Airworthiness Directive

AD 2002-05-04 67 FR 10831 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-5526
Amendment
39-12672
Published
2002-03-11
Effective
2002-04-22
Models covered
1
Last live check
2026-10-02
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AD

2002-05-04

FR doc 02-5526 · 67 FR 10831

AD 2002-05-04Published 2002-03-11Effective 2002-04-22

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 repetitively inspect the engine mount assembly for cracks, repair any cracks found, and modify the brackets on airplanes with right angle engine mounts.

Full official abstract

This amendment supersedes Airworthiness Directive (AD) 77-15- 06, which applies to all SOCATA--Groupe AEROSPATIALE (Socata) Models MS 892A-150, MS 892E-150, MS 893A, MS 893E, Rallye 150T, and Rallye 150ST airplanes. AD 77-15-06 currently requires you to repetitively inspect the engine mount assembly for cracks, repair any cracks found, and modify the brackets on airplanes with right angle engine mounts. This AD is the result of the French airworthiness authority's determination that updated service information and additional aircraft should be added to the applicability of AD 77-15-06. This AD retains the inspection and repair requirements of the current AD and adds the information communicated by the French airworthiness authority. The actions specified by this AD are intended to detect and correct cracks in the engine mount assembly. Such a condition could cause the engine mount assembly to fail, which could result in loss of control of the airplane.

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All SOCATA Rallye / MS 880 directives

Applies to 1 model in our index