AD/SWSA226/49 Amdt 1 - Fuel Vent Line and Electrical Wire Bundle Support Clamps - Installation
1AD/SWSA226/49 Amdt 1 - Fuel Vent Line and Electrical Wire Bundle Support Clamps - Installation
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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Fairchild (Swearingen) SA226 and SA227 Series Aeroplanes
AD/SWSA226/49
Amdt 1
Applicability: All model;
Fuel Vent Line and Electrical Wire Bundle Support Clamps - Installation
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SA226-T, S/Nos T201 to 275, 277 to 291.
SA226-T(B), S/Nos T(B)276, 292 to 417. SA226-AT, S/Nos AT001 to 74.
SA226-TC, S/Nos TC201 to 419. SA227-TT, S/Nos TT421 to 555. SA227-AT, S/Nos AT423 to 544.
SA227-AC, S/Nos AC406, 415, 416 and 420 to 547.
Requirement: 1. Fairchild Aircraft Corporation SB No. 226-28-008.
- Fairchild Aircraft Corporation SB No. 227-28-001. Compliance: Within 30 hours time in service after 31 January 1985.
Note: For SA227 series aeroplanes, compliance with the previous issue of this Directive satisfies compliance with this amendment.
Background: This Directive has been amended to include SA226 series aeroplanes in the applicability. Support clamps are installed to prevent chafing between the fuel vent system line and electrical wire bundle located within the wing flap well.