AD 85-25-12

Airworthiness directive · Turbine-To-Compressor-Coupling · Rolls-Royce 250-C28B and 250-C28C

Effective
January 6, 1986
Models
250-C28B, 250-C28C
Data sheet
TCDSE1GL
Registered aircraft
130 matched by model
Product
Engine
Amendment
39-5191

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

85-25-12 ALLISON GAS TURBINE DIVISION, GENERAL MOTORS CORP. (ALLISON, formerly DETROIT DIESEL ALLISON): Amendment 39-5191. Applies to Allison Model 250-C28B and -C28C engines, which incorporate P/N 23008080 turbine-to-compressor-coupling, installed in rotorcraft certificated in any category. Compliance is required as indicated unless already accomplished. To prevent possible cracks in turbine-to-compressor coupling P/N 23008080 from progressing to where a disconnect failure could occur and subsequently could result in an overspeed uncontained failure of the gas producer turbine rotor, accomplish the following: Within the next 100 hours time-in-service after the effective date of this AD, or at the next turbine repair/inspection when access to P/N 23008080 coupling is gained, whichever occurs first, but not later than March 6, 1986, perform the following: Replace P/N 23008080 turbine-to-compressor-coupling with P/N 23032345 and install two P/N AS 3085- 018 O-rings on the aft end of the spur adapter gearshaft in accordance with Allison Commercial Engine Alert Bulletin CEB-A-72-2127, Revision 1, dated September 15, 1985, or FAA approved equivalent. 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. Upon request, an equivalent means of compliance with the requirements of this AD may be approved by the Manager, Chicago Aircraft Certification Office, FAA, 2300 East Devon Avenue, Des Plaines, Illinois 60018. Upon submission of substantiating data by an owner or operator through an FAA maintenance inspector, the Manager, Chicago Aircraft Certification Office may adjust the compliance time specified in this AD. Allison CEB-A-72-2127, Revision 1, dated September 15, 1985, is incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to Allison Gas Turbine Division, General Motors Corp., P.O. Box 420, Indianapolis, IN 46206-0420. These documents also may be examined at the Office of Regional Counsel, FAA, ATTN: Rules Docket No. 85-ANE-40, 12 New England Executive Park, Burlington, Massachusetts 01803, weekdays, except Federal holidays, between 8:00 a.m. and 4:30 p.m. This amendment becomes effective January 6, 1986.

Affected TCDS · 1

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

Registered aircraft · 130

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
  • Bell Helicopter Textron45 aircraft
  • Bell29 aircraft
  • Hiller15 aircraft
  • Enstrom Helicopter9 aircraft
  • Cessna7 aircraft
  • Other makers1525 aircraft
By year built
19602005
Registered aircraft by year built: 114 aircraft
19601
19624
19641
19652
19663
19671
19682
19722
19731
19741
19764
19772
19783
19797
198014
198112
19825
198311
19841
19851
19861
19871
19881
19922
19943
19967
19973
19984
19992
20006
20023
20042
20051

16 with no year recorded

By model

Aircraft

See all 130 aircraft