飞机管理指导方针 Aircraft management guidelines(121)

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c) all bulletins, notices, and directives or maintenance programmes published by the manu-facturer of the airframe and the hoist should be on hand and incorporated into the overall maintenance programme as appropriate;
d) all lifting devices (baskets, straps, personnel harnesses, personnel lifting devices, and any ancillary associated lifting equipment) that attach to the hoist cable should also be included in the maintenance programme.
e) electrical hoist assemblies that do not have specified bonding tests and parameters should have the electrical bonding tested as follows:
i) test the electrical bonding between all adjacent component parts of the hoist assembly, including, but not limited to, control box, electric motor casing, hoist body, hoist arm and attachment bracket, and between the hoist assembly and the aircraft. The maxi-mum permitted resistance is 0.010 OHM, using a bonding tester capable of resolving to 0.002 OHM;
ii) testing is to be completed every 24 months, or more frequently depending on fre-quency of installation and use; and
iii) results of testing should be recorded in the aircraft maintenance log.

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Appendix 10 Contents
A10 Airborne geophysical survey 153
A10.1 Risk analysis..............................................................................................................................................................153
A10.2 Aircraft equipment standards...............................................................................................................................153
A10.3 Personal equipment standards..............................................................................................................................153
A10.4 Minimum crew........................................................................................................................................................153
A10.5 General pilot experience.......................................................................................................................................154
A10.6 Pilot flight & duty times.......................................................................................................................................154
A10.7 Minimum survey height.......................................................................................................................................154
A10.8 Minimum survey speed..........................................................................................................................................155
A10.9 SAR coverage............................................................................................................................................................155
A10.10 Minimum fuel reserves..........................................................................................................................................155
　
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