AD 2004-15-22

final rule
Data completeness: 70%

Airworthiness Directives; Sikorsky Aircraft Corporation Model S-61L, S-61N, S-61-NM, and S-61R Helicopters

AD Number
2004-15-22
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-SW-35-AD
FR Citation
69 FR 46095

Applicability

TypeManufacturerModelDetails
aircraft Sikorsky Aircraft Corporation Model S-61L Airworthiness Directives; Sikorsky Aircraft Corporation Model S-61L, S-61N, S-61-NM, and S-61R Helicopters

Unsafe Condition

Failure of the engine's Number 5 bearing, resulting in erratic movement of the high-speed engine-to-transmission shaft, oil leakage, an in-flight fire, and an emergency landing.

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

Required Actions

Install a Number 5 bearing chip detector in each engine, install an on-board chip detector annunciation system, and revise the Rotorcraft Flight Manual (RFM) to include procedures for crew response to an on-board chip detector annunciation.

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

Compliance Time

Within 60 days

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

Affected Aircraft

Sikorsky Aircraft Corporation Model S-61L, S-61N, S-61-NM, and S-61R helicopters, certificated in any category.

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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