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33 Cards in this Set
- Front
- Back
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State the general safety procedures that must be observed while pressure refueling
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keep clear of tail rotor, minimize traffic, check pressure switches, check fuel sample
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State and identify the SH-60B danger areas
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* APU, ECS, and engines exhaust area
* main and tail rotor blades when engaged *servicing platforms when blades are being folded *Pylon when it is being folded *Chaff dispencer, ALQ-144 when powered |
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Discuss the Warnings, Cautions and Notes to be observed prior to applying external power
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*Be sure that area arond stab is clear of personel
*If tail pylon or stab is folded, be sure that stab power circuit breaker and stab system circuit breaker are open *DO NOT connect or disconnect AC power cable while energized *be sure weight on wheel circuit breaker is closed *if WOW light does not go on disconnect electrical power |
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Discuss Hazards of Beryllium
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Dust corrosion and other fine particles generated
*DO NOT sand file or drill |
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Discuss hazards of lithium batteries
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Reacts violently to water
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Describe the overall dimensions and clearances of the SH-60B
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*Folded- 40ft. 11in
*Overall - 64ft. 10 in Ground to tail clearance 6ft 8in *Turning radius 41ft 7in *Clearance 180 degrees 84ft |
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Discuss the following physical characteristics and capabilities of the SH-60B aircraft
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Cargo hook 6000 lbs & jaw opening of 2.12 foward rast probe
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Describe fuel cell contruction and capacity
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2 cells 2040 lbs ,300 gal. expansion to 184 lbs,27 gal
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Discuss emergency exits in accordance with passengeer saftey cards
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Pilot and ATO jettison windows push foward and push out
*cabin cargo door window pull aft and push out *SO window pull aft and push out |
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State the three methods by which the main rotor blades may be folded
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Manual
*blade fold box *auto fold |
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State the reason why battery power is required when folding the tail rotor pylon
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*index the tail
*keeps from auto rotor |
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State the wind restrictions for Folding the main rotor blades and tail rotor pylon
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Over 45 knots
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Identify the positon of the stabilator during the tow/park of the helicopter
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Zero or full up
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Identify the location of Aircraft tiedown/securing points installed on the SH-60B
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3 each side
2 main 1 tail |
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State the purpose of a hydralic patch test
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Primary contamination method
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State the purpose of a blade inspection method (BMI)
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indicates nitrogen pressure in the spar (white pressure good, black no pressure)
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State the purpose of a conducting a flight control system rigging
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to ensure correct rotary wing and rudder blade angles
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Identify the location of the vibratio absorbers
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*nose
*lateral *cabin foward *cabin aft |
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Identify the location and state the purpose of the main rotor head dampers and accumilator
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Between spindles and hub
dampeners lead and lag |
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State the three objectives of first aid
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*save life
*prevent further injury *prevent infection |
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Discuss the importance of the Coral Sea conflict
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7-8 may 1942, U.S. broke japanese navy code, the worlds first carrier vs carrier battle (Lexinton was sunk)
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What is the name of the first Naval Aircraft Carrier
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U.S.S Langley
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What the first jet powered naval aircraft
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Fj-1 Fury
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Who was the first naval aviator in space
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Alan Shepard
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State the purpose of the NAVAIR 01-1A-509
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provide information on materials and procedures for the prevention and repair of corrosion damage to equipment
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The term "WARNING" means?
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may result in injury or death
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The term "Caution" means?
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may result in damage to equipment
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The term "Note" means?
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procedure, practice or condition the must be emphasized
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The term "Shall" means?
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Mandatory
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The term "May" means?
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Optional
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Explain the operating characteristics of the Emergency Locator Transmitter (ELT)
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Distress signals up to 100 miles
*altitude at about 10,000 ft, will survive 5g impact* *tone varies at rate of 2 to 3 per second |
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Explain the requirments for aircraft grounding during weapons load/unload
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*aircraft to ground
*ground tested semi annually *resistance between aircraft and ground 10,000 ohms or less |
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State the purpose of a stray voltage check
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Must be performed before loading
*ensure |
