AD 66-19-04

final rule
Data completeness: 70%

Airworthiness Directives; Sikorsky Models S-58 and S-61 Series Helicopters

AD Number
66-19-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Sikorsky Aircraft Corporation S-58A Airworthiness Directives; Sikorsky Models S-58 and S-61 Series Helicopters
aircraft Sikorsky Aircraft Corporation S-58B Airworthiness Directives; Sikorsky Models S-58 and S-61 Series Helicopters
aircraft Sikorsky Aircraft Corporation S-58BT Airworthiness Directives; Sikorsky Models S-58 and S-61 Series Helicopters
aircraft Sikorsky Aircraft Corporation S-58C Airworthiness Directives; Sikorsky Models S-58 and S-61 Series Helicopters
aircraft Sikorsky Aircraft Corporation S-58D Airworthiness Directives; Sikorsky Models S-58 and S-61 Series Helicopters
aircraft Sikorsky Aircraft Corporation S-58DT Airworthiness Directives; Sikorsky Models S-58 and S-61 Series Helicopters
aircraft Sikorsky Aircraft Corporation S-58E Airworthiness Directives; Sikorsky Models S-58 and S-61 Series Helicopters
aircraft Sikorsky Aircraft Corporation S-58ET Airworthiness Directives; Sikorsky Models S-58 and S-61 Series Helicopters
aircraft Sikorsky Aircraft Corporation S-58F Airworthiness Directives; Sikorsky Models S-58 and S-61 Series Helicopters
aircraft Sikorsky Aircraft Corporation S-58FT Airworthiness Directives; Sikorsky Models S-58 and S-61 Series Helicopters

Unsafe Condition

Tail rotor blades with flex shank area of the spar having less than minimum hardness requirements.

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

Required Actions

Inspect S 1615-30100, S 6115-30001, and S 6117-30001 series tail rotor blades as per Sikorsky Service Bulletin 58B15-6A or 61B15-5A. Remove from service blades not meeting minimum hardness requirements before further flight.

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

Compliance Time

within the next 50 hours' time in service after the effective date of this AD unless already accomplished

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

Affected Aircraft

Sikorsky Models S-58 and S-61 Series Helicopters equipped with tail rotor blades with serial numbers listed in Sikorsky Service Bulletin 58B15-6A or 61B15-5A.

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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