AD/SD3-30/2 - Fuselage Top Skin Sealing - Inspection
1AD/SD3-30/2 - Fuselage Top Skin Sealing - 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 Short SD3-30 Series Aeroplanes
AD/SD3-30/2 Fuselage Top Skin Sealing - Inspection 11/81
Applicability: All model SD3-30 with S/Nos. SH3002 to SH3072. Document: Shorts SB No. SD3-53-41 Rev. 1.
Compliance: Within 300 hours time in service after 30 November 1981 and thereafter at intervals not exceeding 2400 hours time in service.
Background: Instances of fuel spillage entering the passenger compartment through joints in the top skin have been reported to the manufacturer.