AD 79-18-13

final rule
Data completeness: 70%

DETROIT DIESEL ALLISON Model 250-C28B and 250-C28C Series Engines

AD Number
79-18-13
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce Corporation 250-C28B DETROIT DIESEL ALLISON Model 250-C28B and 250-C28C Series Engines
engine Rolls-Royce Corporation 250-C28C DETROIT DIESEL ALLISON Model 250-C28B and 250-C28C Series Engines

Unsafe Condition

Third stage turbine wheel blade failure due to use of turbine wheels with part numbers 6898553 or 6898773, which could cause engine power loss.

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

Required Actions

Remove from service third stage turbine wheels with part numbers 6898553 or 6898773. Compliance is required before reaching 325 hours total time in service for wheels with less than 300 hours, or within 25 hours time in service for wheels with over 300 hours.

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

Compliance Time

Before reaching 325 hours total time in service for turbine wheels with less than 300 hours total time in service; within 25 hours time in service for turbine wheels with more than 300 hours total time in service.

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

Affected Aircraft

Rolls-Royce Corporation Model 250-C28B and 250-C28C engines equipped with third stage turbine wheel part numbers 6898553 or 6898773 installed in Bell 206L-1 rotorcraft.

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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