AD 93-01-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 400A | BEECH Model 400A Series Airplanes |
| aircraft | Textron Aviation Inc. | 400T | BEECH Model 400A Series Airplanes |
Unsafe Condition
Snagging of the end clevis fitting and kinking of the emergency release cable of the main landing gear, which may prevent extension of the main landing gear.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the existing link assembly from the uplink mechanism of the main landing gear door with an improved link assembly per Beechcraft Service Bulletin 2447 dated June 1992. Alternative methods of compliance or adjustments to compliance time may be approved by the Manager, Wichita Aircraft Certification Office. Special flight permits may be issued under FAR 21.197 and 21.199 to operate to a location where AD requirements can be met.
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Compliance Time
Within 100 flight hours after the effective date of this AD
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Affected Aircraft
BEECH Model 400A series airplanes with serial numbers RK-1 through RK-32; Model 400T series with serial numbers TT-1 through TT-6
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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