Airworthiness Directive · Amendment 39-10843 · Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes
Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes
Airplane models listed below, certificated in any category. Model Serial No. B200.................................. BB-1158, BB-1167, BB-1193 through BB-1263, BB-1265 through BB-1286, BB-1287, BB- 1288, BB-1290 through BB-1300, BB-1302 through BB-1425, BB- 1427 through BB-1447, BB-1449, BB-1450, BB-1453, BB-1455, BB- 1456, and BB-1458 through BB- 1559. B200C................................. BL-124 through BL-140. B200CT (FW-II)........................ FG-1 and FG-2. B200T/B200T........................... BT-31 through BT-38. 300................................... FA-1 through FA-230 and FF-1 through FF-19. B300.................................. FL-1 through FL-159. B300C................................. FM-1 through FM-9 and FN-1. A200CT (C-12D)........................ BP-46 through BP-51. A200CT (C-12F)........................ BP-52 through BP-63. A200CT (RC-12K)....................... FE-1 through FE-9. A200CT (RC-12N)....................... FE-10 through FE-24. A200CT (RC-12P)....................... FE-25 through FE-31, FE-33, and FE-35. A200CT (RC-12Q)....................... FE-32, FE-34, and FE-36. B200C (C-12F)......................... BP-64 through BP-71, BL-73 through BL-112, and BL-118 through BL-123. B200C (UC-12F)........................ BU-1 through BU-10. B200CT (RC-12F)....................... BU-11 and BU-12. B200C (UC-12M)........................ BV-1 through BV-10. B200C (RC-12M)........................ BV-11 and BV-12. B200C (C-12R)......................... BW-1 through BW-29.
This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C airplanes. This AD requires replacing the main landing gear left and right actuator clevis assembly. Reports of main landing gear failure on two of the affected airplanes prompted this action. The actions specified by this AD are intended to prevent 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.
The aircraft, engines and makers this AD names, by the model designations in its text. A model listed here may still be outside the AD's serial ranges.
