AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2002-19-01 67 FR 59137 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-23513
Amendment
39-12881
Published
2002-09-20
Effective
2002-10-29
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/2002-19-01 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

2002-19-01

FR doc 02-23513 · 67 FR 59137

AD 2002-19-01Published 2002-09-20Effective 2002-10-29

Superseded by 2017-15-15

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 perform a test on the flight control system and adjust the control roll stop if jamming occurs during the test.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all SOCATA--Groupe AEROSPATIALE (Socata) Model TBM 700 airplanes. This AD requires you to perform a test on the flight control system and adjust the control roll stop if jamming occurs during the test. 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 the flight control wheels from traveling beyond normal roll control limits, which could result in the control wheel becoming jammed. Such a condition could lead to reduced or loss of control of the airplane.

More directives for SOCATA/Daher TBM 700

  1. AD 2025-26-02 Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously H... 2026-01-08
  2. AD 2025-02-08 Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously H... 2025-02-12
  3. AD 2025-01-04 Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously H... 2025-02-04
  4. AD 2023-11-12 Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously H... 2023-06-16
  5. AD 2021-25-10 Airworthiness Directives; Daher Aerospace (Type Certificate Previously H... 2021-12-20

All SOCATA/Daher TBM 700 directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2002-19-01 (opens in a new tab)

Applies to 1 model in our index