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Airworthiness Directives
28 records · 1 superseded record nested above
AD
2023-05-03
FR doc 2023-05082 · 88 FR 15604
AD 2023-05-03Published 2023-03-14Effective 2023-04-18
Alexander Schleicher GmbH & Co. Segelflugzeugbau Gliders
Requires repetitively inspecting the wing root ribs for cracks, looseness, and damage and replacing any root rib with a crack, a loose rib or lift pin bushing, or any damage.
Full official abstract
Airworthiness Directives; Alexander Schleicher GmbH & Co. Segelflugzeugbau Gliders
The FAA is adopting a new airworthiness directive (AD) for all Alexander Schleicher GmbH & Co. Segelflugzeugbau Model ASW-15 gliders. 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 identifies the unsafe condition as wing root damage. This AD requires repetitively inspecting the wing root ribs for cracks, looseness, and damage and replacing any root rib with a crack, a loose rib or lift pin bushing, or any damage. The FAA is issuing this AD to address the unsafe condition on these products.
Source: Federal Register document 2022-15419, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
Airworthiness Directives; Alexander Schleicher GmbH & Co. Segelflugzeugbau Gliders
The FAA is superseding Airworthiness Directive (AD) 2022-14- 14, which applied to all Alexander Schleicher GmbH & Co. Segelflugzeugbau Model ASW-15 gliders. AD 2022-14-14 required repetitively inspecting the wing root ribs for cracks, looseness, and damage and replacing any root rib with a crack, a loose rib or lift pin bushing, or any damage. Since the FAA issued AD 2022-14-14, the European Union Aviation Safety Agency (EASA) superseded its mandatory continuing airworthiness information (MCAI) to add all Model ASW-15B gliders to the applicability. This AD is prompted by MCAI originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. This AD retains the requirements from AD 2022-14-14 of repetitively inspecting the wing root ribs for cracks, looseness, and damage and replacing any root rib with a crack, a loose rib or lift pin bushing or any damage; and revises the applicability by adding Model ASW-15B gliders and specifying that this AD applies to all Model ASW-15 and ASW-15B gliders equipped with wooden wing root ribs. The FAA is issuing this AD to address the unsafe condition on these products.
Source: Federal Register document 2023-05082, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2022-12-07Published 2022-06-16Effective 2022-07-21
Alexander Schleicher GmbH & Co. Segelflugzeugbau Gliders
Requires repetitively inspecting the glue joint at elevator rib number 1 and repairing any damage found.
Full official abstract
Airworthiness Directives; Alexander Schleicher GmbH & Co. Segelflugzeugbau Gliders
The FAA is superseding Airworthiness Directive (AD) 75-23-03 for all Alexander Schleicher GmbH & Co. Segelflugzeugbau (Alexander Schleicher) Model Ka2B, Ka 6, Ka 6 B, Ka 6 BR, Ka 6 C, Ka 6 CR, K 7, K 8, and AS-K 13 gliders. AD 75-23-03 required visually inspecting the glue joint between the elevator nose rib number 1 and the nose plywood skin and replacing the glue joint if insufficient glue adhesion was found. Since the FAA issued AD 75-23-03, the European Union Aviation Safety Agency (EASA) superseded prior EASA ADs for the unsafe condition on these products. This AD adds the Model K 8 B gliders to the applicability and requires repetitively inspecting the glue joint at elevator rib number 1 and repairing any damage found. The FAA is issuing this AD to address the unsafe condition on these products.
Source: Federal Register document 2022-12869, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2017-25-07Published 2017-12-14Effective 2018-01-18
Alexander Schleicher GmbH & Co. Segelflugzeugbau Gliders
Requires actions to address the unsafe condition on these products.
Full official abstract
Airworthiness Directives; Alexander Schleicher GmbH & Co. Segelflugzeugbau Gliders
We are adopting a new airworthiness directive (AD) for all Alexander Schleicher GmbH & Co. Segelflugzeugbau Models ASH 25M and ASH 26E 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 fatigue cracks found on the exhaust silencer. We are issuing this AD to require actions to address the unsafe condition on these products.
Source: Federal Register document 2017-26620, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2017-02-11Published 2017-02-10Effective 2017-03-17
Alexander Schleicher GmbH & Co. Gliders
Requires actions to address the unsafe condition on these products.
Full official abstract
Airworthiness Directives; Alexander Schleicher GmbH & Co. Gliders
We are adopting a new airworthiness directive (AD) for Alexander Schleicher GmbH & Co. Model ASK 21 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 cable slack in gliders equipped with a rudder hand control system leading to a short-term blockage of the rudder control system and reduced control. We are issuing this AD to require actions to address the unsafe condition on these products.
Source: Federal Register document 2017-01769, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2014-06-07Published 2014-04-03Effective 2014-05-08
Alexander Schleicher, Segelflugzeugbau Gliders
Requires actions to address the unsafe condition on these products.
Full official abstract
Airworthiness Directives; Alexander Schleicher, Segelflugzeugbau Gliders
We are adopting a new airworthiness directive (AD) for all Alexander Schleicher, Segelflugzeugbau Model ASK 21 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 inadequate guidance for spin training operations. We are issuing this AD to require actions to address the unsafe condition on these products.
Source: Federal Register document 2014-06627, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2013-16-05Published 2013-08-30Effective 2013-10-04
Alexander Schleicher GmbH & Co. Segelflugzeugbau Sailplanes
Requires actions to address the unsafe condition on these products.
Full official abstract
Airworthiness Directives; Alexander Schleicher GmbH & Co. Segelflugzeugbau Sailplanes
We are superseding an existing airworthiness directive (AD) for all Alexander Schleicher GmbH & Co. Segelflugzeugbau Models AS - K13, Ka2B, Ka 6, Ka 6 B, Ka 6 BR, Ka 6 C, Ka 6 CR, K7, K8, and K 8 B 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 misalignment of the automatic elevator control connection. We are issuing this AD to require actions to address the unsafe condition on these products.
Source: Federal Register document 2013-21075, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2004-11-12Published 2004-06-08Effective 2004-07-27
Alexander Schleicher Model ASW 27 Sailplanes
Requires you to install a warning placard requiring pilots weighing more than 105 kg (231.
Full official abstract
Airworthiness Directives; Alexander Schleicher Model ASW 27 Sailplanes
The FAA adopts a new airworthiness directive (AD) for all Alexander Schleicher Model ASW 27 sailplanes equipped with integrated (wet inner surface) water ballast tanks in the wings, which could put the center of gravity (CG) of the sailplane out of the acceptable range. This AD requires you to install a warning placard requiring pilots weighing more than 105 kg (231.5 lbs) to use the rearmost backrest hinge position; and requires you to determine the forward empty CG and make any necessary adjustments. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to correct the CG to the acceptable range when integrated ballast water tanks are installed. Failure of the sailplane to be within the acceptable CG range could result in loss of sailplane control.
Source: Federal Register document 04-12574, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2004-10-08Published 2004-05-21Effective 2004-07-06
Alexander Schleicher GmbH & Co. Segelflugzeugbau Model ASH 25M Sailplanes
Requires you to inspect the fuel line for correct fittings, and, if any incorrect fitting is found, replace the fuel line.
Full official abstract
Airworthiness Directives; Alexander Schleicher GmbH & Co. Segelflugzeugbau Model ASH 25M Sailplanes
The FAA adopts a new airworthiness directive (AD) for all Alexander Schleicher GmbH & Co. Segelflugzeugbau (Alexander Schleicher) Model ASH 25M sailplanes equipped with fuel injected engine IAE50R-AA. This AD requires you to inspect the fuel line for correct fittings, and, if any incorrect fitting is found, replace the fuel line. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to detect and correct any fuel lines with improper fittings, which could result in fuel leakage and a possible fire hazard.
Source: Federal Register document 04-11370, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD not statedPublished 2000-03-08Effective 2000-04-25
Alexander Schleicher GmbH & Co. Model ASW-27 Sailplanes
Requires inspecting the elevator control circuit clearance inside the fuselage tail boom to the fin intersection to assure a clearance of at least 2.
Full official abstract
Airworthiness Directives; Alexander Schleicher GmbH & Co. Model ASW-27 Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to certain Alexander Schleicher GmbH & Co. (Alexander Schleicher) Model ASW-27 sailplanes. This AD requires inspecting the elevator control circuit clearance inside the fuselage tail boom to the fin intersection to assure a clearance of at least 2.5 millimeters (mm) (\1/10\-inch wide), and adjusting any clearance that does not meet the criteria. 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 interference in the elevator control circuit, which, if not corrected, could result in the elevator control jamming with possible loss of control of the sailplane.
Source: Federal Register document 00-5134, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2000-04-16Published 2000-03-01Effective 2000-03-20
Alexander Schleicher Segelflugzeugbau Models ASH 25M and ASH 26E Sailplanes
Requires that you accomplish the following: <bullet> Check to see if the sailplane has a muffler marked with an X on the front plate; <bullet> Accomplish pre-flight checks on the carbon reinforced plastic fairing for signs of…
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Models ASH 25M and ASH 26E Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to all Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Models ASH 25M and ASH 26E sailplanes. This AD requires that you accomplish the following: <bullet> Check to see if the sailplane has a muffler marked with an X on the front plate; <bullet> Accomplish pre-flight checks on the carbon reinforced plastic fairing for signs of overheat traces and/or perform boroscope inspections, depending on the number of sailplane hours accumulated; and <bullet> Replace the muffler with an improved design muffler either at a certain time period or immediately if discrepancies are found during any 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 excessive radiation from causing the carbon fiber shroud on the engine muffler to delaminate. The carbon fiber shroud serves the same function as a firewall and delamination could cause a fire to spread throughout the sailplane.
Source: Federal Register document 00-4434, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 99-15-13Published 1999-07-26Effective 1999-09-13
Alexander Schleicher Segelflugzeugbau Model ASH 26E Sailplanes
Requires replacing the internal cooling air fan with a fan that incorporates a white impeller on all Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model ASH 26E sailplanes.
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Model ASH 26E Sailplanes
This amendment supersedes Airworthiness Directive (AD) 98-09- 09, which currently requires replacing the internal cooling air fan with a fan that incorporates a white impeller on all Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model ASH 26E sailplanes. This AD requires inspecting the internal cooling air fan for damage, and replacing any fan that does not incorporate a black impeller with a fan that incorporates a black impeller either immediately or at a certain time period, 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 failure of the internal cooling system air fan caused by a certain design configuration of the impeller, which could cause the engine to overheat with possible engine failure.
Source: Federal Register document 99-18625, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 95-11-15 R1Published 1999-06-21Effective 1999-07-25
Alexander Schleicher Segelflugzeugbau Model ASK 21 Gliders
Requires replacing the parallel rocker with a part of improved design and incorporating flight manual revisions, but only for those gliders with the automatic elevator connection incorporated.
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Model ASK 21 Gliders
This action confirms the effective date of Airworthiness Directive (AD) 95-11-15 R1, which applies to Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model ASK 21 gliders. AD 95-11- 15 R1 requires replacing the parallel rocker with a part of improved design and incorporating flight manual revisions, but only for those gliders with the automatic elevator connection incorporated. AD 95-11- 15 was the result of two incidents of the parallel rocker breaking at the elevator connection on the affected gliders. Since that time, the FAA has determined that the AD should only affect those Model ASK 21 gliders equipped with the automatic elevator connection. The actions specified in this AD are intended to continue to prevent possible loss of elevator control that could result from a broken parallel rocker.
Source: Federal Register document 99-15619, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 99-09-09Published 1999-04-28Effective 1999-06-07
Alexander Schleicher Segelflugzeugbau Model ASH 26E Sailplanes
Requires inspecting the red silicone tube of the rotor interior air cooling system (just in front of the carburetor ) for oil leaks and the heat damping layer of the lower exhaust damper fairing for oil contamination, and…
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Model ASH 26E Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to all Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model ASH 26E sailplanes. This AD requires inspecting the red silicone tube of the rotor interior air cooling system (just in front of the carburetor ) for oil leaks and the heat damping layer of the lower exhaust damper fairing for oil contamination, and replacing the applicable parts where oil leakage or contamination is found. 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 any oil- contaminated exhaust damper fairing caused by oil leakage in the red silicone tube of the rotor interior air cooling system, which could result in an exhaust fire and/or an explosion.
Source: Federal Register document 99-10169, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 95-11-15 R1Published 1999-04-26Effective 1999-07-25
Alexander Schleicher Segelflugzeugbau Model ASK 21 Gliders
Requires replacing the parallel rocker with a part of improved design and incorporating flight manual revisions on all Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model ASK 21 gliders.
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Model ASK 21 Gliders
This amendment revises Airworthiness Directive (AD) 95-11-15, which currently requires replacing the parallel rocker with a part of improved design and incorporating flight manual revisions on all Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model ASK 21 gliders. AD 95-11-15 was the result of two incidents of the parallel rocker breaking at the elevator connection on the affected gliders. Since that time, the FAA has determined that the AD should only affect those Model ASK 21 gliders equipped with the automatic elevator connection. This AD retains the actions of AD 95-11-15, but only for those gliders with the automatic elevator connection incorporated. The actions specified in this AD are intended to continue to prevent possible loss of elevator control that could result from a broken parallel rocker.
Source: Federal Register document 99-10313, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 98-18-05Published 1998-08-27Effective 1998-10-12
Alexander Schleicher Segelflugzeugbau Models K 8 and K 8 B Sailplanes
Requires inspecting the canopy hood lock assembly to assure that the height of the cam is at least 2 millimeters (mm), and modifying or replacing any canopy hood lock assembly where the cam is less than 2 mm in height.
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Models K 8 and K 8 B Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to all Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Models K 8 and K 8 B sailplanes. This AD requires inspecting the canopy hood lock assembly to assure that the height of the cam is at least 2 millimeters (mm), and modifying or replacing any canopy hood lock assembly where the cam is less than 2 mm in height. 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 canopy from coming open in flight because the height of the locking cam is less than 2 mm, which could result in loss of the canopy with consequent pilot injury.
Source: Federal Register document 98-22823, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 98-17-02Published 1998-08-12Effective 1998-09-26
Alexander Schleicher Segelflugzeugbau Model ASW-19 Sailplanes
Requires inspecting the tow release cable guide fittings for the correct mounting, and, if the fittings are mounted in the front of the bulkhead, moving the fitting to the rear of the bulkhead and adjusting the neutral travel of the cable.
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Model ASW-19 Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to certain Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model ASW-19 sailplanes. This AD requires inspecting the tow release cable guide fittings for the correct mounting, and, if the fittings are mounted in the front of the bulkhead, moving the fitting to the rear of the bulkhead and adjusting the neutral travel of the cable. 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 premature release of the tow cable during take-off, which could result in loss of the sailplane.
Source: Federal Register document 98-21492, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 98-13-05Published 1998-06-16Effective 1998-08-01
Alexander Schleicher Segelflugzeugbau Model AS-K13 Sailplanes
Requires inspecting the main spar fitting for excessive tolerance, traces, movement, etc.
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Model AS-K13 Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to certain Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model AS-K13 sailplanes. This AD requires inspecting the main spar fitting for excessive tolerance, traces, movement, etc., and repairing the main spar fitting if any of the above conditions exist. 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 main spar caused by excessive movement of the main spar fitting, which could result in loss of control of the sailplane.
Source: Federal Register document 98-15889, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 98-12-03Published 1998-06-04Effective 1998-07-14
Alexander Schleicher Segelflugzeugbau Models ASW-19 and ASK 21 Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to certain Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Models ASW-19 and ASK 21 sailplanes.
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Models ASW-19 and ASK 21 Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to certain Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Models ASW-19 and ASK 21 sailplanes. This AD requires: modifying the rudder surface panels; replacing the airbrake bellcrank; and modifying the rear canopy hinge structure. 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 loss of the canopy caused by design deficiency, airbrake failure caused by cracking, and rudder panel flutter caused by high density altitude conditions, all of which could result in reduced sailplane controllability.
Source: Federal Register document 98-14617, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 98-10-07Published 1998-05-13Effective 1998-06-26
Alexander Schleicher Segelflugzeugbau Model ASK 21 Sailplanes
Requires changing the sailplane flight manual's weight and balance information.
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Model ASK 21 Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to all Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model ASK 21 sailplanes that have certain modifications installed. This AD requires changing the sailplane flight manual's weight and balance information. 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 operator from using inaccurate weight and balance information provided in the sailplane flight manual (SFM), which could lead to hazardous flight conditions.
Source: Federal Register document 98-12380, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 98-09-13Published 1998-04-28Effective 1998-06-14
Alexander Schleicher Segelflugzeugbau Model ASK 21 Sailplanes
Requires inspecting the S- shaped rudder pedal tube for displacement, and correcting any displacement of the plastic tube.
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Model ASK 21 Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to certain Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model ASK 21 sailplanes. This AD requires inspecting the S- shaped rudder pedal tube for displacement, and correcting any displacement of the plastic 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 rudder control jamming, which could result in loss of directional control of the sailplane.
Source: Federal Register document 98-11006, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 98-09-09Published 1998-04-24Effective 1998-06-01
Alexander Schleicher GmbH Segelflugzeugbau Model ASH-26E Sailplanes
Requires replacing the internal cooling air fan with a fan that incorporates a certain modification.
Full official abstract
Airworthiness Directives; Alexander Schleicher GmbH Segelflugzeugbau Model ASH-26E Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to certain Alexander Schleicher GmbH Segelflugzeugbau (Alexander Schleicher) Model ASH-26E sailplanes. This AD requires replacing the internal cooling air fan with a fan that incorporates a certain modification. 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 internal cooling system air fan caused by the impeller slipping, which could result in loss of compression and power and possible engine failure.
Source: Federal Register document 98-10593, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 98-08-29Published 1998-04-20Effective 1998-05-18
Alexander Schleicher Segelflugzeugbau Model ASK 21 Sailplanes
Requires removing certain pages from the sailplane flight manual and replacing these pages with new pages having different information regarding spin and stall recovery.
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Model ASK 21 Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to certain Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model ASK 21 sailplanes. This AD requires removing certain pages from the sailplane flight manual and replacing these pages with new pages having different information regarding spin and stall recovery. This action 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 operators from using inaccurate stall and spin recovery information provided in the sailplane flight manual (SFM), which could result in the inability to recover from a spin or stall during flight.
Source: Federal Register document 98-10179, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 98-06-38Published 1998-03-20Effective 1998-04-28
Alexander Schleicher Segelflugzeugbau Model ASK-21 Sailplanes
Requires drilling a drainage hole in the elevator pushrod, inspecting the elevator pushrod for corrosion damage, and replacing any elevator pushrod if a certain amount of corrosion damage is found.
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Model ASK-21 Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model ASK-21 sailplanes that do not have a certain automatic elevator connection installed. This AD requires drilling a drainage hole in the elevator pushrod, inspecting the elevator pushrod for corrosion damage, and replacing any elevator pushrod if a certain amount of corrosion damage is found. 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 elevator pushrod caused by corrosion damage, which could result in loss of control of the sailplane.
Source: Federal Register document 98-7232, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 98-06-37Published 1998-03-20Effective 1998-04-28
Alexander Schleicher Segelflugzeugbau Model ASK-21 Sailplanes
Requires replacing any tow release cable assembly that does not have a swivel-type end with a cable assembly that does have a swivel-type end.
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Model ASK-21 Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to certain Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model ASK-21 sailplanes. This AD requires replacing any tow release cable assembly that does not have a swivel-type end with a cable assembly that does have a swivel-type end. 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 inability to release the tow rope because of the design of the cable assembly, which could result in loss of control of the sailplane during towing operations.
Source: Federal Register document 98-7249, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 98-04-46Published 1998-02-27Effective 1998-04-03
Alexander Schleicher Segelflugzeugbau Model ASW-19 Sailplanes
Requires modifying the inspection hole cover in the fuselage area.
Full official abstract
Airworthiness Directives; Alexander Schleicher Segelflugzeugbau Model ASW-19 Sailplanes
This amendment adopts a new airworthiness directive (AD) that applies to certain Alexander Schleicher Segelflugzeugbau (Alexander Schleicher) Model ASW-19 sailplanes. This AD requires modifying the inspection hole cover in the fuselage area. 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 loss of aileron control caused by an inspection hole cover entering the fuselage, which could result in loss of control of the sailplane.
Source: Federal Register document 98-4244, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 95-11-15Published 1995-06-07Effective 1995-07-14
Alexander Schleicher GmbH & Co. Model ASK 21 Gliders
Requires replacing the parallel rocker with a part of improved design, and incorporating flight manual revisions.
Full official abstract
Airworthiness Directives; Alexander Schleicher GmbH & Co. Model ASK 21 Gliders
This amendment adopts a new airworthiness directive (AD) that applies to Alexander Schleicher GmbH & Co. (Alexander Schleicher) Model ASK 21 gliders. The required action requires replacing the parallel rocker with a part of improved design, and incorporating flight manual revisions. Two incidents of the parallel rocker breaking at the elevator connection on the affected gliders prompted this action. The actions specified by this AD are intended to prevent possible loss of elevator control that could result from a broken parallel rocker.
Source: Federal Register document 95-12948, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 95-09-12Published 1995-05-08Effective 1995-06-09
Alexander Schleicher Models ASW-12, ASW-15, ASW-15B, and ASW-17 Gliders
Requires repetitively inspecting the wing spar of Alexander Schleicher Models ASW-15 and ASW-15B gliders for wood rot, and replacing any wing spar where wood rot is found.
Full official abstract
Airworthiness Directives; Alexander Schleicher Models ASW-12, ASW-15, ASW-15B, and ASW-17 Gliders
This amendment supersedes Airworthiness Directive (AD) 88-11- 05, which currently requires repetitively inspecting the wing spar of Alexander Schleicher Models ASW-15 and ASW-15B gliders for wood rot, and replacing any wing spar where wood rot is found. Alexander Schleicher Models ASW-12 and ASW-17 gliders are of a similar type design to Models ASW-15 and ASW-15B gliders, and the Federal Aviation Administration (FAA), in working with the Civil Aviation Authority of Germany, has decided that the actions referenced in AD 88-11-05 should also apply to Models ASW-12 and ASW-17 gliders. The actions specified by this AD are intended to prevent failure of the wing spar caused [[Page 22500]] by wood rot, which, if not detected and corrected, could result in loss of control of the airplane.
Source: Federal Register document 95-10831, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17