Closed Book Flashcards
____altitude is the altitude at which 100% torque is no longer available
Critical
(T/F) Although there is no limit for operation at maximum continuous power, sustained operation at maximum power may significantly reduce engine service life.
True
Maximum _______ speed is the maximum speed at which an abort may be started and the aircraft stopped within the remaining runway length.
Abort
Increase takeoff speeds by ____% of the gust increment up to a maximum of 10 knots.
50%
The engine has been flat-rated to produce _______ shaft horsepower.
1100
The SCU will activate the red Oil PX annunciator if oil pressure falls below ____ psi when the engine is above ____ idle power.
40 / Idle
The SCU will activate the OIL PX annunciator if the oil pressure drops below ___ psi at idle power.
15
During an auto start or normal operation with the ignition switch set to ____, the PMU will energize and de-energize the igniters as required.
NORM
(T/F) When the ignition control toggle switch is set to ON, or when the igniters are activated in the AUTO mode, a green IGN SEL annunciator is illuminated.
True
Power for the starter control (START) is provided through the ____ bus.
Battery
Power for the ignition system (IGN) is provided through the ____ bus.
Battery
The chip detector is mounted in the ____ to detect metal contamination in the oil.
RGB
The ____ and the ____ automatically control the propeller blade angle (pitch) and propeller speed (Np).
PMU, PIU
The propeller system is designed to maintain a constant speed of _____ rpm (100% Np) during most flight conditions.
2000
(T/F) With the PMU not functioning, Np may peak above 100% during power changes and then return to the governed range.
True
The PMU provides two operating modes, ground and flight, which are controlled by the ____.
Weight-on-wheels switch on the main landing gear struts
In the ground mode, the engine idle N1 is ____% and in the flight mode, idle is normally ____%.
60, 67
illumination of both the ____ and ____ annunciators indicates the system is in the manual mode.
PMU FAIL, PMU STATUS
(T/F) Engine starts are recommended with the PMU in the manual mode.
False
A PMU STATUS light in flight indicates
Weight-on-wheels switch fault and/or mismatch
The PMU is normally powered by ____.
PMA
During inverted flight, the inverted flight fuel pickup provides ____ of fuel supply, and prevents air ingestion into the fuel system.
Min of 15 seconds
(T/F) When correcting a fuel imbalance, set the MANUAL FUEL BAL switch to whichever wing tank is “lighter”.
True
If a fuel probe fails, ____ will continue to provide an accurate indication of minimum fuel level.
the low fuel warning lights
If the hydraulic pressure in the emergency accumulator drops below ____ psi, an amber EHYD PX LO annunciator will illuminate.
2400 (+/- 150)
A normal gear extension/retraction sequence takes approximately ____ seconds.
6
(T/F) Pulling the emergency landing gear extension handle will extend the gear and flaps.
False
Normal cockpit indications when the emergency extension system is used are:
three green gear lights
red main gear lights, red light in the gear handle
The wheel brake system ____ affected by a failure of the aircraft hydraulic system.
is not
Normal flap operation and indications are unavailable anytime:
A. the battery bus has failed
B. when the aux battery is the only source of electrical power
C. the generator bus has failed
D. either a or b
D. either a or b
The trim system control circuits give ____ priority if trim selection conflicts between cockpits.
the rear cockpit
The ____ senses torque, altitude, airspeed, and pitch rate and computes a desired rudder trim tab position.
TAD
If the hydraulic reservoir fluid level indicator shows in the area labeled FULL AC or FULL AD:
the system is fully serviced
When flying solo, failure to secure the rear seat oxygen regulator will result in the loss of ability to:
deactivate OBOGS from the front seat
To preclude unnecessary wear to nose wheel steering and tire, ____ nose wheel steering prior to executing sharp turns with differential braking.
disengage
Any fault discovered during the ____ check is reason for a ground abort.
OVERSPEED GOVERNOR
Do not delay ejection while attempting airstart below ____ feet AGL.
2000
If an airstart is successful, useful power will be available after approximately ____ seconds from starter engagement.
40
The emergency oxygen bottle provides approximately ____ minutes of oxygen.
10
Illumination of the L FUEL LO annunciator indicates that approximately ____ pounds of usable fuel remains in the left wing tank.
110
Recommend minimum altitudes for ejection are ____ feet AGL for controlled ejection, and ____ feet AGL for uncontrolled ejection.
2000, 6000
Maximum oil pressure during start is ____ psi.
200
Do not connect external power if the battery voltage is below ____ volts.
22
Maximum airspeed for flying through turbulence is ____ KIAS.
207
The maximum permissible crosswind for a wet runway is ____ knots.
10
Taxi over arresting cables at ____. Steer to avoid nose and main gear contact with cable support donuts.
as slow as possible
The canopy shall not be opened in the ground when the surface winds exceed ____ knots.
40
If the flaps are set to any position other than UP, the speed brake will:
A. remain extended if already extended
B. retract if already extended
C. remain retracted if the pilot attempts to extend it after the flaps are extended
D. b and c above
D. b and c above
Best glide speed in clean configuration is approximately ____ KIAS with a sink rate of ____ feet per minute and a glide ratio of 2.0 NM/1000 feet.
125, 1350
A stick shaker, activated by the angle-of-attack system, provides artificial stall warning in each cockpit a minimum of ____ knots before the stall is reached.
5
