Document ID: chunk:federal_register_of_legislation:F2006L02522:body:0:p1
Version: federal_register_of_legislation:F2006L02522
Segment Type: other
Provision Reference: 
Character Range: 0–3476

AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.001(1) of CASR 1998.  The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Beechcraft 200 (Super King Air) Series Aeroplanes
AD/BEECH 200/73  Main Landing Gear Actuator Nut  9/2006

Applicability:  Main Landing Gear (MLG) Actuator nut assembly, part number (P/N)
                GMD115-810029-17 or P/N GMD115-810029-23, for the right MLG actuator installed on, but not limited to, the following Raytheon Aircraft Company (Raytheon) (formerly Beech) aeroplanes that are not equipped with a hydraulic MLG or modified to a hydraulic MLG.
                Models            Serial Nos.
                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).
                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).
                200T and B200T     BT-1 through BT-30 (except aircraft that incorporate Beech Kit No. 101-8018).
                200C and B200C     BL-1 through BL-72 (except aircraft that incorporate Beech Kit No. 101-8018).
                200CT and B200CT   BN-1 through BN-4 (except aircraft that incorporate Beech Kit No. 101-8018).
                A200CT (FWC–12D)   FG-1 and FG-2 (except aircraft that incorporate Beech Kit No. 101-8018).

Requirement:     1. 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.

                 2. If you find as a result of the check required by requirement 1 of this AD that there is no record of the specified assembly replacement, inspect the aeroplane, in accordance with General Machine Diecron Inc. Service Bulletin GM-D
                 32-30-01/102505 dated 21 November 2005, for installation of the following:

                   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.

              You may choose to do the inspection detailed in requirement 2 of this AD without doing the maintenance records check detailed in requirement 1 of this AD.

                 3. If during the check required by requirement 1 or the inspection required by requirement 2 of this AD, you find either actuator nut assembly, P/N
                 GMD115-810029-17 or P/N