AD 98-14-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | ATP | Airworthiness Directives; British Aerospace BAe Model ATP Airplanes |
Unsafe Condition
Failure of the spring strut assembly of the forward door of the main landing gear (MLG), which could result in inability to extend the MLG.
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Required Actions
Perform a visual inspection for discrepancies of the fork end of the spring strut assembly within 600 flight hours after the effective date. If discrepancies are found, replace the spring strut assembly with a new or serviceable part before further flight. Repeat inspections every 1,500 flight hours until the improved spring strut assembly is installed via Service Bulletin ATP-32-87 within 18 months after the effective date.
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Compliance Time
Within 600 flight hours after the effective date of this AD, and within 18 months after the effective date for the replacement.
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Affected Aircraft
BAE Systems (Operations) Limited Model ATP airplanes listed in British Aerospace Alert Service Bulletin ATP-32-85, Revision 1, dated March 20, 1998, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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