AD 83-01-04

Airworthiness directive · Turbine Assemblies · Rolls-Royce 250-C28B and 250-C28C

Effective
January 24, 1983
Models
250-C28B, 250-C28C
Data sheet
TCDSE1GL
Registered aircraft
130 matched by model
Product
Engine
Amendment
39-4539

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

83-01-04 DETROIT DIESEL ALLISON: Amendment 39-4539. Applies to Detroit Diesel Allison (DDA) Model 250-C28B and -C28C series engines with turbine assembly serial numbers CAT 70001 thru 70186, 70188, and 70191. Compliance required, as indicated, unless already accomplished. To prevent possible damage to the first stage turbine wheel due to oil fires caused by the improper U-ring gasket or the proper U-ring gasket incorrectly installed at the No. 8 bearing retainer plate, accomplish the following: a. Within the next 5 hours time in service after the effective date of this AD, inspect and pressure test the No. 8 bearing sump area, in accordance with Detroit Diesel Allison Commercial Engine Alert Bulletin CEB- A-72-2082, dated January 3, 1983, or later FAA approved revisions, on affected turbine assemblies that meet either of the following conditions: 1. Turbine Assemblies with less than 500 hours time since new. 2. Turbine Assemblies that are experiencing or have experienced oil consumption in excess of one quart (0.9 liter) per hour. NOTE: Turbine Assemblies that have been overhauled and have had the pressure check accomplished or have been operated for more than 500 hours time since new, and have less than one quart (0.9 liter) per hour oil consumption are not required to have the inspection and pressure test. b. Inspect and pressure test, before initial flight, uninstalled affected turbine assembly No. 8 bearing sump area per Detroit Diesel Allison Commercial Engine Alert Bulletin CEB-A-2082, dated January 3, 1983, or later FAA approved revisions. Special flight permits may be issued in accordance with FARs 21.197 and 21.199 to operate aircraft to a base where compliance with this AD can be accomplished. Upon request of the operator, an equivalent means of compliance with the requirements of this AD may be approved by the Manager, Chicago Aircraft Certification Office, Federal Aviation Administration, 2300 East Devon Avenue, Des Plaines,Illinois 60018. This amendment becomes effective January 24, 1983.

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