AD/PA-32/75 - Stabilator Attach Fitting Corrosion
1AD/PA-32/75 - Stabilator Attach Fitting Corrosion
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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-32/75 Stabilator Attach Fitting Corrosion 5/87
Applicability: All models listed in Piper SB No 856. Requirement: Action in accordance with Piper SB No 856.
Compliance: At the next scheduled inspection for Maintenance Release issue after 7 May 1987 and thereafter at intervals not exceeding one year.
Background: The manufacturer reports instances of severe corrosion between the steel attach fittings and fuselage structure.