AD 2012-22-09

final rule
Data completeness: 70%

Airworthiness Directives; Sikorsky Aircraft Corporation Helicopters

AD Number
2012-22-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2012-0216
FR Citation
77 FR 68061

Applicability

TypeManufacturerModelDetails
aircraft Sikorsky Aircraft Corporation Airworthiness Directives; Sikorsky Aircraft Corporation Helicopters

Unsafe Condition

A loose or missing fastener, a crack, damage, or corrosion on the tail rotor (T/R) pylon that could result in failure of the T/R pylon or other T/R components, 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

Inspect the T/R pylon for a loose or missing fastener, crack, damage, or corrosion. If any of these conditions are found, repair or replace the T/R pylon and install a doubler on the aft shear deck tunnel assembly. If no crack is found, replace the T/R pylon and install the doubler.

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

Compliance Time

Within 25 hours time-in-service (TIS) for helicopters with 500 or more hours TIS, and thereafter at intervals not to exceed 10 hours TIS.

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 rotor (T/R) pylon, part number (P/N) 92000-06102-041, certificated in any category.

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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