AD Amdt-39-10241
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | British | Aerospace (Jetstream) Model 4101 | Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes |
Unsafe Condition
Separation of the tailplane (horizontal stabilizer) from the fin, which could lead to reduced controllability of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a one-time inspection of the attachment bolts and surrounding area of the horizontal stabilizer leading edges for discrepancies in accordance with Jetstream Service Bulletin J41-55-002, Revision 1. If any discrepancy is found, correct the discrepancy prior to further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 3,000 hours time-in-service or 11 months after the effective date of this AD, whichever occurs first.
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Affected Aircraft
Jetstream Model 4101 airplanes, constructors numbers 41005 through 41069 inclusive, and 41071 through 41078 inclusive.
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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