The RGB is a two-stage planetary reduction drive to reduce the power turbine output shaft speed of over _______ RPM to the propeller operating speed of _____ RPM.
30,000; 2,000
Placing the PCL to OFF triggers a microswitch activating the feather dump solenoid valve that _____________.
dumps oil pressure allowing the feathering spring and counterweights to feather the propeller
When feathered, the propeller blades are ___________.
aligned nearly straight into the wind
If PMU function is lost or deactivated, the mechanical flyweight overspeed governor modulates oil pressure to the propeller pitch change piston to maintain Np at or below _____.
100±2% RPM
With the PMU functioning, the mechanical overspeed governor modulates oil pressure to the propeller pitch change piston to limit Np below ____.
106% RPM
Non-engine related functions performed by the EDM include _________.
fuel balancing and quantity indication
determination and display of cockpit pressure altitude and differential pressure
determination and display of DC volts and DC amps
determination and display of hydraulic pressure and NACWS
The power management unit (PMU) is normally powered by the ______.
permanent magnet alternator (PMA)
T or F: The PMU also provides engine protection for airstart capability. During an airstart, automatic N1, ITT and torque limit protection is available; however the pilot should still monitor all parameters and abort the start manually if necessary.
false
Illumination of both the PMU FAIL and PMU STATUS annunciators indicates what condition?
Faults prevent the PMU from setting the requested power or respecting engine limits
PMU has been switched OFF
PMU system is in the manual mode
In relation to the Fire Warning System, power for FIRE 2 is provided through a circuit breaker, placarded FIRE 2, located on ___________.
Generator Bus
Illumination of the PMU STATUS annunciator one minute after landing (weight-on-wheels activation) indicates what?
Fault conditions that are not serious enough to revert the system to manual were encountered in flight
Illumination of the PMU STATUS annunciator in flight indicates all but which of the following?
Fault conditions exist that are not serious enough to revert the system to manual
The fuel system provides approximately _____ of usable fuel through the single point refueling system.
1100 pounds
Which of the following is NOT a result of pulling the emergency firewall shutoff handle?
The engine compartment extinguisher bottle is armed
If gravity (over the wing) refueling is accomplished, fuel quantity increases by ____ pounds (approximately ____ gallons).
100; 15
T or F: With FP FAIL annunciation, the low fuel warning lights will no longer provide an accurate indication of minimum fuel level.
False
The electric boost pump:
provides fuel for engine start
serves as a backup to the engine-driven low pressure fuel pump
If the red GEN annunciator illuminates, what equipment is automatically shed?
air conditioning
If the FUEL PX annunciator illuminates and the boost pump activates during inverted flight, _______.
cease inverted maneuvers and notify maintenance after flight
The inverted fuel pickup system provides a minimum _____ supply of fuel regardless of orientation.
15 seconds
If the generator has failed and the BUS TIE switch is in the NORM position, then the battery will power:
all items except the air conditioner
If the generator bus has failed (red GEN BUS annunciator illuminated) and the BUS TIE switch is in the NORM position, _______.
The items on the generator bus will not be powered
The generator will continue to power the battery bus and charge the battery
What do the red bands on the brake reservoir filler plug indicate?
The system requires servicing (top) or is overserviced (lower)
If the generator fails while the BUS TIE annunciator is illuminated, expect a minimum of ___ of battery power to the battery bus items.
30 minutes
The hydraulic pump pressurizes the normal system and emergency accumulator to ______ psi.
3000 ± 120
Once hydraulic pressure exceeds ____ psi, the system can power the landing gear, main gear doors, flaps, speed brake, and nose wheel steering.
1800
The T-6 hydraulic system powers which of the following systems?
landing gear and main gear doors
nosewheel steering
T or F: If the hydraulic fluid level is not FULL AC or FULL AD, then depressurize the emergency accumulator by pulling the manual pressure release handle until the fluid level indicates FULL AD.
false
What does an amber EHYD PX LO annunciator signify?
Pulling the emergency gear extension handle in the front cockpit:
allows emergency extension of the landing gear and flaps
isolates the main hydraulic system at the power pack slide assembly
releases the emergency accumulator pressure through independent emergency lines for the respective hydraulic components
The aural landing gear position warning indicates:
Gear handle not DOWN, PCL below approximately 87% N1, airspeed below 120 KIAS, and flaps UP or TAKEOFF
All gear not indicating down and locked with flaps LDG
Weight on wheels with the gear handle not DOWN
What are the cockpit indications after emergency extension of the landing gear?
Red light in the gear handle, green nose gear indication, red and green indicators for each main gear
T or F: The landing gear cannot be retracted after being extended with the emergency system.
True
T or F: Electrical power is not required to use the emergency gear extension system.
True
TO indicates the takeoff flap setting and corresponds with ____ degree deflection. LDG indicates the landing flap setting and corresponds with ____ degree deflection.
23; 50
The nosewheel is a free castoring type with ______ degrees of castor (______ degrees either side of center).
160; 80
T or F: In the event of wing flap failure, the flaps are hinged to the lower surface of the wing and can be visually verified from the rear cockpit.
False
Which of the following will NOT cause the speed brake to automatically retract?
Raise landing gear handle
What is true regarding flap operation when the auxiliary battery is the only source of electrical power?
Normal flap operation is unavailable
Flap position indication is unavailable
Emergency flap operation is not available
How can the flaps be retracted after emergency extension?
The flaps cannot be retracted until the aircraft is serviced by maintenance
Which of the following is in both the FCP and RCP?
None of the above are in both cockpits
Describe the action required by both pilots to relinquish aircraft control with the intercom OUT.
PF smoothly pushes the rudder pedals and the PNF shakes the stick
Accomplish a G-awareness exercise on sorties that include maneuvers that may result in ___ or more Gs.
3
G loading during the G-X should increase to approximately ______ Gs.
four (4)
For planning purposes, use approximately _____ - _____ knots minimum for a level to slightly descending turn in the G-awareness exercise
200; 220
When accomplishing the G-awarenes exercise, the G onset rate should be __________, allowing sufficient time to evaluate the effectiveness of your AGSM and determine your G tolerance.
