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Additional resources for Aircraft Elevators (ch588)
As a minimum, the rope should have the same construction and number of wires as the existing ropes. This is necessary to ensure the modulus of elasticity is equal for all ropes within the hitch group. All the wire ropes in the affected hitch group should be retensioned monthly for three months to remove the constructional stretch of the new rope. b. A single damaged wire rope with a service life of more than one year but less than three years requires replacement of the hitch group. If the elevator has a low frequency of operation, lengthy ship’s availabilities during the service period or scheduled periods that would allow tension checks, it may be acceptable to replace only the damaged wire rope.
Inspect hydraulic system components and piping for: 1 Leakage from connections and valves 2 Excessive hydraulic pump and motor shaft leakage 3 Broken or damaged sight glasses 4 Improperly calibrated gauges 5 Corrosion 6 Fill connection locking caps installed 7 Clear vent for atmospheric tanks. d. Electrical system. Inspect the electrical motors, controllers, limit switches and wiring for: 1 Moisture damage 2 Frayed and cracked insulation 3 Loose wires and connections 4 Evidence of arcing 5 Rough or burned contact points 6 Deteriorated or damaged gaskets 7 Cracked or missing indicator light lenses 8 Loose, bent, corroded or missing limit switch arms.
7 WIRE ROPE INSTALLATION. Aircraft elevator wire rope is prestressed by the manufacturer to remove constructional stretch. Constructional stretch is the lengthening of a wire rope caused by individual wires within the rope becoming seated within the strands as a load is applied. Prestressing does not remove all the constructional stretch. Much of the benefit of prestressing is lost during shipment and installation. After reeving and prior to cutting to length for the platform end poured fitting, all slack must be taken out of the wire rope.