AD 85-04-51

final rule
Data completeness: 60%

GARRETT TURBINE ENGINE COMPANY (GTEC) (formerly AiResearch Manufacturing Company of Arizona) Model ATF3-6-2C Engines

AD Number
85-04-51
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Honeywell International Inc. ATF3-6 GARRETT TURBINE ENGINE COMPANY (GTEC) (formerly AiResearch Manufacturing Company of Arizona) Model ATF3-6-2C Engines
engine Honeywell International Inc. ATF3-6A GARRETT TURBINE ENGINE COMPANY (GTEC) (formerly AiResearch Manufacturing Company of Arizona) Model ATF3-6-2C Engines

Unsafe Condition

The possibility of an uncontained engine failure due to seal/rotor contact and/or seal looseness in the stationary seal/sixth stage low pressure turbine rotor assembly area of engines with exhaust deflector liner and seal assembly, Garrett Part Numbers 3001313-10 through -14, and not incorporating the bolted flange system.

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

Required Actions

Within 25 operational hours after the effective date, inspect for seal/rotor contact and seal looseness. Subsequent inspections every 75 operational hours. Disassemble and modify/replace components if inspections fail. Incorporate bolted flange system within 500 operational hours or upon rotor assembly removal.

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

Compliance Time

Compliance is required as indicated unless already accomplished. The amendment becomes effective June 24, 1985, except for those under telegraphic AD T85-04-51 effective March 1, 1985.

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

Affected Aircraft

Garrett Turbine Engine Company (GTEC) Model ATF3-6-2C engines with exhaust deflector liner and seal assembly, Garrett Part Numbers 3001313-10 through -14, and not incorporating the bolted flange system specified in paragraph (d).

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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