AD 2002-01-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Raytheon | Aircraft Company Beech Models 65-90 | Airworthiness Directives; Raytheon Aircraft Company Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-4, B90, C90, C90A, E90, and H-90 Airplanes |
Unsafe Condition
Fatigue cracks in the main landing gear upper and lower torque knees could result in failure of the main landing gear, leading to loss of control during takeoff, landing, or ground operations.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Repetitively inspect the main landing gear upper and lower torque knees for fatigue cracks. Replace any torque knee with evidence of fatigue cracks.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
Raytheon Aircraft Company Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-4, B90, C90, C90A, E90, and H-90 airplanes.
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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