AD/DO-27/11 - Wing Flap Position Selector
1AD/DO-27/11 - Wing Flap Position Selector
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.