AD/PA-38/23 - Upper Forward and Aft Vertical Fin Spar - Inspection and Reinforcement
1AD/PA-38/23 - Upper Forward and Aft Vertical Fin Spar - Inspection and Reinforcement
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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-38 (Tomahawk) Series Aeroplanes
AD/PA-38/23 Upper Forward and Aft Vertical Fin
Spar - Inspection and Reinforcement Applicability: All model PA-38-112 with S/Nos. 38-78A0001 to 38-82A0122. Document: Piper Service Bulletin No. 763.
9/83
Compliance: On vertical fins which have achieved 500 hours time in service, within 25 hours time in service and thereafter at intervals not exceeding 100 hours time in service until Kit 764-965 is installed.
Background: Field reports indicate that cracks have occurred in the area where the horizontal stabiliser attachment brackets attach to the upper end of the vertical fin forward and aft spars.