AD Amdt-39-15016
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Raytheon | Various | Airworthiness Directives; Raytheon Aircraft Company Beech Models 45 (YT-34), A45 (T-34A, B-45), and D45 (T-34B) Airplanes |
Unsafe Condition
Failure of the front and/or rear horizontal stabilizer spars caused by fatigue cracks.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the front and rear horizontal stabilizer spars using the surface eddy current method. Replace any stabilizer found cracked prior to further flight. Continue repetitive inspections at intervals not exceeding 500 hours time-in-service (TIS).
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Compliance Time
Within 30 days after April 16, 2007, or as specified in the compliance schedule based on previous inspections.
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Affected Aircraft
Raytheon Aircraft Company Beech Models 45 (YT-34), A45 (T-34A, B-45), and D45 (T-34B) airplanes, all serial numbers.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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