Airworthiness Directive

AD 2005-20-24 70 FR 59240 Active

Federal Aviation Administration · 14 CFR part 39

FR document
05-19930
Amendment
39-14320
Published
2005-10-12
Effective
2005-11-09
Models covered
1
Last live check
2026-10-01
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AD

2005-20-24

FR doc 05-19930 · 70 FR 59240

AD 2005-20-24Published 2005-10-12Effective 2005-11-09

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 inspect the fuselage skin in the VHF1 antenna mounting area for cracks and loose rivets.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for certain SOCATA--Groupe AEROSPATIALE (SOCATA) Model TBM 700 airplanes. This AD requires you to inspect the fuselage skin in the VHF1 antenna mounting area for cracks and loose rivets. This AD also requires you to modify the area if you find cracks or loose rivets. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. We are issuing this AD to detect and correct cracks in the fuselage skin, which could result in loss of aircraft pressurization. Loss of aircraft pressurization could lead to flight crew incapacitation.

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All SOCATA/Daher TBM 700 directives

Applies to 1 model in our index