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12 Cards in this Set
- Front
- Back
state the number of tie-down points on the F/A-18 and identify their locaitions
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their are 12 tie-down poins. ring 1&2 are located on the nose landing gear. rings 4,6&8 are located on the left main landing gear. 5,7&9 are located on the right main landing gear. rings 3,10,11,&12 are located on the fuselage and wing pylons
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state the proper procedures for aircraft grounding
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connect grounding cable to approved ground receptacle first then connect other end to one of the 9 locations on the aircraft
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state the purpose of aircraft plugs and covers
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to prtect a/c openings/protruding surfaces from physical/evironmental damage/fod intrusion
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discuss the requiremants, duties, and responsibilities of the move director
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prime resonsibility lies with the director for the aircraft movement
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discuss the requiremants, duties, and responsibilities of the brake rider
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conducts a premovement inspection of A/C ensureing all safety equipment installed stays alert durning entire A/C move while not leaving the cockpit untill A/C is final spotted
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discuss the requiremants, duties, and responsibilities of the chock walker
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pulls and installs chocks when instructed
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discuss the requiremants, duties, and responsibilities of the safety observers
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conducts a pre-tow inspection of the A/C ensures A/C will clear all obstructions durning movement
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discuss the requiremants, duties, and responsibilities of the tractor driver
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tows A/C at a slow walking speed avoiding sudden stops or starts. pre-ops tractor ensureing the support equipmentis up and ready.
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discuss towing preparations
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-minimum structural access doors must be installed to prevent damage
-radom must be closed and secured -do not tow A/C with 68 r/l open -brake accumulator pressure gauge reads 2900 psi -A/C is clear of all obstacles/support equipment |
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state the purpose of the landing gear aircraft ground safety pins
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landing gear safety pins safeties nose main landing gear in the down position, preventing gear retraction
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describe the hazards associated with canopy static buildup
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durning flight a high voltage static electrical charce may build up and be stored in the windshield/camopy
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briefly discuss the canopy static discharge process
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make shure the A/C is properly grounded. ensure static charge removal kit has had a continuity check within the last 30 days. Connect kit to aircrakt nose landing gear wheel ground receptacle. run kit mitten over canopy and windshield until static discharged is gone
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