# AD 91-15-01: Rudder Pedal Connection Rod - Type: Airworthiness directive - Status: Current - Products: ATR - GIE Avions de Transport R gional ATR42-200, ATR42-300, ATR72-101, ATR72-102, ATR72-201, ATR72-202, ATR72-211, ATR72-212 and ATR72-212A - Effective: July 17, 1991 - Superseded by: Nothing supersedes this AD - Product type: Aircraft, Large airplane - Amendment: 39-7064 - Docket: 91-NM-123-AD - Registered aircraft: 45 may be affected, by airframe or engine model (OpenAirDocs) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/29B3EC5433DC525F86256982006FF28A.0001 - DRS record last changed: May 30, 2024 - Page: https://openairdocs.org/ad/91-15-01 ## The airworthiness directive 91-15-01 AEROSPATIALE: Amendment 39-7064. Docket No. 91-NM-123-AD. Applicability: Model ATR42-200 and -300 series airplanes, serial numbers 003 to 208, 213, 214, 218, 221, 225, 226, and 228; and Model ATR72-100 and -200 series airplanes, serial numbers 126 to 189, 195, 198, and 210; certificated in any category. Compliance: Required as indicated, unless previously accomplished. To prevent failure of the rudder pedal connection rod and subsequent reduced controllability of the airplane, accomplish the following: (a) Within 10 days after the effective date of this AD, perform a visual inspection of the rudder pedal connection rod (captain side) to determine the rod vendor, in accordance with Aerospatiale Service Bulletin ATR42-27-0052 (for Model ATR42 series airplanes), Revision 1, dated April 4, 1991; or Aerospatiale Service Bulletin ATR72-27-1015 (for Model ATR72 series airplanes), Revision 1, dated April 4, 1991; as applicable. (1) If the rod is manufactured by TAC, no further action is required. (2) If the rod is manufactured by SARMA, vendor P/N 14132B, prior to further flight, replace the rod with a TAC rod; or a SARMA rod, vendor P/N 14132-C; in accordance with the applicable service bulletin. (b) As of the effective date of this AD, no SARMA rudder pedal connection rod, P/N 14132B, shall be installed on any airplane. (c) An alternative method of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Standardization Branch, ANM-113. (d) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD. (e) The inspection and replacement requirements shall be done in accordance with Aerospatiale Service Bulletin ATR42-27-0052 (for Model ATR42 series airplanes), Revision 1, dated April 4, 1991; or Aerospatiale Service Bulletin ATR72-27-1015 (for Model ATR72 series airplanes), Revision 1, dated April 4, 1991; which include the following list of affected pages: Service Bulletin Page Number Revision Level Date 1, 3, 4, 7 1 April 4, 1991 ATR42-27-0052 2, 5-6, 8 through 17 (Original) March 7, 1991 1, 2, 5 1 April 4, 1991 ATR72-27-1015 3, 4, 6 through 15 (Original) March 7, 1991 This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Aerospatiale, 316 Route de Bayonne, 31060 Toulouse, Cedex 03, France. Copies may be inspected at the FAA, Transport Airplane Directorate, Renton, Washington; or at the Office of the Federal Register, 1100 L Street N.W., Room 8401, Washington, D.C. This amendment (39-7064, AD 91-15-01) becomes effective on July 17, 1991. ## Affected data sheets (1) (OpenAirDocs) The type certificate data sheets whose models the AD names. - [TCDS A53EU](https://openairdocs.org/tcds/A53EU): ATR – GIE Avions de Transport Régional; names 9 of 11 models: ATR72-202, ATR72-101, ATR72-212A, ATR72-212, ATR42-300, ATR72-211, ATR72-102, ATR42-200… ## Registered aircraft it may apply to (OpenAirDocs) Matched by airframe and engine model; the AD's applicability may narrow it by serial number, part number or equipment. - Aircraft: 45 (45 by airframe model, 0 by engine model) - Makers: Atr-Gie Avions De Trnsp Rgnl 15, Aerospatiale/Aeritalia 13, Aerospatiale 9, Aerospatiale/Alenia 3, ATR 3, Aerospatiale/Atr 2 Models with the most aircraft: - [Atr-Gie Avions De Trnsp Rgnl ATR 72-212A](https://openairdocs.org/model/atr-gie-avions-de-trnsp-rgnl-atr-72-212a): 14 aircraft (airframe model) - [Aerospatiale/Aeritalia ATR 42-300](https://openairdocs.org/model/aerospatiale-aeritalia-atr-42-300): 12 aircraft (airframe model) - [Aerospatiale ATR 72-212](https://openairdocs.org/model/aerospatiale-atr-72-212): 9 aircraft (airframe model) - [Aerospatiale/Alenia ATR-72-212](https://openairdocs.org/model/aerospatiale-alenia-atr-72-212): 3 aircraft (airframe model) - [ATR ATR72-212A](https://openairdocs.org/model/atr-atr72-212a): 3 aircraft (airframe model) - [Aerospatiale/Atr ATR 72 202](https://openairdocs.org/model/aerospatiale-atr-atr-72-202): 2 aircraft (airframe model) - [Atr-Gie Avions De Trnsp Rgnl ATR 42-300](https://openairdocs.org/model/atr-gie-avions-de-trnsp-rgnl-atr-42-300): 1 aircraft (airframe model) - [Aerospatiale/Aeritalia ATR72-212](https://openairdocs.org/model/aerospatiale-aeritalia-atr72-212): 1 aircraft (airframe model) All 8 models: https://openairdocs.org/ad/91-15-01/models.md Every aircraft: https://openairdocs.org/ad/91-15-01/aircraft.md Its text cites no advisory circulars or STCs. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.