Technical Notes| Name | Revision | Lang | Subject | Date |
|---|
| TN 1/69 |
|
en |
Askubal, Ball Bearing Rod Ends | 10/20/1969 |
| TN 1/70 |
|
en |
Inspection Hole Covered with a Plexiglass Window on Upper Side of Elevator at Connection of Elevator Control Rod ((Instructions, SM)) | 06/16/1970 |
| TN 1/71 |
|
en |
Installation of Water Tanks in Wing ((FM)) | 06/04/1971 |
| TN 1/73 |
|
en |
Outer Wing Sections Built in a Pure Glass Fiber Plastic Layup without Foam Sandwich | 07/10/1973 |
| TN 1/73 |
|
en |
Supporting Core Material of Wing Spar Web | 03/02/1973 |
| TN 2/70 |
|
en |
Elevator Control Connection, Hook of Control Rod and its Bearings ((Drawing)) | 09/24/1970 |
| TN 2/72 |
|
en |
Increase of Maximum Permitted All-Up Weight from 330 kg (727.5 lb) to 390 kg (860 lb) ((FM)) | 03/03/1986 |
| TN 2/73 |
|
en |
Towing Hook Control and Operating Device of Rudder Pedal Adjustment in Cockpit ((FM)) | 09/14/1973 |
| TN 2/73 |
|
en |
Towing Hook Control and Operating Device of Rudder Pedal Adjustment in Cockpit ((FM)) | 09/14/1973 |
| TN 3/73 |
|
en |
Rudder with Fabric Covering | 11/14/1973 |
| TN 9 |
|
en |
Glue Joint between Bulkhead on Fuselage Tail End and Lower Half of Fuselage Plywood Shell | 01/20/1969 |
| TN 265-5 |
|
en |
Identification Plate | 01/15/1975 |
| TN 265-6 |
|
en |
Elevator Drive. Tail Parachute. Horizontal Tailplane. Amendments of Flight and Service Manual ((FM)) | 04/27/1982 |
| TN 265-7 |
|
en |
Flight Manual ((FM)) | 03/28/1984 |
| TN 265-8 |
|
en |
Airbrake Control System in Wing | 02/11/1985 |
| TN 265-9 |
|
en |
Extension of Service Time | 12/06/1985 |
| TN 265-10 |
|
en |
Control Rod Coupling Balls on Airbrake Actuating Lever Inside Fuselage ((Appendix, SM)) | 11/05/1992 |
| TN 265-11 |
|
en |
"L'Hotellier" Ball and Swivel Joints ((Appendix, FM)) | 04/20/1993 |
| TN 265-12 |
|
en |
"Wedekind" Safety Sleeve for "L'Hotellier" Ball and Swivel Joint Connectors No. AMZ-9, 41 (Having a Wedge-Shaped Locking Plate) (Appendix, FM, Safety Device) | 02/08/1994 |
| TN 265-13 |
|
en |
Backrest, Lap Belt Position, Supplementation of Flight Manual and GFRP-Covering Above Aileron Control at Fuselage Steel Frame Work ((Appendix, FM)) | 03/11/2007 |
| TN 278-1 |
|
en |
Inspection Hole Covered with a Plexiglass Window on Upper Side of Elevator at Connection of Elevator Control Rod ((Instructions, SM)) | 06/16/1970 |
| TN 278-2 |
|
en |
Elevator Control Connection, Hook of Control Rod and its Bearings ((Drawing)) | 09/24/1970 |
| TN 278-3 |
|
en |
Installation of Water Tanks in Wing ((FM)) | 06/04/1971 |
| TN 278-5 |
|
en |
Increase of Maximum Permitted All-Up Weight from 330 kg (727.5 lb) to 390 kg (860 lb) ((FM)) | 03/03/1986 |
| TN 278-6 |
|
en |
Supporting Core Material of Wing Spar Web | 03/02/1973 |
| TN 278-8 |
|
en |
Towing Hook Control and Operating Device of Rudder Pedal Adjustment in Cockpit ((FM)) | 09/14/1973 |
| TN 278-11 |
|
en |
Identification Plate | 01/15/1975 |
| TN 278-12 |
|
en |
Air Brakes | 01/23/1975 |
| TN 278-13 |
|
en |
Wing | 01/23/1975 |
| TN 278-14 |
|
en |
Water Tanks and Water Draining System ((FM)) | 06/12/1975 |
| TN 278-15 |
|
en |
Attachment and Control Connection of Horizontal Tail Plane ((SM)) | 06/30/1975 |
| TN 278-17 |
|
en |
Fuselage Steel Tube Frame | 12/08/1975 |
| TN 278-18 |
|
en |
Molded Glass Fiber Seat | 12/08/1975 |
| TN 278-19 |
|
en |
Ball Bearings of Wing Attachment at Fuselage Root Ribs ((SM)) | 06/15/1976 |
| TN 278-20 |
|
en |
Wing Shell | 05/10/1976 |
| TN 278-21 |
|
en |
Fuselage, Inspection Hole | 01/24/1977 |
| TN 278-23 |
|
en |
Ball Joints on Air Brake Drive Lever in Fuselage (SM for Standard, Standard B, Standard CS) | 12/31/1978 |
| TN 278-24 |
|
en |
Main Landing Wheel | 08/03/1979 |
| TN 278-25 |
|
en |
Elevator Drive | 09/17/1980 |
| TN 278-26 |
|
en |
Attachment of Elevator (T-Fitting) ((SM)) | 02/05/1992 |
| TN 278-27 |
|
en |
Installation of a C/G Release Mechanism (FM for Standard, Standard CS; SM for Standard, Standard CS) | 09/01/1980 |
| TN 278-28 |
|
en |
Extension of Service Life ((SM)) | 09/26/1995 |
| TN 278-30 |
|
en |
Amendments of Flight Manual, Replacement of Data and Reference Placards ((FM for Standard B, Standard G)) | 10/20/1986 |
| TN 278-31 |
|
en |
Wing Tip Extensions | 02/05/1992 |
| TN 278-32 |
|
en |
Airbrakes ((Appendix)) | 03/10/1992 |
| TN 278-33 |
|
en |
Vertical Elevator Actuating Rod Inside Fin ((Appendix)) | 11/19/1992 |
| TN 278-34 |
|
en |
"L'Hotellier" Ball and Swivel Joints (Appendix; FM for Standard, Standard G) | 04/20/1993 |
| TN 278-35 |
|
en |
"Wedekind" Safety Sleeve for "L'Hotellier" Ball and Swivel Joint Connectors No. AMZ-9, 41 (Having a Wedge-Shaped Locking Plate) (Appendix; FM for Standard, Standard G) | 02/08/1994 |
| TN 278-36 |
|
en |
Attachment of Horizontal Tailplane ((Appendix)) | 11/11/1994 |
| TN 278-36 |
revised |
en |
Attachment of Horizontal Tailplane | 06/11/2001 |
| TN 278-37 |
|
en |
Retro - Fitting a Nose Tow Release Mechanism (SM; FM for Standard, Standard G) | 02/02/2000 |
| TN 278-38 |
|
en |
Retro-Fitting of Winglets (Appendix, Repair Inst; FM for Standard, Standard B, Standard CS) | 02/14/2006 |
| TN 278-39 |
|
en |
Increase of Maximum Mass without Water Ballast. Increase of Maximum Mass of Non-Load Carrying Parts. Supplementation of Flight Manual (Work Inst, FM for Std Cirrus, Std Cirrus G, Std Cirrus B, Std Cirrus CS 11-75L) | 04/06/2007 |
| TN 278-40 |
1 |
en |
Application of Color Markings for Elevator Attachment, Exchange of Manual Pages | 11/12/2020 |
| TN 286-2 |
|
en |
Outer Wing Sections Built in a Pure Glass Fiber Plastic Layup without Foam Sandwich | 07/10/1973 |
| TN 286-3 |
|
en |
Towing Hook Control and Operating Device of Rudder Pedal Adjustment in Cockpit ((FM)) | 09/14/1973 |
| TN 286-4 |
|
en |
Rudder with Fabric Covering | 11/14/1973 |
| TN 286-6 |
|
en |
Identification Plate | 01/15/1975 |
| TN 286-7 |
|
en |
Attachment and Control Connection of Horizontal Tail Plane ((SM)) | 03/28/1975 |
| TN 286-8 |
|
en |
Increase of Maximum Permitted All-Up Weight from 530 kg (1168 lb) to 580 kg (1278 lb) and Increase of Maximum Permitted Speed from 250 km/h (155 mph, 135 kt) to 270 km/h (168 mpg, 145 kt) ((FM)) | 01/23/1986 |
| TN 286-9 |
|
en |
Ball Bearings of Wing Attachment at Fuselage Root Ribs ((SM)) | 09/01/1976 |
| TN 286-11 |
|
en |
Change of Nimbus-2 into Nimbus-2B ((FM)) | 09/20/1978 |
| TN 286-13 |
|
en |
Mounting Provision for Trim Ballast, Safety Harnesses, Control Cables and Aerotow Release (MM, SM; FM for Nimbus-2C, Nimbus-3/24.5) | 09/07/1983 |
| TN 286-14 |
|
en |
C.G. Towing Hook (SM for Nimbus-2, Nimbus-2B, Nimbus-2C) | 06/12/1980 |
| TN 286-15 |
|
en |
Installation of a Nose and C.G. Towing Hook (MM; FM for Nimbus-2, Nimbus-2B, Nimbus-2C, Nimbus-3, Nimbus-3/24.5; SM for Nimbus-2, Nimbus-2B, Nimbus-2C) | 11/03/1982 |
| TN 286-16 |
|
en |
Flight Manual ((FM)) | 05/17/1982 |
| TN 286-17 |
|
en |
Conversion of Sailplane Nimbus-3 into Nimbus-3/24.5 ((MM)) | 02/24/1983 |
| TN 286-18 |
|
en |
U.S. Type Certification of Pre-Maturely Exported Sailplanes ((FM)) | 04/05/1984 |
| TN 286-19 |
|
en |
Wheel Brake ((FM, MM)) | 12/12/1983 |
| TN 286-20 |
|
en |
Increase of Maximum Permitted A.U.W. of Sailplane "Nimbus 3/24.5" ((FM, MM)) | 05/20/1983 |
| TN 286-22 |
|
en |
Extension of Service Time (FM for Nimbus-2, Nimbus-2B; SM for Nimbus-2B, Nimbus-2C) | 01/14/1994 |
| TN 286-23 |
|
en |
Installation of a Tail Wheel (MM, SM; FM for Nimbus-2C, Nimbus-3/24.5) | 12/22/1986 |
| TN 286-24 |
|
en |
Elevator Drive | 08/14/1987 |
| TN 286-25 |
|
en |
Tilt-Up Instrument Panel ((FM, MM)) | 04/19/1989 |
| TN 286-26 |
|
en |
Nose and C/G Tow Release Mechanisms (FM for Nimbus-3, Nimbus-3/24.5; MM for Nimbus-3, Nimbus-3/24.5; SM for Nimbus-2, Nimbus-3, Nimbus-3/24.5) | 03/09/1990 |
| TN 286-27 |
|
en |
Larger Wing Span ((FM, MM)) | 04/12/1990 |
| TN 286-28 |
|
en |
Vertical Elevator Actuating Rod Inside Fin ((Appendix)) | 11/19/1992 |
| TN 286-29 |
|
en |
"L'Hotellier" Ball and Swivel Joint ((Appendix, FM)) | 03/26/1993 |
| TN 286-30 |
|
en |
"L'Hotellier" Ball and Swivel Joints (Appendix; FM for Nimbus-2, Nimbus-2B, Nimbus-2C) | 04/20/1993 |
| TN 286-31 |
|
en |
"Wedekind" Safety Sleeve for "L'Hotellier" Ball and Swivel Joint Connectors No. AMZ-9, 41 (Having a Wedge-Shaped Locking Plate) (FM for Nimbus-2, Nimbus-2B, Nimbus-2C) | 02/08/1994 |
| TN 286-32 |
|
en |
"Wedekind" Safety Sleeve for "L-Hotellier" Ball and Swivel Joint Connectors No. RMZ-9,41 (Having a Wedge-Shaped Locking Plate) ((FM for Nimbus-3, Nimbus-3/24.5)) | 03/04/1994 |
| TN 286-33 |
|
en |
Attachment of Horizontal Tailplane ((Appendix)) | 11/11/1994 |
| TN 286-33 |
revised |
en |
Attachment of Horizontal Tailplane | 06/11/2001 |
| TN 286-34 |
|
en |
Extension of Service Time and Supplements of Maintenance Manual ((MM)) | 09/23/2002 |
| TN 286-35 |
|
en |
Flap Drive Mechanism in Fuselage ((Appendix)) | 06/24/2005 |
| TN 286-36 |
1 |
en |
Application of Color Markings for Elevator Attachment, Exchange of Manual Pages | 11/12/2020 |
| TN 295-1 |
|
en |
Installation of Water Tanks in Wing ((FM)) | 02/06/1976 |
| TN 295-3 (FM) |
|
en |
Retrofitting Watertanks in Wings | 07/01/1977 |
| TN 295-4 (FM) |
|
en |
Increase of Weight of Non-Lifting Parts Up to 440 kg; Simple Aerobatic; Supplements of Flight Manual | 07/01/1977 |
| TN 295-6 |
|
en |
Tail Brake Chute Omitted (MM; FM for Janus, Janus B, Janus C) | 09/10/1980 |
| TN 295-7 |
|
en |
Difference from Basic Model and Variants (Drawing, MM; FM for Janus B, Janus C) | 03/31/1983 |
| TN 295-9 |
|
en |
Installation of a Nose and C.G. Towing Hook (MM; FM for Janus, Janus B, Janus C; SM for Janus, Janus B) | 02/14/2002 |
| TN 295-10 |
Iss 2 |
en |
Mounting Provision for Trim Ballast, Safety Harness and Control Cables ((FM for Janus B, Janus C)) | 10/26/1981 |
| TN 295-11 |
|
en |
Extension of Service Time and Supplements to Maintenance Manual (Technical Data, FM, SM) | 03/06/1991 |
| TN 295-13 |
|
en |
Main Wheel Brake (MM; FM for Janus, Janus B, Janus C; SM for Janus, Janus B) | 12/19/1983 |
| TN 295-15 |
|
en |
Directional Control - Rudder Control System ((Appendix)) | 02/21/1986 |
| TN 295-16 |
|
en |
Extension of Service Time and Supplements to Maintenance Manual ((Technical Data, MM)) | 03/15/1991 |
| TN 295-17 |
|
en |
Installation of a Tail Wheel (MM, SM; FM for Janus B, Janus C) | 12/30/1986 |
| TN 295-18 |
|
en |
Mounting Provision for Trim Ballast ((FM for Janus B, Janus C)) | 05/27/1987 |
| TN 295-19 |
|
en |
Elevator Drive (Drawing HS5-30.055/1 attached to TN) | 08/14/1987 |
| TN 295-20 |
|
en |
Nose Tow Release, C/G Tow Release and Weak Link (MM; FM for Janus, Janus B, Janus C; SM for Janus, Janus B) | 04/25/1990 |
| TN 295-21 |
|
en |
Elevator Control System ((Appendix)) | 11/05/1990 |
| TN 295-22 |
|
en |
Vertical Elevator Actuating Rod Inside Fin ((Appendix)) | 11/19/1992 |
| TN 295-23 |
|
en |
"L'Hotellier" Ball and Swivel Joints (Appendix; FM for Janus, Janus B, Janus C, Janus Ce) | 04/20/1993 |
| TN 295-24 |
|
en |
"Wedekind" Safety Sleeve for "L'Hotellier" Ball and Swivel Joint Connectors No. AMZ-9, 41 (Having a Wedge-Shaped Locking Plate) (Safety Device; FM for Janus, Janus B, Janus C, Janus Ce) | 02/08/1994 |
| TN 295-25 |
|
en |
Enlarged Fin/Rudder Unit and Stiffer Horizontal Stabilizer (FM, MM, MM/2) | 06/28/1994 |
| TN 295-26 |
|
en |
Attachment of Horizontal Tailplane ((Appendix)) | 11/11/1994 |
| TN 295-26 |
revised |
en |
Attachment of Horizontal Tailplane | 06/11/2001 |
| TN 295-27 |
|
en |
Horizontal Tailplane - Elevator Mass Balance ((Appendix, MM)) | 06/30/1999 |
| TN 295-28 |
|
en |
Flight Manual ((FM)) | 07/16/1999 |
| TN 295-29 |
|
en |
Flight Manual - Minimum Front Seat Load with Both Seats Occupied (FM for Janus, Janus B, Janus C, Janus Ce) | 04/14/2000 |
| TN 295-30 |
|
en |
Elevator Control System ((Appendix)) | 09/27/2004 |
| TN 295-32 |
|
en |
Change of Allowed Hinge Moments and Weights of Control Surfaces ((MM)) | 10/27/2008 |
| TN 295-33 |
1 |
en |
Application of Color Markings for Elevator Attachment, Exchange of Manual Pages | 11/12/2020 |
| TN 328-4 |
|
en |
Mounting Provision for Trim Ballast ((FM)) | 11/08/1979 |
| TN 328-5 |
|
en |
Landing Gear | 01/11/1980 |
| TN 328-6 |
|
en |
U.S. Type Certification of Pre-Maturely Exported Sailplanes ((FM for Mimi-Nimbus B, Mini-Nimbus HS7)) | 04/05/1984 |
| TN 328-7 |
|
en |
Extension of Service Time and Supplements to Flight Manual (FM for Mini-Nimbus B, Mini-Nimbus C, Mini-Nimbus HS7; MM for Mini-Nimbus B, Mini-Nimbus C, Mini-Nimbus HS7) | 12/06/1985 |
| TN 328-8 |
|
en |
Elevator Drive | 08/14/1987 |
| TN 328-8 |
|
en |
Elevator Drive | 09/05/1988 |
| TN 328-9 |
|
en |
Flight Manual ((FM)) | 04/04/1990 |
| TN 328-10 |
|
en |
Vertical Elevator Actuating Rod Inside Fin ((Appendix)) | 11/19/1992 |
| TN 328-11 |
|
en |
Attachment of Horizontal Tailplane ((Appendix)) | 11/11/1994 |
| TN 328-11 |
revised |
en |
Attachment of Horizontal Tailplane | 06/11/2001 |
| TN 328-12 |
|
en |
Retrofit of a Nose Tow Release Mechanism (Appendix; FM for Mini-Nimbus B, Mini-Nimbus C, Mini-Nimbus HS7) | 02/23/1999 |
| TN 328-13 |
|
en |
Flap Drive Mechanism in Fuselage ((Appendix)) | 06/24/2005 |
| TN 328-14 |
1 |
en |
Application of Color Markings for Elevator Attachment, Exchange of Manual Pages | 11/12/2020 |
| TN 349-1 |
|
en |
Mounting Provisions for Trim Ballas, Safety Harness, Control Cables and Aerotow Release (MM; FM for Ventus b, Ventus b/16.6) | 09/14/1983 |
| TN 349-3 |
|
en |
Installation of a Nose Tow Release Mechanism (FM for Ventus a, Ventus a/16.6, Ventus b; MM for Ventus a, Ventus b) | 01/08/1992 |
| TN 349-4 |
|
en |
Changes to Flight Manual for All Gliders Exported to Canada (FM for Ventus a, Ventus a/16.6, Ventus b, Ventus b/16.6) | 04/13/1989 |
| TN 349-6 |
|
en |
Conversion of Sailplane "Ventus a" into Variant "Ventus a/16.6", Conversion of Sailplane "Ventus b" into Variant "Ventus b/16.6" (FM for Ventus a/16.6, Ventus a/16.6, Ventus b/16.6, Ventus b/16.6, Ventus b/16.6) | 10/29/1985 |
| TN 349-8 |
|
en |
Installation of a Tail Wheel (FM for Ventus a/16.6, Ventus b/16.6; MM for Ventus a/16.6, Ventus b/16.6) | 10/08/1987 |
| TN 349-9 |
|
en |
Flap Drive Inside Fuselage ((Appendix)) | 06/29/2001 |
| TN 349-10 |
|
en |
Winglets ((MM for Ventus a, Ventus b)) | 05/06/1992 |
| TN 349-11 |
|
en |
Redesignation of Sailplanes "Ventus a/16.6" and "Ventus b/16.6" to "Ventus c" ((FM)) | 10/21/1987 |
| TN 349-12 |
|
en |
Flight and Maintenance Manual (FM for Ventus a, Ventus b, Ventus b/16.6, Ventus c; MM for Ventus a, Ventus b, Ventus b/16.6, Ventus c) | 02/26/1988 |
| TN 349-13 |
|
en |
Airbrakes | 05/11/1988 |
| TN 349-14 |
|
en |
Forward Hinged (Tilt-Up) Instrument Panel (FM for Ventus a, Ventus a/16.6, Ventus b, Ventus b/16.6, Ventus c; MM for Ventus a, Ventus a/16.6, Ventus b, Ventus b/16.6) | 02/20/1996 |
| TN 349-15 |
|
en |
Nose Tow Release and C/G Tow Release (FM for Ventus a, Ventus a/16.6, Ventus b/16.6, Ventus c; MM for Ventus a, Ventus a/16.6, Ventus b, Ventus b/16.6, Ventus c) | 02/28/1991 |
| TN 349-16 |
|
en |
Vertical Elevator Actuating Rod Inside Fin ((Appendix)) | 11/19/1992 |
| TN 349-17 |
|
en |
"L'Hotellier" Ball and Swivel Joints (Appendix; FM for Ventus a, Ventus a/16.6, Ventus c) | 04/20/1993 |
| TN 349-18 |
|
en |
"Wedekind" Safety Sleeve for "L'Hotellier" Ball and Swivel Joint Connectors No. AMZ-9, 41 (Having a Wedge-Shaped Locking Plate) (Appendix; FM for Ventus a, Ventus a/16.6, Ventus c) | 02/08/1994 |
| TN 349-19 |
|
en |
U.S. Standard Airworthiness Certificate for Prematurely Imported Sailplanes ((FM, MM)) | 07/13/2004 |
| TN 349-20 |
|
en |
Special Requirements for Export to U.S.A. | 07/13/2004 |
| TN 349-21 |
|
en |
Maximum All-Up Mass for 18m Wing Span ((FM, MM)) | 09/15/1997 |
| TN 349-22 |
|
en |
Wheel Brake (Appendix, FM, MM) | 09/10/1997 |
| TN 349-23 |
|
en |
Flight and Maintenance Manual (FM for Ventus 2a/2b, Ventus 2c; MM for Ventus 2a/2b, Ventus 2c) | 12/05/1997 |
| TN 349-24 |
|
en |
Extension of Service Time (MM for Ventus a, Ventus a/16.6, Ventus b, Ventus b/16.6, Ventus c) | 10/27/1998 |
| TN 349-25 |
|
en |
Landing Gear ((Appendix, MM)) | 07/20/2001 |
| TN 349-26 |
|
en |
C.G. Release, Installation Position ((Appendix, MM)) | 12/21/2001 |
| TN 349-27 |
|
en |
Tail Unit and Maughmer Winglets ((FM, MM)) | 01/20/2003 |
| TN 349-28 |
|
en |
Elevator, Fixing of Mass Balance Weights ((Appendix)) | 09/16/2003 |
| TN 349-29 |
|
en |
Horizontal Stabilizer ((Appendix)) | 01/20/2005 |
| TN 349-30 |
|
en |
Fuselage, Bearing of Automatic Control Attachment | 09/20/2005 |
| TN 349-31 |
|
en |
Installation of an Emergency Bail Out Assistance System for Occupant (FM for Ventus 2a/2b, Ventus b, Ventus b/16.6, Ventus c, Ventus 2c, Ventus 2c) | 12/14/2006 |
| TN 349-32 |
|
en |
Increase of Maximum Permitted All-Up Mass on 600 kg for 18 m Wing Span ((FM, MM)) | 05/17/2006 |
| TN 349-33 |
|
en |
Optional Installation of a Beringer 5-Inch-Wheel with Tire (Work Inst, Drawing, MM, MM2) | 10/17/2007 |
| TN 349-34 |
|
en |
Inspection of Wing Shear Web for Damage ((Appendix)) | 04/08/2008 |
| TN 349-35 |
|
en |
Back Rest Adjustment | 07/11/2008 |
| TN 349-36 |
|
en |
Optional Use of Maughmer Wingets and Horizontal Tail Unit of Sailplane Ventus-2a(x) ((FM, MM)) | 03/24/2009 |
| TN 349-37 |
|
en |
New Maughmer-Winglets for 15m-Wingspan ((Work Inst)) | 07/13/2012 |
| TN 349-38 |
|
en |
New Winglets for 18m Wingtips ((Work Inst)) | 05/19/2014 |
| TN 349-39 |
|
en |
Inspection of Overlap Between Airbrake Panels ((Work Inst)) | 01/22/2016 |
| TN 349-42 (WI) |
|
en |
Inspection of Flaperon Control in Wings for Corrosion & Other Damage | 08/31/2020 |
| TN 349-43 |
|
en |
Inspection of Automatic Airbrake Control Connections ((Work Inst)) | 08/09/2022 |
| TN 360-2 |
|
en |
Mounting Provision for Trim Ballast, Safety Harnesses, Control Cable, Aerotow Release and Find Tank Water Dump Valve (if Installed) ((FM, MM)) | 07/28/1989 |
| TN 360-3 |
|
en |
Installation of a Tail Wheel ((FM, MM)) | 11/11/1986 |
| TN 360-4 |
|
en |
U.S. Airworthiness Certificates of "Prematurely" Exported Sailplanes ((FM)) | 11/18/1986 |
| TN 360-5 |
|
en |
Flight and Maintenance Manual ((FM, MM)) | 01/29/1988 |
| TN 360-6 |
|
en |
Forward Hinged Instrument Panel ((FM, MM)) | 05/03/1988 |
| TN 360-7 |
|
en |
Nose and C/G Tow Release Mechanism ((FM, MM)) | 02/04/1992 |
| TN 360-8 |
|
en |
Static Pressure Ports for ASI ((FM)) | 11/02/1989 |
| TN 360-9 |
|
en |
Vertical Elevator Actuating Rod Inside Fin ((Appendix)) | 11/19/1992 |
| TN 360-10 |
|
en |
"L'Hotellier" Ball and Swivel Joints ((Appendix, FM)) | 04/20/1993 |
| TN 360-11 |
|
en |
Extension of Service Time ((MM for Discus a/b, Discus cs)) | 01/12/1994 |
| TN 360-12 |
|
en |
"Wedekind" Safety Sleeve for "L'Hotellier" Ball and Swivel Joint Connectors No. AMZ-9, 41 (Having a Wedge-Shaped Locking Plate) ((FM, Safety Device)) | 02/08/1994 |
| TN 360-13 |
|
en |
Winglets (FM for Discus a/b, Discus a/b, Discus CS) | 06/28/1994 |
| TN 360-14 |
|
en |
Retro-Fitting a Nose Tow Release Mechanism | 01/24/2000 |
| TN 360-15 |
|
en |
Wingtip with Winglet (Appendix, FM, MM) | 01/02/2001 |
| TN 360-16 |
|
en |
Wingtip with Winglet | 02/09/2001 |
| TN 360-17 |
|
en |
Landing Gear ((Appendix, MM)) | 07/20/2001 |
| TN 360-18 |
|
en |
C.G. Release, Installation Position ((Appendix, MM)) | 12/21/2001 |
| TN 360-19 |
|
en |
Horizontal Tailplane and Elevator Pushrod | 12/20/2002 |
| TN 360-20 |
|
en |
Elevator, Fixing of Mass Balance Weights | 09/16/2003 |
| TN 360-21 |
|
en |
Wing, Bonding of Spar Cap to Spar Web ((Appendix)) | 09/25/2003 |
| TN 360-22 |
|
en |
Installation of an Emergency Bail Out Assistance System for Occupant (FM for Discus a/b, Discus 2a/2b, Discus Cs, Discus 2c) | 12/14/2006 |
| TN 360-23 |
|
en |
Retrofit of New Winglets on Wing Tip with Winglets ((Appendix)) | 04/21/2006 |
| TN 360-24 |
|
en |
Optional Installation of a Beringer 5-Inch-Wheel with Tire (Work Inst, Drawing; MM for Discus-2a/2b, Discus-2c) | 03/26/2008 |
| TN 360-25 |
|
en |
Back Rest Adjustment | 07/11/2008 |
| TN 360-26 |
|
en |
Backrest Adjustment ((Work Inst)) | 06/23/2009 |
| TN 360-27 |
|
en |
Increase of Maximum Weight of Non-Lifting Parts ((FM)) | 11/27/2013 |
| TN 360-29 |
|
en |
Inspection of Overlap between Airbrake Panels ((Work Inst)) | 01/22/2016 |
| TN 373-1 |
|
en |
Nose and C/G Tow Release Mechanism ((MM)) | 02/15/1990 |
| TN 373-2 |
|
en |
Mounting Provision for Trim Ballast Weights ((FM)) | 01/30/1992 |
| TN 373-3 |
|
en |
Maintenance Manual - Rigging Data and Control Surface Deflections ((MM)) | 02/13/1992 |
| TN 373-4 |
|
en |
Wing Tip Extensions ((MM)) | 11/05/1992 |
| TN 373-5 |
|
en |
Vertical Elevator Actuating Rod Inside Fin ((Appendix)) | 11/19/1992 |
| TN 373-6 |
|
en |
"L'Hotellier" Ball and Swivel Joint ((Appendix, FM)) | 03/26/1993 |
| TN 373-7 |
|
en |
"Wedekind" Safety Sleeve for "L-Hotellier" Ball and Swivel Joint Connectors No. RMZ-9,41 (Having a Wedge-Shaped Locking Plate) ((FM)) | 03/04/1994 |
| TN 373-8 |
|
en |
Extension of Service Time. Supplements of Maintenance Manual | 12/20/1999 |
| TN 373-9 |
|
en |
Elevator Control System ((Appendix)) | 09/27/2004 |
| TN 380-1 |
|
en |
Canopy Locking Mechanism ((Appendix)) | 07/02/2004 |
| TN 380-2 |
1 |
en |
Inspection of Airbrake Bell Cranks at Root Rib of Wings and of Respective Drive Funnels on Fuselage Side in Fuselage-Wing-Fairing ((Work Inst)) | 07/13/2015 |
| TN 380-3 (WI) |
|
en |
Inspection of Elevator U-Bracket for Damages | 02/28/2022 |
| TN 396-3 |
|
en |
Use of a Fin-Mounted Pitot Tube (for ASI) ((FM, MM)) | 02/02/1996 |
| TN 396-4 |
|
en |
Manual Operated Rudder Control ((FM, MM)) | 02/22/2005 |
| TN 396-5 |
|
en |
Maximum Permitted Speed on Aerotow ((FM, MM)) | 01/10/2000 |
| TN 396-6 |
|
en |
Canopy Locking Mechanism ((Appendix)) | 07/02/2004 |
| TN 396-7 |
|
en |
Airbrake Control Mechanism ((Appendix)) | 01/31/2002 |
| TN 396-8 |
|
en |
Wing, Bonding of Spar Cap to Spar Web ((Appendix)) | 07/31/2003 |
| TN 396-9 |
|
en |
Wing, Bonding of Spar Cap to Spar Web ((Appendix)) | 01/30/2004 |
| TN 396-10 |
|
en |
Removable Aft Control Stick ((Appendix)) | 08/30/2004 |
| TN 396-11 |
|
en |
Flight Manual ((FM)) | 09/20/2005 |
| TN 396-12 |
|
en |
Retrofit of Winglets (Appendix, FM, MM) | 02/17/2006 |
| TN 396-13 |
|
en |
Increase of Maximum Permitted All-Up Mass to 750 kg ((FM, MM)) | 06/12/2007 |
| TN 396-15 |
|
en |
Substitution of Nose Wheel by a Nose Skid ((FM, MM)) | 06/20/2007 |
| TN 396-16 |
|
en |
Optional Use of Fuselages According to Modification Bulletins No. 396-15 ("Duo Discus x") or No. 396-16 ("Duo Discus xL") (Working Inst, FM, FM, MM, MM) | 02/12/2008 |
| TN 396-17 |
1 |
en |
Inspection of Airbrake Bell Cranks at Root Rib of Wings and of Respective Drive Funnels on Fuselage Side in Fuselage-Wing-Fairing ((Work Inst)) | 07/13/2015 |
| TN 396-18 |
|
en |
Extension of Empty Mass Range for Determination of Minimum Cockpit Load in Maintenance Manual ((MM)) | 07/05/2015 |
| TN 396-20 (WI-Act1) |
|
en |
Exchange of Plastic Bushings on Airbrake End Stops | 09/18/2020 |
| TN 396-20 (WI-Act2) |
|
en |
Check of Overlap between Airbrake Panels | 09/18/2020 |
| TN 396-22 (WI) |
|
en |
Inspection of Elevator U-Bracket for Damages | 02/28/2022 |
| TN 798-1 |
|
en |
"L'Hotellier" Ball and Swivel Joints ((Appendix)) | 04/20/1993 |
| TN 798-2 |
|
en |
"Wedekind" Safety Sleeve for "L'Hotellier" Ball and Swivel Joint Connectors No. AMZ-9, 41 (Having a Wedge-Shaped Locking Plate) ((Appendix)) | 02/08/1994 |
| TN 798-3 |
|
en |
Attachment of Horizontal Tailplane ((Appendix)) | 11/11/1994 |
| TN 798-3 |
revised |
en |
Attachment of Horizontal Tailplane | 06/11/2001 |
| TN 798-4 |
1 |
en |
Application of Color Markings for Elevator Attachment, Exchange of Manual Pages | 11/12/2020 |
| TN 809-1 |
|
en |
Propeller Mounting Structure - Diagonal Struts | 02/12/1997 |
| TN 809-2 |
|
en |
External Power Receptacle ((FM, MM)) | 07/12/1985 |
| TN 809-3 |
|
en |
Fuel Supply System ((MM)) | 04/11/1986 |
| TN 809-4 |
|
en |
Engine Accessories and Cockpit Placards (Appendix, FM, MM) | 12/15/1986 |
| TN 809-5 |
|
en |
Installation of an Engine "Rotax 535 C" ((FM, MM)) | 11/24/1987 |
| TN 809-6 (FM) |
|
en |
Propeller Types | 04/01/1990 |
| TN 809-7 |
|
en |
C/G Tow Release ((FM, MM)) | 04/12/1990 |
| TN 809-8 |
|
en |
Elevator Control System ((Appendix)) | 11/05/1990 |
| TN 809-9 |
|
en |
Vertical Elevator Actuating Rod Inside Fin ((Appendix)) | 11/20/1992 |
| TN 809-10 |
|
en |
"L'Hotellier" Ball and Swivel Joints ((Appendix, FM)) | 04/20/1993 |
| TN 809-11 |
|
en |
"Wedekind" Safety Sleeve for "L'Hotellier" Ball and Swivel Joint Connectors No. AMZ-9, 41 (Having a Wedge-Shaped Locking Plate) (Appendix; FM for Janus CM, Janus CT) | 02/08/1994 |
| TN 809-12 |
|
en |
Use of a New Electronic Box (DUCATI) with Modified Wiring on Stator Plate | 05/05/1995 |
| TN 809-13 |
|
en |
Flight Manual - Minimum Seat Load with Two Occupants ((FM)) | 02/06/1998 |
| TN 809-14 |
|
en |
Extension of Service Time ((MM)) | 10/12/1998 |
| TN 809-15 |
|
en |
Horizontal Tailplane - Elevator Mass Balance ((MM)) | 06/30/1999 |
| TN 809-16 |
|
en |
Elevator Control System ((Appendix)) | 09/24/2004 |
| TN 809-17 |
|
en |
Engine Controls - Manual Primer (Appendix, FM, MM) | 12/21/2004 |
| TN 809-18 |
|
en |
Change of Allowed Hinge Moments and Weights of Control Surfaces ((MM)) | 10/27/2008 |
| TN 825-2 |
|
en |
Engine Control Box ((FM, MM)) | 11/09/1984 |
| TN 825-3 |
|
en |
Power Plant Controls - Decompression Value Actuating System ((FM, MM)) | 09/18/1985 |
| TN 825-4 |
|
en |
Maintenance Manual ((MM)) | 01/30/1986 |
| TN 825-10 |
|
en |
Airbrakes | 05/11/1999 |
| TN 825-17 |
|
en |
Vertical Elevator Actuating Rod Inside Fin ((Appendix)) | 11/20/1992 |
| TN 825-21 |
|
en |
Extension of Service Time (MM for Ventus bT, Ventus cM, Ventus cT) | 06/14/1999 |
| TN 825-22 |
|
en |
Toothed Belt Tension. Spindle-to-Pylon Attachment Bracket. Mechanical Spindle Drive Overload Safety Device. Limit Switch "Pylon Retracted". Propeller Brake System. Rectifier Regulator. Fuel Reserve Quality. Flight Manual. Maintenance Manual. Engine Manual ((FM, MM)) | 10/15/1999 |
| TN 825-23 |
|
en |
Engine Mount Structure (Pylon) ((Appendix, MM)) | 01/11/2000 |
| TN 825-24 |
|
en |
Attachment of Forward Spindle Drive Mounting Bracket. Attachment of Engine/Propeller Pylon. Maintenance Manual | 09/20/2000 |
| TN 825-25 |
|
en |
Noise Certificate - Flight Manual ((FM)) | 11/21/2000 |
| TN 825-27 |
|
en |
Landing Gear (Appendix; MM for Ventus-2cM, Ventus-2cT) | 07/20/2001 |
| TN 825-27 |
revised |
en |
Landing Gear | 05/23/2003 |
| TN 825-29 |
|
en |
Flap Drive Inside Fuselage ((Appendix)) | 07/06/2001 |
| TN 825-30 |
|
en |
C.G. Release, Installation Position (Appendix; MM for Ventus-2cM, Ventus-2cT, Ventus cM) | 12/21/2001 |
| TN 825-31 |
|
en |
Hub of Propeller Bearing. Spindle Drive Overload Safety Devise. Supplements Maintenance Manual | 11/15/2002 |
| TN 825-32 |
|
en |
Replacement of Electronic Boxes for Engine SOLO 2625-01/02 ((Appendix, MM)) | 01/07/2004 |
| TN 825-33 |
|
en |
Mounting of a Slip Clutch "Friction Clutch" (Appendix, MM, Solo SB) | 02/20/2004 |
| TN 825-34 |
|
en |
Horizontal Stabilizer ((Appendix)) | 01/20/2005 |
| TN 825-35 |
|
en |
Fuselage, Bearing of Automatic Control Attachment | 09/20/2005 |
| TN 825-36 |
|
en |
Installation of an Emergency Bail Out Assistance System for Occupant (FM for Ventus bT, Ventus cM, Ventus cT, Ventus cT, Ventus 2cT, Ventus 2cT) | 12/14/2006 |
| TN 825-37 |
|
en |
Increase of Maximum Permitted All-Up Mass on 600 kg for 18 m Wing Span ((FM, MM)) | 05/17/2006 |
| TN 825-37 |
Iss 2 |
en |
Increase of Maximum Permitted All-Up Mass on 600 kg for 18 m Wing Span ((FM, MM)) | 06/25/2005 |
| TN 825-38 |
|
en |
Engine Mounting Structure (Pylon) ((Appendix)) | 07/19/2006 |
| TN 825-39 |
|
en |
Engine Mounting Structure (Pylon) (AppendixFM, FM2, MM, MM2) | 07/18/2006 |
| TN 825-40 |
|
en |
Additional Inspections of Optional Slip Clutch on Engine SOLO 2625-01 (Solo SB, MM1, MM1.1) | 01/11/2007 |
| TN 825-41 |
|
en |
Optional Installation of a Beringer 5-Inch-Wheel with Tire (Work Inst, Drawing; MM for Ventus-2cM, Ventus-2cM, Ventus-2cT, Ventus-2cT) | 10/17/2007 |
| TN 825-42 |
|
en |
New Engine Control Unit TB05 ((FM, MM)) | 07/23/2007 |
| TN 825-44 |
|
en |
Installation of Transponder Antenna on Upper Side of Fuselage Behind Engine Compartment | 01/21/2008 |
| TN 825-45 |
|
en |
Inspection of Wing Shear Web for Damage ((Appendix)) | 04/08/2008 |
| TN 825-46 |
|
en |
Installation of Transponder Antenna on Upper Side of Fuselage Behind Engine Compartment | 03/14/2008 |
| TN 825-47 |
|
en |
Connection to Fuselage of Front Suspension of Extension/Retraction Mechanism for Engine for Self-Launching Gliders Manufactured in 2007/2008 ((Work Inst)) | 12/19/2008 |
| TN 825-48 |
|
en |
Installation of a Manually Operated Propeller Brake (FM, FM2, MM, MM2) | 08/20/2010 |
| TN 825-49 |
|
en |
Amendment of Daily Inspection and Exchange of Starter Ring Gear ((FM)) | 02/08/2010 |
| TN 825-50 |
|
en |
Installation of a Steerable Tail Wheel with Wheel Size 150x30 and Steel Fork | 12/09/2014 |
| TN 825-51 |
1 |
en |
Amendment of Flight Manual and Repair Method for Engine Pylon (FM for Ventus cT, Ventus 2cT, Ventus 2cT) | 07/06/2011 |
| TN 825-52 |
|
en |
Engine Mounting Structure (Pylon) (FM for Ventus cT, Ventus bT; MM for Ventus cT, Ventus bT) | 07/19/2011 |
| TN 825-53 |
|
en |
New Winglets for 18m Wingtips ((Work Inst)) | 05/19/2014 |
| TN 825-55 |
|
en |
Inspection of Overlap between Airbrake Panels ((Work Inst)) | 01/22/2016 |
| TN 825-57 (WI) |
|
en |
Inspection of Flaperon Control in Wings for Corrosion & Other Damage | 08/31/2020 |
| TN 831-9 |
|
en |
"L'Hotellier" Ball and Swivel Joint ((Appendix)) | 03/26/1993 |
| TN 831-10 |
|
en |
"Wedekind" Safety Sleeve for "L-Hotellier" Ball and Swivel Joint Connectors No. RMZ-9,41 (Having a Wedge-Shaped Locking Plate) | 03/04/1994 |
| TN 831-11 |
|
en |
Extension of Service Time Up to 12000 Flight Hours. Supplements of Maintenance Manual ((Nimbus-3T MM [de])) | 10/21/2005 |
| TN 831-12 |
|
en |
Installation of Transponder Antenna on Upper Side of Fuselage Behind Engine Compartment | 01/21/2008 |
| TN 847-1 |
|
en |
Mounting Provision for Trim Ballast Weights ((FM for Nimbus-3DT, Nimbus-3DM)) | 01/30/1992 |
| TN 847-2 |
|
en |
Maintenance Manual - Rigging Data and Control Surface Deflections ((MM for Nimbus-3DT, Nimbus-3DM)) | 02/13/1992 |
| TN 847-3 |
|
en |
Wing Tip Extensions ((FM, MM)) | 02/09/1992 |
| TN 847-4 |
|
en |
Vertical Elevator Actuating Rod Inside Fin ((Appendix)) | 11/20/1992 |
| TN 847-5 |
|
en |
"L'Hotellier" Ball and Swivel Joint ((Appendix)) | 03/26/1993 |
| TN 847-6 |
|
en |
"Wedekind" Safety Sleeve for "L-Hotellier" Ball and Swivel Joint Connectors No. RMZ-9,41 (Having a Wedge-Shaped Locking Plate) | 03/04/1994 |
| TN 847-7 |
|
en |
Use of a New Electronic Box (DUCATI) with Modified Wiring on Stator Plate | 05/05/1995 |
| TN 847-8 |
|
en |
Extension of Service Time. Supplements of Maintenance Manual ((MM)) | 02/03/2002 |
| TN 847-9 |
|
en |
Elevator Control System ((Appendix)) | 09/27/2004 |
| TN 847-10 |
|
en |
Installation of Transponder Antenna on Upper Side of Fuselage Behind Engine Compartment | 03/14/2008 |
| TN 863-2 |
|
en |
Fuel System ((Inst)) | 12/04/1990 |
| TN 863-3 |
|
en |
Vertical Elevator Actuating Rod Inside Fin ((Appendix)) | 11/20/1992 |
| TN 863-4 |
|
en |
Winglets ((FM for Discus bM, Discus bT)) | 03/29/1996 |
| TN 863-5 |
|
en |
Extension of Service Time ((MM)) | 07/05/1999 |
| TN 863-6 |
|
en |
Engine Mount Structure (Pylon) ((Appendix)) | 01/11/2000 |
| TN 863-7 |
|
en |
Hub of Propeller Bearing. Spindle Drive Overload Safety Devise. Supplements Maintenance Manual ((MM)) | 11/15/2002 |
| TN 863-8 |
|
en |
Elevator, Fixing of Mass Balance Weights ((Appendix)) | 09/16/2003 |
| TN 863-9 |
|
en |
Wing, Bonding of Spar Cap to Spar Web ((Appendix)) | 09/25/2003 |
| TN 863-10 |
|
en |
Amendment of Manuals and Optional Installation of a Slip Clutch ((FM, MM)) | 12/22/2009 |
| TN 863-11 |
|
en |
Installation of an Emergency Bail Out Assistance System for Occupant (FM for Discus-2cT, Discus-2T, Discus bT) | 12/14/2006 |
| TN 863-12 |
|
en |
Retrofit of New Winglets on Wing Tip with Winglets ((Appendix)) | 04/21/2006 |
| TN 863-13 |
|
en |
Engine Mounting Structure (Pylon) ((Appendix)) | 07/19/2006 |
| TN 863-14 |
|
en |
Engine Mounting Structure (Pylon) (Appendix; FM for Discus-2cT, Discus-2T; MM for Discus-2cT, Discus-2T) | 07/18/2006 |
| TN 863-15 |
|
en |
Optional Installation of a Beringer 5-Inch-Wheel with Tire (Work Inst, Drawing; MM for Discus-2T, Discus-2cT) | 03/26/2008 |
| TN 863-16 |
|
en |
New Engine Control Unit TB05 (FM for Discus-2cT, Discus-2T; MM for Discus-2cT, Discus-2T) | 10/12/2007 |
| TN 863-17 |
|
en |
Installation of Transponder Antenna on Upper Side of Fuselage Behind Engine Compartment | 01/21/2008 |
| TN 863-18 |
|
en |
Installation of Transponder Antenna on Upper Side of Fuselage Behind Engine Compartment | 03/14/2008 |
| TN 863-19 |
|
en |
Back Rest Adjustment | 07/11/2008 |
| TN 863-20 |
1 |
en |
Amendment of Flight Manual and Repair Method for Engine Pylon (FM for Discus bT, Discus 2T, Discus 2cT) | 07/27/2011 |
| TN 863-21 |
|
en |
Engine Mounting Structure (Pylon) ((FM, MM)) | 07/19/2011 |
| TN 863-22 |
|
en |
Inspection of Overlap between Airbrake Panels ((Work Inst)) | 01/22/2016 |
| TN 868-1 |
|
en |
Capacity of Fuel Tank in Inboard. Wing Panel(s) ((FM, MM)) | 11/21/1996 |
| TN 868-2 |
|
en |
Vent Line of Fuel Tank in Inboard. Wing Panel(s) (Appendix, FM, MM) | 12/09/1996 |
| TN 868-3 |
|
en |
Toothed Belt Tension & Crankshaft Bearing. Spindle-to-Pylon Attachment Strut. Mechanical Spindle Drive Overload Safety Device. Limit Switch "Pylon Retracted". Propeller Brake System. Fuel Reserve Quantity. Flight Manual. Maintenance Manual. Engine Manual ((FM, MM)) | 11/08/1999 |
| TN 868-4 |
|
en |
Canopy Locking Mechanism ((Appendix)) | 02/15/2005 |
| TN 868-5 |
|
en |
Hub of Propeller Bearing. Spindle Drive Overload Safety Devise. Supplements Maintenance Manual ((MM)) | 11/15/2002 |
| TN 868-6 |
|
en |
Replacement of the Electronic Boxes for Engine SOLO 2625-01/02 (Appendix; MM for Nimbus-4DM, Nimbus-4M) | 01/07/2004 |
| TN 868-7 |
|
en |
Mounting of a Slip Clutch "Friction Clutch" (Appendix, Solo SB; MM for Nimbus-4DM, Nimbus-4M) | 02/20/2004 |
| TN 868-8 |
|
en |
Replacement of Electronic Boxes at Engine Rotax 535C and 505A (Appendix; MM for Nimbus-4DM, Nimbus-4DM, Nimbus-4M) | 10/20/2004 |
| TN 868-8 |
Iss 2 |
en |
Replacement of Electronic Boxes at Engine Rotax 535C and 505A ((MM)) | 02/16/2010 |
| TN 868-9 |
|
en |
Maximum Weight by Power Plant Removed (FM for Nimbus-4DM, Nimbus-4DT, Nimbus-4T; MM for Nimbus-4DM, Nimbus-4DT, Nimbus-4M, Nimbus-4T) | 07/08/2005 |
| TN 868-10 |
|
en |
Increase of Maximum Permitted All-Up Mass on 850 kg (Work Inst; FM for Nimbus-4M, Nimbus-4M, Nimbus-4T; MM for Nimbus-4M, Nimbus-4M, Nimbus-4T) | 04/10/2012 |
| TN 868-11 |
|
en |
Propeller | 09/22/2006 |
| TN 868-12 |
|
en |
Additional Inspections of Optional Slip Clutch on Engine SOLO 2625-02 (Solo SB; MM for Nimbus-4M, Nimbus-4DM) | 01/11/2007 |
| TN 868-15 |
|
en |
Reduction of Max. RPM for Engine Operation (FM for Nimbus-4M, Nimbus-4DM; MM for Nimbus-4M, Nimbus-4DM) | 04/30/2007 |
| TN 868-16 |
|
en |
Installation of Transponder Antenna on Upper Side of Fuselage Behind Engine Compartment | 01/21/2008 |
| TN 868-17 |
|
en |
Installation of Transponder Antenna on Upper Side of Fuselage Behind Engine Compartment | 03/14/2008 |
| TN 868-18 |
|
en |
Connection to Fuselage of Front Suspension of Extension/Retraction Mechanism for Engine for Self-Launching Gliders Manufactured in 2007/2008 ((Work Inst)) | 12/19/2008 |
| TN 868-19 |
|
en |
Installation of a Manually Operated Propeller Brake (FM for Nimbus-4DM, Nimbus-4DM, Nimbus-4M; MM for Nimbus-4DM, Nimbus-4DM, Nimbus-4M) | 08/20/2010 |
| TN 868-20 |
|
en |
Amendment of Daily Inspection and Exchange of Starter Gear Ring ((FM for Nimbus-4DM, Nimbus-4M)) | 02/08/2010 |
| TN 868-21 |
|
en |
Amendment of Flight Manual and Maintenance Manual ((FM, MM)) | 10/15/2012 |
| TN 868-22 |
|
en |
Inspection of Airbrake Bell Cranks at Root Rib of Wings and of Respective Drive Funnels on Fuselage Side in Fuselage-Wing-Fairing ((Work Inst)) | 07/13/2015 |
| TN 868-22 |
1 |
en |
Inspection of Airbrake Bell Cranks at Root Rib of Wings and of Respective Drive Funnels on Fuselage Side in Fuselage-Wing-Fairing ((Work Inst)) | 07/13/2015 |
| TN 868-24 (WI) |
|
en |
Inspection of Elevator U-Bracket for Damages | 02/28/2022 |
| TN 890-1 |
|
en |
Airbrake Control Mechanism ((Appendix)) | 01/31/2002 |
| TN 890-2 |
|
en |
Manual Operated Rudder Control ((FM, MM)) | 11/17/2003 |
| TN 890-3 |
|
en |
Wing, Bonding of Spar Cap to Spar Web ((Appendix)) | 07/31/2003 |
| TN 890-4 |
|
en |
Removable Aft Control Stick ((Appendix, FM)) | 08/30/2004 |
| TN 890-5 |
|
en |
Canopy Locking Mechanism ((Appendix)) | 02/15/2005 |
| TN 890-6 |
|
en |
Flight Manual ((FM)) | 09/20/2005 |
| TN 890-7 |
|
en |
Retrofit of Winglets (Appendix, FM, MM) | 02/17/2006 |
| TN 890-8 |
|
en |
Propeller | 09/22/2006 |
| TN 890-9 |
|
en |
Increase of Maximum Permitted All-Up Mass to 750 kg and of Maximum Weight of Non-Lifting Parts to 500 kg ((FM, MM)) | 06/12/2007 |
| TN 890-11 |
|
en |
Substitution of Nose Wheel by a Nose Skid ((FM, MM)) | 06/20/2007 |
| TN 890-13 |
|
en |
Amendment of Flight Manual and Maintenance Manual (FM, FM MM, MM) | 10/15/2012 |
| TN 890-13 |
Iss 2 |
en |
Amendment of Flight Manual and Maintenance Manual ((MM)) | 03/05/2013 |
| TN 890-14 |
1 |
en |
Inspection of Airbrake Bell Cranks at Root Rib of Wings and of Respective Drive Funnels on Fuselage Side in Fuselage-Wing-Fairing ((Work Inst)) | 07/13/2015 |
| TN 890-16 (WI) |
|
en |
Exchange of Plastic Bushings on Airbrake End Stops | 09/18/2020 |
| TN 890-18 (WI) |
|
en |
Inspection of Elevator U-Bracket for Damages | 02/28/2022 |
| TN A532-1 |
|
en |
Amendment of Flight Manual and Maintenance Manual ((FM, MM)) | 10/15/2012 |
| TN A532-2 |
|
en |
Improvements on Airbrakes ((Work Inst)) | 02/21/2014 |
| TN A532-10 (WI) |
|
en |
Inspection of Elevator U-Bracket for Damages | 02/28/2022 |
