AD 67-29-06

final rule
Data completeness: 70%

Airworthiness Directives; Sikorsky Model S-51 Helicopters

AD Number
67-29-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Sikorsky Aircraft Corporation S-51 Airworthiness Directives; Sikorsky Model S-51 Helicopters

Unsafe Condition

Failure of sleeve and tube assembly P/N S535180 could lead to loss of tail rotor power.

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

Required Actions

Perform torsional checks every 50 aircraft hours' time in service, including applying rotor brake, inducing torsional force on tail rotor drive shafting, and inspecting shaft ends for movement. Daily inspect for loose rivets indicated by black fretting residue or movement, and cracks at tube and sleeve joints. Replace assembly if movement or cracks are found; loose rivets may be replaced with specified rivets after drilling holes to specified diameters.

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

Compliance Time

Immediately upon the effective date of this AD and every 50 aircraft hours' time in service thereafter

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

Affected Aircraft

Sikorsky Model S-51 Helicopters, all serial numbers

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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