AD 2005-13-13

final rule
Data completeness: 70%

Airworthiness Directives; Sikorsky Aircraft Corporation Model S-92A Helicopters

AD Number
2005-13-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-21588
FR Citation
70 FR 36333

Applicability

TypeManufacturerModelDetails
aircraft Sikorsky Aircraft Corporation Model S-92A Airworthiness Directives; Sikorsky Aircraft Corporation Model S-92A Helicopters

Unsafe Condition

Fatigue failure of the tail gear box output housing, part number 92358-06109-043, with 600 or more hours time-in-service (TIS), leading to loss of tail rotor drive and subsequent loss of control of the helicopter.

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

Required Actions

Replace each tail gear box output housing, P/N 92358-06109-043, with 600 or more hours TIS with an airworthy part with less than 600 hours TIS before further flight. Revise the Airworthiness Limitations section of the maintenance manual to reduce the life limit of the tail gear box output housing from 4500 hours TIS to 600 hours TIS.

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

Compliance Time

Before further flight

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

Affected Aircraft

Sikorsky Aircraft Corporation Model S-92A helicopters with a tail gear box output housing, part number 92358-06109-043, installed.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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