AD 91-15-01

Active

Rudder Pedal Connection Rod

Key Information
91-15-01
Active
July 17, 1991
Not specified
91-NM-123-AD
39-7064
Applicability
["Aircraft"]
["Large Airplane"]
ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional ATR - GIE Avions de Transport R gional
ATR42-200 ATR42-300 ATR72-101 ATR72-102 ATR72-201 ATR72-202 ATR72-211 ATR72-212 ATR72-212A
Regulatory Text

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.

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References
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FAA Documents