AD 68-26-01

final rule
Data completeness: 70%

Airworthiness Directives; Hughes Models 269A, 269A-1, 269A-2, and 269B Helicopter

AD Number
68-26-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Schweizer Aircraft Corporation 269A Airworthiness Directives; Hughes Models 269A, 269A-1, 269A-2, and 269B Helicopter
aircraft Schweizer Aircraft Corporation 269A-1 Airworthiness Directives; Hughes Models 269A, 269A-1, 269A-2, and 269B Helicopter
aircraft Schweizer Aircraft Corporation 269B Airworthiness Directives; Hughes Models 269A, 269A-1, 269A-2, and 269B Helicopter

Unsafe Condition

Failures of the lower coupling drive shaft (Hughes P/N 269A5504-3) or lower coupling drive shaft assembly (Hughes P/N 80-269A5504-5 or 269A5504-5) due to cracks.

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

Required Actions

Inspect the entire shaft per Hughes Service Information Notice No. N-55.1 or equivalent. Retire and replace shaft if cracks are found; identify the shaft if no cracks are found. Ensure inspection or identification is accomplished before installing replacement shafts.

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

Compliance Time

within 25 hours of helicopter operation after the effective date of this airworthiness directive

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

Affected Aircraft

Schweizer Aircraft Corporation Models 269A (Serial Nos. 0011 through 0893 except TH-55A), 269A-1 (Serial Nos. 0001 through 0041), 269A-2 (Serial Nos. 0001 and 0002), 269B (Series Nos. 0001 through 0359) with specified lower coupling drive shaft parts installed.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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