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Airworthiness Directive

AD 2001-05-03 66 FR 14308 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires you to apply Loctite on attaching bolt/ screw threads of inboard, central, and outboard carriages; increase tightening torques of associated hardware; and replace central carriage attaching bolts.

Superseded by AD 2002-09-11Federal Register (opens in a new tab)

FR document
01-5274
Amendment
39-12139
Published
2001-03-12
Effective
2001-04-27
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2001-05-03 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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AD

2001-05-03

FR doc 01-5274 · 66 FR 14308

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

Superseded by 2002-09-11

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 apply Loctite on attaching bolt/ screw threads of inboard, central, and outboard carriages; increase tightening torques of associated hardware; and replace central carriage attaching bolts.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain SOCATA--Groupe AEROSPATIALE (Socata) Model TBM 700 airplanes. This AD requires you to apply Loctite on attaching bolt/ screw threads of inboard, central, and outboard carriages; increase tightening torques of associated hardware; and replace central carriage attaching bolts. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by this AD are intended to prevent loose, or the loss of, flap attaching bolts/screws, which could cause rough or irregular control. Such rough or irregular control could lead to the loss of control of the airplane.

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All SOCATA/Daher TBM 700 directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2001-05-03 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index