Document ID: chunk:federal_register_of_legislation:F2006B07174:body:0
Version: federal_register_of_legislation:F2006B07174
Segment Type: other
Provision Reference: 
Character Range: 0–828

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/SWSA226/34 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

            2. 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.