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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
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
state the proper procedures for aircraft grounding
connect grounding cable to approved ground receptacle first then connect other end to one of the 9 locations on the aircraft
state the purpose of aircraft plugs and covers
to prtect a/c openings/protruding surfaces from physical/evironmental damage/fod intrusion
discuss the requiremants, duties, and responsibilities of the move director
prime resonsibility lies with the director for the aircraft movement
discuss the requiremants, duties, and responsibilities of the brake rider
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
discuss the requiremants, duties, and responsibilities of the chock walker
pulls and installs chocks when instructed
discuss the requiremants, duties, and responsibilities of the safety observers
conducts a pre-tow inspection of the A/C ensures A/C will clear all obstructions durning movement
discuss the requiremants, duties, and responsibilities of the tractor driver
tows A/C at a slow walking speed avoiding sudden stops or starts. pre-ops tractor ensureing the support equipmentis up and ready.
discuss towing preparations
-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
state the purpose of the landing gear aircraft ground safety pins
landing gear safety pins safeties nose main landing gear in the down position, preventing gear retraction
describe the hazards associated with canopy static buildup
durning flight a high voltage static electrical charce may build up and be stored in the windshield/camopy
briefly discuss the canopy static discharge process
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