General NATOPS Knowledge Flashcards
State the total fuel capacity for the E-2C in LBs and Gallons.
1,824 Gallons
12,400 Pounds
State the WARNING associated with the fuel Quantity Indicating System.
WARNING
1. Due to fuel quantity indicator tolerances, the low-fuel-level warning lights should be used as the primary indication of low-fuel state.
State the Warning associated with the FUEL DUMP system.
WARNING
1) RADAR shall be placed in STBY before dumping fuel to prevent possible ignition of released fuel and vapors.
State the electrical parameters of the HE2K Electrical Power Supply System Generators.
GENs
60/90 kVA ac producing, 115volt, three phase, 400 Hz power to the ac electrical distribution system.
The GCU will command the generator off line when any of what conditions are detected.
- Under Freq
- Under Voltage
- Over Voltage
- Incorrect phase rotation
- Feeder Faults
State two WARNINGS associated with CBs
WARNING
1. Resetting tripped circuit breakers or continuous recycles of electrical equipment in the course of troubleshooting may induce circuit malfunctions, smoke and fumes, and/or a chain reaction fire in associated wire bundles.
- Circuit breakers should be reset in flight if the associated equipment is essential to the safety of flight and then only reset once.
State which subsystems the Combined hydraulic system supplies fluid under pressure to.
- Landing Gear
- Tail Skid
- Wing Flaps
- Wing fold and automatic jury strut
- Wheel brakes
- Arresting hook
- Dome rotation
- Windshield wipers
- Nose wheel steering
- Emergency Generator
State the systems the Flight hydraulic system provide fluid to under pressure.
- Primary Flight controls (rudders, elevators, ailerons)
- AFCS actuators
- Pressure-operated hydraulic isolation valve
When will the Flight and Combined Hydraulic Low Lights illuminate?
- 0 Gallon (Flight)
2. 1 Gallons (Combined)
What subsystems does the Solenoid-Operated Hydraulic Isolation Valve isolate when the switch is set to FLIGHT?
- Landing Gear
- Tail Skid
- Wheel Brakes
- Wing fold and automatic jury strut
- Arresting Hook
- Nose Wheel Steering
- Windshield wipers
State the functions 14th stage bleed air provides.
- Engine anti-ice
- Radar waveguide pressurization
- Wing/tail de-ice
- Inflatable door seals
- Air-conditioning
- Aircraft pressurization
- Side window de-fog
- PDS nose antenna anti-icing
- Engine oil cooler elector vales (on deck)
- Engine compartment cooling (on deck)
- Closes 5th and 10th stage bleed air valves
- Hydraulic reservoir pressurization
- Cross Bleed starts
