Closed Book

Question 1

____altitude is the altitude at which 100% torque is no longer available

Answer 1

Critical

Question 2

(T/F) Although there is no limit for operation at maximum continuous power, sustained operation at maximum power may significantly reduce engine service life.

Answer 2

True

Question 3

Maximum _______ speed is the maximum speed at which an abort may be started and the aircraft stopped within the remaining runway length.

Answer 3

Abort

Question 4

Increase takeoff speeds by ____% of the gust increment up to a maximum of 10 knots.

Answer 4

50%

Question 5

The engine has been flat-rated to produce _______ shaft horsepower.

Answer 5

1100

Question 6

The SCU will activate the red Oil PX annunciator if oil pressure falls below ____ psi when the engine is above ____ idle power.

Answer 6

40 / Idle

Question 7

The SCU will activate the OIL PX annunciator if the oil pressure drops below ___ psi at idle power.

Answer 7

15

Question 8

During an auto start or normal operation with the ignition switch set to ____, the PMU will energize and de-energize the igniters as required.

Answer 8

NORM

Question 9

(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.

Answer 9

True

Question 10

Power for the starter control (START) is provided through the ____ bus.

Answer 10

Battery

Question 11

Power for the ignition system (IGN) is provided through the ____ bus.

Answer 11

Battery

Question 12

The chip detector is mounted in the ____ to detect metal contamination in the oil.

Answer 12

RGB

Question 13

The ____ and the ____ automatically control the propeller blade angle (pitch) and propeller speed (Np).

Answer 13

PMU, PIU

Question 14

The propeller system is designed to maintain a constant speed of _____ rpm (100% Np) during most flight conditions.

Answer 14

2000

Question 15

(T/F) With the PMU not functioning, Np may peak above 100% during power changes and then return to the governed range.

Answer 15

True

Question 16

The PMU provides two operating modes, ground and flight, which are controlled by the ____.

Answer 16

Weight-on-wheels switch on the main landing gear struts

Question 17

In the ground mode, the engine idle N1 is ____% and in the flight mode, idle is normally ____%.

Answer 17

60, 67

Question 18

illumination of both the ____ and ____ annunciators indicates the system is in the manual mode.

Answer 18

PMU FAIL, PMU STATUS

Question 19

(T/F) Engine starts are recommended with the PMU in the manual mode.

Answer 19

False

Question 20

A PMU STATUS light in flight indicates

Answer 20

Weight-on-wheels switch fault and/or mismatch

Question 21

The PMU is normally powered by ____.

Answer 21

PMA

Question 22

During inverted flight, the inverted flight fuel pickup provides ____ of fuel supply, and prevents air ingestion into the fuel system.

Answer 22

Min of 15 seconds

Question 23

(T/F) When correcting a fuel imbalance, set the MANUAL FUEL BAL switch to whichever wing tank is “lighter”.

Answer 23

True

Question 24

If a fuel probe fails, ____ will continue to provide an accurate indication of minimum fuel level.

Answer 24

the low fuel warning lights

Question 25

If the hydraulic pressure in the emergency accumulator drops below ____ psi, an amber EHYD PX LO annunciator will illuminate.

Answer 25

2400 (+/- 150)

Question 26

A normal gear extension/retraction sequence takes approximately ____ seconds.

Answer 26

6

Question 27

(T/F) Pulling the emergency landing gear extension handle will extend the gear and flaps.

Answer 27

False

Question 28

Normal cockpit indications when the emergency extension system is used are:

Answer 28

three green gear lights

red main gear lights, red light in the gear handle

Question 29

The wheel brake system ____ affected by a failure of the aircraft hydraulic system.

Answer 29

is not

Question 30

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

Answer 30

D. either a or b

Question 31

The trim system control circuits give ____ priority if trim selection conflicts between cockpits.

Answer 31

the rear cockpit

Question 32

The ____ senses torque, altitude, airspeed, and pitch rate and computes a desired rudder trim tab position.

Answer 32

TAD

Question 33

If the hydraulic reservoir fluid level indicator shows in the area labeled FULL AC or FULL AD:

Answer 33

the system is fully serviced

Question 34

When flying solo, failure to secure the rear seat oxygen regulator will result in the loss of ability to:

Answer 34

deactivate OBOGS from the front seat

Question 35

To preclude unnecessary wear to nose wheel steering and tire, ____ nose wheel steering prior to executing sharp turns with differential braking.

Answer 35

disengage

Question 36

Any fault discovered during the ____ check is reason for a ground abort.

Answer 36

OVERSPEED GOVERNOR

Question 37

Do not delay ejection while attempting airstart below ____ feet AGL.

Answer 37

2000

Question 38

If an airstart is successful, useful power will be available after approximately ____ seconds from starter engagement.

Answer 38

40

Question 39

The emergency oxygen bottle provides approximately ____ minutes of oxygen.

Answer 39

10

Question 40

Illumination of the L FUEL LO annunciator indicates that approximately ____ pounds of usable fuel remains in the left wing tank.

Answer 40

110

Question 41

Recommend minimum altitudes for ejection are ____ feet AGL for controlled ejection, and ____ feet AGL for uncontrolled ejection.

Answer 41

2000, 6000

Question 42

Maximum oil pressure during start is ____ psi.

Answer 42

200

Question 43

Do not connect external power if the battery voltage is below ____ volts.

Answer 43

22

Question 44

Maximum airspeed for flying through turbulence is ____ KIAS.

Answer 44

207

Question 45

The maximum permissible crosswind for a wet runway is ____ knots.

Answer 45

10

Question 46

Taxi over arresting cables at ____. Steer to avoid nose and main gear contact with cable support donuts.

Answer 46

as slow as possible

Question 47

The canopy shall not be opened in the ground when the surface winds exceed ____ knots.

Answer 47

40

Question 48

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

Answer 48

D. b and c above

Question 49

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.

Answer 49

125, 1350

Question 50

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.

Answer 50

5