AD/PA-32/34 Amdt 1 - Main Landing Gear Cylinder Cracking
1AD/PA-32/34 Amdt 1 - Main Landing Gear Cylinder 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-32/34
Amdt 1
Main Landing Gear Cylinder Cracking 12/85
Applicability: All models with fixed landing gear.
Requirement: Visually inspect the landing gear cylinder for cracks at the base of each torque link attachment lug.
Compliance: Within 100 hours time in service after 31 December 1974 and there- after at each issue of a new Maintenance Release.
Background: This amendment revises the compliance requirement to coincide with varying periodic inspection intervals.