AD 94-11-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 400A | Airworthiness Directives; Beech Model 400A and 400T Airplanes |
| aircraft | Textron Aviation Inc. | 400T | Airworthiness Directives; Beech Model 400A and 400T Airplanes |
Unsafe Condition
Damage to the wire harness in the wheel well of the main landing gear (MLG) due to abrasion, which could cause loss of control of the fuel supply to the engine or loss of control of the retraction/extension system for the MLG and MLG door.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a general visual inspection of the MLG wire harness per Service Bulletin 2479, Revision 1. If damage is found, modify the wiring prior to further flight. Alternative methods of compliance may be approved by the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 200 hours time-in-service after the effective date of this AD (July 7, 1994).
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Affected Aircraft
Beech Model 400A (serial numbers RK-1 through RK-41) and Model 400T (serial numbers TT-2 through TT-19 inclusive).
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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