AD 84-19-51 R1

final rule
Data completeness: 70%

Airworthiness Directives; SIKORSKY AIRCRAFT Model S-76A Helicopters

AD Number
84-19-51 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 AIRCRAFT Model S-76A Helicopters

Unsafe Condition

Damaged, bent, or fractured center firewall support stiffeners or doublers could cut into the tail rotor driveshaft and cause loss of directional control of the helicopter.

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

Required Actions

Inspect forward center firewall sections for missing fasteners and proper fit per Sikorsky Alert Service Bulletin 76-53-25. Remove and replace cracked or non-conforming doubler Part Number 76070-20057-101. Ensure rivets are installed correctly. Remove core section from specified horizontal seal parts. Inspect stiffeners and doublers for fractures, distortions, or damage. Check clearance between tail rotor driveshaft and firewall; contact Boston Aircraft Certification Office if inadequate. Helicopters not modified per Customer Service Notice 76-111 must perform specific inspections. Alternate compliance may be approved by the Boston office.

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

Compliance Time

prior to further flight

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

Affected Aircraft

Sikorsky Aircraft Corporation Model S-76A helicopters with Serial Numbers 76006, 76007, 760001 through 760339

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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