AD 92-21-05

Active

Auxiliary Power Units

Key Information
92-21-05
Active
November 24, 1992
Not specified
92-NM-94-AD
39-8385
Applicability
["Appliance"]
Not specified
Airbus SAS The Boeing Company Garrett Auxiliary Power Division
A320-111 A320-211 A320-212 A320-214 A320-231 A320-232 A320-233 737-100 Series 737-200 Series 737-200C Series 737-300 Series 737-400 Series 737-500 Series 737-600 Series 737-700 Series 737-700C Series 737-800 Series 737-900 Series DC-9-81 (MD-81) DC-9-82 (MD-82) DC-9-83 (MD-83) DC-9-87 (MD-87) Auxiliary Power Units
Regulatory Text

92-21-05 GARRETT AUXILIARY POWER DIVISION: Amendment 39-8385. Docket No. 92-NM-94-AD. \n\n\tApplicability: Garrett Model GTCP 36-300 auxiliary power units (APU), as installed in, but not limited to, Airbus Industrie Model A320 series airplanes; Garrett Model GTCP 36-280(D) APU's, serial numbers prior to P-80346, as installed in, but not limited to, McDonnell Douglas Model DC-9-80 series airplanes; and Garrett Model GTCP 36-280(B) APU's, serial numbers prior to P-40182, as installed in, but not limited to, Boeing Model 737 series airplanes; certificated in any category. \n\n\tCompliance: Required as indicated, unless accomplished previously. \n\n\tTo prevent damage to the titanium APU fire wall due to APU tieshaft separation, which could lead to a reduction in the fire protection capability of the APU compartment, accomplish the following: \n\n\t(a)\tFor airplanes equipped with Garrett Model GTCP 36-300 APU's: Within 30 months after the effective date of this AD, modify the APU, in accordance with Garrett Service Bulletin GTCP36-49-A6642, dated May 1, 1992. \n\n\t(b)\tFor airplanes equipped with Garrett Model GTCP 36-280 APU's: Within 30 months after the effective date of this AD, modify the APU, in accordance with Garrett Service Bulletin GTCP36-49-A6653, dated May 1, 1992. \n\n\t(c)\tAn alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Los Angeles Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Los Angeles ACO. \n\n\tNOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Los Angeles ACO. \n\n\t(d)\tSpecial flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished. \n\n\t(e)\tThe modification shall be done in accordance with either Garrett Service Bulletin GTCP36-49-A6642, dated May 1, 1992, or Garrett Service Bulletin GTCP36-49-A6653, dated May 1, 1992, as applicable. 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 Garrett Airlines Services Division, Technical Publications, Department 65-70, P.O. Box 52170, Phoenix, Arizona 85072-2170. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at FAA, Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. \n\n\t(f)\tThis amendment becomes effective on November 24, 1992.

AD Assistant

Get AI-powered answers about this AD, check applicability, and find compliance steps.

Sign Up to Unlock
References
This information is not available.
--- - Part 39
FAA Documents