AD/PA-31/119 - Aileron Control System
1AD/PA-31/119 - Aileron Control System
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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 Piper PA-31 Series Aeroplanes
AD/PA-31/119 Aileron Control System 4/93
Applicability: Model PA-31 Series.
Requirement: Colour code the aileron balance cable and the bellcrank lug of both aileron control systems with red enamel paint in accordance with Figure 1 of this Directive.
Note: FAA AD 92-27-05 Amdt 39-8438 refers.
Compliance: The next time the aileron cables are disconnected for any reason or prior to 1 April 1994, whichever occurs first.
Background: The FAA has received several reports of improper connections of the aileron control systems on the affected aircraft.
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES