AD 91-10-04

Airworthiness directive · Exhaust Transition Flange Bolts · Lycoming Engines TIO-540-AE2A

Effective
May 21, 1991
Model
TIO-540-AE2A
Data sheet
TCDSE14EA
Registered aircraft
5,565 matched by model
Product
Engine
Amendment
39-6981
Docket
91-ANE-10

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.

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The airworthiness directive

91-10-04 TEXTRON LYCOMING: Amendment 39-6981. Docket No. 91-ANE-10. Applicability: Textron Lycoming Model TIO-540-AE2A engines, with serial numbers up to but not including L9161-61A, except L9157-61A, installed in Piper Malibu Mirage aircraft. Compliance: Required as indicated, unless previously accomplished. To prevent engine power loss, engine fire, and possible loss of aircraft, accomplish the following: (a) Remove and replace exhaust transition flange bolts, within the next 10 hours in service, after the effective date of this AD, in accordance with the following procedures: (1) Apply penetrating oil to existing exhaust transition flange bolts and remove the two bolts. (2) Install the following hardware in place of the removed bolts:

LYCOMING PART NO. DESCRIPTION QUANTITY LW-31SS-1.19 Bolt 2 77611 Gasket 1 STD-2043 Nut 2

(3) Torque the bolts to 17 ft.-lbs. (Do not use lockwashers on the bolts.) It may be necessary to start thelock nut prior to torqueing. (4) Install the locknuts on the protruding threads of the bolts, and insure that the bolts do not loosen during installation. (5) Recheck torque on bolt heads to ensure proper torque is retained (17 ft.-lbs.) NOTE: Further information can be obtained from Textron Lycoming Service Bulletin No. 491A, dated February 21, 1990. (b) Aircraft may be ferried in accordance with the provisions of FAR 21.197 and 21.199 to a base where the AD can be accomplished. (c) Upon submission of substantiating data by an owner or operator through an FAA Inspector (maintenance, avionics, or operations, as appropriate), an alternate method of compliance with the requirements of this AD or adjustments to the compliance schedule specified in this AD may be approved by the Manager, New York Aircraft Certification Office, ANE-170, Engine and Propeller Directorate, Aircraft Certification Service, FAA, New England Region, 181 South Franklin Avenue, Room 202, Valley Stream, New York 11581. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Textron Lycoming/Subsidiary of Textron Inc., Williamsport, Pennsylvania 17701. These documents may be examined at the FAA, New England Region, Office of the Assistant Chief Counsel, Room 311, 12 New England Executive Park, Burlington, Massachusetts. This amendment (39-6981, AD 91-10-04) becomes effective on May 21, 1991.

Affected TCDS · 1

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

Registered aircraft · 5,565

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
  • Piper4,110 aircraft
  • Cessna633 aircraft
  • Mooney222 aircraft
  • Aero Commander117 aircraft
  • Bellanca111 aircraft
  • Other makers55372 aircraft
By year built
19472026
Registered aircraft by year built: 5,003 aircraft
19471
19491
19541
19552
19561
19581
19592
196011
196114
196228
196327
196479
1965157
1966206
1967165
1968124
1969219
197071
197193
1972105
1973152
1974162
1975179
1976347
1977213
1978253
1979138
1980145
1981128
198263
198345
198442
19856
19865
19874
19881
198949
199037
199127
199211
199330
199428
199527
199640
199761
199867
1999142
2000155
2001119
2002101
200386
2004171
2005171
200636
200717
200868
200914
201031
201129
201243
201338
201433
201528
201622
20175
201816
201917
20208
202115
202211
202319
202420
202514
20266

562 with no year recorded

By model

Aircraft

See all 5,565 aircraft