Airworthiness directives › 99-09-15
AD 99-09-15 Airworthiness Directive; Raytheon Aircraft Company Beech Models A36, B36TC, 58, 58A, C90A, B200, B300, and 1900D Airplanes
Makes named: beech, raytheon. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
The following Beech airplane models and serial numbers, certificated in any category: ------------------------------------------------------------------------ Model Serial Nos. ------------------------------------------------------------------------ A36.......................... E-3058 through E-3156, E-3158 through E- 3170, E-3172 through E-3177, E-3180 through E-3185, E-3187 through E-3198, E- 3200, and E-3202. B36TC........................ EA-594 through EA-610, EA-613, EA-615, EA- 616, EA-618, EA-619, and EA-621. 58 and 58A................... TH-1806 through TH-1840, TH-1842 through TH-1854, TH-1856, TH-1860 through TH- 1867, and TH-1870. C90A......................... LJ-1459 through LJ-1504, LJ-1506 through LJ-1523, and LJ-1525 through LJ-1530. B200......................... BB-1551 through BB-1591, BB-1593 through BB-1622, and BB-1624 through BB-1627. B300......................... FL-152 through FL-179, FL-181 through FL- 187, FL-189, FL-190, FL-192, FL-194, FL- 196 through FL-205, FL-207, FL-210, and FL-211. 1900D........................ UE-1 through UE-319, UE-321, UE-323 through UE-328, UE-330 and UE-332. ------------------------------------------------------------------------ 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 (e) 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 as indicated in the body of this AD, unless already accomplished. To prevent any components or wiring from interfering with the flight control mechanism caused by inadequate clearance, which could result in reduced or loss of aileron and/or elevator control, accomplish the following: (a) Within the next 25 hours time-in-service after the effective date of this AD, inspect for interference or inadequate clearance between the flight control mechanism and any component located forward of the instrument panel. Perform this action in accordance with the Accomplishment Instructions in Raytheon Mandatory Service Bulletin SB 27-3232, Issued: March, 1999. (b) If interference or inadequate clearance is found during the inspection required by paragraph (a) of this AD, prior to further flight, secure all components clear of the flight control mechanism as specified in the service bulletin. (c) If the actions required in paragraphs (a) and (b) of this AD have been accomplished in accordance with Raytheon Safety Communique No. 149, Rev. 1, dated November 1998, or Raytheon Safety Communique No. 149, dated August 1998, then no further action is required by this AD. (d) 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. (e) An alternative method of compliance or adjustment of the compliance times that provides an equivalent level of safety may be approved by the Manager, Wichita Aircraft Certification Office (ACO), 1801 Airport Road, Room 100, Mid-Continent Airport, 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 ACO. Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita ACO. (f) The inspection and modification required by this AD shall be done in accordance with Raytheon Mandatory Service Bulletin SB 27- 3232, Issued: March, 1999. 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. (g) This amendment becomes effective on May 18, 1999. Issued in Kansas City, Missouri, on April 19, 1999. James E. Jackson, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 99-10314 Filed 4-27-99; 8:45 am] BILLING CODE 4910-13-P
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You just looked this one up by hand
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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