AD Amdt-39-10090

Recurring final rule
Data completeness: 70%

Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes

AD Number
Amdt-39-10090
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 97-NM-137-AD
FR Citation
62 FR 40267

Applicability

TypeManufacturerModelDetails
aircraft British Aerospace (Jetstream) Model 4101 Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes

Unsafe Condition

Fatigue cracking in the roller guide shear cleats of the passenger door could result in structural failure of the passenger door and consequent rapid depressurization or loss of the door during flight.

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

Required Actions

Conduct repetitive detailed visual inspections to detect cracks in the shear cleats of the roller guide structural support of the passenger door. Replace any cracked shear cleat with a new one. An optional terminating modification is available to cease repetitive inspections.

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

Compliance Time

Before further flight

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

Affected Aircraft

British Aerospace (Jetstream) Model 4101 airplanes with the affected passenger door configuration.

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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