Document ID: chunk:federal_register_of_legislation:F2006B02982:body:0
Version: federal_register_of_legislation:F2006B02982
Segment Type: other
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Character Range: 0–1036

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Boeing 737 Series Aeroplanes

 AD/B737/80
 Amdt 1

 Wing Leading Edge Panel 4/95

 Applicability: Model 737-300, -400, and -500 series aircraft, with line numbers 1001 through 1976,
            1978 through 2197, and 2199.

            Requirement: Modify the leading edge slat and internal structure at Front Spar Station 250.663 in accordance with Boeing Service Bulletin 737-57-1221.

            Note: FAA AD 94-06-11 Amdt 39-8858 and AD 94-26-13 Amdt 39-9108 refer.

 Compliance: Unless already accomplished, prior to 21 April 1996.

            Background: Reports were received of fuel leakage from the fuel line at front spar station 250.663, which then flowed through a drain hole in a slat access panel and into the turbine exhaust area.

            Amendment 1 is issued in response to a new FAA AD which expands the applicability to include additional affected aircraft.