appendix)) | 07/12/2021 | |
TN 26 | de | Limitation of Operating Envelope ((Appendix)) | 07/12/2021 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | en | Strengthening of Plywood Web on Outer Spar at Aileron Bell Crank | 10/29/1963 | |
TN 1 | de | Strengthening of Plywood Web on Outer Spar at Aileron Bell Crank | 10/29/1963 | |
TN 2 | en | Removing Fittings to Carry Ballast Weights | 10/29/1963 | |
TN 2 | de | Removing Fittings to Carry Ballast Weights | 10/29/1963 | |
TN 3 | en | Changing of Middle Elevator Bearing Support | 10/29/1963 | |
TN 3 | de | Changing of Middle Elevator Bearing Support | 10/29/1963 | |
TN 4 | de | Tubular Steel Hood (Flying Clouds) | 03/01/1961 | |
TN 5 | de | Reinforcement of Tubular Steel Rods of Hull | 03/21/1961 | |
TN 6 | de | Additional Support of Elevator Bumper | 11/24/1961 | |
TN 7 | en | Additional Support of Elevator Push Rod | 11/24/1961 | |
TN 7 | de | Additional Support of Elevator Push Rod | 11/24/1961 | |
TN 8 | en | Double Flanges for Control Circuit Intersection | 09/12/1962 | |
TN 8 | de | Double Flanges for Control Circuit Intersection | 09/12/1962 | |
TN 9 | de | Strengthening of Connecting Lap of Forked Airbrake Push Rod in Fuselage | 09/13/1962 | |
TN 9 | en | Strengthening of Connecting Lap of Forked Airbrake Push Rod in Fuselage | 09/13/1962 | |
TN 10 | de | Strengthening of Inner Bearing of Airbrake Bellcrank at Main Bulkhead | 10/25/1962 | |
TN 10 | en | Strengthening of Inner Bearing of Airbrake Bellcrank at Main Bulkhead | 10/25/1962 | |
TN 11 | de | Alternative Option for Lower Billet Bearing (Instead of Buco Shaft Joint, Universal Joint Made of Steel) | 03/29/1963 | |
TN 12 | de | Support of Front Side Fin Connection | 06/25/1963 | |
TN 13 | de | Replacement of Steel Universal Joint Block (TM No. 11) with One Made of Superlene | 11/26/1964 | |
TN 14 | de | Hood with Large Glazing (Swiss Version) | 11/27/1964 | |
TN 15 | de | Reinforcement of Lower Rudder Bearing Block on Fin | 03/08/1965 | |
TN 16 | de | Installation of Pressure Tapping Points for Dynamic Pressure Anemometers (in Tip of Fuselage) | 11/16/1965 | |
TN 17 | en | Installation of Tost Universal / 53-Kombi54 Resp. of Modified Tost Universal 53 | 12/14/1965 | |
TN 17 | de | Installation of Tost Universal / 53-Kombi54 Resp. of Modified Tost Universal 53 | 12/14/1965 | |
TN 18 | de | Material Exchange, (Material 1.7214 can also be Used Instead of Material 1.7734) | 09/30/1966 | |
TN 19 | de | Installation of a Removable Balance Weight | 11/01/1975 | |
TN 19 | en | Installation of a Removable Balance Weight | 11/01/1975 | |
TN 20 | de | Exchange of Material | 08/17/1976 | |
TN 20 | en | Exchange of Material | 08/17/1976 | |
TN 21 | de | Examination of Canopy Lock | 05/12/1980 | |
TN 21 | en | Examination of Canopy Lock | 05/12/1980 | |
TN 22 | de | Installation of a Pneumatic Tailwheel in Exchange for Tailskid | 02/05/1986 | |
TN 22 | en | Installation of a Pneumatic Tailwheel in Exchange for Tailskid | 02/05/1986 | |
TN 23 | en | Elevator | 10/04/1989 | |
TN 23 | de | Elevator | 10/04/1989 | |
TN 24 | en | A1) Canopy Retaining Cord; A2) Rudder Pedals; A3) Elevator Control Linkage; A4) Inspection of Fuselage Tube Skeleton & Control Linkages for Corrosion; B1) Amendment of AFM & OM; B2) Specification of Max Diameter for Wing Attachment Pins | 12/04/1995 | |
TN 24 | de | A1) Canopy Retaining Cord; A2) Rudder Pedals; A3) Elevator Control Linkage; A4) Inspection of Fuselage Tube Skeleton & Control Linkages for Corrosion; B1) Amendment of AFM & OM; B2) Specification of Max Diameter for Wing Attachment Pins | 12/04/1995 | |
TN 25 | de | Conversion of Skid Landing Gear to a Fixed Nose Wheel Landing Gear Made of GRP-CFRP (No Welding Work) | 01/30/1996 | |
TN 26 | de | Modification of Trim ((Appendix [en])) | 12/09/2005 | |
TN 27 | en | Modification Open Canopy Convertible | 12/20/2005 | |
TN 27 | de | Modification Open Canopy Convertible ((FM)) | 12/20/2005 | |
TN 28 | de | Inspection of Central Support of Elevator | 05/25/2010 | |
TN 28 | en | Inspection of Central Support of Elevator | 05/25/2010 | |
TN 29 | de | Installation of a Transponder Antenna Behind Landing Gear ((MI)) | 03/11/2011 | |
TN 30 | en | Inspection of Automatic Elevator Control Connection | 08/30/2012 | |
TN 30 | 1 | en | Inspection of Automatic Elevator Control Connection | 01/08/2013 |
TN 30 | 1 | de | Inspection of Automatic Elevator Control Connection | 01/08/2013 |
TN 31 | de | Inspection of Elevator ((Appendix)) | 07/12/2021 | |
TN 31 | en | Inspection of Elevator ((Appendix)) | 07/12/2021 | |
TN 31 | Iss 2 | en | Inspection of Elevator ((Appendix R1)) | 11/01/2023 |
TN 31 | Iss 2 | de | Inspection of Elevator ((Appendix R1)) | 11/01/2023 |
TN 32 | en | Limitation of Operating Envelope ((Appendix)) | 07/12/2021 | |
TN 32 | de | Limitation of Operating Envelope ((Appendix)) | 07/12/2021 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Elevator | 10/04/1989 | |
TN 1 | en | Elevator | 10/04/1989 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Skid Attachment to Start Hook by Means of a Joint | 02/24/1955 | |
TN 2 | de | Secure Detachable Joystick on Front Seat with 6 mm Screws. Auto. Elevator Connection, Trim, Foldable Hood | 07/22/1955 | |
TN 3 | de | Plocking Spring on Front BK Hand Lever - Interchangeable Socket Pin for Elevator Fin Attachment | 10/26/1955 | |
TN 4 | en | Strengthening of Plywood Web on Outer Spar at Aileron Bell Crank | 10/29/1963 | |
TN 4 | de | Strengthening of Plywood Web on Outer Spar at Aileron Bell Crank | 10/29/1963 | |
TN 5 | de | Rudder Pedals Mounted on Top with Adjustment Option. Glue in BK Area Corner Blocks | 08/17/1960 | |
TN 6 | en | Strengthening of Bulkhead 2 | 10/29/1963 | |
TN 6 | de | Strengthening of Bulkhead 2 | 10/29/1963 | |
TN 7 | en | Additional Support of the Elevator Push Rod at Bulkhead 23 | 07/04/1962 | |
TN 7 | de | Additional Support of the Elevator Push Rod at Bulkhead 23 | 07/04/1962 | |
TN 8 | de | Check of Stick Attachment in Rear Cockpit | 04/16/1963 | |
TN 8 | en | Check of Stick Attachment in Rear Cockpit | 04/16/1963 | |
TN 9 | de | Installation of Tost Universal / 53-Kombi54 Resp. of Modified Tost Universal 53 | 12/14/1965 | |
TN 9 | en | Installation of Tost Universal / 53-Kombi54 Resp. of Modified Tost Universal 53 | 12/14/1965 | |
TN 10 | de | Replace Sheets 10 & 11 of AFM & OM with Sheets 10/2 & 11/2, Delete Weight Tables Entered on Sheet 18 Below, Insert Sheet 18a Instead ((FM)) | 06/29/1978 | |
TN 11 | en | Elevator | 10/04/1989 | |
TN 11 | de | Elevator | 10/04/1989 | |
TN 12 | de | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 04/12/1990 | |
TN 12 | en | New Production Series Tow Release Couplings for Aerotow and Winch Launch | 04/12/1990 | |
TN 13 | en | Inspection of Automatic Elevator Control Connection | 08/30/2012 | |
TN 13 | 1 | en | Inspection of Automatic Elevator Control Connection | 01/08/2013 |
TN 13 | 1 | de | Inspection of Automatic Elevator Control Connection | 01/08/2013 |
TN 14 | de | Installation of a Transponder Antenna on Bottom of Fuselage Behind Landing Gear Inside Fuselage ((MI)) | 07/18/2012 | |
TN 15 | de | Inspection of Elevator ((FM)) | 11/01/2021 | |
TN 15 | en | Inspection of Elevator ((FM)) | 11/01/2021 | |
TN 16 | de | Limitation of Operating Envelope ((Appendix)) | 11/01/2021 | |
TN 16 | en | Limitation of Operating Envelope ((Appendix)) | 11/01/2021 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Rear Joystick with Bag Casing | 07/27/1955 | |
TN 2 | de | Bearing Block on Wing Rib 16 (Fastening with 4 Screws) | 07/26/1955 | |
TN 3 | de | Attachment of Imitation Leather to Wheel Arch Against Sand Penetration | 11/27/1956 | |
TN 4A | de | Improvement: Skid Attachment at Front by Means of a Joint; Support of Front Rubber Buffer Bracket; Reinforcement of Rudder Spar Planking; Installation of a Weight Trim for Pilots of 55-65 kg | 09/30/1957 | |
TN 4b | de | A/M 4/1: Replaceable Pins of Height Fin Attachment in Case of Wear; Ä/M 2: Additional Pulleys in Height & Side Control; Ä/M 3b: Relocation of Rope Guide on Wing Strut to Center | 08/18/1958 | |
TN 5 | en | Shearing of Split Pins at Aileron Cable Connection at Control Shaft by Wheel Case | 10/29/1963 | |
TN 5 | de | Shearing of Split Pins at Aileron Cable Connection at Control Shaft by Wheel Case | 10/29/1963 | |
TN 6 | de | Control of Connection of Shoulder Strut Main Spar by Means of a Handhole Cover During Hard Landings | 03/24/1959 | |
TN 7 | en | Strengthening of Upper Vertical-Rudder Bearing-Jack | 11/28/1963 | |
TN 7 | de | Strengthening of Upper Vertical-Rudder Bearing-Jack | 11/28/1963 | |
TN 8 | de | Strengthening of Wing Nose Rib No. 4a and Spar Plate | 10/29/1963 | |
TN 8 | en | Strengthening of Wing Nose Rib No. 4a and Spar Plate | 10/29/1963 | |
TN 9 | de | Free Pass of Elevator Cable at Control Shaft | 11/28/1963 | |
TN 9 | en | Free Pass of Elevator Cable at Control Shaft | 11/28/1963 | |
TN 10 | en | Check of Stick Attachment in Rear Cockpit | 04/25/1963 | |
TN 10 | de | Check of Stick Attachment in Rear Cockpit | 04/25/1963 | |
TN 11 | de | Installation of Tost Universal / 53-Kombi54 Resp. of Modified Tost Universal 53 | 12/22/1965 | |
TN 11 | en | Installation of Tost Universal / 53-Kombi54 Resp. of Modified Tost Universal 53 | 12/22/1965 | |
TN 12 | de | Installation of Aileron Mass-Balance | 10/11/1967 | |
TN 12 | en | Installation of Aileron Mass-Balance | 10/11/1967 | |
TN 13 | en | Strengthening of Control Shaft | 06/23/1975 | |
TN 13 | de | Strengthening of Control Shaft | 06/23/1975 | |
TN 14 | en | Clevis Pin for Aileron Control Cable Connection at Main Control Shaft | 09/15/1977 | |
TN 14 | de | Clevis Pin for Aileron Control Cable Connection at Main Control Shaft | 09/15/1977 |
Name | Revision | Lang | Subject | Date |
---|---|---|---|---|
TN 1 | de | Extension of Fin Bulkhead No. 24 Until Rib 2 of Fin | 06/21/1957 | |
TN 2/1 | de | Appearance of Wear | 10/29/1963 | |
TN 2/1 | en | Appearance of Wear | 10/29/1963 | |
TN 2/2 | en | Appearance of Wear | 10/29/1963 | |
TN 2/2 | de | Appearance of Wear | 10/29/1963 | |
TN 3 | en | Strengthening of Plywood Web on Outer Spar at Aileron Bell Crank | 10/29/1963 | |
TN 3 | de | Strengthening of Plywood Web on Outer Spar at Aileron Bell Crank | 10/29/1963 | |
TN 4 | de | Additional Support of Elevator Push Rod at Bulkhead 20 | 10/24/1961 | |
TN 4 | en | Additional Support of Elevator Push Rod at Bulkhead 20 | 10/24/1961 | |
TN 5 | de | Fuselage Covering Out of FRP | 07/18/1962 | |
TN 6 | de | Double Clip at Air Brake Push Rod Fork | 09/12/1962 | |
TN 7 | en | Strengthening of Connecting Lap of Forked Airbrake Push Rod in Fuselage | 09/13/1962 | |
TN 7 | de | Strengthening of Connecting Lap of Forked Airbrake Push Rod in Fuselage | 09/13/1962 | |
TN 8 | de | Alternative Option for Lower Push Stick Bearing (Instead of Buco Shaft Joint: Universal Joint Out of Steel) | 03/29/1963 | |
TN 9 | de | Minimized Wing Setting Discontinuance of Rudder Balance Horn | 04/18/1963 | |
TN 10 | de | Reinforcement of Aerodynamically Features through Modification of Wing Leading Edge after Suggestion of Dr. F.X. Wortmann | 05/20/1964 | |
TN 11 | de | Extension of Wing Covering Behind Spar on Upper Side for Reinforcement of Aerodynamically Features | 11/26/1964 | |
TN 12 | de | Exchange of Push Stick Cardan Joint Block Out of Steel Against Push Stick Cardan Joint Block Out of Supralen | 11/26/1964 | |
TN 13 | en | Installation of Tost Universal / 53-Kombi54 Resp. of Modified Tost Universal 53 | 12/14/1965 | |
TN 13 | de | Installation of Tost Universal / 53-Kombi54 Resp. of Modified Tost Universal 53 | 12/14/1965 | |
TN 14 | de | Exchange Possibility of Material Exchange of Steel Plate 1.7214 Against 1.7734 | 09/30/1966 | |
TN 15 | de | Exchange of Swivel Head L-205.44-232 Against Swivel Head SMX Size 8 of Hirschmann | 09/30/1966 | |
TN 16 | de | Cockpit Extension | 03/17/1967 | |
TN 17 | en | Suspension of Thermos Bottles Below Baggage Compartment | 09/13/1968 | |
TN 17 | de | Suspension of Thermos Bottles Below Baggage Compartment | 09/13/1968 | |
TN 18 | de | Tube Spar of Elevator | 10/30/1970 | |
TN 18 | en | Tube Spar of Elevator | 10/30/1970 | |
TN 19 | de | Applicability of Airspeed Indicator 30 - 200 km/h (Winter 6 FMS 2) Instead of Airspeed Indicators with Measuring Range 1.05 . VNE = 210 km/h | 11/24/1977 | |
TN 20 | de | Replacement of Elevator Pushrod Guide Made Out of Felt for a Roller Bearing Guide | 03/27/1986 | |
TN 20 | en | Replacement of Elevator Pushrod Guide Made Out of Felt for a Roller Bearing Guide | 03/27/1986 | |
TN 21 | en | Elevator | 10/04/1989 | |
TN 22 | de | Installation of a Forward Towing Release ((FM)) | 05/02/2000 | |
TN 22 | en | Installation of a Forward Towing Release | 05/02/2000 | |
TN 23 | de | Canopy (Open Canopy) ((FM [en])) | 04/29/2005 | |
TN 24 | de | Installation for Transponder Antennas Behind Landing Gear Inside Fuselage ((MI)) | 07/04/2008 | |
TN 25 | en | Inspection of Central Support of Elevator | 05/25/2010 | |
TN 25 | de | Inspection of Central Support of Elevator | 05/25/2010 | |
TN 26 | en | Inspection of Automatic Elevator Control Connection | 08/30/2012 | |
TN 26 | 1 | en | Inspection of Automatic Elevator Control Connection | 01/08/2013 |
TN 26 | 1 | de | Inspection of Automatic Elevator Control Connection | 01/08/2013 |
TN 27 | en | Inspection of Elevator | 07/12/2021 | |
TN 27 | Iss 2 | en | Inspection of Elevator ((Appendix)) | 11/30/2021 |
TN 27 | Iss 2 | de | Inspection of Elevator ((Appendix)) | 11/30/2021 |
TN 27 | Iss 3 | en | Inspection of Elevator ((Appendix R1)) | 11/01/2023 |
TN 27 | Iss 3 | de | Inspection of Elevator ((Appendix R1)) | 11/01/2023 |
TN 28 | en | Limitation of Operating Envelope ((Appendix)) | 07/12/2021 | |
TN 28 | Iss 2 | en | Limitation of Operating Envelope ((Appendix)) | 11/30/2021 |
TN 28 | Iss 2 | de | Limitation of Operating Envelope ((Appendix)) | 11/30/2021 |