Document ID: chunk:federal_register_of_legislation:F2006B07184:body:0
Version: federal_register_of_legislation:F2006B07184
Segment Type: other
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Character Range: 0–815

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/SWSA226/44 Main Landing Gear Door System - Inspection 1/83

            Applicability: Models SA226-T(B), S/N T(B)276, T(B)292 thru T(B) 397. SA226-T, S/N T201 thru T275 and T277 thru T291. SA226-AT, S/N AT001 thru AT074. SA226-TC, S/N TC201 thru TC396.

 Document: Fairchild Swearingen SB No. 32-026.

            Note: FAA AD 82-23-06 Amendment 39-4493 refers.

 Compliance: Unless already accomplished, within 100 hours time in service after 31 January, 1983.

            Background: Shifting of the main landing gear doors has occurred which resulted in the landing gear locking in the up position.