Service Information: Schempp-Hirth Flugzeugbau
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Table of Contents
Maintenance Information • Modification Bulletins • Service Bulletins • Technical Notes • Transponder-Installation Drawings
| Name | Revision | Lang | Subject | Date |
|---|---|---|---|---|
| MI SHK-M-01-22 | en | Duo Discus - General, without Trailing Edge Flap, with Trailing Edge Flap | 01/26/2022 |
| Name | Revision | Lang | Subject | Date |
|---|---|---|---|---|
| MB 396-10 | en | Maximum Permitted Speed on Aerotow | 01/10/2000 | |
| MB 825-38 | en | Noise Certificate - Flight Manual | 11/21/2000 |
| Name | Revision | Lang | Subject | Date |
|---|---|---|---|---|
| SB 2 | en | Standard Cirrus G - Improvement of Locking Device for Horizontal Tail Plane | 04/11/1980 |
| 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 | Supporting Core Material of Wing Spar Web | 03/02/1973 | |
| TN 1/73 | en | Outer Wing Sections Built in a Pure Glass Fiber Plastic Layup without Foam Sandwich | 07/10/1973 | |
| 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 278-25 | 1 | en | Elevator Drive | 07/09/2024 |
| 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 | rev | 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 | rev | 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 | Iss2 | 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 | rev | 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 | 09/05/1988 | |
| TN 328-8 | en | Elevator Drive | 08/14/1987 | |
| 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 | rev | 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-Act2) |
en | Check of Overlap between Airbrake Panels | 09/18/2020 | |
| TN 396-20 (WI-Act1) |
en | Exchange of Plastic Bushings on Airbrake End Stops | 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 | rev | 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 | rev | 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 | Iss2 | 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 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 | Iss2 | 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 | Iss2 | 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 |
| Name | Revision | Lang | Subject | Date |
|---|---|---|---|---|
| HM02-10.160 | en | Janus CT (MM), Janus CM (MM) | ||
| HM02-10.160 | en | Janus (MM), Janus B (MM), Janus C (MM) | ||
| HM02-10.161 | en | Janus CT (MM), Janus CM (MM) | ||
| HM02-10.161 | en | Janus Ce (MM) | ||
| HS02-10.132 | en | Cirrus (MM) | ||
| HS04-10.115 | en | Standard Cirrus (MM), Standard Cirrus CS 11.75L (MM), Standard Cirrus G (MM), Standard Cirrus B (MM) | ||
| HS05-10.125 | en | Nimbus-2 (MM), Nimbus-2B (MM), Nimbus-2C (MM) | ||
| HS08-10.135 | en | Ventus a (MM), Ventus a/16.6 (MM), Ventus c (MM), Discus a (MM) | ||
| HS08-10.136 | en | Mini Nimbus HS7 (MM), Mini Nimbus B (MM), Mini Nimbus C (MM), Ventus b (MM), Ventus b/16.6 (MM), Ventus c (MM), Discus b (MM), Discus CS (MM), Ventus bT (MM), Ventus cT (MM), Ventus cM (MM), Discus bM (MM), Discus bT (MM) | ||
| ZRE 109 | en | Nimbus-3D (MM), Nimbus-4D (MM), Duo Discus (MM), Nimbus-3DM (MM) (MM), Nimbus-3DT (MM), Nimbus-4DT (MM), Nimbus-4DM (MM), Duo Discus T (MM) | ||
| ZRE 110 | en | Ventus 2b (MM), Ventus 2c (MM), Discus-2b (MM), Discus-2c (MM), Ventus 2cT (MM), Ventus 2cxT (MM), Ventus 2cM (MM), Ventus 2cxM (MM), Discus-2T (MM), Discus-2cT (MM) | ||
| ZRE 112 | en | Duo Discus x (MM), Duo Discus xT (MM) | ||
| ZRE 114 | en | Nimbus-3/24.5 (MM), Ventus 2a (MM), Ventus 2c(x) (MM), Discus-2a (MM), Nimbus-3T (MM) | ||
| ZRE 116 | en | Nimbus-4M (MM) | ||
| ZRE 117 | en | Nimbus-4 (MM), Nimbus-4T (MM) | ||
| ZRE 118 | en | SHK (MM), Standard Austria S (MM), Standard Austria SH (MM), Standard Austria SH1 (MM) |