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2026-07-03

final rule

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

Unsafe Condition: Engine mount cracking near the propeller head on DG-1000M powered gliders has been reported, which could result in loss of power transmission to the propeller and reduced or loss of control of the ...

Effective: Apr 20, 2026 Category: engine Compliance: Before further flight, or within 30 days of the effective date.

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

2025-13-08

final rule

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

Unsafe Condition: Reports of propeller separation from DG Aviation GmbH Model DG-1000T gliders, where the rubber of the damper element sheared off completely, which could lead to separation of the propeller, resulti...

Effective: Jul 25, 2025 Category: propeller Compliance: Within 3 days after the effective date of this AD

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

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2024-19-12

final rule

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

Unsafe Condition: Broken rod end at the upper end of the elevator pushrod in the fin, caused by excessive tightening of the elevator play adjustment screw, leading to jamming of the roller inside the funnel and subs...

Effective: Oct 15, 2024 Category: aircraft Compliance: Within 12 months of the effective date (October 15, 2024).

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

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2023-03-22 Recurring

final rule

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

Unsafe Condition: Occurrences of rupture of the eccentric axle on Solo Model 2350 C and 2350 D engines, which are installed on DG Flugzeugbau GmbH Model DG-1000T gliders and Schempp-Hirth Model Duo Discus T gliders ...

Effective: Apr 5, 2023 Category: engine Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH and Schempp-Hirth Flugzeugbau GmbH Gliders

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

2022-04-01

final rule

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

Unsafe Condition: failure of the bearing of the upper pulley of the belt driven reduction gear resulting in separation of the propeller from the engine

Effective: Mar 29, 2022 Category: engine Compliance: Within 12 months after the effective date of this AD

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH and Schempp-Hirth Flugzeugbau GmbH Gliders

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2021-24-19

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: an error in the engine control unit (ECU) software that can cause brief injection of fuel into one cylinder when the ECU is activated

Effective: Jan 27, 2022 Category: engine Compliance: Within 3 months after the effective date of this AD

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

2021-18-14

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: damaged polyurethane (PU) fuel hoses due to environmental and fatigue deterioration

Effective: Nov 4, 2021 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

2020-13-09

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: Occurrences have been reported where the rear locking rod of the rear canopy rotated out of the threads of the operating mechanism. This condition, if not detected and corrected, could lead to bloc...

Effective: Aug 26, 2020 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

2018-10-09

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: failure of the connecting rod bearing resulting from too much load on the rod bearings from the engine control unit

Effective: Jun 26, 2018 Category: engine Compliance: Within 2 work-hours

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

2018-07-22

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: The potential of an in-flight shut-down and engine fire resulting in loss of control due to failure of the connecting stud for the two fuel injector mounts of the engine redundancy system on glider...

Effective: May 25, 2018 Category: engine Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2017-13-06

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: Manufacturing defect in certain textile fabric covered fuel hoses, which could cause the fuel hose to fail.

Effective: Jul 31, 2017 Category: aircraft Compliance: Within 30 days after July 31, 2017

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

2017-11-03

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: Failure of the connecting rod bearing resulting from too much load on the rod bearings from the engine control unit.

Effective: Jun 29, 2017 Category: engine Compliance: Within 60 days after June 29, 2017

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

2017-08-09

final rule

Airworthiness Directives; DG Flugzeugbau GmbH

Unsafe Condition: Failure of the connecting stud for the two fuel injector mounts of the engine redundancy system.

Effective: May 26, 2017 Category: engine Compliance: Within 60 days after May 26, 2017

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH

Amdt-39-18492

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: Engine shaft failure and consequent propeller detachment.

Effective: Jun 6, 2016 Category: engine Compliance: Before further flight.

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

2015-09-04

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: Engine shaft failure with consequent propeller detachment.

Effective: May 26, 2015 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Amdt-39-17968

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: Engine shaft failure and consequent propeller detachment.

Effective: Oct 20, 2014 Category: engine Compliance: Within 12 months of the effective date (October 20, 2014).

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

2013-22-14

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: Engine shaft failure and consequent propeller detachment.

Effective: Nov 25, 2013 Category: engine Compliance: Within 0 flight hours (immediate compliance required as of the effective date).

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

2013-22-12

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: Defective starter motor control unit, which could activate the starter motor without pressing the starter button.

Effective: Nov 18, 2013 Category: aircraft Compliance: Within 10 days after November 18, 2013

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

2013-03-09

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: Material defect within the propeller shaft, most likely caused by a manufacturing error.

Effective: Mar 19, 2013 Category: propeller Compliance: Within 25 hours time-in-service (TIS) after March 19, 2013, or 6 months after March 19, 2013, whi...

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2012-06-15

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Sailplanes

Unsafe Condition: 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.

Effective: May 15, 2012 Category: aircraft Compliance: Within 30 days and 3 months after May 15, 2012

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Sailplanes

2012-06-13

final rule

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Unsafe Condition: 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.

Effective: May 4, 2012 Category: aircraft Compliance: Within 30 days after May 4, 2012, inspect the bulkhead of the CG tow hook and the bulkhead's glue...

Why matched: Airworthiness Directives; DG Flugzeugbau GmbH Gliders

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

2011-09-16

final rule

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

Unsafe Condition: The bolt at the landing gear control bellcrank was found mounted in the wrong direction, which could interfere and damage the air brake control pushrod and the wing flap control pushrod if the land...

Effective: May 2, 2011 Category: aircraft Compliance: Before further flight

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

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

2009-24-16

final rule

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

Unsafe Condition: Zinc-coated starter ring gears installed on Solo 2625 01 and 2625 02 engines have shown to be prone to cracking. Painted starter ring gears with lightening holes are also subject to cracks.

Effective: Dec 21, 2009 Category: aircraft Compliance: Before further flight

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

2008-23-06

final rule

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

Unsafe Condition: The bolt of a bearing stand which is the pivot for a bell crank failed in a DG-500 ELAN Trainer, suspected due to a loose nut fixing the bell crank. Additionally, during aerobatics, a suspension of...

Effective: Nov 26, 2008 Category: aircraft Compliance: Before further flight

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

2008-17-08

final rule

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

Unsafe Condition: Some bolts of the extension retraction mechanism fractured due to fatigue stress from increasing push-pull loads acting on incorrectly tightened screws, leading to uncommanded retraction of the pow...

Effective: Sep 23, 2008 Category: aircraft Compliance: Within 30 days after September 23, 2008

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