AD 82-25-01 R1

final rule
Data completeness: 70%

Airworthiness Directives; SIKORSKY Model S-76A Helicopters

AD Number
82-25-01 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

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

Unsafe Condition

Failure of the S-76 main left and right landing gear positioning rod end fittings, Part Number KR10MEAK, due to cracks.

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

Required Actions

Inspect for cracks and replace rod end fittings as required per Sikorsky Alert Service Bulletin 76-32-10 and modifications. Replace rod end fitting P/N KR10MEAK with P/N 1945E235 and install improved parts from kit P/N 76070-25004-011 per CSN 76-134 or 76-134A. Revise aircraft weight and balance.

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

Compliance Time

Within the next 25 hours' time in service after the effective date (December 1, 1986) if rod ends have 1,500+ hours' time in service, or before 1,525 hours' time in service if less than 1,500 hours. Thereafter, inspections at intervals not exceeding 100 hours' time in service. Replacement must be done within 300 hours' time in service or 6 months after effective date.

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

Affected Aircraft

Sikorsky Model S-76A helicopters with serial numbers prior to 760308.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.