Propeller
Engines
Hydraulics
Landing Gear
Flight Controls
Fuel
100

Consisting of two concentric tubes, this component routes engine oil to and from the cylinder and piston.

Beta tube

100

What three sections is the engine divided into?

PGB section, Torquemeter assembly section, and power section.

100

What are the reservoir quantities of the three different supply hydraulic systems?

Utility 5.5gal, booster 3.1gal, aux 5.3gal.

100

What valve is responsible for routing hydraulic pressure to retract and extend the NLG and MLG?

Landing gear selector valve.

100

What flight control surface is constantly supplied with 3,000 PSI of hydraulic pressure? What makes this flight control surface different?

Elevator.

It doesn't have any diverter panels.

100

What two components control and monitor fuel and fuel components, including fuselage tank fuel and components.

Fuel management controller and tanker equipment control unit.

200

Installed on the GMAD, what component controls the propeller blade angle by directing engine oil flow to the cylinder and piston

Pitch Control Unit

200

What are the angled sections in the compressor, which ones are stationary, and which ones spin as air travels through?

Compressor vanes and compressor rotors.

200

What are the operating pressures of the suction boost pumps and it's thermal cut off temperature?

70-90 PSI, 250 degrees Fahrenheit. 

200

What component used pressurized hydraulic fluid to spin the applicable linkages to rise and lower the MLG?

Hydraulic motor

200

When is the rudder hydraulic pressure de-boosted?

When flaps are less than 15 percent.

200

What are the output pressures of the boost pumps, transfer pumps? How are they turned on and off?

15-24 PSI, engine start switches in RUN

28-40 PSI, From switch (arrow) on the fuel management panel.


300

What components boost engine oil pressure for operation and provide protection in the event of propeller speeds being too high?

High-pressure pump and overspeed governor 

300
What components are attached to the power unit accessory drive?

Fuel pump metering unit, starter, power unit lube and scavenge pump, and alternator stator.

300

What does each hydraulic system provide hydraulic pressure to?

Utility - Flight controls, MLG & NLG extension and retraction, NLG steering, normal brakes, flaps, normal AR.

Booster - Flight controls

Aux - Cargo ramp and door, NLG emergency extension, emergency brakes, emergency AR

300

What are the different ways to lower MLG and NLG?

MLG - Normal via the landing gear panel, hydraulically override via the landing gear selector valve, manually via T-handle and/or stub shaft, and via quick disconnects.

NLG - Normal via the landing gear panel, hydraulically override, hydraulically emergency extension, manual emergency extension handle.

300

What component bypasses the pressure reducer and sends 3,000 psi of hydraulic fluid to the acutating assembly?

Diverter valve

300
What type of vent lines are in each tank?

Outboard - end to end

Inboard - wrap around

Aux - wrap around

External - straight up and out

400

Which sensors are used to relay the propeller blade angle to the FADEC? 

Rotary variable differential transducers (RVDT)

400

What components are mounted on the gearbox mounted accessory drive?

AC generator, hydraulic pump, PGB lube and scavenge pump, PCU, and propeller overspeed governor and high pressure pump.

400

What two valves open and close, isolating the hydraulic fluid from going to the hydraulic pump and from the hydraulic pump? What two whys can they be opened and closed?

Suction shutoff valve and pressure shutoff valve.

Engine pump switches or fire handle.

400
What two valves route pressurized hydraulic fluid to the brakes and where are they located?

Brake control valves, located under the flight station floorboards just aft of the rudder pedals. 

400

Located in the booster manifold, the position of this valve determines the direction of pressure and return flow to the actuator.

Booster control valve

400

How much fuel does each vent collector tank hold and how does it drain?

8 U.S. gal, drained by suction effect from the boost pumps when running?

500

What are the two names of the different characteristics of the propeller operations on the ground and in flight?

Controllable Pitch Propeller and Constant Speed Propeller.

500

The compressor variable geometry moves and controls what?

Inlet guide vane and the first five rows of the compressor stator vanes.

500

What line aids in proper cooling and lubrication of the engine hyd pumps?

Case drain line.

500

What component controls brake pressure and prevents skids? What two configurations is this component not being utilized?

Anti-skid.

The parking brake is set, or when emergency brakes are selected.

500

What holds the flaps in position and how is it released?

Flap break assembly.

Released by hydraulic pressure.

500

What are the two types of probes in each tank? How are they constructed? How are they different? 

Fuel quantity probe and compensator probe.

Outer tube and inner tube.

Fuel quantity - fuel inside the probes creates capacitance, more fuel, more capacitance, less fuel, less capacitance. Quantity reflects.

Compensator - Instead of capacitance with fuel level, capacitance varies with fuel density.  

600

What component attached to the pitch control unit modulates high pressure oil to the beta tube to change the propeller blade pitch?

Servo valve

600

What is displayed on the Engine ACAWS page and what are they measuring?

Horsepower(HP), Measured Gas Temperature(MGT) temp in the power turbine section, Gas Generator Speed(NG) speed of the compressor, propeller speed(NP), fuel flow(FF), gearbox oil pressure(GPSI) oil pressure in the GMAD L&SP, engine oil pressure(EPSI) PUAD L&SP, oil temp(TEMP), oil quantity(QTY).

600

At what PSI is the system pressure relief valve fully open?

3,850 PSI

600

What valve is actuated by a rod, which is connected to a pivoted rocker arm, that allows pressurized hydraulic fluid to enter and exit the NLG cylinders?

NLG steering control valve.

600

What actuates/trips in the event of a flap control cable breaks?

Flap cable failure switch

600

State 540 FPM sink rate criteria. 

Gross weight - 142,000 LBS

Fuel in tank NO.1 or NO.4 - 7,320 LBS each

Fuel in all Main tanks - 28,000 LBS