Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

Flight questions > MQF SEP 2021 - 151-200 > Flashcards

MQF SEP 2021 - 151-200 Flashcards

1
Q

Normal holding airspeed in the T-6 is _____ KIAS.
A. 150
B. 160
C. 180
D. 125
Proctor Reference: AETCMAN 11-248

A

A. 150

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Power-On Stalls: Aircraft pitch and bank angle held constant until control effectiveness lost indicated by uncommanded nose drop or unplanned rolling motion. Recover to a wings level, climbing attitude. An entry speed of 160 KIAS results in about _____ - ______ feet altitude gain.
A. 500-1000
B. 1000-1500
C. 1500-2000
D. 2000-3000
Proctor Reference: AETCMAN 11-248

A

C. 1500-2000

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

The AGSM demonstration cycle should last from 10 to 15 seconds with at least 4 to 5 breathing cycles.
True
False
Proctor Reference: AETCMAN 11-248

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

P-Factor is normally caused by:
A. AOA being higher on the upward moving propeller blade than on the downward moving propeller blade.
B. AOA being higher on the downward moving propeller blade than on the upward moving propeller blade.
C. The propeller rotating at a constant speed
D. A low PCL setting
Proctor Reference: AETCMAN 11-248

A

B. AOA being higher on the downward moving propeller blade than on the upward moving
propeller blade.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Maximum abort speed calculations allow for a ______ second reaction time to select idle power and a ______ second period to apply the brakes after idle is selected. Speed may increase up to ______ knots during this period.
A. 3, 2, 10
B. 2, 2, 15
C. 4, 4, 20
D. 3, 3, 20
Proctor Reference: T.O. 1T-6A-1

A

D. 3, 3, 20

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Add ______ feet to charted take off distance for formation wing take offs, assuming lead is using no less than ______ % torque.
A. 1000, 85
B. 85, 100
C. 1000, 80
D. 1000, 75
Proctor Reference: T.O. 1T-6A-1

A

A. 1000, 85

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Although there is no time limit for operation at maximum power, sustained operation at maximum power may significantly reduce engine service life.
True
False
Proctor Reference: T.O. 1T-6A-1

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Critical altitude is defined as ______ . This occurs at approximately ______ feet MSL on a
standard day with the PCL at MAX.
A. The altitude where delta-P begins to increase / 8,000
B. The altitude at which 100% torque is no longer available with the PCL at MAX / 16,000
C. The altitude at which the power curve is non-linear / 10,000
D. The optimum cruise altitude / 16,000
Proctor Reference: T.O. 1T-6A-1

A

B. The altitude at which 100% torque is no longer available with the PCL at MAX / 16,000

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

If the PCL is placed in cutoff with the PMU in OFF and the PROP SYS circuit breaker pulled, the propeller will not rapidly feather and may not fully feather until after landing.
True
False
Proctor Reference: T.O. 1T-6A-1

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

The engine data manager (EDM) monitors engine operating parameters and ______ .
A. governs propeller RPM
B. illuminates the appropriate annunciator when necessary
C. is activated by a weight-on-wheels switch
D. allows near linear power response with PCL position
Proctor Reference: T.O. 1T-6A-1

A

B. illuminates the appropriate annunciator when necessary

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

The engine has been flat-rated to produce ______ shaft horsepower.
A. 900
B. 1100
C. 1300
D. 1500

A

B. 1100

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Oil cooling is accomplished by routing scavenged oil through an oil cooler located ______ before returning to the oil tank.
A. in the lower aft cowl assembly
B. in the RGB
C. in the left main gear well
D. next to the oil fill port
Proctor Reference: T.O. 1T-6A-1

A

A. in the lower aft cowl assembly

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

If the rate of change of propeller RPM exceeds the PMU sensor validity check limit, the PMU will assume a sensor failure has occurred, and dashes will be displayed for Np and Torque. If the dashes were caused by a propeller RPM rate limit exceedence:
A. smoothly advance the PCL until normal indications appear
B. a reset is not possible
C. cycling the PMU switch will restore the displays
D. cycle the PROP SYS circuit breaker
Proctor Reference: T.O. 1T-6A-1

A

C. cycling the PMU switch will restore the displays

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Placing the starter switch in the AUTO/RESET position automatically:
A. energizes the battery bus
B. engages the starter
C. energizes the ignition system
D. both b and c
Proctor Reference: T.O. 1T-6A-1

A

D. both b and c

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

During an auto start or normal operation with the ignition switch set to ______ , the PMU will
energize and deenergize the igniters as required.
A. ON
B. NORM
C. AUTO
D. AUTO/RESET
Proctor Reference: T.O. 1T-6A-1

A

B. NORM

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

When the IGNITION switch is set to ON, or when the igniters are activated in AUTO mode, a green IGN SEL annunciator is illuminated.
True
False
Proctor Reference: T.O. 1T-6A-1

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

The reduction gearbox (RGB) is driven by the power turbine, which is driven by hot gases from the gas generator section. There is no mechanical connection between the gas generator section
and the RGB.
True
False
Proctor Reference: T.O. 1T-6A-1

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

The PCLs are interconnected with a push-pull rod so that movement of one PCL moves the
other.
True
False
Proctor Reference: T.O. 1T-6A-1

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

The propeller system is designed to maintain a constant speed of ______rpm (100% Np) during most flight conditions.
A. 30,000
B. 3000-5000
C. 2000
D. None of the above
Proctor Reference: T.O. 1T-6A-1

A

C. 2000

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

When feathered, the propeller blades are aligned nearly ________ the wind.
A. flat against
B. opposite of
C. straight into
D. diagonal to
Proctor Reference: T.O. 1T-6A-1

A

C. straight into

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Propeller feather may be selected to minimize drag during engine failure by placing the ______ to ______.
A. PCL, OFF
B. PROP, FEATHER
C. PCL, IDLE
D. None of the above
Proctor Reference: T.O. 1T-6A-1

A

A. PCL, OFF

22
Q

With the PMU functioning, the mechanical overspeed governor modulates oil pressure to the propeller pitch change piston to limit Np below _____ percent.
A. 100
B. 103
C. 106
D. 110
Proctor Reference: T.O. 1T-6A-1

A

C. 106

23
Q

Power for the engine/systems display (ENG SYS DIS) is provided through the ______ bus.
A. battery
B. generator
C. aux battery
D. AC
Proctor Reference: T.O. 1T-6A-1

A

B. generator

24
Q

In the ground mode, the engine idle N1 is ______ % and in the flight mode, idle is approximately ______ %.
A. 67, 40
B. 60-61, 67
C. 40, 60
D. 67, 60
Proctor Reference: T.O. 1T-6A-1

A

B. 60-61, 67

25
Q

Power setting is linear with PCL position throughout the operating envelope of the aircraft.
True
False

A

True

26
Q

Engine starts are NOT recommended with the PMU in the manual mode.
True
False
Proctor Reference: T.O. 1T-6A-1

A

True

27
Q

If faults prevent the PMU from setting the requested power or respecting engine limits, or the pilot switches the PMU OFF, the system will revert to the manual mode.
True
False
Proctor Reference: T.O. 1T-6A-1

A

True

28
Q

During a normal (auto) start, the PMU can automatically abort the start if necessary to avoid a hung/hot start or if any engine start parameter is exceeded.
True
False
Proctor Reference: T.O. 1T-6A-1

A

True

29
Q

If the auto fuel balance system shuts off without reducing the fuel imbalance to ______ pounds
or less, the auto balance system may be reset to provide an additional ______ minutes to
balance the fuel load.
A. 50, 3
B. 30, 3
C. 30, 2
D. 20, 3
Proctor Reference: T.O. 1T-6A-1

A

C. 30, 2

30
Q

During an normal (auto) engine start, the PMU:
A. activates the starter
B. activates the boost pump
C. activates the igniters
D. adds fuel at the proper N1
E. all of the above
Proctor Reference: T.O. 1T-6A-1

A

E. all of the above

31
Q

The PCL may be advanced to IDLE any time N1 is at or above ______ .
A. 60%
B. 70%
C. 50%
D. 30%
Proctor Reference: T.O. 1T-6A-1

A

A. 60%

32
Q

After the PCL has been advanced past the start ready position, the PMU will not cut off fuel to terminate a start.
True
False
Proctor Reference: T.O. 1T-6A-1

A

True

33
Q

The start may be manually aborted by:
A. placing the PCL back to OFF
B. reselecting the STARTER switch to AUTO/RESET (if PCL is not past idle gate)
C. de-energizing the PMU
D. either a or b above
Proctor Reference: T.O. 1T-6A-1

A

D. either a or b above

34
Q

If a start attempt is automatically or manually aborted:
A. advance the PCL past the idle gate
B. immediately attempt a restart to burn any residual fuel
C. wait 10 minutes to allow residual fuel to evaporate
D. perform the Abort Start Procedure
Proctor Reference: T.O. 1T-6A-1

A

D. perform the Abort Start Procedure

35
Q

Illumination of the fire warning light accompanied by one or more of the following indications is confirmation of an engine fire:
A. smoke
B. engine vibration
C. unusual sounds
D. fluctuating oil pressure, oil temperature, or hydraulic pressure
E. all of the above
Proctor Reference: T.O. 1T-6A-1

A

E. all of the above

36
Q

Flattening, twisting, kinking or denting of the fire detection loop will affect test or flight operation.
True
False
Proctor Reference: T.O. 1T-6A-1

A

False

37
Q

During inverted flight, the inverted flight fuel pickup provides ______ fuel supply regardless of aircraft orientation, and prevents air ingestion into the fuel system.
A. a 40 gallon
B. a minimum 60 seconds
C. a maximum 90 seconds
D. an unlimited
Proctor Reference: T.O. 1T-6A-1

A

B. a minimum 60 seconds

38
Q

The fuel auto balance system (provided by the EDM) detects fuel imbalances:
A. using actual fuel quantity
B. using indicated fuel flow
C. as displayed on the fuel gauge
D. as calculated using the fuel control
Proctor Reference: T.O. 1T-6A-1

A

C. as displayed on the fuel gauge

39
Q

Selecting the MANUAL FUEL BAL switch to L will:
A. stop motive flow fuel from feeding from the right tank.
B. drain fuel from the left wing
C. add fuel to the left wing
D. stop motive flow fuel from feeding from the left tank.
Proctor Reference: T.O. 1T-6A-1

A

D. stop motive flow fuel from feeding from the left tank.

40
Q

The generator provides 28 volts DC, which is sufficient to power:
A. all equipment on the generator
B. the battery bus equipment
C. charge the battery
D. all the above
E. only a. and b
Proctor Reference: T.O. 1T-6A-1

A

D. all the above

41
Q

If the generator control switch (GEN) has been set to on in either cockpit, and the occupant of the
other cockpit selects ON:
A. generator function is interrupted momentarily, then
B. it trips the GEN switch in the other cockpit to OFF
C. generator function is controlled by the switch set to ON
D. all of the above
E. b and c above
Proctor Reference: T.O. 1T-6A-1

A

E. b and c above

42
Q

While the PMU should normally abort a hot/hung/no start, the pilot should manually abort a start in the following situations:
A. Normal N1 increase is halted (hung start)
B. No rise of ITT is evident within 10sec after fuel flow indications (no start)
C. BAT BUS annunciator illuminates during the start sequence
D. PCL is moved or the ST READY annunciator extinguishes during the start sequence
E. All of the above
Proctor Reference: T.O. 1T-6A-1

A

E. All of the above

43
Q

Preflight testing of the auxiliary battery power level is accomplished:
A. prior to application of battery power
B. using the AUX BAT switch and making a radio call
C. using the AUX BAT test switch and light
D. both a and b above
E. both a and c above
Proctor Reference: T.O. 1T-6A-1

A

E. both a and c above

44
Q

In an emergency situation, the auxiliary battery will power the standby instruments, backup UHF radio, standby instrument lighting and FIRE 1 fire warning system for approximately ______ .
A. 3-5 minutes
B. 10 minutes
C. 30 minutes
D. 1 hour
Proctor Reference: T.O. 1T-6A-1

A

C. 30 minutes

45
Q

The hydraulic system consists of one engine-driven pump with approximately a ______ capacity. The hydraulic pump pressurizes the normal system and emergency accumulator to ______ psi.
A. 1 gallon, 3000, +/- 150
B. 5 quart, 3000 +/- 120
C. 1 gallon, 1800
D. 5 quart, 1800-3000
Proctor Reference: T.O. 1T-6A-1

A

B. 5 quart, 3000 +/- 120

46
Q

A normal gear extension/retraction sequence takes approximately ______ seconds.
A. 5
B. 6
C. 10-15
D. 30
Proctor Reference: T.O. 1T-6A-1

A

B. 6

47
Q

The wheel brake system ______ affected by a failure of the aircraft hydraulic system.
A. is
B. is not
Proctor Reference: T.O. 1T-6A-1

A

B. is not

48
Q

The pilot applying the most wheel brake pedal force determines the amount of braking being used.
True
False
Proctor Reference: T.O. 1T-6A-1

A

True

49
Q

Flap position is controlled by a three-position flap selector marked:
A. UP, TO, LDG
B. UP, 50%, 100%
C. UP, HALF, FULL
D. UP, TO, DN
Proctor Reference: T.O. 1T-6A-1

A

A. UP, TO, LDG

50
Q

Normal flap operation and indications are NOT available whenever:
A. the battery bus has failed
B. when the auxiliary battery is the only source of electrical power
C. the generator bus has failed
D. either a or b above
E. either b or c above
Proctor Reference: T.O. 1T-6A-1

A

D. either a or b above

Flight questions (27 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions