Document ID: chunk:federal_register_of_legislation:F2006B03246:body:0
Version: federal_register_of_legislation:F2006B03246
Segment Type: other
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Character Range: 0–1105

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

 Boeing 747 Series Aeroplanes

 AD/B747/66
 Amdt 2

 Lower Lobe Cargo Door Locking System 3/91

 Applicability: Model 747 series line number 001 and subsequent.

            Requirement: Unless already accomplished; action in accordance with the technical requirements of FAA AD 90-09-06 Amdt 39-6581.

            Note: Boeing SB's 747-52A2206 and 747-52A2209 refer.

 Compliance: As specified in the Requirement Document.

            Background: A lower lobe forward cargo door partially opened in flight due to damaged lock sectors. Amendment 1 was raised in response to the FAA decision, following a second occurrence, to accelerate the compliance time previously required by AD 88- 12-04, and for installation of certain modifications as well as additional inspections and tests in the interim.

            This amendment is raised to reflect an additional requirement of FAA Amdt 39-6581, AD 90-09-02; which supersedes Amdt 39-6166, AD 89-05-54.