AD Amdt-39-10974
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | British | Aerospace Jetstream Model 3101 | Airworthiness Directives; British Aerospace Jetstream Model 3101 Airplanes |
Unsafe Condition
A strength deficiency exists in the area of the lower fuselage skin panels between the main and rear spar frames (Frame Stations 223 and 257.8), which could result in reduced or loss of control of the airplane during maximum speed limit operations.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install additional stringers at the lower fuselage skin panels between the main and rear spar frames (Frame Stations 223 and 257.8) in accordance with British Aerospace Jetstream Service Bulletin 53-JM7297, Original Issue: May 10, 1984.
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 3101 airplanes, constructors numbers 601 through 607 and 609 through 619, 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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.