AD 89-05-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 35 | Airworthiness Directives; Beech Model 35-33, 35-A33, 35-B33, 35-C33, E33, 35-C33A, E33A, E33C, 35, 35R, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35-TC, V35A, V35A-TC, 36, 95-55, 95-A55, 95-B55, 95-B55A, 95-C55, 95-C55A, D55, D55A, 56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 35-33 | Airworthiness Directives; Beech Model 35-33, 35-A33, 35-B33, 35-C33, E33, 35-C33A, E33A, E33C, 35, 35R, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35-TC, V35A, V35A-TC, 36, 95-55, 95-A55, 95-B55, 95-B55A, 95-C55, 95-C55A, D55, D55A, 56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 35-A33 | Airworthiness Directives; Beech Model 35-33, 35-A33, 35-B33, 35-C33, E33, 35-C33A, E33A, E33C, 35, 35R, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35-TC, V35A, V35A-TC, 36, 95-55, 95-A55, 95-B55, 95-B55A, 95-C55, 95-C55A, D55, D55A, 56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 35-B33 | Airworthiness Directives; Beech Model 35-33, 35-A33, 35-B33, 35-C33, E33, 35-C33A, E33A, E33C, 35, 35R, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35-TC, V35A, V35A-TC, 36, 95-55, 95-A55, 95-B55, 95-B55A, 95-C55, 95-C55A, D55, D55A, 56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 35-C33 | Airworthiness Directives; Beech Model 35-33, 35-A33, 35-B33, 35-C33, E33, 35-C33A, E33A, E33C, 35, 35R, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35-TC, V35A, V35A-TC, 36, 95-55, 95-A55, 95-B55, 95-B55A, 95-C55, 95-C55A, D55, D55A, 56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 35-C33A | Airworthiness Directives; Beech Model 35-33, 35-A33, 35-B33, 35-C33, E33, 35-C33A, E33A, E33C, 35, 35R, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35-TC, V35A, V35A-TC, 36, 95-55, 95-A55, 95-B55, 95-B55A, 95-C55, 95-C55A, D55, D55A, 56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 35R | Airworthiness Directives; Beech Model 35-33, 35-A33, 35-B33, 35-C33, E33, 35-C33A, E33A, E33C, 35, 35R, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35-TC, V35A, V35A-TC, 36, 95-55, 95-A55, 95-B55, 95-B55A, 95-C55, 95-C55A, D55, D55A, 56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 36 | Airworthiness Directives; Beech Model 35-33, 35-A33, 35-B33, 35-C33, E33, 35-C33A, E33A, E33C, 35, 35R, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35-TC, V35A, V35A-TC, 36, 95-55, 95-A55, 95-B55, 95-B55A, 95-C55, 95-C55A, D55, D55A, 56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 45 (Military YT-34) | Airworthiness Directives; Beech Model 35-33, 35-A33, 35-B33, 35-C33, E33, 35-C33A, E33A, E33C, 35, 35R, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35-TC, V35A, V35A-TC, 36, 95-55, 95-A55, 95-B55, 95-B55A, 95-C55, 95-C55A, D55, D55A, 56TC, 95, B95, B95A, D95A and E95 Airplanes |
| aircraft | Textron Aviation Inc. | 56TC | Airworthiness Directives; Beech Model 35-33, 35-A33, 35-B33, 35-C33, E33, 35-C33A, E33A, E33C, 35, 35R, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35-TC, V35A, V35A-TC, 36, 95-55, 95-A55, 95-B55, 95-B55A, 95-C55, 95-C55A, D55, D55A, 56TC, 95, B95, B95A, D95A and E95 Airplanes |
Unsafe Condition
Failure of the magnesium elevator control fittings.
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Required Actions
Determine the composition of the elevator control fittings within 100 hours time-in-service after the effective date using Beech Service Bulletin No. 2242, Revision 1. If magnesium, visually inspect every 100 hours TIS for cracks. Replace cracked magnesium fittings with aluminum fittings before further flight. Inspections are no longer required once aluminum fittings are installed on both elevators.
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Compliance Time
Within 100 hours time-in-service after the effective date of this AD
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Affected Aircraft
Beech Models 35-33, 35-A33, 35-B33, 35-C33, E33 (CD-1-CD-1234); 35-C33A, E33A (CE-1-CE-289); E33C (CJ-1-CJ-25); 35, 35R, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35-TC, V35A, V35A-TC (D-1-D-9068, D-15001-D-15002); 36 (E-1-E-184); 95-55, 95-A55, 95-B55, 95-B55A (TC-1-TC-1287); 95-C55, 95-C55A, D55, D55A (TE-1-TE-767); 56TC (TG-2-TG-83); 95, B95, B95A, D95A, E95 (TD-2-TD-721); military models T34A, T34B, T42A modified for civil certification.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
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