AD 92-08-51

Airworthiness directive · Engine Fuel Control · Honeywell International ALF502R-3, ALF502R-3A, ALF502R-4 and 2 more

Effective
March 18, 1993
Models
ALF502R-3, ALF502R-3A, ALF502R-4, ALF502R-5, ALF502R-6
Data sheet
TCDSE6NE
Registered aircraft
35 matched by model
Product
Engine
Amendment
39-8344
Docket
92-ANE-13

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

On this page

The airworthiness directive

92-08-51 TEXTRON LYCOMING: Amendment 39-8344. Docket 92-ANE-13. Applicability: Textron Lycoming Model ALF502R series turbofan engines installed on British Aerospace BAe-146 airplanes. Compliance: Required as indicated, unless accomplished previously. To prevent uncommanded in-flight engine power reduction of engines during inclement weather or icing conditions, accomplish the following: (a) Replace the existing engine fuel control, Part Number (P/N) 2-163-810-07, 2-163-810-12, or 2-163- 810-15 with an improved fuel control, P/N 2-163-810-20, 2-163-810-21, or 2-163-810-23, or rework the existing engine fuel control, in accordance with Textron Lycoming Alert Service Bulletin (ASB) No. A-ALF 502R 73-12, Revision 1, dated April 7, 1992, at the first maintenance access of the engine fuel control or within 300 operating cycles after the effective date of this AD, whichever occurs first. (b) An 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, Engine Certification Office, FAA, Engine and Propeller Directorate. The request should be forwarded through an FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Engine Certification Office. NOTE: Information concerning the existence of approved alternative methods of compliance with this airworthiness directive, if any, may be obtained from the Engine Certification Office. (c) Special 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. (d) The replacement or rework of the engine fuel control shall be done in accordance with the following Textron Lycoming Alert Service Bulletin (ASB):

Document No. Pages Version Date Textron Lycoming 1,2,4,5 Rev. 1 April 7, 1992 ASB A-ALF-502R 73-12 3,6,7,8 Original April 1, 1992 Total pages: 8This 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 Textron Lycoming, Stratford Division, 550 Main Street, Stratford, Connecticut 06497. Copies may be inspected at the FAA, Office of the Assistant Chief Counsel, 12 New England Executive Park, Burlington, Massachusetts; or at the Office of the Federal Register, 800 North Capitol Street, NW., Suite 700, Washington, DC 20001. (e) This amendment becomes effective on March 18, 1993, to all persons except those persons to whom it was made immediately effective by telegraphic AD T92-08-51, issued April 8, 1992, which contained the requirements of this amendment.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 35

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Canadair25 aircraft
  • British Aerospace10 aircraft
By year built
19811991
Registered aircraft by year built: 25 aircraft
19815
19828
19833
19851
19861
19871
19881
19892
19901
19912

10 with no year recorded

By model

Aircraft

See all 35 aircraft