Aircraft model

DG Flugzeugbau

DG Flugzeugbau GmbH

Airworthiness Directives
54
Service Bulletins
0
Last live check
2026-08-1754 of 54 re-verified
What this page is: a restatement of what the official Federal Register and manufacturer records show as of the date listed below each item. It is not a determination that any specific aircraft or engine is, or is not, in compliance. Under 14 CFR §91.403 and §91.417, the aircraft owner/operator is responsible for maintaining airworthiness and required records. Always verify against the official FAA and manufacturer sources linked below before making a maintenance or airworthiness decision.

Airworthiness Directives

54 records · 4 superseded records nested above
AD

2026-07-03

FR doc 2026-06534 · 91 FR 16815

AD 2026-07-03Published 2026-04-03Effective 2026-04-20

DG Aviation GmbH (Type Certificate Previously Held by DG Flugzeugbau GmbH) Gliders

Requires updating the maintenance manual, inspecting the engine mount for cracks, and taking corrective actions if cracks are found.

Full official abstract

Airworthiness Directives; DG Aviation GmbH (Type Certificate Previously Held by DG Flugzeugbau GmbH) Gliders

The FAA is adopting a new airworthiness directive (AD) for all DG Aviation GmbH (Type Certificate Previously Held by DG Flugzeugbau GmbH) Model DG-1000M gliders. This AD was prompted by reports of engine mount cracking near the propeller head. This AD requires updating the maintenance manual, inspecting the engine mount for cracks, and taking corrective actions if cracks are found. This AD also requires performing a powerplant belt tension inspection and, depending on the results of the inspection, adjusting the belt tension. This AD also requires balancing the propeller assembly and installing a carbon fiber reinforced plastic (CFRP) bracket. This AD also prohibits accomplishing certain maintenance actions in the maintenance manual. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2026-06534, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2025-13-08

FR doc 2025-12875 · 90 FR 30575

AD 2025-13-08Published 2025-07-10Effective 2025-07-25

DG Aviation GmbH (Type Certificate Previously Held by DG Flugzeugbau GmbH) Gliders

Requires revising the glider flight manual and installing "Motor INOP" placards to prohibit operation with the powerplant.

Full official abstract

Airworthiness Directives; DG Aviation GmbH (Type Certificate Previously Held by DG Flugzeugbau GmbH) Gliders

The FAA is adopting a new airworthiness directive (AD) for all DG Aviation GmbH (type certificate previously held by DG Flugzeugbau GmbH) Model DG-1000T gliders. This AD was prompted by reports of propeller separation. This AD requires revising the glider flight manual and installing "Motor INOP" placards to prohibit operation with the powerplant. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2025-12875, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2024-19-12

FR doc 2024-22321 · 89 FR 79425

AD 2024-19-12Published 2024-09-30Effective 2024-10-15

DG Aviation GmbH (Type Certificate Previously Held by DG Flugzeugbau GmbH) Gliders

Requires revising your existing glider maintenance manual to incorporate new procedures for elevator control circuit free play adjustment, performing an operational check of the free play adjustment of the automatic elevator…

Full official abstract

Airworthiness Directives; DG Aviation GmbH (Type Certificate Previously Held by DG Flugzeugbau GmbH) Gliders

The FAA is adopting a new airworthiness directive (AD) for certain DG Aviation GmbH (type certificate previously held by DG Flugzeugbau GmbH) Model DG-400 gliders and all Model DG-500 Elan Orion, DG-500 Elan Trainer, DG-500/20 Elan, DG-500/22 Elan, DG-500M, DG-500MB, DG-800A, DG-800B, DG-808C, DG-1000M, DG-1000S, and DG-1000T gliders. This AD was prompted by a report of a broken rod end at the upper end of the elevator pushrod in the fin (vertical tail) of a DG Aviation GmbH Model DG-300 glider. Depending on the glider model, this AD requires revising your existing glider maintenance manual to incorporate new procedures for elevator control circuit free play adjustment, performing an operational check of the free play adjustment of the automatic elevator hook-up, accomplishing corrective actions as required, and replacing the elevator pushrod end with a new part. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2024-22321, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2023-03-22

FR doc 2023-03997 · 88 FR 12820

AD 2023-03-22Published 2023-03-01Effective 2023-04-05

DG Flugzeugbau GmbH and Schempp-Hirth Flugzeugbau GmbH Gliders

Supersedes 2015-09-04 R1 — see below

Requires repetitive replacement of the eccentric axle, adds the Schempp-Hirth Model Duo Discus T gliders to the applicability, and retains from AD 2015-09-04 R1 the option of operating the glider with the engine non-operative…

1 AD superseded by this one retired · earliest 2016-05-02
AD

2015-09-04 R1

FR doc 2016-08961 · 81 FR 26124

AD 2015-09-04 R1Published 2016-05-02Effective 2016-06-06

DG Flugzeugbau GmbH Gliders

Superseded by 2023-03-22 — see above

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

We are revising Airworthiness Directive (AD) 2015-09-04 for DG Flugzeugbau GmbH Model DG-1000T gliders equipped with a Solo Kleinmotoren Model 2350 C engine. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as engine shaft failure and consequent propeller detachment. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2016-08961, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH and Schempp-Hirth Flugzeugbau GmbH Gliders

The FAA is superseding Airworthiness Directive (AD) 2015-09-04 R1, which applied to DG Flugzeugbau GmbH Model DG-1000T gliders equipped with a Solo Kleinmotoren GmbH (currently Solo Vertriebs-und Entwicklungs-GmbH) (Solo) Model 2350 C engine. AD 2015-09-04 R1 prohibited operation of the engine and required performing a magnetic particle or dye penetrant inspection of the propeller shaft and reporting the results of the inspection to Solo. This AD is prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as occurrences of rupture of the eccentric axle on Solo Model 2350 C engines (installed on DG Flugzeugbau GmbH Model DG-1000T gliders in the United States) and an occurrence on a Solo Model 2350 D engine (installed on Schempp-Hirth Flugzeugbau GmbH (Schempp-Hirth) Model Duo Discus T gliders in the United States). This AD requires repetitive replacement of the eccentric axle, adds the Schempp-Hirth Model Duo Discus T gliders to the applicability, and retains from AD 2015-09-04 R1 the option of operating the glider with the engine non-operative instead of replacing the eccentric axle. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2023-03997, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2022-04-01

FR doc 2022-03591 · 87 FR 9437

AD 2022-04-01Published 2022-02-22Effective 2022-03-29

DG Flugzeugbau GmbH and Schempp-Hirth Flugzeugbau GmbH Gliders

Requires replacing a certain hex-nut and establishing a life limit for the ball bearing assembly.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH and Schempp-Hirth Flugzeugbau GmbH Gliders

The FAA is adopting a new airworthiness directive (AD) for DG Flugzeugbau GmbH Model DG-1000T gliders and Schempp-Hirth Flugzeugbau GmbH Model Duo Discus T gliders with a Solo Kleinmotoren GmbH Solo Model 2350C or 2350D engine installed. This AD was prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as failure of the bearing of the upper pulley of the belt driven reduction gear resulting in separation of the propeller from the engine. This AD requires replacing a certain hex-nut and establishing a life limit for the ball bearing assembly. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2022-03591, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2021-24-19

FR doc 2021-27636 · 86 FR 72827

AD 2021-24-19Published 2021-12-23Effective 2022-01-27

DG Flugzeugbau GmbH Gliders

Requires updating the ECU software.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

The FAA is adopting a new airworthiness directive (AD) for all DG Flugzeugbau GmbH Model DG-500MB and DG-1000M gliders with a Solo Kleinmotoren GmbH Solo Model 2625 02i engine installed. This AD was prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as an error in the engine control unit (ECU) software. This AD requires updating the ECU software. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2021-27636, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2021-18-14

FR doc 2021-21095 · 86 FR 54037

AD 2021-18-14Published 2021-09-30Effective 2021-11-04

DG Flugzeugbau GmbH Gliders

Requires inspecting the polyurethane (PU) fuel hoses, replacing the PU fuel hoses if there is damage, and establishing a life limit for the PU fuel hoses.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

The FAA is adopting a new airworthiness directive (AD) for all DG Flugzeugbau GmbH Models DG-808C and DG-1000T gliders. This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as damaged fuel hoses due to environmental and fatigue deterioration. This AD requires inspecting the polyurethane (PU) fuel hoses, replacing the PU fuel hoses if there is damage, and establishing a life limit for the PU fuel hoses. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2021-21095, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2020-13-09

FR doc 2020-17043 · 85 FR 47638

AD 2020-13-09Published 2020-08-06Effective 2020-08-26

DG Flugzeugbau GmbH Gliders

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

The FAA is adopting a new airworthiness directive (AD) for all DG Flugzeugbau GmbH Models DG-500 Elan Orion, DG-500 Elan Trainer, DG- 500/20 Elan, DG-500/22 Elan, DG-500M, and DG-500MB gliders and certain Models DG-1000S and DG-1000T gliders. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as the rear locking rod of the rear canopy rotating out of the threads of the operating mechanism, which could lead to blocking of the canopy emergency release system, preventing safe escape of occupants from the glider. The FAA is issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2020-17043, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2018-10-09

FR doc 2018-10583 · 83 FR 23575

AD 2018-10-09Published 2018-05-22Effective 2018-06-26

DG Flugzeugbau GmbH Gliders

Supersedes 2017-11-03 — see below

Requires actions to address the unsafe condition on these products.

1 AD superseded by this one retired · earliest 2017-05-25
AD

2017-11-03

FR doc 2017-10392 · 82 FR 24015

AD 2017-11-03Published 2017-05-25Effective 2017-06-29

DG Flugzeugbau GmbH Gliders

Superseded by 2018-10-09 — see above

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

We are adopting a new airworthiness directive (AD) for DG Flugzeugbau GmbH Model DG-500MB gliders that are equipped with a Solo 2625 02 engine that has been modified with a fuel injection system following the instructions of Solo Kleinmotoren GmbH Service Bulletin (SB)/Technische Mitteilung (TM) 4600-3 "Fuel Injection System" and re-identified as Solo 2625 02i. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as failure of the connecting rod bearing resulting from too much load on the rod bearings from the engine control unit. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2017-10392, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

We are superseding Airworthiness Directive (AD) 2017-11-03 for DG Flugzeugbau GmbH Model DG-500MB gliders that are equipped with a Solo 2625 02 engine modified with a fuel injection system following the instructions of Solo Kleinmoteren GmbH Technische Mitteilung 4600-3 and identified as Solo 2625 02i. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as failure of the connecting rod bearing resulting from too much load on the rod bearings from the engine control unit. This AD adds a model to the applicability. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2018-10583, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2018-07-22

FR doc 2018-07970 · 83 FR 17478

AD 2018-07-22Published 2018-04-20Effective 2018-05-25

DG Flugzeugbau GmbH Gliders

Supersedes 2017-08-09 — see below

Requires actions to address the unsafe condition on these products.

1 AD superseded by this one retired · earliest 2017-04-21
AD

2017-08-09

FR doc 2017-07776 · 82 FR 18694

AD 2017-08-09Published 2017-04-21Effective 2017-05-26

DG Flugzeugbau GmbH

Superseded by 2018-07-22 — see above

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH

We are adopting a new airworthiness directive (AD) for DG Flugzeugbau GmbH Model DG-500MB gliders that are equipped with a Solo 2625 02 engine modified with a fuel injection system following the instructions of Solo Kleinmotoren GmbH Technische Mitteilung (TM)/ Service Bulletin (SB) 4600-3 "Fuel Injection System" and identified as Solo 2625 02i. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as possible in-flight engine shut-down and engine fire due to failure of the connecting stud for the two fuel injector mounts of the engine redundancy system. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2017-07776, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

We are superseding Airworthiness Directive (AD) 2017-08-09 for DG Flugzeugbau GmbH Model DG-500MB gliders that are equipped with a Solo 2625 02 engine modified with a fuel injection system following the instructions of Solo Kleinmotoren GmbH Technische Mitteilung Nr. 4600-3 and identified as Solo 2625 02i. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as the potential of an in-flight shut-down and engine fire due to failure of the connecting stud for the two fuel injector mounts of the engine redundancy system on gliders equipped with a Solo 2625 02i engine. We are issuing this AD to add a model to the applicability and require actions to address the unsafe condition on these products.

Source: Federal Register document 2018-07970, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2017-13-06

FR doc 2017-13127 · 82 FR 28758

AD 2017-13-06Published 2017-06-26Effective 2017-07-31

DG Flugzeugbau GmbH Gliders

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

We are adopting a new airworthiness directive (AD) for all DG Flugzeugbau GmbH Models DG-400, DG-500M, DG-500MB, DG-800A, and DG-800B gliders. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as a manufacturing defect in certain textile fabric covered fuel hoses, which could cause the fuel hose to fail. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2017-13127, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2015-09-04

FR doc 2015-09928 · 80 FR 25591

AD 2015-09-04Published 2015-05-05Effective 2015-05-26

DG Flugzeugbau GmbH Gliders

Supersedes 2013-22-14 R1 — see below

Requires actions to address the unsafe condition on these products.

1 AD superseded by this one retired · earliest 2014-09-15
AD

2013-22-14 R1

FR doc 2014-21761 · 79 FR 54895

AD 2013-22-14 R1Published 2014-09-15Effective 2014-10-20

DG Flugzeugbau GmbH Gliders

Superseded by 2015-09-04 — see above

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

We are revising an airworthiness directive (AD) 2013-22-14 for any DG Flugzeugbau GmbH Model DG-1000T glider equipped with a Solo Kleinmotoren Model 2350 C engine. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as engine shaft failure and consequent propeller detachment. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2014-21761, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

We are adopting a new airworthiness directive (AD) for DG Flugzeugbau GmbH Model DG-1000T gliders equipped with a Solo Kleinmotoren Model 2350 C engine that supersedes AD 2013-22-14 R1. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as engine shaft failure with consequent propeller detachment. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2015-09928, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2013-22-12

FR doc 2013-25955 · 78 FR 67013

AD 2013-22-12Published 2013-11-08Effective 2013-11-18

DG Flugzeugbau GmbH Gliders

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

We are adopting a new airworthiness directive (AD) for all DG Flugzeugbau GmbH Models DG-800A, DG-800B, DG-500MB gliders. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as a defective starter motor control unit, which could activate the starter motor without pressing the starter button. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2013-25955, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2013-22-14

FR doc 2013-25954 · 78 FR 65869

AD 2013-22-14Published 2013-11-04Effective 2013-11-25

DG Flugzeugbau GmbH Gliders

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

We are adopting a new airworthiness directive (AD) for any DG Flugzeugbau GmbH Model DG-1000T glider equipped with a Solo Kleinmotoren Model 2350 C engine. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as engine shaft failure and consequent propeller detachment. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2013-25954, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2013-03-09

FR doc 2013-02718 · 78 FR 9792

AD 2013-03-09Published 2013-02-12Effective 2013-03-19

DG Flugzeugbau GmbH Gliders

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

We are adopting a new airworthiness directive (AD) for DG Flugzeugbau GmbH Model DG-1000T gliders equipped with Solo Kleinmotoren Model 2350 C engines. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as a material defect of the propeller shaft, most likely caused by a manufacturing error. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2013-02718, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2012-06-15

FR doc 2012-7003 · 77 FR 21400

AD 2012-06-15Published 2012-04-10Effective 2012-05-15

DG Flugzeugbau GmbH Sailplanes

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Sailplanes

We are adopting a new airworthiness directive (AD) for DG Flugzeugbau GmbH Models DG-500 Elan Orion, DG-500 Elan Trainer, DG-500/ 20 Elan, and DG-500/22 Elan sailplanes and Models DG-500M and DG-500MB powered sailplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as incorrect re-installation of the rear cockpit securing rope for the headrest of the rear seat during maintenance, which could cause the rear seat to interfere with the control stick of the sailplane. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2012-7003, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2012-06-13

FR doc 2012-7002 · 77 FR 19063

AD 2012-06-13Published 2012-03-30Effective 2012-05-04

DG Flugzeugbau GmbH Gliders

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

We are adopting a new airworthiness directive (AD) for DG Flugzeugbau GmbH Models DG-500 Elan Orion, DG-500 Elan Trainer, DG-500/ 20 Elan, DG-500/22 Elan, DG-500M, and DG-500MB gliders. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as damage to the bulkhead of the glider's center of gravity (CG) tow hook that, if not detected and corrected, may lead to failure of the fiberglass structure during a winch launch. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2012-7002, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2011-09-16

FR doc 2011-10006 · 76 FR 23169

AD 2011-09-16Published 2011-04-26Effective 2011-05-02

DG Flugzeugbau GmbH Glaser-Dirks Model DG-808C Gliders

Prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Glaser-Dirks Model DG-808C Gliders

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Source: Federal Register document 2011-10006, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2009-24-16

FR doc E9-28455 · 74 FR 62689

AD 2009-24-16Published 2009-12-01Effective 2009-12-21

DG Flugzeugbau GmbH Models DG-500MB, DG-808C and DG-800B Gliders

Prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Models DG-500MB, DG-808C and DG-800B Gliders

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Source: Federal Register document E9-28455, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2009-20-13

FR doc E9-23543 · 74 FR 50688

AD 2009-20-13Published 2009-10-01Effective 2009-10-21

Glaser-Dirks Flugzeugbau GmbH Model DG-100 Gliders

Prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG-100 Gliders

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Source: Federal Register document E9-23543, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2009-20-04

FR doc E9-23047 · 74 FR 49803

AD 2009-20-04Published 2009-09-29Effective 2009-10-19

Glaser-Dirks Flugzeugbau GmbH Model DG-100 Gliders

Prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG-100 Gliders

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Source: Federal Register document E9-23047, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2008-23-06

FR doc E8-26236 · 73 FR 65972

AD 2008-23-06Published 2008-11-06Effective 2008-11-26

DG Flugzeugbau GmbH Models DG-1000S and DG-1000T Gliders

Prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Models DG-1000S and DG-1000T Gliders

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Source: Federal Register document E8-26236, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2008-17-08

FR doc E8-18809 · 73 FR 48292

AD 2008-17-08Published 2008-08-19Effective 2008-09-23

DG Flugzeugbau GmbH Model DG-500MB Powered Sailplanes

Prompted by mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Model DG-500MB Powered Sailplanes

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Source: Federal Register document E8-18809, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2007-26-25

FR doc E7-25212 · 73 FR 400

AD 2007-26-25Published 2008-01-03Effective 2008-02-07

DG Flugzeugbau GmbH Model DG-500MB Gliders

Prompted by mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Model DG-500MB Gliders

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Source: Federal Register document E7-25212, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2007-21-01

FR doc E7-19682 · 72 FR 56891

AD 2007-21-01Published 2007-10-05Effective 2007-10-25

DG Flugzeugbau GmbH Model DG-500 Elan Series, DG-500M, and DG-500MB Gliders

Prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Model DG-500 Elan Series, DG-500M, and DG-500MB Gliders

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Source: Federal Register document E7-19682, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2007-19-18

FR doc E7-18474 · 72 FR 53923

AD 2007-19-18Published 2007-09-21Effective 2007-10-26

DG Flugzeugbau GmbH Model DG-1000T Gliders

Prompted by mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Model DG-1000T Gliders

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Source: Federal Register document E7-18474, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2007-17-08

FR doc 07-4090 · 72 FR 46551

AD 2007-17-08Published 2007-08-21Effective 2007-09-10

DG Flugzeugbau GmbH Model DG-500MB Gliders and Glaser-Dirks Flugzeugbau GmbH Model DG-800B Gliders

Prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Model DG-500MB Gliders and Glaser-Dirks Flugzeugbau GmbH Model DG-800B Gliders

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Source: Federal Register document 07-4090, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2006-16-20

FR doc E6-13135 · 71 FR 46393

AD 2006-16-20Published 2006-08-14Effective 2006-09-18

DG Flugzeugbau GmbH Model DG-1000S Sailplanes

Requires you to modify the elevator control at the stabilizer assembly, replace a placard on the fin, and incorporate changes in the FAA-approved sailplane flight manual (SFM).

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Model DG-1000S Sailplanes

We are adopting a new airworthiness directive (AD) for all DG Flugzeugbau GmbH Model DG-1000S sailplanes. This AD requires you to modify the elevator control at the stabilizer assembly, replace a placard on the fin, and incorporate changes in the FAA-approved sailplane flight manual (SFM). This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent the rigging of the horizontal stabilizer without properly connecting the elevator, which, if not prevented, could lead to an inoperative elevator. An inoperative elevator could lead to loss of control of the sailplane.

Source: Federal Register document E6-13135, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2006-02-12

FR doc 06-735 · 71 FR 5584

AD 2006-02-12Published 2006-02-02Effective 2006-03-15

Glaser-Dirks Flugzeugbau GmbH Models DG-100 and DG-400 Sailplanes and DG Flugzeugbau GmbH Models DG-500 Elan Series and DG-500M Sailplanes

Requires you to modify or replace the complete rudder mount assembly and ensure that the securing washer, castellated nut, and new split pins are installed.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Models DG-100 and DG-400 Sailplanes and DG Flugzeugbau GmbH Models DG-500 Elan Series and DG-500M Sailplanes

The FAA adopts a new airworthiness directive (AD) for all Glaser-Dirks Flugzeugbau GmbH Models DG-100 and DG-400 sailplanes and certain DG Flugzeugbau GmbH Models DG-500 Elan Series and DG-500M sailplanes. This AD requires you to modify or replace the complete rudder mount assembly and ensure that the securing washer, castellated nut, and new split pins are installed. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent the universal bearing of the lower rudder mounting from slipping out of the bearing support. The universal bearing slipping out could result in the rudder separating from its support. This failure could lead to loss of sailplane control during flight operations.

Source: Federal Register document 06-735, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2005-26-11

FR doc 05-24481 · 70 FR 76681

AD 2005-26-11Published 2005-12-28Effective 2006-02-07

DG Flugzeugbau GmbH Models DG-800B and DG-500MB Sailplanes

Requires you to modify the connection of the starter ring gear to the lower drive belt pulley adapter.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Models DG-800B and DG-500MB Sailplanes

The FAA adopts a new airworthiness directive (AD) for certain DG Flugzeugbau GmbH Models DG-800B and DG-500MB sailplanes. This AD requires you to modify the connection of the starter ring gear to the lower drive belt pulley adapter. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent the bolts currently used to connect the starter ring gear to the drive belt pulley adapter from shearing off and the bolt heads falling into the engine compartment. Failure of this connection could render the engine inoperative. Consequently, this failure could lead to loss of control of the sailplane.

Source: Federal Register document 05-24481, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2005-10-23

FR doc 05-9975 · 70 FR 29440

AD 2005-10-23Published 2005-05-23Effective 2005-06-30

DG Flugzeugbau GmbH Model DG-500MB Sailplanes and Glaser-Dirks Flugzeugbau GmbH Model DG-800B Sailplanes

Requires you to inspect the propeller for damage, specifically foam core separation, and replace any damaged propeller.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Model DG-500MB Sailplanes and Glaser-Dirks Flugzeugbau GmbH Model DG-800B Sailplanes

The FAA adopts a new airworthiness directive (AD) for all DG Flugzeugbau GmbH Model DG-500MB sailplanes equipped with a Solo engine and Glaser-Dirks Flugzeugbau GmbH Model DG-800B sailplanes equipped with a Solo engine. This AD requires you to inspect the propeller for damage, specifically foam core separation, and replace any damaged propeller. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to detect and correct damage to the propeller, which could result in failure of the propeller to perform properly. This failure could lead to reduced or loss of control of the sailplane.

Source: Federal Register document 05-9975, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2005-08-13

FR doc 05-7790 · 70 FR 20710

AD 2005-08-13Published 2005-04-21Effective 2005-06-06

Glaser-Dirks Flugzeugbau GmbH Model DG-800B Sailplanes

Requires you to modify the coolant pump and fuel pump electrical circuits, remove the non-resettable digital engine indicator (DEI) circuit breaker (4-ampere) and replace with a resettable 5-ampere circuit breaker, secure (for…

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG-800B Sailplanes

The FAA adopts a new airworthiness directive (AD) for all Glaser-Dirks Flugzeugbau GmbH (DG Flugzeugbau) Model DG-800B sailplanes equipped with a SOLO 2625 engine or a Mid-West AE 50T engine. This AD requires you to modify the coolant pump and fuel pump electrical circuits, remove the non-resettable digital engine indicator (DEI) circuit breaker (4-ampere) and replace with a resettable 5-ampere circuit breaker, secure (for sailplanes with a SOLO 2625 engine) the choke butterfly valve axis, install edge protection at the sharp edges of the resettable 5-ampere DEI circuit breaker, and incorporate changes in the FAA-approved sailplane flight manual. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent electrical failure of the fuel and coolant pumps if a non-resettable circuit breaker trips. This could result in power loss with the inability to restart the fuel pump during a critical phase of flight (for example, takeoff under own power).

Source: Federal Register document 05-7790, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2004-18-12

FR doc 04-20310 · 69 FR 55321

AD 2004-18-12Published 2004-09-14Effective 2004-10-22

DG Flugzeugbau GmbH, Model DG-500MB Sailplanes

Requires you to replace the engine pylon extension/retraction Warner LA10 spindle drive with an improved designed Stross BSA 10 spindle drive and to modify the electrical system following applicable service information.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH, Model DG-500MB Sailplanes

The FAA adopts a new airworthiness directive (AD) for certain DG Flugzeugbau GmbH Model DG-500MB sailplanes. This AD requires you to replace the engine pylon extension/retraction Warner LA10 spindle drive with an improved designed Stross BSA 10 spindle drive and to modify the electrical system following applicable service information. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent failure of the Warner LA10 spindle drive, which could result in failure of the engine pylon extension/retraction mechanism. This condition could cause an unstable engine pylon assembly during flight with loss of control of the sailplane.

Source: Federal Register document 04-20310, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2002-14-18

FR doc 02-17304 · 67 FR 46100

AD 2002-14-18Published 2002-07-12Effective 2002-08-23

Glaser-Dirks Flugzeugbau GmbH Models DG-400 and DG-800A Sailplanes

Requires you to inspect the rear plate of the propeller mount for marks and/or cracks and replace if necessary.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Models DG-400 and DG-800A Sailplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Glaser-Dirks Flugzeugbau GmbH (DG Flugzeugbau) Models DG-400 and DG-800A sailplanes. This AD requires you to inspect the rear plate of the propeller mount for marks and/or cracks and replace if necessary. This AD also requires you to inspect the mounting blocks for cracks and replace if necessary. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to detect and correct cracks in the propeller mount plate and mounting blocks, which could result in reduced structural integrity of the propeller mounting structure. This could lead to a hazardous flight condition or loss of control of the sailplane.

Source: Federal Register document 02-17304, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2001-07-01

FR doc 01-8067 · 66 FR 18047

AD 2001-07-01Published 2001-04-05Effective 2001-05-26

DG Flugzeugbau GmbH Model DG-800B Sailplanes

Requires you to install an additional filter for the primer valve; inspect and align the exhaust system; modify the placement of the fuel lines if the fuel filter is installed at the front mounting point of the spindle drive; and…

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Model DG-800B Sailplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain DG Flugzeugbau GmbH (DG Flugzeugbau) Model DG-800B sailplanes. This AD requires you to install an additional filter for the primer valve; inspect and align the exhaust system; modify the placement of the fuel lines if the fuel filter is installed at the front mounting point of the spindle drive; and secure the gas strut piston rod end using Loctite if the piston rod does rotate. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent failure of the fuel line, exhaust system, and piston rod of the gas strut, which could result in failure of the engine. Such failure could lead to loss of power during critical stages of flight.

Source: Federal Register document 01-8067, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2001-05-01

FR doc 01-5276 · 66 FR 14304

AD 2001-05-01Published 2001-03-12Effective 2001-04-27

DG Flugzeugbau GmbH Model DG-500MB Sailplanes

Requires you to install additional access holes in the propeller mount and modify the engine.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Model DG-500MB Sailplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain DG Flugzeugbau GmbH (DG Flugzeugbau) Model DG-500MB sailplanes equipped with a SOLO 2625 02 engine. This AD requires you to install additional access holes in the propeller mount and modify the engine. This AD also requires you to do a ground test run and replace the digital engine indicator circuit breaker. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the Federal Republic of Germany. The actions specified by this AD are intended to correct an inadequate circuit breaker and unsatisfactory drive belt tension that could cause damage to the engine crankshaft. Such damage could lead to engine failure and loss of control of the sailplane.

Source: Federal Register document 01-5276, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2000-23-32

FR doc 00-29920 · 65 FR 71235

AD 2000-23-32Published 2000-11-30Effective 2001-01-13

DG Flugzeugbau GmbH Models DG-500 Elan Series, DG-500M, and DG-500MB Sailplanes

Requires you to visually inspect the elevator control system for proper movement, obtain and incorporate a repair scheme if improper movement is found, and modify and install resin thickened cottonflock reinforcements to the…

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Models DG-500 Elan Series, DG-500M, and DG-500MB Sailplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain DG Flugzeugbau GmbH (DG Flugzeugbau) Models DG-500 Elan Series, DG-500M, and DG-500MB sailplanes. This AD requires you to visually inspect the elevator control system for proper movement, obtain and incorporate a repair scheme if improper movement is found, and modify and install resin thickened cottonflock reinforcements to the elevator control system as a way to increase the stiffness of the elevator control support stand. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the Federal Republic of Germany. The actions specified by this AD are intended to detect and correct improper movement in the elevator control system and to increase the stiffness of the elevator control support stand. Without accomplishing these actions, the pilot's capability to use full elevator control deflection could be limited, which could require increased force in moving the elevator control with a consequent potentially uncontrolled flight condition.

Source: Federal Register document 00-29920, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2000-20-10

FR doc 00-25550 · 65 FR 60848

AD 2000-20-10Published 2000-10-13Effective 2000-11-27

DG Flugzeugbau GmbH Model DG-800B Sailplanes

Requires you to measure and correct improper propeller drive belt tension.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Model DG-800B Sailplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain DG Flugzeugbau (DG Flugzeugbau) GmbH Model DG 800B sailplanes. This AD requires you to measure and correct improper propeller drive belt tension. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the Federal Republic of Germany. The actions specified in this AD are intended to correct improper drive belt tension and consequent engine crankshaft or connecting rod bearing damage. Such damage could result in loss of propulsion during critical phases of flight.

Source: Federal Register document 00-25550, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-19-17

FR doc 98-24641 · 63 FR 49653

AD 98-19-17Published 1998-09-17Effective 1998-10-30

Glaser-Dirks Flugzeugbau GmbH Model DG- 400 Gliders'

Requires inspecting the powerplant mount and the propeller mount for any loose parts.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG- 400 Gliders'

This amendment adopts a new airworthiness directive (AD) that applies to certain Glaser-Dirks Flugzeugbau GmbH (Glaser-Dirks) Model DG-400 gliders. This AD requires inspecting the powerplant mount and the propeller mount for any loose parts. This AD also requires modifying the starter motor, retrofitting the holder for the starter motor, and checking the engine ignition timing; either immediately or at a certain time depending on the results of the inspection. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent damage to the engine caused by vibration, which could result in loss of engine power during critical phases of flight.

Source: Federal Register document 98-24641, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-17-03

FR doc 98-21493 · 63 FR 43072

AD 98-17-03Published 1998-08-12Effective 1998-09-26

Glaser-Dirks Flugzeugbau GmbH Model DG- 400 Gliders

Requires replacing the propeller shaft, the bearings, and the front drive belt retaining rings with ones of improved design.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG- 400 Gliders

This amendment adopts a new airworthiness directive (AD) that applies to all Glaser-Dirks Flugzeugbau GmbH (Glaser-Dirks) Model DG- 400 gliders. This AD requires replacing the propeller shaft, the bearings, and the front drive belt retaining rings with ones of improved design. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent failure of the propeller shaft caused by an ineffective design, which could result in loss of glider propulsion during critical phases of flight.

Source: Federal Register document 98-21493, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-15-20

FR doc 98-19333 · 63 FR 39229

AD 98-15-20Published 1998-07-22Effective 1998-09-09

Glaser-Dirks Flugzeugbau GmbH Model DG- 500M Gliders

Requires inspecting the center of gravity (C.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG- 500M Gliders

This amendment adopts a new airworthiness directive (AD) that applies to all Glaser-Dirks Flugzeugbau GmbH (Glaser-Dirks) Model DG- 500M gliders. This AD requires inspecting the center of gravity (C.G.) tow release cable pulley for correct positioning, and replacing the C.G. tow release cable pulley with one made of aluminum either immediately or eventually depending on the results of the inspection. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent the C.G. tow release cable from coming off the pulley because of incorrect positioning, which could result in the pilot being unable to release from tow operations.

Source: Federal Register document 98-19333, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-13-06

FR doc 98-15893 · 63 FR 33537

AD 98-13-06Published 1998-06-19Effective 1998-08-02

Glaser-Dirks Flugzeugbau GmbH Model DG- 400 Gliders

Requires replacing the bungees that secure the left engine restraining cable and the bowden cable of the rear engine door.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG- 400 Gliders

This amendment adopts a new airworthiness directive (AD) that applies to certain Glaser-Dirks Flugzeugbau GmbH (Glaser-Dirks) Model DG-400 gliders. This AD requires replacing the bungees that secure the left engine restraining cable and the bowden cable of the rear engine door. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent the engine from locking in flight and not extending because of the left restraining cable or bowden cable of the rear door making contact with the engine, which could result in loss of glider power and potential loss of control.

Source: Federal Register document 98-15893, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-15894

FR doc 98-15894 · 63 FR 32720

AD not statedPublished 1998-06-16Effective 1998-08-02

Glaser-Dirks Flugzeugbau GmbH Models DG-100 and DG-400 Gliders

Requires repetitively inspecting the airbrakes to assure they retract at their outboard end first, and repairing the airbrakes if they do not retract at their outboard end first; and repetitively inspecting the airbrake torque…

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Models DG-100 and DG-400 Gliders

This amendment adopts a new airworthiness directive (AD) that applies to all Glaser-Dirks Flugzeugbau GmbH (Glaser-Dirks) Models DG- 100 and DG-400 gliders. This AD requires repetitively inspecting the airbrakes to assure they retract at their outboard end first, and repairing the airbrakes if they do not retract at their outboard end first; and repetitively inspecting the airbrake torque tube in the fuselage for cracks or deformations, and reinforcing or replacing, as necessary, if cracks or deformations are found in the airbrake torque tube. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent overloading of the airbrake control system caused by free play between the bellcrank and airbrake plate, which could result in failure of the operating lever of the airbrake torque tube in the fuselage.

Source: Federal Register document 98-15894, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-12-04

FR doc 98-14618 · 63 FR 30372

AD 98-12-04Published 1998-06-04Effective 1998-07-21

Glaser-Dirks Flugzeugbau GmbH Model DG- 500M Gliders

Requires installing a rudder gap seal and modifying the cooling liquid reservoir mount.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG- 500M Gliders

This amendment adopts a new airworthiness directive (AD) that applies to all Glaser-Dirks Flugzeugbau GmbH (Glaser-Dirks) Model DG- 500M gliders. This AD requires installing a rudder gap seal and modifying the cooling liquid reservoir mount. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent rudder vibrations caused by flow separation at the rudder gap, which could result in flutter with consequent loss of rudder control.

Source: Federal Register document 98-14618, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-11-17

FR doc 98-13818 · 63 FR 29099

AD 98-11-17Published 1998-05-28Effective 1998-07-10

Glaser-Dirks Flugzeugbau GmbH Model DG- 400 Gliders

Requires replacing the Bosch electrical system regulator, part number (P/N) 0212920001, with a type 4 E 26 regulator.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG- 400 Gliders

This amendment adopts a new airworthiness directive (AD) that applies to all Glaser-Dirks Flugzeugbau GmbH (Glaser-Dirks) Model DG- 400 gliders. This AD requires replacing the Bosch electrical system regulator, part number (P/N) 0212920001, with a type 4 E 26 regulator. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent failure of the electrical system regulator, which could result in smoke entering the cockpit with consequent passenger injury.

Source: Federal Register document 98-13818, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-11-18

FR doc 98-13823 · 63 FR 29100

AD 98-11-18Published 1998-05-28Effective 1998-07-10

Glaser-Dirks Flugzeugbau GmbH Model DG- 400 Gliders

Requires replacing the upper rubber shock mounts with mounts made of stainless steel.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG- 400 Gliders

This amendment adopts a new airworthiness directive (AD) that applies to all Glaser-Dirks Flugzeugbau GmbH (Glaser-Dirks) Model DG- 400 gliders. This AD requires replacing the upper rubber shock mounts with mounts made of stainless steel. This AD will also require inspecting the rear plate of the propeller mount for cracks and proper mounting, and replacing or modifying as necessary. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent failure of the propeller suspension system caused by cracks in the propeller mounts, which could result in loss of the propeller with consequent reduced glider controllability.

Source: Federal Register document 98-13823, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-04-30

FR doc 98-7887 · 63 FR 14603

AD 98-04-30Published 1998-03-26Effective 1998-05-15

Glaser-Dirks Flugzeugbau GmbH Model DG- 500M Gliders

Requires repetitively inspecting the propeller mounting plate for cracks, replacing any cracked propeller mounting plate, and modifying the bolt connections of the propeller mounting plate.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG- 500M Gliders

This action confirms the effective date of Airworthiness Directive (AD) 98-04-30, which applies to Glaser-Dirks Flugzeugbau GmbH Model DG-500M gliders. AD 98-04-30 requires repetitively inspecting the propeller mounting plate for cracks, replacing any cracked propeller mounting plate, and modifying the bolt connections of the propeller mounting plate. This AD was the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified in this AD are intended to prevent the propeller mounting plate from separating from the glider, which could result in propeller separation and possible loss of control of the glider.

Source: Federal Register document 98-7887, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-04-30

FR doc 98-3795 · 63 FR 9734

AD 98-04-30Published 1998-02-26Effective 1998-05-15

Glaser-Dirks Flugzeugbau GmbH Model DG- 500M Gliders

Requires repetitively inspecting the propeller mounting plate for cracks, replacing any cracked propeller mounting plate, and modifying the bolt connections of the propeller mounting plate.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG- 500M Gliders

This amendment adopts a new airworthiness directive (AD) that applies to all Glaser-Dirks Flugzeugbau GmbH (DG Flugzeugbau) Model DG- 500M gliders. This AD requires repetitively inspecting the propeller mounting plate for cracks, replacing any cracked propeller mounting plate, and modifying the bolt connections of the propeller mounting plate. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified in this AD are intended to prevent the propeller mounting plate from separating from the glider, which could result in propeller separation and possible loss of control of the glider.

Source: Federal Register document 98-3795, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

96-04-12

FR doc 96-3970 · 61 FR 6937

AD 96-04-12Published 1996-02-23Effective 1996-03-29

Glaser-Dirks Flugzeugbau GmbH DG-500M Sailplanes

Requires replacing the airbrake control hook-up shaft with a part of improved design.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH DG-500M Sailplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain Glaser-Dirks Flugzeugbau GmbH (Glaser-Dirks) DG-500M sailplanes. This action requires replacing the airbrake control hook-up shaft with a part of improved design. Reports of cracks in the welding of the lever to the torsion tube of the airbrake control prompted this action. The actions specified in this AD are intended to prevent an unintended extension of the airbrakes caused by failure of the lever to the torsion tube of the airbrake control, which could result in flutter, excessive rate of descent, and loss of control of the sailplane.

Source: Federal Register document 96-3970, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

95-14-01

FR doc 95-15928 · 60 FR 35324

AD 95-14-01Published 1995-07-07Effective 1995-08-24

Glaser-Dirks Flugzeugbau GmbH Model DG- 100 Sailplanes

Requires inspecting (one-time) the tailplane main fitting to ensure the part is accurately welded, and modifying the tailplane main fitting if not accurately welded.

Full official abstract

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG- 100 Sailplanes

This amendment adopts a new airworthiness directive (AD) that applies to Glaser-Dirks Flugzeugbau GmbH (Glaser-Dirks) Model DG-100 sailplanes equipped with the main L4 fitting of the all flying tailplane. This action requires inspecting (one-time) the tailplane main fitting to ensure the part is accurately welded, and modifying the tailplane main fitting if not accurately welded. A report of tailplane main fitting failure on one of the affected sailplanes, where the welding did not completely cover the entire wall thickness of the fitting, prompted this action. The actions specified by this AD are intended to prevent loss of control of the sailplane because of tailplane main fitting failure.

Source: Federal Register document 95-15928, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

Corrections whose original AD is not yet indexed

1 record
Correction

2007-26-15

FR doc E8-830 · 73 FR 4051

AD 2007-26-15Published 2008-01-24Effective 2008-02-07

DG Flugzeugbau GmbH Model DG-500MB Gliders

Requires that you modify the affected parts and exchange pages in the flight, maintenance, and repair manuals.

Full official abstract

Airworthiness Directives; DG Flugzeugbau GmbH Model DG-500MB Gliders

This document makes a correction to Airworthiness Directive (AD) 2007-26-15, which was published in the Federal Register on January 3, 2008 (73 FR 400), and applies to all DG Flugzeugbau GmbH Model DG- 500MB gliders. AD 2007-26-15 requires that you modify the affected parts and exchange pages in the flight, maintenance, and repair manuals. The FAA incorrectly referenced the AD number as "2007-26-25" instead of "2007-26-15." Current language in Sec. 39.13 [Amended] of AD 2007-26-15 references "AD 2007-26-25" instead of "2007-26-15." This document corrects that paragraph by replacing the reference of "2007-26-25" with "2007-26-15."

This document corrects or clarifies a previously issued AD of the same number — it is not a separate, additional requirement. Its "Effective" date above may predate its own "Published" date because it restates the original AD's effective date.

Source: Federal Register document E8-830, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

Service Bulletins

0 records

No Service Bulletins in our index yet for this airframe. We only list SBs we have individually sourced from the manufacturer — we never invent one.

This page indexes 54 ADs and 0 SBs from primary sources. The FAA may have issued additional directives for this airframe that are not yet included.

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