AD 89-05-02
final rule
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 |
| aircraft | Textron Aviation Inc. | 95 | 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. | 95-55 | 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. | 95-A55 | 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. | 95-B55 | 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. | 95-B55A | 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. | 95-B55B | 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. | 95-C55 | 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. | 95-C55A | 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. | A35 | 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. | A45 (Military T-34A, B-45) | 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. | B35 | 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. | B95 | 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. | B95A | 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. | C35 | 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. | D35 | 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. | D45 (Military T-34B) | 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. | D55 | 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. | D55A | 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. | D95A | 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. | E33 | 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. | E33A | 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. | E33C | 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. | E35 | 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. | E95 | 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. | F35 | 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. | G35 | 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. | H35 | 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. | J35 | 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. | K35 | 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. | M35 | 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. | N35 | 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. | P35 | 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. | S35 | 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. | V35 | 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. | V35A | 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.
AI-generated summary from the source AD text. Verify against the official source before acting.
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.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 100 hours time-in-service after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
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.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Elevator Control Fittings
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_89-05-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 89-05-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Beech Model 35-33, 35-A33, 35-B33, 35-C33, E33, 35-C33A, E33A, E33C, 35, ...Show more Subject: Elevator Control Fittings Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/24/1989 Make: Textron Aviation Inc. Model: 35 | 35-33 | 35-A33 | 35-B33 | 35-C33 | 35-C33A | 35R | 36 | 45 (Military YT-34) | 56TC | 95 | 95-55...Show more Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 89-05-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6144 AD NUMBER: 89-05-02 SUBJECT HEADING: 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 ACTION: SUMMARY: DATES: Effective March 24, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 89-05-02 BEECH: Amendment 39-6144. Applicability: The airplanes listed below, certificated in any category: MODELS SERIAL NUMBERS 35-33, 35-A33, 35-B33, 35-C33, E33 CD-1 through CD-1234 35-C33A, E33A CE-1 through CE-289 E33C CJ-1 through 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 through D-9068, D-15001 and D-15002 36 E-1 through E-184 95-55, 95-A55, 95-B55, 95-B55A TC-1 through TC-1287 95-C55, 95-C55A, D55, D55A TE-1 through TE-767 56TC TG-2 through TG-83 95, B95, B95A, D95A, E95 TD-2 through TD-721 This AD also applies to any of the following military airplanes which have been modified for civil certification as described on the applicable Federal Aviation Administration Type Certificate Data Sheet or Aviation Specification: T34A, T34B (Commercial Model 45 Series) T42A (Commercial Model 95-B55B) NOTE: The magnesium fittings may have been installed as original equipment or as replacement spares. Compliance: Required as indicated, unless already accomplished. To prevent the failure of the magnesium elevator control fittings, accomplish the following: (a) Within 100 hours time-in-service (TIS) after the effective date of this AD, determine the composition of the elevator control fittings in accordance with the instructions contained in Beech Service Bulletin No. 2242, Revision 1, dated August 1988. (1) If the fittings are determined to be aluminum, no further action is required by this AD. (2) If the fittings are determined to be magnesium, accomplish the actions specified below. (b) At the time of the inspection per paragraph (a), and every 100 hours TIS thereafter, visually inspect each magnesium elevator control fitting for cracks in accordance with the above referenced Service Bulletin. (c) If any fitting is found to be cracked, prior to further flight replace the cracked fitting with an aluminum fitting as described in the above referenced Service Bulletin. (d) The above inspections are no longer required when aluminum fittings have been installed on both elevators. (e) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished. (f) An equivalent means of compliance with this AD may be used if approved by the Manager, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209; Telephone (316) 946-4400. All persons affected by this directive may obtain copies of the documents referred to herein upon request to Beechcraft Aero and Aviation Centers; Beech Aircraft Corporation, Commercial Service, Dept. 52, P.O. Box 85, Wichita, Kansas 67201-0085, or may examine these documents at the FAA, Office of the Assistant Chief Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106. This amendment (39-6144, AD 89-05-02) becomes effective on March 24, 1989. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_89-05-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 89-05-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Beech Model 35-33, 35-A33, 35-B33, 35-C33, E33, 35-C33A, E33A, E33C, 35, ...Show more Subject: Elevator Control Fittings Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/24/1989 Make: Textron Aviation Inc. Model: 35 | 35-33 | 35-A33 | 35-B33 | 35-C33 | 35-C33A | 35R | 36 | 45 (Military YT-34) | 56TC | 95 | 95-55...Show more Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 89-05-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6144 AD NUMBER: 89-05-02 SUBJECT HEADING: 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 ACTION: SUMMARY: DATES: Effective March 24, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 89-05-02 BEECH: Amendment 39-6144. Applicability: The airplanes listed below, certificated in any category: MODELS SERIAL NUMBERS 35-33, 35-A33, 35-B33, 35-C33, E33 CD-1 through CD-1234 35-C33A, E33A CE-1 through CE-289 E33C CJ-1 through 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 through D-9068, D-15001 and D-15002 36 E-1 through E-184 95-55, 95-A55, 95-B55, 95-B55A TC-1 through TC-1287 95-C55, 95-C55A, D55, D55A TE-1 through TE-767 56TC TG-2 through TG-83 95, B95, B95A, D95A, E95 TD-2 through TD-721 This AD also applies to any of the following military airplanes which have been modified for civil certification as described on the applicable Federal Aviation Administration Type Certificate Data Sheet or Aviation Specification: T34A, T34B (Commercial Model 45 Series) T42A (Commercial Model 95-B55B) NOTE: The magnesium fittings may have been installed as original equipment or as replacement spares. Compliance: Required as indicated, unless already accomplished. To prevent the failure of the magnesium elevator control fittings, accomplish the following: (a) Within 100 hours time-in-service (TIS) after the effective date of this AD, determine the composition of the elevator control fittings in accordance with the instructions contained in Beech Service Bulletin No. 2242, Revision 1, dated August 1988. (1) If the fittings are determined to be aluminum, no further action is required by this AD. (2) If the fittings are determined to be magnesium, accomplish the actions specified below. (b) At the time of the inspection per paragraph (a), and every 100 hours TIS thereafter, visually inspect each magnesium elevator control fitting for cracks in accordance with the above referenced Service Bulletin. (c) If any fitting is found to be cracked, prior to further flight replace the cracked fitting with an aluminum fitting as described in the above referenced Service Bulletin. (d) The above inspections are no longer required when aluminum fittings have been installed on both elevators. (e) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished. (f) An equivalent means of compliance with this AD may be used if approved by the Manager, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209; Telephone (316) 946-4400. All persons affected by this directive may obtain copies of the documents referred to herein upon request to Beechcraft Aero and Aviation Centers; Beech Aircraft Corporation, Commercial Service, Dept. 52, P.O. Box 85, Wichita, Kansas 67201-0085, or may examine these documents at the FAA, Office of the Assistant Chief Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106. This amendment (39-6144, AD 89-05-02) becomes effective on March 24, 1989. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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