Airworthiness directives › 95-02-17
AD 95-02-17 Airworthiness Directives; Beech Aircraft Corporation Model 1900D Airplanes
Makes named: beech. Models named: 1900D. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model 1900D airplanes, serial numbers UE-1 through UE-131, certificated in any category. 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 use the authority provided in paragraph (c) of this AD to request approval from the FAA. This approval may address either no action, if the current configuration eliminates the unsafe condition, or different actions necessary to address the unsafe condition described in this AD. Such a request should include an assessment of the effect of the changed configuration on the unsafe condition addressed by this AD. In no case does the presence of any modification, alteration, or repair remove any aircraft from the applicability of this AD.
Compliance
Required prior to further flight after the effective date of this AD, unless already accomplished. To prevent in-flight separation of the elevator trim tab control cable, which could lead to loss of control of the airplane, accomplish the following: (a) In accordance with Beech 1900D Maintenance Manual, part number 129-590000-15A11, Chapters 5-20-07, page 203; 6-40-00, page 3; 6-50-00, page 16; and 27-30-04, pages 202 and 203: (1) Remove access panel Number 333ATC, which is located on the top surface of the horizontal stabilizer, to gain access to the elevator trim tab cable, guides, and pulleys; (2) Inspect the cable routing to ensure that cables (at the left, right, and crossover pulleys) are correctly routed around the pulleys, within the cable guide pins, and are not contacting any structure; and (3) Replace any cable that is incorrectly routed (cable that does not meet the criteria above in paragraph (a)(2) of this AD) or is chafed. Note 2: The procedures listed in Beech Communique 1900D-112, dated January 1995, ``Inspection of Elevator Trim Tab Control Cables'', are similar to those included in this priority letter AD. Complying with all procedures in Beech Communique 1900D-112 is considered equivalent to the requirements of paragraphs (a)(1), (a)(2), and (a)(3) of this AD, and is considered ``unless already accomplished'' for this portion of the AD. Note 3: The compliance time specified in this AD takes precedence over that specified in Beech Communique 1900D-112, dated January 1995, ``Inspection of Elevator Trim Tab Control Cables''. (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 (ACO), FAA, 1801 Airport Road, 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 4: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita ACO. (d) Information that relates to this AD may be examined at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106. (e) This amendment (39-9184) becomes effective on April 17, 1995, to all persons except those persons to whom it was made immediately effective by priority letter AD 95-02-17, issued January 25, 1995, which contained the requirements of this amendment. Issued in Kansas City, Missouri, on March 24, 1995. Dwight A. Young, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 95-7784 Filed 3-29-95; 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