AD/PA-32/15 Amdt 2 - Rudder Trim Arm Assembly Cracking
1AD/PA-32/15 Amdt 2 - Rudder Trim Arm Assembly Cracking
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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-32 (Cherokee Six) Series Aeroplanes
AD/PA-32/15
Amdt 2
Applicability: All models.
Rudder Trim Arm Assembly Cracking 12/85
Requirement: Inspect the rudder trim arm assembly for cracking at or near the rudder pedal bar attachment bolt.
Compliance: Within 100 hours time in service after 29 September 1969 and thereafter at each issue of a new Maintenance Release.
Background: This amendment revises the compliance requirements to coincide with varying periodic inspection intervals.