AD Amdt-39-10958
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | British | Aerospace (Jetstream) Model 4101 | Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes |
Unsafe Condition
Fatigue cracking in the shear cleats of the roller guide structural support of the passenger door, which could result in structural failure or loss of the passenger door, and consequent rapid depressurization of the airplane during flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the shear cleats of the roller guide structural support of the passenger door for cracks, replace any cracked shear cleat as specified, and modify the passenger door (Modification No. JM41576) at all four roller guide locations in accordance with Jetstream Service Bulletin J41-52-050.
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Compliance Time
Within 4,000 landings or 2 years after accomplishment of the initial inspection, or within 6 months after the effective date of this AD.
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Affected Aircraft
British Aerospace (Jetstream) Model 4101 airplanes, constructor's numbers 41004 through 41099 inclusive, 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 6, 2026
Rights: U.S. Government Public Domain
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