Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Fairchild (Swearingen) SA226 and SA227 Series Aeroplanes
AD/SWSA226/69 Wing - Upper Skin at WS 81 5/95
Applicability: Models SA226-T, SA226-T(B), SA226-AT and SA226-TC listed in Fairchild Service Bulletin (SB) 226-57-018 Revised October 25, 1993.
Models SA227-TT, SA227-AT, SA227-AC and SA227-BC listed in Fairchild SB 227-57-005 Revised July 1 1993. Models SA227-CC and SA227-DC listed in Fairchild SB CC7-57-002 Revised July 1, 1993.
Requirement: 1. Visually inspect the wing upper surface skin at the top aft outboard corner of the battery box for cracking.
Inspect in accordance with paragraph 2 ACCOMPLISHMENT INSTRUCTIONS, sub paragraph A Inspection, of the applicable Fairchild SB.
2. Dye penetrant inspect the edges of P/N 27-31130 straps for cracking.
Inspect in accordance with paragraph 2 ACCOMPLISHMENT INSTRUCTIONS, sub paragraph A Inspection, of the applicable Fairchild SB.
3. Modify the upper wing skin in accordance with paragraph 2 ACCOMPLISHMENT INSTRUCTIONS, sub paragraph B Removal, and sub para C Installation, of the applicable Fairchild SB.
Note: FAA AD 94-07-10 refers.
Compliance: 1. Initially inspect in accordance with Requirement 1 before 2500 hours time in service or within 100 hours time in service after 27 April 1995, which ever is the later. Re-inspect at intervals not to exceed 500 hours time in service.
2. If cracks are found as a result of Requirement 1 inspection, inspect in accordance with Requirement 2 before further flight. Re-inspect at intervals not to exceed 50 hours time in service.
3. Modify in accordance with Requirement 3 before further flight if cracks are found as a result of Requirement 2 inspection.
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