Fuel
APU
Engines
Pre-flight
Electrical
100

Each engine is supplied either directly from its own main fuel tank, or from any tank through the __________ system

Cross-ship manifold

100

The APU provides Air and Energy for what systems?

Air for Air Conditioning and Engine start, and power for the Electrical Systems

100

What does FF stand for on the Engine Status page for the HDD, and what is it measured in?

Fuel Flow, measured in Pounds per Hour

100

Oxygen Regulator limitations

270-455 static

270-340 with flow

100

How many batteries are on the plane and what are they called.

Two batteries, Utility and Avionic.

200

How much fuel can the Fuselage tank hold in gallons?

3600 Gallons

200

The APU provides shaft power to drive a ____ generator

40-kVA AC

200

What is the oil tank capacity of the engine, how much oil is actually in it, and how much oil is in the reservoir for the Aux feather pump.

20 Gallon oil tank, 12 gallons for oil, and 8 gallons reserved for air space. 0.66 gallons for the Aux feather pump.

200

O2 Walk around bottle Limitations

375 +-  75

200

What does the Utility supply power to?

Utility power Bus and Isolated dc bus

300

All the fuel tanks, except for the fuselage tank, are equipped with a ____ systems fabricated from reticulated, explosion-suppressant, conductive foam.

Baffles Systems

300

The APU receives fuel from tank ______ through a motor operated ______. 

No.2 main Tank, Shutoff Valve.


Bonus question: If there is below ___ amount of fuel, the APU cannot gravity feed.

300

The Engine control system consists of two identical single channels _____ (A and B). During engine operation, how many are on, and how many are in actual control?

FADEC (Full Authority Digital Electronic Control

Both are functioning, but only one is in actual control.

300

Where does the Nose Landing Gear Ground Lock pin get installed? and what does it prevent?

Inserted in a hole in the nose landing gear actuator rod-end and prevents release of the internal downlock in the actuator

300

The Battery Switch is a 3-Position (On, Test, or Off) lever lock system.

True or False?

False. The Battery Switch is a 2-position(On or off) lever lock switch.

400

Tanks No.2,No.3, left, and right auxiliary tanks have a _____ vent system

Wrap-around vent system

400

In the event of an Emergency start, what are not available for the APU?

Automatic shutdown and Aural alarm in the event of fire.

400

What components are on the PUAD

FPMU, Alternator Stator, Starter, and Power unit lube and scavenge pump

400

What does RVSM, RWR, and MWS stand for? What do they look like?

Reduced Vertical Separation Minimum, Radar Warning Receiver, and Missile Warning System. 

The RWR is the "hockey puck" and the MWS is the "fish eye"

400

Tripped, Pulled or Strapped ECBs are displayed in what color on the HDD?

Yellow

500

"All useable fuel except approximately ____ pounds in each main tank may be dumped."

1520 Pounds

500

What are the two APU inlet door positions, when or why do they differ, and when does the APU inlet door close during shutdown.

15 Degrees in-flight, 35 degrees on the ground. It closes at 18 Percent RPM.

500

The aircraft is powered by four _______ engines

AE 2100D3 Turboprop

500

What does the P symbology stand for on your pre-flight check-list

Items preceeded by the symbol "P" shall be checked prior to applying external or APU power to the aircraft

500

The electrical system parameters are displayed on the HDD system status page, when selected through the AMU. What is displayed on this page? 

Hint: Five things

Voltage of all three phases for all five generators

Percent of the maximum rated load (average of all three phases for all five generators

Percent of the maximum rated load for the four regulated TRs

Essential DC bus Voltage

Main DC bus voltage