AD 2017-07-02

final rule
Data completeness: 70%

Airworthiness Directives; Sikorsky Aircraft Corporation Helicopters

AD Number
2017-07-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2016-9291
FR Citation
82 FR 15120

Applicability

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

Unsafe Condition

Failure of the engine side drive shaft due to loss of alignment between the lower pulley shaft and the engine output shaft, leading to fracture. Increased cyclic torsional loading inaccurately applied in previous fatigue analysis necessitates reduced life limits.

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

Required Actions

Remove from service any engine side drive shaft P/N SKCP2738-7 and pulley side drive shaft P/N SKCP2738-5 that has reached or exceeded its new life limit. Inspect drive shaft alignment and components for cracks, corrosion, pitting, nicks, dents, and scratches. Inspect bolted joints and frames for movement and fretting corrosion. Replace both drive shafts if any inspection fails. Inspect lower pulley to engine alignment and adjust as necessary.

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 269D and Model 269D Configuration A helicopters with KAflex drive shaft (engine side) P/N SKCP2738-7 and KAflex drive shaft (pulley side) P/N SKCP2738-5 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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.