AD 71-24-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 35-C33 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 35-C33A | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 36 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 56TC | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 58 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 95-B55 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 95-B55A | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 95-C55 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 95-C55A | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | A36 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
Unsafe Condition
Failure of control wheel adapters not stamped with two Beech inspection stamps could result in control wheel detachment during flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Ascertain two Beech inspection stamps on one tip of each control wheel adapter. Replace adapters without stamps with specified part numbers or equivalent approved parts.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 50 hours' time in service after August 1, 1973, for airplanes not complying with AD 71-12-04, or within 300 hours' time in service after August 1, 1973, for those that do comply with AD 71-12-04
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35A, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 with specified serial ranges, and models with P/N 60-524080 series control wheels including clock and light provisions.
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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