Document ID: chunk:federal_register_of_legislation:F2006B03901:body:0
Version: federal_register_of_legislation:F2006B03901
Segment Type: other
Provision Reference: 
Character Range: 0–1972

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

 Beechcraft 36 (Bonanza) Series Aeroplanes

                          AD/BEECH 36/45 Inspection for Flight Control Interference with Wiring

 Applicability: This Directive is applicable to the following aircraft:

            Model Serial Numbers

7/99 DM

                    A36  E-3058 through E-3156 inclusive, E-3158 through E-3170 inclusive, E-3172 through E-3177 inclusive, E-3180 through E-3185 inclusive, E-3187 through E-3198 inclusive, E-3200 and E-3202.

                    B36TC  EA-594 through EA-610 inclusive, EA-613, EA-615, EA-616, EA-618, EA-619 and EA-621.

 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.