Document ID: chunk:federal_register_of_legislation:F2006B08358:body:0
Version: federal_register_of_legislation:F2006B08358
Segment Type: other
Provision Reference: 
Character Range: 0–974

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

 Cessna 400 Series Aeroplanes

AD/CESSNA 400/75 Horizontal Stabiliser Leading Edge Assembly
and Elevator Trim Tab Actuator - Replacement

 Applicability: All models 404 with S/Nos. 404-0001 to 404-0637.

             Requirement: 1. Modify the horizontal stabiliser by replacing the leading edge assembly in accordance with Cessna Service Kit SK404-31 as revised 23 June 1980.

10/80

             2. Modify the elevator trim system by replacing the trim tab actuator in accordance with Cessna Service Kit SK404-31 as revised 23 June 1980.

 Compliance: 1. Before 1 March 1981.

            2. Unless already accomplished, before 1 March 1981.

            Background:  These replacements will eliminate the RPM limitation and the recurring trim tab actuator screw replacement requirement of Cessna SIL ME80-2, Revision 2.