AD/PL 12/19 - Stub Wing Internal Structure - Inspection and Re-Protection
1AD/PL 12/19 - Stub Wing Internal Structure - Inspection and Re-Protection
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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 Transavia PL 12 Series Aeroplanes
AD/PL 12/19 Stub Wing Internal Structure - Inspection
and Re-Protection
7/80
Applicability: All PL-12 Series. Document: Transavia SB No. 30.
Compliance: 1. For aircraft which have achieved 3 years time in service since manufacture, initially inspect not later than the next major inspection and thereafter in accordance with SB No. 30.
- For other aircraft, initially inspect not later than next major inspection after achieving 3 years time in service after manufacture and thereafter in accordance with SB No. 30.
Background: Corrosion of the interior structure of the steel stub wing has been observed in some aircraft.