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Airworthiness directives › 98-21-35

AD 98-21-35 Airworthiness Directives; Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes

1998-11-23
1998-10-16
39-10843
97-CE-148-AD
Airframe
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Makes named: raytheon. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

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. ------------------------------------------------------------------------ Note 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (c) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.

Compliance

Required within the next 200 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished. 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, accomplish the following: (a) Replace the left and right main landing gear (MLG) actuator clevis assembly with a new MLG actuator clevis assembly of improved design in accordance with the Accomplishment Instructions section in Raytheon Aircraft Mandatory Service Bulletin No. 2728, Issued: June, 1997, Revision No. 1, February, 1998. (b) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. (c) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be approved by the Manager, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Wichita, Kansas 67209. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Wichita Aircraft Certification Office. Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita Aircraft Certification Office. (d) The replacements required by this AD shall be done in accordance with Raytheon Aircraft Mandatory Service Bulletin No. 2728, Issued: June, 1997, Revision No. 1, February, 1998. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from the Raytheon Aircraft Company, P.O. Box 85, Wichita, Kansas 67201-0085. Copies may be inspected at the FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW, suite 700, Washington, DC. [[Page 55530]] (e) This amendment becomes effective on November 23, 1998. Issued in Kansas City, Missouri, on October 7, 1998. Marvin R. Nuss, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 98-27604 Filed 10-15-98; 8:45 am] BILLING CODE 4910-13-U

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1