Document ID: chunk:federal_register_of_legislation:F2006B03715:body:0
Version: federal_register_of_legislation:F2006B03715
Segment Type: other
Provision Reference: 
Character Range: 0–1793

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Beechcraft 200 (Super King Air) Series Aeroplanes

 AD/BEECH 200/62 Inspection for Flight Control
                          Interference with Wiring

 Applicability: This Directive is applicable to the following aircraft

            Model Serial Numbers

7/99 DM

                  B200 BB-1551 through BB-1591 inclusive, BB-1593 through BB-1622 inclusive, and BB-1624 through BB-1627 inclusive.

 Requirement: Unless previously accomplished;

              1. Inspect for interference or inadequate clearance between the flight control mechanism and any component located forward of the instrument in accordance with Raytheon Mandatory Service Bulletin (SB) 27-3232 dated March 1999.

2.    If interference or inadequate clearance is found during the Requirement 1 inspection then secure all components clear of the flight control mechanisms in accordance with SB 27-3232.

            Note 1. If Raytheon Safety Communiqué No 149 dated August 1998 or No 149 Rev 1 dated November 1998 has been carried out no further action is required.

            Note 2. FAA AD 99-09-15 refers.

 Compliance: 1. Within 25 hours time in service after 19 May 1999.

            2. Prior to further flight after inspection.

            This Airworthiness Directive becomes effective on 19 May 1999.

            Background: There has been a reported incident were a Raytheon Beech Model 1900 aeroplane temporarily lost aileron and elevator control when the control column became restricted. Upon investigation the cause was found to be electrical/avionics wiring located forward of the instrument panel entangled in the flight control system "T" column.