AD 95-04-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 35-33 | Airworthiness Directives; Beech Aircraft Corporation 33, 35, and 36 Series Airplanes |
| aircraft | Textron Aviation Inc. | 35-A33 | Airworthiness Directives; Beech Aircraft Corporation 33, 35, and 36 Series Airplanes |
| aircraft | Textron Aviation Inc. | 35-B33 | Airworthiness Directives; Beech Aircraft Corporation 33, 35, and 36 Series Airplanes |
| aircraft | Textron Aviation Inc. | 35-C33 | Airworthiness Directives; Beech Aircraft Corporation 33, 35, and 36 Series Airplanes |
| aircraft | Textron Aviation Inc. | 35-C33A | Airworthiness Directives; Beech Aircraft Corporation 33, 35, and 36 Series Airplanes |
| aircraft | Textron Aviation Inc. | 36 | Airworthiness Directives; Beech Aircraft Corporation 33, 35, and 36 Series Airplanes |
| aircraft | Textron Aviation Inc. | A36 | Airworthiness Directives; Beech Aircraft Corporation 33, 35, and 36 Series Airplanes |
| aircraft | Textron Aviation Inc. | A36TC | Airworthiness Directives; Beech Aircraft Corporation 33, 35, and 36 Series Airplanes |
| aircraft | Textron Aviation Inc. | B36TC | Airworthiness Directives; Beech Aircraft Corporation 33, 35, and 36 Series Airplanes |
| aircraft | Textron Aviation Inc. | E33 | Airworthiness Directives; Beech Aircraft Corporation 33, 35, and 36 Series Airplanes |
Unsafe Condition
Cracks in the wing front spar carry-through frame structure could result in spar carry-through frame structure failure, leading to severe structural damage to the wing.
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Required Actions
Inspect the wing front spar carry-through frame (web) structure for cracks in accordance with Beech Service Bulletin No. 2360, repair or reinforce any cracked structure, and repeat inspections as specified.
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Compliance Time
Required initially with whichever of the following is applicable, and thereafter as indicated: Upon the accumulation of 1,500 hours time-in-service (TIS) or within the next 100 hours TIS after the effective date of this AD, whichever occurs later; within 500 hours TIS after the inspection required by superseded AD 92-08-07; or within 500 hours TIS after the last inspection required by AD 91-14-13.
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Affected Aircraft
Beech Aircraft Corporation models 35-33, 35-A33, 35-B33, 35-C33, E33, F33, G33 (serials CD-1 through CD-1304); 35-C33A, E33A, F33A (CE-1 through CE-1192); E33C, F33C (CJ-1 through CJ-179); H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B (D-4866 through D-10403); 36, A36 (E-1 through E-2397); A36TC, B36TC (EA-1 through EA-471).
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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