AD Amdt-39-11258

final rule
Data completeness: 70%

Airworthiness Directives; Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, 269C-1, and 269D Helicopters

AD Number
Amdt-39-11258
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 99-SW-31-AD
FR Citation
64 FR 44823

Applicability

TypeManufacturerModelDetails
aircraft Schweizer Various Airworthiness Directives; Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, 269C-1, and 269D Helicopters

Unsafe Condition

Undersized tail rotor swashplate shaft nut looseness and potential undersized shafts could lead to shaft failure 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 tail rotor swashplate shaft nut for looseness. If loose, inspect the shaft for proper size. Inspect all shafts not previously inspected. Replace any undersized shafts prior to further flight.

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

Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, 269C-1, and 269D helicopters.

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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