AD 75-24-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | A45 (Military T-34A, B-45) | Airworthiness Directives; BEECH Models A45 (Military T-34A, B-45) and D45 (Military T-34B) Airplanes |
| aircraft | Textron Aviation Inc. | D45 (Military T-34B) | Airworthiness Directives; BEECH Models A45 (Military T-34A, B-45) and D45 (Military T-34B) Airplanes |
Unsafe Condition
Failure of the P/N 45-524504 and 45-524505 rudder-aileron bungee interconnect cable assemblies and the P/N 45-524697 or P/N 45-524028 bellcrank assemblies due to frayed, internally broken, excessively worn cables, elongation exceeding 0.02 inches, or cracks in the bellcrank holes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Disconnect and visually inspect the rudder-aileron bungee interconnect cable assemblies, replacing frayed, internally broken, or excessively worn cables. Disconnect AN 161-8RS forks from the bellcrank assembly, inspect for elongation or cracks, replace the bellcrank if elongation exceeds 0.02 inches or cracks are found, and lubricate holes prior to reinstallation. Compliance intervals depend on pulley and bushing part numbers.
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Compliance Time
Within 50 hours' time in service after the effective date (November 28, 1975), and thereafter at intervals not exceeding 100 or 300 hours' time in service depending on configuration.
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Affected Aircraft
BEECH Models A45 (Military T-34A, B-45) and D45 (Military 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 8, 2026
Rights: U.S. Government Public Domain
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