AD Amdt-39-13496
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Raytheon | Various | Airworthiness Directives; Raytheon Aircraft Corporation Beech Models 45 (YT-34), A45 (T-34A, B-45), and D45 (T-34B) Airplanes |
Unsafe Condition
Fatigue cracks in the wing spar assemblies could lead to wing spar failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Repetitively inspect the wing spar assembly for cracks. Replace any wing spar assembly found cracked unless the spar assembly has a crack indication in the filler strip where the direction of the crack is toward the outside edge of the filler strip. Report the results of the initial inspection and maintain the flight and operating restrictions required by AD 99-12-02 until the initial inspection is completed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance time specified in the original AD 2001-13-18.
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Affected Aircraft
Raytheon Aircraft Corporation Beech Models 45 (YT-34), A45 (T-34A, B-45), and D45 (T-34B) 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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