AD 93-24-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 35-33 | Airworthiness Directives; Beech Models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33, 35-C33A, E33A, F33A, E33C, F33C, 36, A36, A36TC and B36TC Airplanes |
| aircraft | Textron Aviation Inc. | 35-A33 | Airworthiness Directives; Beech Models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33, 35-C33A, E33A, F33A, E33C, F33C, 36, A36, A36TC and B36TC Airplanes |
| aircraft | Textron Aviation Inc. | 35-B33 | Airworthiness Directives; Beech Models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33, 35-C33A, E33A, F33A, E33C, F33C, 36, A36, A36TC and B36TC Airplanes |
| aircraft | Textron Aviation Inc. | 35-C33 | Airworthiness Directives; Beech Models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33, 35-C33A, E33A, F33A, E33C, F33C, 36, A36, A36TC and B36TC Airplanes |
| aircraft | Textron Aviation Inc. | 35-C33A | Airworthiness Directives; Beech Models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33, 35-C33A, E33A, F33A, E33C, F33C, 36, A36, A36TC and B36TC Airplanes |
| aircraft | Textron Aviation Inc. | 36 | Airworthiness Directives; Beech Models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33, 35-C33A, E33A, F33A, E33C, F33C, 36, A36, A36TC and B36TC Airplanes |
| aircraft | Textron Aviation Inc. | A36 | Airworthiness Directives; Beech Models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33, 35-C33A, E33A, F33A, E33C, F33C, 36, A36, A36TC and B36TC Airplanes |
| aircraft | Textron Aviation Inc. | A36TC | Airworthiness Directives; Beech Models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33, 35-C33A, E33A, F33A, E33C, F33C, 36, A36, A36TC and B36TC Airplanes |
| aircraft | Textron Aviation Inc. | B36TC | Airworthiness Directives; Beech Models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33, 35-C33A, E33A, F33A, E33C, F33C, 36, A36, A36TC and B36TC Airplanes |
| aircraft | Textron Aviation Inc. | E33 | Airworthiness Directives; Beech Models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33, 35-C33A, E33A, F33A, E33C, F33C, 36, A36, A36TC and B36TC Airplanes |
Unsafe Condition
Separation of the rudder from the airplane caused by cracks in the forward rudder spar.
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Required Actions
Inspect the rudder forward spar for cracks within 100 hours time-in-service or at 1,000 hours time-in-service, whichever occurs later. If cracks are found, replace the rudder assembly or install specified kits and brackets. If no cracks, reinspect at intervals not exceeding 500 hours TIS or install specified modifications.
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Compliance Time
Required as indicated after the effective date of this AD, unless already accomplished.
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Affected Aircraft
Beech Models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33 (CD-1 through CD-1304); 35-C33A, E33A, F33A (CE-1 through CE-1425); E33C, F33C (CJ-1 through CJ-179); 36, A36 (E-1 through E-2518); A36TC, B36TC (EA-1 through EA-500).
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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