Document ID: chunk:federal_register_of_legislation:F2006B09295:body:0
Version: federal_register_of_legislation:F2006B09295
Segment Type: other
Provision Reference: 
Character Range: 0–713

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

 Dornier DO-27 Series Aeroplanes

AD/DO-27/11 Wing Flap Position Selector 2/89

 Applicability: All models.

 Requirement: Action in accordance with Dornier Service Bulletin 1116-0000.

            Note: LBA AD 88-109 refers.

 Compliance: Prior to 1 March 1989.

            Note: Flight Manual to be amended to G1 status restricting maximum flap deflection to 35 degrees prior to 1 March 1989 unless accomplished previously.

            Background:  This modification is to improve the longitudinal controllability of the aircraft in the landing configuration.