AD 94-08-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | Jetstream Model 4101 | Airworthiness Directives; Jetstream Aircraft Limited Model 4101 Airplanes |
Unsafe Condition
Incorrectly manufactured trunnion pins in the main landing gear shock struts and drag braces may fail to break away during excessive landing loads, compromising wing fuel tank structural integrity and causing fuel spillage and fire hazard.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install new fusible trunnion pins in the main landing gear shock struts and drag braces per Service Bulletin J41-32-017 within 300 hours time-in-service after April 29, 1994. Prohibit installation of shock strut assemblies with part number AIR83072-8 and drag brace assemblies with part number AIR84352-2.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 300 hours time-in-service after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Jetstream Model 4101 airplanes with constructors numbers 41004 through 41027 inclusive
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.