AD 2006-12-25 Airworthiness Directives; General Machine-Diecron, Inc. Actuator Nut Assembly for the Right Main Landing Gear Installed on Certain Raytheon Aircraft Company (Formerly Beech) Airplanes

Makes named: beech, raytheon. Read the applicability below — it usually turns on serial or part numbers too.

This AD affects any actuator nut assembly, part number (P/N) GMD115-810029-17 or P/N GMD115-810029-23, for the right main landing gear (MLG) actuator installed on, but not limited to, the following Raytheon Aircraft Company (Raytheon) (formerly Beech) airplanes that are certificated in any category and not equipped with a hydraulic MLG or modified to a hydraulic MLG.   Models Serial Nos. (1) F90 LA-2 through LA-225 (except aircraft that incorporate Beech Kit No. 90-8011). (2) 99, 99A, A99, and B99 U-1 through U-49 and U51 through U164 (except aircraft that incorporate Beech Kit No. 99-8010-1 or factory installed hydraulic landing gear). (3) 100 and A100 B-1 through B-94, B-100 through B-204, and B-206 through B-247. (4) B100 BE-1 through BE-137. (5) 200 BB-2, BB-6 through BB-733, BB-735 through BB-792, BB-794 through BB-828, BB-830 through BB-853, BB-872, BB-873, BB-892, BB-893, and BB-912 (except aircraft that incorporate Beech Kit No. 101-8018). (6) B200 BB-734, BB-793, BB-829, BB-854 through BB-870, BB-874 through BB-891, BB-894, BB-896 through BB-911, BB-913 through BB-1157, BB-1159 through BB-1166, and BB-1168 through BB-1192 (except aircraft that incorporate Beech Kit No. 101-8018). (7) 200T and B200T BT-1 through BT-30 (except aircraft that incorporate Beech Kit No. 101-8018). (8) 200C and B200C BL-1 through BL-72 (except aircraft that incorporate Beech Kit No. 101-8018). (9) 200CT and B200CT BN-1 through BN-4 (except aircraft that incorporate Beech Kit No. 101-8018). (10) A200CT (FWC-12D) FG-1 and FG-2 (except aircraft that incorporate Beech Kit No. 101-8018).

To address this problem, you must do the following:   Actions Compliance Procedures (1) Maintenance Records Check: (i) Check the maintenance records to determine whether the following replacements have been made: (A) Actuator nut assembly, P/N GMD115-810029-17, for the right MLG actuator; or (B) Actuator nut assembly, P/N GMD115-810029-23, for the right MLG actuator. (ii) The owner/operator holding at least a private pilot certificate as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7) may make this check. You must make an entry into the aircraft records that shows compliance with this portion of the AD in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). Within the next 50 hours time-in-service (TIS) or 30 calendar days after July 28, 2006 (the effective date of this AD), whichever occurs first, unless already done No special procedures necessary to check the maintenance records. (2) If you find as a result of the check required by paragraph (e)(1) of this AD that there is no record of the specified assembly replacement, inspect the airplane for installation of the following: (i) Actuator nut assembly, P/N GMD115-810029-17, for the right MLG actuator; or (ii) Actuator nut assembly, P/N GMD115-810029-23, for the right MLG actuator. (iii) You may choose to do the inspection without doing the maintenance records check. Within the next 50 hours TIS or 30 calendar days after July 28, 2006 (the effective date of this AD), whichever occurs first, unless already done Follow General Machine Diecron, Inc. Service Bulletin GM-D 32-30-01/102505, dated November 21, 2005. (3) If during the check required by paragraph (e)(1) or the inspection required by paragraph (e)(2) of this AD, you find either actuator nut assembly, P/N GMD115-810029-17 or P/N GMD115-810029-23, for the right MLG actuator, replace the specific assembly, with a new actuator nut assembly, P/N GMD115-810029-23B or FAA-approved equivalent P/N Before further flight after the check required by paragraph (e)(1) or the inspection required by paragraph (e)(2) of this AD Follow General Machine Diecron, Inc. Service Bulletin GM-D 32-30-01/102505, dated November 21, 2005. (4) Do not install any actuator nut assembly, P/N GMD115-810029-17 or P/N GMD115-810029-23, for the right MLG actuator As of July 28, 2006 (the effective date of this AD) Not Applicable. Alternative Methods of Compliance (AMOCs) (f) The Manager, Atlanta Aircraft Certification Office (ACO), FAA, ATTN: Don Buckley, Aerospace Engineer, FAA, Atlanta ACO, Airframe and Propulsion Branch, ACE-117A, One Crown Center, 1895 Phoenix Boulevard, Suite 450, Atlanta, Georgia 30337-2748, telephone: (770) 703-6086; facsimile: (770) 703-6097, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Material Incorporated by Reference (g) You must do the actions required by this AD following the instructions in General Machine Diecron, Inc. Service Bulletin GM-D 32-30-01/102505, dated November 21, 2005. The Director of the Federal Register approved the incorporation by reference of this service bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. To get a copy of this service information, contact General Machine—Diecron, Inc., 3131 U.S. Highway 41, Griffin, Georgia 30224, telephone: (770) 228-6200; facsimile: (770) 228-6299. To review copies of this service information, go to the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html or call (202) 741-6030. To view the AD docket, go to the Docket Management Facility; U.S. Department of Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, Washington, DC 20590-001 or on the Internet at http://dms.dot.gov. The docket number is FAA-2005-23334; Directorate Identifier 2005-CE-53-AD. Issued in Kansas City, Missouri, on June 9, 2006. James E. Jackson, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 06-5429 Filed 6-15-06; 8:45 am] BILLING CODE 4910-13-P

This AD results from several reports of failures of the actuator nut assembly, P/N GMD115-810029-17 and P/N GMD115-810029-23, on the right MLG actuator. The actions specified in this AD are intended to prevent failure of the actuator nut assembly for the right MLG actuator, which could result in failure of the MLG. This failure could prevent the extension or retraction of the MLG.