AD Amdt-39-10126

final rule
Data completeness: 70%

Airworthiness Directives; Sikorsky Aircraft Corporation Model S- 61A, D, E, L, N, NM, R, and V Helicopters; Correction

AD Number
Amdt-39-10126
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 97-SW-18-AD
FR Citation
63 FR 45170

Applicability

TypeManufacturerModelDetails
aircraft Sikorsky Aircraft Corporation Model S- 61A Airworthiness Directives; Sikorsky Aircraft Corporation Model S- 61A, D, E, L, N, NM, R, and V Helicopters; Correction

Unsafe Condition

The anodizing process performed by Poly-Metal Company between October 1, 1996, and December 31, 1996, may have resulted in a degradation of the pocket assemblies on certain main rotor blades, leading to potential failure of the pocket assemblies.

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

Required Actions

Inspect main rotor blades to determine the anodizing date of pocket assemblies. Replace blades with anodized pocket assemblies from Poly-Metal Company between October 1, 1996, and December 31, 1996, with airworthy blades before further flight.

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

Sikorsky Aircraft Corporation Model S-61A, D, E, L, N, NM, R, and V helicopters with main rotor blades having pocket assemblies anodized by Poly-Metal Company between October 1, 1996, and December 31, 1996.

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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