AD 98-07-01

final rule
Data completeness: 70%

Airworthiness Directives; British Aerospace BAe Model ATP Airplanes

AD Number
98-07-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
94-NM-212-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft BAE Systems (Operations) Limited ATP Airworthiness Directives; British Aerospace BAe Model ATP Airplanes

Unsafe Condition

Failure of the engine power cables could cause loss of function of the power control levers on the console and subsequent loss of normal control of engine power.

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

Required Actions

Perform a detailed visual inspection and tests for damage of the engine power cables in accordance with Jetstream Service Bulletin ATP-76-16. Replace any damaged cable with a new cable. The inspection must be repeated at intervals not exceeding 1,000 landings, unless modified to 5,000 landings by installing the pulley assembly modification per ATP-76-18.

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

Compliance Time

Required as indicated, unless accomplished previously. The initial inspection must be done by the earlier of 1,000 total landings on the engine power cable or within 200 landings after the effective date of this AD, whichever occurs later, and within 75 days after the effective date. Replacement of damaged cables must be done prior to further flight.

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

Affected Aircraft

BAE Systems (Operations) Limited Model ATP airplanes, constructor's numbers 2002 through 2063 inclusive.

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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