AD/SWSA226/34 - Fuselage Skin and Aft Belly Fairing - Inspection
1AD/SWSA226/34 - Fuselage Skin and Aft Belly Fairing - Inspection
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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/SWSA226/34 Fuselage Skin and Aft Belly Fairing - Inspection
Applicability: All model SA226T with S/Nos. T201 to T275 and T277 to T291; All model
9/81
SA226AT with S/Nos. AT001 to AT074; All model SA226TC with S/Nos. TC201 to TC407.
Document: 1. Swearingen SB No. 53-006, and
- FAA AD 81-15-01 refers.
Compliance: Unless already accomplished, within 250 hours time in service after 30 September 1981.
Background: Chafing may occur on the lower fuselage skin due to contact between the aft belly fairing stringers and the fuselage.