AD 68-19-07

final rule
Data completeness: 70%

Airworthiness Directives; Sikorsky Model S-61 Series helicopters

AD Number
68-19-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Sikorsky Aircraft Corporation S-61A Airworthiness Directives; Sikorsky Model S-61 Series helicopters
aircraft Sikorsky Aircraft Corporation S-61D Airworthiness Directives; Sikorsky Model S-61 Series helicopters
aircraft Sikorsky Aircraft Corporation S-61E Airworthiness Directives; Sikorsky Model S-61 Series helicopters
aircraft Sikorsky Aircraft Corporation S-61L Airworthiness Directives; Sikorsky Model S-61 Series helicopters
aircraft Sikorsky Aircraft Corporation S-61N Airworthiness Directives; Sikorsky Model S-61 Series helicopters
aircraft Sikorsky Aircraft Corporation S-61NM Airworthiness Directives; Sikorsky Model S-61 Series helicopters
aircraft Sikorsky Aircraft Corporation S-61R Airworthiness Directives; Sikorsky Model S-61 Series helicopters
aircraft Sikorsky Aircraft Corporation S-61V Airworthiness Directives; Sikorsky Model S-61 Series helicopters

Unsafe Condition

Failure of the main rotor blade spindle due to being salvaged or having accumulated 3000 or more hours' time in service.

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

Required Actions

Remove and replace main rotor blade spindles with specified part numbers if salvaged or exceeding 3000 hours' time in service. Replace non-salvaged spindles before accumulating 3000 hours' time in service. Remove specific serial numbered spindles before further flight.

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

Compliance Time

Before further flight or before the accumulation of 3000 hours' time in service as applicable.

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

Affected Aircraft

Sikorsky Model S-61A, S-61D, S-61E, S-61L, S-61N, S-61NM, S-61R, S-61V helicopters with main rotor blade spindles P/Ns S6110-23325-1, S6110-23325-2, and S6112-23025-1.

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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