AD 77-15-12

final rule
Data completeness: 70%

DETROIT DIESEL ALLISON Model 250-B15 and B17 and 250-C18 and C20 Series Engines

AD Number
77-15-12
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce Corporation 250-B15A DETROIT DIESEL ALLISON Model 250-B15 and B17 and 250-C18 and C20 Series Engines
engine Rolls-Royce Corporation 250-B15E DETROIT DIESEL ALLISON Model 250-B15 and B17 and 250-C18 and C20 Series Engines
engine Rolls-Royce Corporation 250-B15G DETROIT DIESEL ALLISON Model 250-B15 and B17 and 250-C18 and C20 Series Engines
engine Rolls-Royce Corporation 250-B17 DETROIT DIESEL ALLISON Model 250-B15 and B17 and 250-C18 and C20 Series Engines
engine Rolls-Royce Corporation 250-B17B DETROIT DIESEL ALLISON Model 250-B15 and B17 and 250-C18 and C20 Series Engines
engine Rolls-Royce Corporation 250-B17C DETROIT DIESEL ALLISON Model 250-B15 and B17 and 250-C18 and C20 Series Engines
engine Rolls-Royce Corporation 250-B17D DETROIT DIESEL ALLISON Model 250-B15 and B17 and 250-C18 and C20 Series Engines
engine Rolls-Royce Corporation 250-B17E DETROIT DIESEL ALLISON Model 250-B15 and B17 and 250-C18 and C20 Series Engines
engine Rolls-Royce Corporation 250-B17F DETROIT DIESEL ALLISON Model 250-B15 and B17 and 250-C18 and C20 Series Engines
engine Rolls-Royce Corporation 250-B17F/1 DETROIT DIESEL ALLISON Model 250-B15 and B17 and 250-C18 and C20 Series Engines

Unsafe Condition

Power turbine coupling nut failure due to corrosion.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect the power turbine outer coupling nut P/N 6846278 in accordance with specified service letters. Replace the nut before further flight if unacceptable corrosion is found.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Initial compliance within next 100 hours or 90 days from July 27, 1977, for engines with over 400 hours or one year since installation; within 500 hours or one year since installation for others. Repetitive inspections every 500 hours or one calendar year.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Rolls-Royce Corporation models 250-B15A, B15E, B15G, B17, B17B, B17C, B17D, B17E, B17F, etc., and 250-C18, C20 series engines with power turbine outer coupling nuts P/N 6846278 installed.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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