AD 77-15-12

Airworthiness directive · Power Turbine Coupling Nut · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 23 more

Effective
September 23, 1977
Models
250-B15A, 250-B15E, 250-B15G, 250-B17, 250-B17B, 250-B17C and 20 more
Registered aircraft
1,325 matched by model
Product
Engine
Amendment
39-3037

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

77-15-12 DETROIT DIESEL ALLISON: Amendment 39-2977 as amended by Amendment 39-3037. Applies to 250-B15 and B17 and 250-C18 and C20 series engines equipped with power turbine outer coupling nuts Part Number (P/N) 6846278 as installed in aircraft certificated in all categories. NOTE THAT THIS AMENDED VERSION OF AD 77-15-12 REQUIRES THAT ALL POWER TURBINE COUPLING NUTS, BOTH COATED AND UNCOATED, BE INSPECTED ON A REPETITIVE BASIS. Compliance schedule - Compliance required as follows unless previously accomplished. (a) For engines with turbine sections having more than 400 hours or one calendar year time in service since installation in an aircraft, initial compliance must be accomplished within the next 100 hours or 90 days, whichever occurs first, from the effective date of the original amendment of July 27, 1977. (b) For engines with turbine sections having less than 400 hours and less than one calendar year time in service since installation in an aircraft, initial compliance must be accomplished within 500 hours or one year time in service since installation in an aircraft, whichever occurs first. (c) For each turbine section incorporating an acceptable uncoated or coated coupling nut, as defined by the below referenced service letters, repetitive compliance is required at intervals not to exceed 500 hours or one calendar year time since last inspection, whichever occurs first. To preclude possible engine failure resulting from power turbine coupling nut failure: Inspect the power turbine outer coupling nut P/N 6846278 in accordance with Detroit Diesel Allison Commercial Service Letter Numbers 88 for the C18 series, 1060 for the C20 series, 25 for the B15 series, and 1030 for the B17 series engines. All Service Letters are Revision 3 or later FAA approved revisions. If an unacceptable extent of corrosion, as defined by the Service Letter, is found, the nut shall be replaced before further flight except that the aircraft may be flown in accordance with FAR 21.197 to a base where the repair can be performed. Amendment 39-2977 was effective July 27, 1977. This amendment 39-3037 is effective September 23, 1977, and was effective immediately for all recipients of airmail letters dated August 19, 1977 which contained this amendment.

Affected TCDS · 2

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

Registered aircraft · 1,325

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
  • Bell656 aircraft
  • Hughes Helicopters147 aircraft
  • Mcdonnell Douglas Helicopter92 aircraft
  • MD Helicopters61 aircraft
  • Enstrom Helicopter60 aircraft
  • Other makers50309 aircraft
By year built
19472026
Registered aircraft by year built: 1,182 aircraft
19471
19561
19581
19602
19611
19625
19631
19641
19653
19665
19676
196813
196910
197015
197119
197224
197322
197430
197528
197643
197745
197846
197968
198065
198178
198255
198317
198416
198518
198616
198712
198825
198930
199025
199132
199228
199333
199444
199556
199621
199721
199812
19998
200018
200118
200214
20037
20045
200515
200613
200717
200821
200911
20103
20124
20134
20145
20153
20165
20171
20186
20201
20211
20231
20241
20252
20264

143 with no year recorded

By model

See all 36 models

Aircraft

See all 1,325 aircraft