AD 88-05-01 R1

final rule
Data completeness: 70%

Airworthiness Directives; SIKORSKY AIRCRAFT Model S-76B Helicopters

AD Number
88-05-01 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
88-ASW-4
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Sikorsky Aircraft Corporation S-76B Airworthiness Directives; SIKORSKY AIRCRAFT Model S-76B Helicopters

Unsafe Condition

Failure of the helicopter forward engine support cross beam due to cracks in the cap angle and web, specifically Part Numbers 76070-20526-102 and 76070-20526-139, -149, or -158.

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

Required Actions

Visually inspect the forward engine support cross beam cap angle and web for cracks using a flashlight and mirror. If cracks are found, verify with dye penetrant inspection. Replace cracked cap angle parts prior to further flight. Repair or replace cracked web parts with approved methods. Report findings within 10 days. Allow ferry flights under FAR 21.197/199.

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 July 16, 1990, and thereafter every 50 hours' time in service.

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

Affected Aircraft

Sikorsky Model S-76B helicopters with serial numbers 760312, 760314, 760316, 760317, 760318, 760319, 760327, 760330, 760331, and 760337, equipped with original cross beam cap angle P/N 76070-20526-102 and web P/N 76070-20526-139, -149, or -158.

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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