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2003-26-06: Safety Belts and Restraint Systems

FAA order 2003-26-06 is an airworthiness directive in force since February 17, 2004. The FAA's subject line: Safety Belts and Restraint Systems. It names Airbus Helicopters AS332, Airbus Helicopters AS350 AStar (Écureuil), now H125, Daher (Socata) TB 10, Daher (Socata) TB-20, Daher (Socata) TB 9, Daher (Socata) TB200, Daher (Socata) TB21, Daher (Socata) TBM-700 TBM 700 through TBM 960, S.O.C.A.T.A. RALLYE 150, S.O.C.A.T.A. RALLYE 235: about 2,286 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: cabin, seats and restraints.

What it applies to as the FAA lists it

Kind of product
Appliance
Makes
Anjou Aeronautique; Airbus Helicopters; SOCATA; SOCATA
Models
Safety Belts and Restraint Systems, AS332C, AS332L, AS332L1, AS332L2, Rallye 100S, Rallye 150 ST, Rallye 150 T, Rallye 235 E, Rallye 235C, TB 10, TB 20, TB 200, TB 21, TB9, TBM 700, AS350B2
On this site
Airbus Helicopters AS332 8 registered
Airbus Helicopters AS350 AStar (Écureuil), now H125 891 registered
Daher (Socata) TB 10 53 registered
Daher (Socata) TB-20 200 registered
Daher (Socata) TB 9 34 registered
Daher (Socata) TB200 11 registered
Daher (Socata) TB21 57 registered
Daher (Socata) TBM-700 TBM 700 through TBM 960 1,006 registered
S.O.C.A.T.A. RALLYE 150 10 registered
S.O.C.A.T.A. RALLYE 235 16 registered

Dates and paperwork

In force since
February 17, 2004
Published
December 31, 2003 (signed December 17, 2003)
Docket
2003-CE-31-AD
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA adopts a new airworthiness directive (AD) for certain Anjou Aeronautique (ANJOU) (formerly TRW Repa S.A., formerly L'AIGLON) safety belts and restraint systems that are installed in aircraft. This AD requires you to inspect safety belts and restraint systems for defects and service life limits, and, if necessary, repair safety belts and restraint systems that have not reached service life limits; and replace safety belts and restraint systems that have reached service life limits. This AD is the result of reports of inadvertent unbuckling of the ANJOU seat belts and two safety recommendations to take AD action. We are issuing this AD to detect and correct defective safety belts and restraint systems, which could result in failure of the safety belts and restraint systems. This failure could lead to lack of occupant restraint during normal or crash loads.

The order itself the regulatory text, as published

Show the full text (5,815 characters)
2003-26-06 Anjou Aeronautique (Formerly TRW REPA S.A., Formerly L'Aiglon): Amendment 39-13403; Docket No. 2003-CE-31-AD. When Does This AD Become Effective? (a) This AD becomes effective on February 17, 2004. What Other ADs Are Affected by This Action? (b) None. What Airplanes Are Affected by This AD? (c) This AD affects Anjou Aeronautique safety belts and restraint systems specified in paragraph (c)(1) that are installed on, but not limited to, the aircraft specified in paragraph (c)(2) that are certificated in any category: (1) Anjou Aeronautique safety belts and restraint systems: Part Numbers/Types 343, 343-1, 343AM, 343B, 343BM, 343C, 343CM, 343D, and 343M. (2) Affected aircraft: The following is a list of aircraft that may incorporate the affected Anjou Aeronautique safety belts and restraint systems: (i) EUROCOPTER FRANCE Models AS332C, AS332L, AS332L1, AS332L2, and AS350B2 helicopters; and (ii) SOCATA--Groupe AEROSPATIALE TB 9, TB 10, TB 20, TB 21, TB 200, TMB 700, Rallye 100S, Rallye 150T, Rallye 150ST, Rallye 235E, and Rallye 235C airplanes. What Is the Unsafe Condition Presented in This AD? (d) This AD is the result of reports of inadvertent unbuckling of the ANJOU seat belts and two safety recommendations to take AD action. The actions specified in this AD are intended to detect and correct defective safety belts and restraint systems, which could result in failure of the safety belts and restraint systems. This failure could lead to lack of occupant restraint during normal or crash loads. What Must I Do To Address This Problem? (e) To address this problem, you must accomplish the following: Actions Compliance Procedures (1) Inspect the installed Anjou Aeronautique/TRW Repa S.A./L'Aiglon safety belts and restraint systems (types 343, 343-1, 343AM, 343B, 343BM, 343C, 343CM, 343D, or 343M) for: (i) defective buckle latch; and (ii) exceeded service life. Within the next 50hours time-in-service (TIS) after February 17, 2004 (the effective date of this AD) or 4 calendar months after February 17, 2004 (the effective date of this AD), whichever occurs first, unless already accomplished. Repetitively inspect thereafter at every 12 calendar months until the affected safety belt and restraint system is replaced as specified by paragraph (e)(3) of this AD. For types 343, 343AM, 343B, 343BM, 343C, 343CM, 343D, or 343M: Follow Anjou Aeronautique Service Bulletin No. No. 343-25-02, Issue 1, dated October 23, 2001. For type 343-1: Follow Anjou Aeronautique Service Bulletin No. 343-1-25-01, Issue 1, dated October 23, 2001. (2) If any defective buckle latch or safety belt and restraint system with exceeded service life is found during any inspection required by paragraph (e)(1) of this AD: (i) For any defective buckle latch, replace defective parts with new parts. (ii) For any safety belt and restraint system that has exceeded its service life, replace witha non-Anjou Aeronautique/TRW Repa S.A./L'Aiglon FAA-approved safety belt and restraint system. The service life limit for the Anjou Aeronautique/TRW Repa S.A./L'Aiglon is 60 calendar months after the date of manufacture. Prior to further flight after any inspection required by paragraph (e)(1) of this AD. For types 343, 343AM, 343B, 343BM, 343C, 343CM, 343D, or 343M: Follow Anjou Aeronautique Service Bulletin No. No. 343-25-02, Issue 1, dated October 23, 2001. For type 343-1: Follow Anjou Aeronautique Service Bulletin No. 343-1-25-01, Issue 1, dated October 23, 2001. (3) Replace any installed Anjou Aeronautique/TRW Repa S.A./L'Aiglon safety belts and restraint systems (types 343, 343-1, 343AM, 343B, 343BM, 343C, 343CM, 343D, or 343M). Replacement of all safety belts and restraint systems eliminates the need for the repetitive inspections of paragraph (e)(1) of this AD. Prior to exceeding the service life limit of 60 calendar months after the date of manufacture or 4 calendar months after February 17, 2004 (the effective date of this AD), whichever occurs later. Not Applicable. (4) Do not install any Anjou Aeronautique/TRW Repa S.A./L'Aiglon types 343, 343-1, 343-1, 343M, 343AM, 343B, 343BM, 343C, 343CM, and 343D safety belts and restraint systems. As of February 17, 2004 (the effective date of this AD). Not Applicable. Note: All inertia-reel type safety belts and restraint systems or fixed rear safety belts and restraint systems from another manufacturer are not affected by this AD. What About Alternative Methods of Compliance? (f) You may request a different method of compliance or a different compliance time for this AD by following the procedures in 14 CFR 39.13. Send your request to the Manager, Manager, Standards Office, Small Airplane Directorate, FAA. For information on any already approved alternative methods of compliance, contact Karl Schletzbaum, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,Missouri 64106; telephone: (816) 329-4146; facsimile: (816) 329-4090. Is There Material Incorporated by Reference? (g) You must do the actions required by this AD per Anjou Aeronautique Service Bulletin No. 343-25-02, Issue 1, dated October 23, 2001, and Anjou Aeronautique Service Bulletin No. 343-1-25-01, Issue 1, dated October 23, 2001. The Director of the Federal Register approved the incorporation by reference of this service bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. You may get a copy from Anjou Aeronautique, 13 Avenue De L'Osier, 49125 Tierce, France; telephone: 33 0 2 41 42 88 92; facsimile: 33 0 2 41 42 15 77. You may review copies at FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 64106; or at the Office of the Federal Register, 800 North Capitol Street, NW, suite 700, Washington, DC.

Related safety bulletins advice on the same designs, not orders

2021-08-13AIR-21-13 · ENGINE EMERGENCY SHUTDOWN SYSTEM
2019-07-15SW-17-23R2 · Fuel System
2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2018-03-02SW-17-23R1 · Fuel System
2017-08-24SW-17-23 · Fuel System

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 5, 2026. Connections as data: /graph/directive/2003-26-06.json · aircraft systems.