AD 99-19-35

final rule
Data completeness: 70%

Airworthiness Directives; British Aerospace BAe Model ATP Airplanes

AD Number
99-19-35
Status
final_rule
Effective Date
Product Category
aircraft
Docket
98-NM-344-AD
FR Citation
Federal Register: September 22, 1999 (Volume 64, Number 183)

Applicability

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

Unsafe Condition

Nose wheel shimmy, which could lead to the collapse of the nose landing gear during landing.

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

Required Actions

Perform a test for the serviceability of the nose landing gear compensator within 250 flight cycles after the effective date. Repeat the test at intervals not exceeding 4,000 flight cycles. Replace the compensator within 50 flight cycles if it fails the test.

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

Compliance Time

Within 250 flight cycles after the effective date

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

Affected Aircraft

All BAe Model ATP airplanes, certificated in any category.

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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