AD/SWSA226/50 Amdt 1 - Aileron Control Cables
1AD/SWSA226/50 Amdt 1 - Aileron Control Cables
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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/SWSA226/50
Amdt 1
Applicability: All models;
Aileron Control Cables 9/86
SA227-TT with S/N TT 421 to 555.
SA277-AT with S/N AT 423 to 591 except Expediter. SA277-AC with S/N AC 406, 415, 416, and 420 to 599.
Requirement: Action in accordance with Fairchild Aircraft Corporation S.B. No. 227-27-015.
Compliance: Unless already accomplished, within 200 hours time in service after 30 September 1986 or at the next scheduled letter check B after 30 September 1986, whichever occurs first.
Background: The manufacturer has advised of possible aileron control cable wear resulting from contact with the aileron trim tab cable pulley at a specified location. Amdt 1 is issued to change the Requirement Document. The original Service Bulletin was withdrawn by the manufacturer.