AD Amdt-39-9387

final rule
Data completeness: 70%

Airworthiness Directives; Schweizer Aircraft Corporation and Hughes Helicopters, Inc. Model 269A, 269A-1, 269B, 269C, and TH-55A Helicopters

AD Number
Amdt-39-9387
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 94-SW-02-AD
FR Citation
60 FR 53265

Applicability

TypeManufacturerModelDetails
aircraft Schweizer Various Airworthiness Directives; Schweizer Aircraft Corporation and Hughes Helicopters, Inc. Model 269A, 269A-1, 269B, 269C, and TH-55A Helicopters

Unsafe Condition

Structural failure of the main rotor (M/R) drive shaft, separation of the M/R from the helicopter, 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

Conduct one-time radiographic inspection or other non-destructive inspection of certain main rotor drive shafts for cracks, distortion, corrosion, or other surface damage. Expand inspections to additional models and exclude certain drive shafts from specific inspections based on the AD's revised applicability.

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

Affected Aircraft

Schweizer Aircraft Corporation and Hughes Helicopters, Inc. Model 269A, 269A-1, 269B, 269C, and TH-55A helicopters with certain main rotor drive shafts 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

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