Document ID: chunk:federal_register_of_legislation:F2006B02949:body:0
Version: federal_register_of_legislation:F2006B02949
Segment Type: other
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Character Range: 0–685

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Boeing 737 Series Aeroplanes

AD/B737/5 Wing-To-Body Drag Angle 8/85

 Applicability: All model 737 aircraft, Line Numbers 1 to 316.

 Requirement: 1. FAA AD 85-03-06, Amendment 39-4998, up to and including Section C.

 2. Boeing SB 737-53-1031 Revision 3. Compliance: As detailed in Requirement Document No 1.
 Background: There have been numerous reports of cracking in the wing-to-body drag angles.
            Continued operation with failed angles could lead to progressive cracking of adjacent structure and rapid decompression.