Document ID: chunk:federal_register_of_legislation:F2006B03448:body:0
Version: federal_register_of_legislation:F2006B03448
Segment Type: other
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Character Range: 0–1067

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

 Boeing 767 Series Aeroplanes

AD/B767/95 Leading Edge Slat System 4/97

 Applicability: All Model 767 series aircraft.

            Requirement: Inspect in accordance with the technical requirements of FAA AD 96-25-18 Amdt 39- 9861.

            Note: Boeing Alert Service Bulletin 767-27A0137 refers.

            Compliance:  Unless already accomplished, before the accumulation of 10,500 total hours time in service, or within 500 hours time in service after 27 March 1997, whichever occurs later; thereafter at the intervals specified in the requirement document.

            This airworthiness directive becomes effective on 27 March 1997.

            Background: The FAA received reports of skewed panels of an outboard leading edge slat due to the failure of a corroded rotary actuator or the control rod. An undetected skewed slat panel could lead to control difficulty and result in slat structure damage.