AD/SWSA226/37 - Fuselage, Lower L.H. Cargo Area Belt Frames - Inspection and Modification
1AD/SWSA226/37 - Fuselage, Lower L.H. Cargo Area Belt Frames - Inspection and Modification
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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 Fairchild (Swearingen) SA226 and SA227 Series Aeroplanes
AD/SWSA226/37 Fuselage, Lower L.H. Cargo Area Belt
Frames - Inspection and Modification
10/81
Applicability: All model SA226-AT with S/Nos. AT-001 to AT-074. All model SA226-TC with S/Nos. TC-201 to TC-419.
Document: Fairchild Swearingen SB No. 53-007. Compliance: As per Requirement Document.
Background: Cracks may develop in the lower left belt frames at the cargo door latch receptacles.