AD 98-21-35
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 200T | Airworthiness Directives; Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes |
| aircraft | Textron Aviation Inc. | 300 | Airworthiness Directives; Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (C-12D) | Airworthiness Directives; Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (C-12F) | Airworthiness Directives; Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (RC-12H) | Airworthiness Directives; Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (RC-12K) | Airworthiness Directives; Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (RC-12P) | Airworthiness Directives; Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes |
| aircraft | Textron Aviation Inc. | A200CT (RC-12Q) | Airworthiness Directives; Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes |
| aircraft | Textron Aviation Inc. | B200 | Airworthiness Directives; Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes |
| aircraft | Textron Aviation Inc. | B200C | Airworthiness Directives; Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes |
Unsafe Condition
Failure of the actuator clevis assembly in the main landing gear caused by fatigue cracking of the original design part, which could result in loss of control of the airplane during landing operations.
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Required Actions
Replace the left and right main landing gear actuator clevis assembly with a new assembly of improved design in accordance with Raytheon Aircraft Mandatory Service Bulletin No. 2728, Revision No. 1. Special flight permits may be issued to operate the airplane to a location where the requirements can be accomplished.
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Compliance Time
within the next 200 hours time-in-service (TIS) after the effective date of this AD
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Affected Aircraft
Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C airplanes with specific serial numbers listed in the applicability section.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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