AD 75-16-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 56TC | Airworthiness Directives; BEECH Models 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 58, 58A, 56TC, A56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 58 | Airworthiness Directives; BEECH Models 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 58, 58A, 56TC, A56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 58A | Airworthiness Directives; BEECH Models 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 58, 58A, 56TC, A56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 95 | Airworthiness Directives; BEECH Models 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 58, 58A, 56TC, A56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 95-55 | Airworthiness Directives; BEECH Models 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 58, 58A, 56TC, A56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 95-A55 | Airworthiness Directives; BEECH Models 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 58, 58A, 56TC, A56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 95-B55 | Airworthiness Directives; BEECH Models 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 58, 58A, 56TC, A56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 95-B55A | Airworthiness Directives; BEECH Models 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 58, 58A, 56TC, A56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 95-B55B | Airworthiness Directives; BEECH Models 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 58, 58A, 56TC, A56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 95-C55 | Airworthiness Directives; BEECH Models 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 58, 58A, 56TC, A56TC, 95, B95, B95A, D95A and E95 Airplanes |
Unsafe Condition
Failure of elevator trim tab systems due to unairworthy conditions in elevator trim tab control rod assemblies, including eccentric reaming, wall thickness discrepancies, cracks, looseness of end fittings, bending, or rivet material incompatibility.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect elevator trim tab control rod configurations/part numbers and radiographically inspect tubes for eccentric reaming if specific part numbers are installed. Replace defective or non-compliant tubes and rivets with specified part numbers within the required timeframes. Log compliance details including date, method, and parts used.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within specified timeframes (25 or 100 hours time in service after the effective date of this AD, not later than October 15, 1975) unless previously accomplished.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Beech Models 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 58, 58A, 56TC, A56TC, 95, B95, B95A, D95A, E95 with specific serial ranges as listed in the AD.
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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