Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Boeing 727 Series Aeroplanes
AD/B727/150 Main Deck Cargo Door 13/96 DM
Applicability: This Directive is applicable to Model 727-100 and -200 series aeroplanes that have been modified in accordance with Federal Aviation Administration (FAA) Supplemental Type Certificate SA1797SO.
Requirement: 1. If not previously accomplished, perform a visual inspection of the main deck cargo door control box for the following discrepancies:
1. chafed, crimped, crushed, or damaged electrical wires or wire bundles inside the control box;
b. loose electrical wire connections;
c. abnormally pulled or twisted individual wires or wire bundles;
d. any removal of insulation from the conductor in the control box; or
e. any damaged protective grommets.
2. Rectify any discrepancies found during the Requirement 1 inspection.
3. If not previously accomplished, ensure that the electrical wires or wire bundles are properly installed and restrained in accordance with the procedures contained in either of the following documents:
1. FAA Advisory Circular 43.13-1A Change 3 dated 1988 (Acceptable Methods, Techniques and Practices - Aircraft Inspection and Repair) Chapter 11, Sections 1, 3, 5, and 7.
b. Boeing Wiring Diagram Manual - Document D6-54446 Revision 21 dated 1 June 1994, Chapter 20.
4. Modify the wiring and components of the main deck cargo door control box in accordance with Aeronautical Engineers Inc Service Bulletin Report No R-AEID1 Revision A dated 3 September 1996.
Note 1: FAA AD 96-16-08 Amdt 39-9708 refers. Note 2: A flight manual amendment is required. Compliance: Requirement 1 - Prior to 27 October 1996.
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