AD 2006-17-51

final rule
Data completeness: 70%

Airworthiness Directives; Agusta S.p.A. Model AB139 Helicopters

AD Number
2006-17-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-25703
FR Citation
71 FR 51988

Applicability

TypeManufacturerModelDetails
aircraft Agusta S.p.A. Model AB139 Airworthiness Directives; Agusta S.p.A. Model AB139 Helicopters

Unsafe Condition

Cracks in the tailpipe assembly and overheating of the structure in the cowling area, which could lead to separation of a part of the tailpipe assembly and subsequent loss of control of the helicopter.

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

Required Actions

Before further flight, visually inspect each tailpipe assembly inside the cowling for cracks and inspect the surrounding structure for overheating. If overheating is found, inspect for damage to the surrounding structure. If a crack is found, replace the tailpipe assembly with an airworthy one. Repeat inspections at intervals not exceeding 25 hours time-in-service.

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

Compliance Time

Before further flight

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

Affected Aircraft

Agusta S.p.A. Model AB139 helicopters of U.S. registry.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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