AD 2006-11-14

final rule
Data completeness: 80%

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

AD Number
2006-11-14
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-24875
FR Citation
71 FR 30798

Applicability

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

Unsafe Condition

Failure of the main transmission mounting bolt (part number SS5211-10-47) due to wear or corrosion, which could result in loss of support of the main transmission 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 each of the 8 main transmission mounting bolts for wear or corrosion within 100 hours time-in-service (TIS), unless the inspection was completed within the last 500 hours TIS. Replace any bolt found with wear or corrosion, along with the bolt barrel nut and cage, before further flight.

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

Compliance Time

Within 100 hours time-in-service (TIS), unless the inspection was completed within the last 500 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 main transmission mounting bolt (part number SS5211-10-47) installed, 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 4, 2026

Rights: U.S. Government Public Domain

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