AD 2017-14-03

final rule
Data completeness: 80%

Airworthiness Directives; Sikorsky Aircraft Corporation

AD Number
2017-14-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2017-0664
FR Citation
82 FR 34838

Applicability

TypeManufacturerModelDetails
aircraft Sikorsky Various Airworthiness Directives; Sikorsky Aircraft Corporation

Unsafe Condition

Cracks or failure of landing gear components, including main landing gear wheel axles, threaded hinge pins, nose landing gear cylinders, hinge pins, and actuator rod ends, could result in damage and loss of control of the helicopter.

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

Required Actions

Inspect and remove from service landing gear components exceeding specified landing cycle limits. Inspect NLG airframe fitting assemblies for fretting, corrosion, wear, and scratches, and replace if anomalies exceed 0.0005 inch depth. Perform ultrasonic inspection of NLG actuator fittings and replace if anomalies are found.

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 specific landing gear components (P/Ns listed in the AD).

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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