AD 76-12-05

final rule
Data completeness: 70%

AVCO LYCOMING Model T5508D Engines

AD Number
76-12-05
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Honeywell International Inc. T5508D AVCO LYCOMING Model T5508D Engines

Unsafe Condition

Failure of the compressor air bleed band while the engine is operating at a power level requiring the bleed band to be closed, leading to partial power loss.

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

Required Actions

Inspect the compressor air bleed band for edge wear and cracks daily before first flight and repair or replace as necessary per Avco Lycoming Service Bulletin 5508-0003. Replace P/N 2-160-147-02 retaining plate spacers with P/N 2-160-561-01 and P/N 2-161-182-01 compressor air bleed bands with P/N 2-161-182-03 by July 1, 1976, following Service Bulletin 5508-0007.

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

Compliance Time

Prior to the first flight of each day and prior to July 1, 1976.

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

Affected Aircraft

Avco Lycoming T5508D engines equipped with P/N 2-160-147-02 retaining plate spacers and P/N 2-161-182-01 compressor air bleed bands.

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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