AD 2000-26-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | British | Aerospace (Jetstream) Model 4101 | Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes |
Unsafe Condition
Fatigue cracking of certain structural elements could adversely affect the structural integrity of these airplanes.
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Required Actions
Within 30 days after the effective date, revise the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness by incorporating Section 05-10-10, 'Airworthiness Limitations Description and Operation,' dated July 15, 1999, of the British Aerospace J41 Aircraft Maintenance Manual (AMM). No alternative inspections or intervals may be approved for the specified structural elements after this revision.
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Compliance Time
Within 30 days after the effective date of February 7, 2001.
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Affected Aircraft
All British Aerospace (Jetstream) Model 4101 airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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