AD 2018-10-07

final rule
Data completeness: 80%

Airworthiness Directives; Sikorsky Aircraft Corporation

AD Number
2018-10-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2017-0874
FR Citation
83 FR 23355

Applicability

TypeManufacturerModelDetails
aircraft Sikorsky Various Airworthiness Directives; Sikorsky Aircraft Corporation

Unsafe Condition

Wear of the engine collective position transducer (CPT) has resulted in several One Engine Inoperative (OEI) incidents.

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

Required Actions

Inspect the CPT by measuring resistance, linearity resistance movement, and differential voltage. Depending on the outcome of the inspections, replace the CPT.

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

Compliance Time

Within 50 flight hours

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

Affected Aircraft

Sikorsky Model S-76C helicopters with a Turbomeca, S.A., Arriel 2S1 or Arriel 2S2 engine with an engine CPT part number (P/N) 76900-01821-104 installed.

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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