Airworthiness Directive

AD 2001-05-01 66 FR 14304 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-5276
Amendment
39-12137
Published
2001-03-12
Effective
2001-04-27
Models covered
1
Last live check
2026-10-01
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AD

2001-05-01

FR doc 01-5276 · 66 FR 14304

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

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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

Full official abstract

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.

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Applies to 1 model in our index