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MQF Flashcards

2
Q

The maximum landing weight of the King Air 350ER (B300/B300C) is________ pounds.Ref: Pilot’s Operating Handbook Para: Pg: 1-14 & 2-15A. 16,500B. 16,100C. 15,675D. 15,500

A

C. 15,675

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3
Q

Weather Radar - Warning: The area within the scan arc and within _____ of an operating TWR-852 system can be a hazardous area. Do no operate the systems in any mode other than ______ or _______ when the antenna might scan over personnel within that range. Turning the transmitter on while inside the hanger is not advisable.Ref: Pilot’s Operating Handbook Para: Pg: 2-26A. 5 feet, WX, WX+TB. 5 feet, STBY, WXC. 2 feet, STBY, WX+TD. 2 feet, STBY, TEST

A

D. 2 feet, STBY, TEST

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4
Q

It is not required for all wing inspection lights to be operative prior to flight into known or forecast icing condition at night.Ref: Pilot’s Operating Handbook Para: Pg: 2-27A. TrueB. False

A

B. False

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5
Q

Warning: Do not use reverse thrust with one engine inoperative. Care must be exercised when using single-engine ground fine on surfaces with reduced traction.Ref: Pilot’s Operating Handbook Para: Pg: 3-4A. TrueB. False

A

A. True

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6
Q

DOOR UNLOCKED - WARNING: Do not attempt to check the security of the airstair door or cargo door in flight. Remain as far from the door as possible with seatbelts securely fastened.Ref: Pilot’s Operating Handbook Para: Pg: 3-9A. TrueB. False

A

A. True

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7
Q

The MC-12W’s Glide ratio is ______ for each 1000 feet of altitude. Decrease by ______ for each 10 knots of headwindRef: Pilot’s Operating Handbook Para: Pg: 3-11A. 3.1 NM, 1.1 NMB. 1.1 NM, 0.5 NMC. 4.2 NM, 0.3 NMD. 2.3 NM, 0.2 NM

A

D. 2.3 NM, 0.2 NM

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8
Q

________ annunciators may momentarily illuminate during simultaneous wing boot and brake deice operation at low N1 speeds. If annunciators immediately extinguish, they may be disregarded.Ref: Pilot’s Operating Handbook Para: Pg: 3-18A. BLEED FAILB. CABIN ALT HIC. L&R BL AIR OFFD. L&R ENG ANTI-ICE

A

A. BLEED FAIL

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9
Q

Dual Generator Failure: The propeller ground idle stop solenoids will be inoperative rendering the effectiveness of the propeller Ground Fine and Reverse power lever settings ineffective or greatly reduced. Plan on _________.Ref: Pilot’s Operating Handbook Para: Pg: 3-12A. longer landing distances.B. shorter landing distances.C. increased landing speeds.D. decreased landing speeds.

A

A. longer landing distances.

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10
Q

UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION: Pilot action: AP/Trim Disconnect-DEPRESS FULLY & HOLD. NOTE that applies to this step: _______ will disengage and _______ will be interrupted when the disconnect switch is depressed.Ref: Pilot’s Operating Handbook Para: Pg: 3-19A. Autopilot, flight directorB. Autopilot, Rudder BoostC. Yaw Damper, Rudder BoostD. Rudder Boost, Autofeather

A

B. Autopilot, Rudder Boost

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11
Q

Care must be exercised when using single-engine ground fine on surfaces with reduced traction. Do not use reverse thrust with one engine inoperative.Ref: Pilot’s Operating Handbook Para: Pg: 3A-7A. TrueB. False

A

A. True

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12
Q

CROSSFEED (ONE-ENGINE-INOPERATIVE OPERATION): XFR OVERRIDE switch must be in AUTO position on side being crossfed. If the ________ is closed, the supplemental fuel supply will not be available (usable), and the fuel pressure annunciator will remain illuminated on the side supplying fuel.Ref: Pilot’s Operating Handbook Para: Pg: 3A-8A. Standby PumpB. Fuel CrossfeedC. Firewall ValveD. Fuel System test

A

C. Firewall Valve

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13
Q

Do not lift power levers in flight. Lifting the power levers in flight, or moving the power levers in flight below the flight idle position, could result in a nose-down pitch and a descent rate leading to aircraft damage and injury to personnel.Ref: Pilot’s Operating Handbook Para: Pg: 2-7A. TrueB. False

A

A. True

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14
Q

CIRCUIT BREAKER TRIPPED: Essential Circuit (necessary for continued safe flight). Allow CB to cool for a minimum of _____ sec. If CB trips again __________.Ref: Pilot’s Operating Handbook Para: Pg: 3A-11A. 5, do not resetB. 10, do not resetC. 15, reset on more time is allowedD. 10, reset one more time is allowed

A

B. 10, do not reset

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15
Q

Turning on the Avionics Master Pwr Switch removes power that holds the avionics relay open. If the switch fails to the OFF position, pulling the Avionics Master circuit breaker will remove power to the relay and should restore power to the avionics busses.Ref: Pilot’s Operating Handbook Para: Pg: 3A-17A. TrueB. False

A

A. True

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16
Q

To minimize ingestion of ground debris, the engine anti-ice system should be ON for all ground operations.Ref: Pilot’s Operating Handbook Para: Pg: 4-11A. TrueB. False

A

A. True

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17
Q

If no ITT rise is observed within ____ seconds after moving the Condition Lever to LOW IDLE, move the Condition Lever to CUTOFF and release the Ignition and Engine Start Switch to OFF. Allow ____ minutes for fuel to drain and starter to cool, then follow Engine Clearing procedures.Ref: Pilot’s Operating Handbook Para: Pg: 4-14A. 5, 10B. 3, 10C. 3, 5D. 10, 5

A

D. 10, 5

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18
Q

NEVER CONNECT AN EXTERNAL POWER SOURCE TO THE AIRPLANE UNLESS A BATTERY INDICATING A CHARGE OF AT LEAST ____ VOLTS IS IN THE AIRPLANE. If the Battery voltage is less than ____ volts, the battery must be recharged, or replaced with a battery indicating at least _____ volts, before connecting external power.Ref: Pilot’s Operating Handbook Para: Pg: 4-15A. 28B. 23C. 20D. 18

A

C. 20

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19
Q

Operation of the electric pitch trim system should occur only when both elements of the dual-element switch are activated. Any movement of the elevator trim wheel while activating only one element denotes __________.Ref: Pilot’s Operating Handbook Para: Pg: 4-24A. normal operationB. a system malfunctionC. reduced electric pitch trim operationD. limited use of the electric pitch trim

A

B. a system malfunction

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20
Q

ENGINE ANTI-ICE: Either the MAIN or STANDBY actuator must be operational on each engine anti-ice before takeoff.Ref: Pilot’s Operating Handbook Para: Pg: 4-26A. TrueB. False

A

A. True

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21
Q

Operating propeller deice when the propellers are static is authorized.Ref: Pilot’s Operating Handbook Para: Pg: 4-27A. TrueB. False

A

B. False

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22
Q

In order to minimize ice accumulation of unprotected surfaces of the wing, maintain a minimum of ____knots during operations in sustained icing condition. In the event of windshield icing, reduce airspeed to ____ knots or below.Ref: Pilot’s Operating Handbook Para: Pg: 4-31A. 125, 184B. 140, 226C. 140, 184D. 94, 170

A

B. 140, 226

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23
Q

Engine Auto-Ignition must be ARMED for icing flight, precipitation, and operation during turbulence. To prevent prolonged operation of the igniters with system ARMED, do not reduce power levers below ____ % torque.Ref: Pilot’s Operating Handbook Para: Pg: 4-32A. 10B. 12C. 17D. 21

A

C. 17

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24
Q

High ITT at ground idle may be corrected by ________and/or ___________.Ref: Pilot’s Operating Handbook Para: Pg: 2-8A. Taxiing, shutting down engineB. increasing accessory load, reducing N1 rpmC. feathering engine, turn aircraft into the windD. reducing accessory load, increasing N1 rpm

A

D. reducing accessory load, increasing N1 rpm

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25
Q

If residual ice remains on the airplane, increase VREF speeds by ____ knots.Ref: Pilot Operating Handbook-ISR Supplement Para: Pg: 4-35A. 5B. 10C. 15D. 20

A

C. 15

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26
Q

If possible, propellers should be moved out of reverse at approximately _______ to minimize_________. Care must be exercised when reversing on runways with loose sand, dust or snow on the surface. Flying gravel will damage propeller blades, and dust or snow may impair the pilot’s visibility.Ref: Pilot’s Operating Handbook Para: Pg: 4-37A. 40 knots; blade erosionB. 40 knots; brake wearC. 50 knots; blade erosionD. 50 knots; brake wear

A

A. 40 knots; blade erosion

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27
Q

To minimize ingestion of ground debris, the engine anti-ice system should be ON for all ground operations.Ref: Pilot’s Operating Handbook Para: Pg: 4-37A. TrueB. False

A

A. True

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28
Q

ENGINE SHUTDOWN CHECK - CAUTION: Monitor ITT during shutdown. If sustained combustion is observed, proceed immediately to the _________ procedure. During shutdown, ensure that the compressors decelerate freely. Do not close the firewall fuel valves for normal engine shutdown.Ref: Pilot’s Operating Handbook Para: Pg: 4-38A. ENGINE SHUTDOWN CHECKB. HOT/HUNG STARTC. NO LIGHT STARTD. ENGINE CLEARING

A

D. ENGINE CLEARING

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29
Q

If the OAT is ____ degrees C or below and visible moisture will be encountered during the takeoff, engine anti-ice must be turned on.Ref: Pilot’s Operating Handbook Para: Pg: 4-43A. 0B. +5C. +8D. +10

A

B. +5

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30
Q

SIMULATING ONE-ENGINE-INOPERATIVE(ZERO THRUST) - WARNING: Intentional in-flight engine cuts should be simulated by retarding the power lever to zero thrust (5% Torque) at or above the VSSE speed of _____ knots.Ref: Pilot’s Operating Handbook Para: Pg: 4-44A. 140B. 125C. 135D. 94

A

C. 135

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31
Q

VMCA demonstration (stall series) may be required for multi-engine pilot certification. The following procedure shall be used at a safe altitude of at least _____ feet above the ground in clear air only.Ref: Pilot’s Operating Handbook Para: Pg: 4-45A. 10,000B. 7,000C. 5,000D. 3,000

A

C. 5,000

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32
Q

Ensure the ground communications power switch is off before leaving the airplane so a drain on the battery will not occur.Ref: Pilot’s Operating Handbook Para: Pg: 4-47A. TrueB. False

A

A. True

33
Q

Compliance with a TCAS II ______ is necessary unless the pilot considers it unsafe to do so, or unless the pilot has better information about the cause of the ____ and can maintain a safe separation (e.g. observing a fault in the TCAS, or obtaining a visual contact with the intruder in order to maintain a safe separation.)Ref: Pilot’s Operating Handbook Para: Pg: 4-49A. Traffic Advisory (TA)B. Resolution Advisory (RA)C. ATC AdvisoryD. Oral Advisory

A

B. Resolution Advisory (RA)

34
Q

(With ISR Mod) Do not Taxi, Takeoff or Land over any ground obstruction (arresting cable, tiedown cable, etc.). Damage may result due to low clearance of L-3 FairingRef: Pilot Operating Handbook-ISR Supp Para: Pg: 5A. TrueB. False

A

A. True

35
Q

Total usable fuel is_________. Main tank is _______, each Auxiliary tank is ________, each extended range tank is ______(Using 6.7 lbs/gal conversion)Ref: Pilot’s Operating Handbook Para: Pg: 2-11A. 5192 lbs. 1273 lbs, 533 lbs, 790 lbsB. 539 lbs. 190 lbs, 79.5 lbs, 25.4 lbsC. 4000 lbs. 200 lbs, 100 lbs, 60 lbsD. None of the above.

A

A. 5192 lbs. 1273 lbs, 533 lbs, 790 lbs

36
Q

(With ISR Mod) The Left Escape Hatch is blocked by the OP1 rack and is not accessible as an emergency exit. The ________ and the _______are the only two (2) exits that can be accessed from both inside and outside the aircraft.Ref: Pilot Operating Handbook-ISR Supp Para: Pg: 11A. Pilot Windows; Aft ExitB. Left Escape Hatch; Right Escape HatchC. Right Escape Hatch; Airstair/Cargo DoorD. Pilot Windows; Airstair/Cargo Door

A

C. Right Escape Hatch; Airstair/Cargo Door

37
Q

(With ISR Mod) Danger Zone. The turret is remotely controlled and capable of continuous movement from drive motors that are capable of forces that can injure personnel.Ref: Pilot Operating Handbook-ISR Supp Para: Pg: 13A. TrueB. False

A

A. True

38
Q

(With ISR Mod) For a static takeoff, set static takeoff power while holding the brakes then release the brakes. For a rolling takeoff, set static takeoff power within ____ seconds of brake release. Observe ITT limits for all takeoffs. After the Power Levers are set, ensure [L AFX] & [R AFX] or [L AUTOFEATHER] & [R AUTOFEATHER] are illuminated. Upon reaching VR, rotate to ____ degrees maximum pitch attitude. When a positive climb is established, raise the landing gear, maintain airspeed of V35 until clear of obstacles, then set flaps up (as required).Ref: Pilot Operating Handbook-ISR Supplement Para: Pg: 18A. 5; 3 to 5B. 8; 3 to 5C. 3; 10D. 10; 10

A

D. 10; 10

39
Q

(With ISR Mod) Cycle boots as required to remove icing during takeoff roll.Ref: Pilot Operating Handbook-ISR Supp Para: Pg: 17A. TrueB. False

A

B. False

40
Q

(With ISR Mod) Increasing airspeed will cause torque and ITT to increase. Due to the increased takeoff speeds at weights above _______ pounds, the plane may exhibit a galloping tendency during the takeoff roll. The airplane feels ready to lift off prior to Vr.Ref: Pilot Operating Handbook-ISR Supp Para: Pg: 17A. 14,500B. 15,000C. 15,500D. 16,000

A

B. 15,000

41
Q

(With ISR Mod) For a Balked landing (or Go Around), set the power to maximum allowable. Maintain _____ until clear of obstacles then establish a normal climb. Raise the flaps to approach at ______, raise the landing gear when a positive climb is established, and set the flaps to UP at _____ knots minimum.Ref: Pilot Operating Handbook-ISR Supplement Para: Pg: 20A. VREF + 15; VREF + 10;B. VAPP; VAPP; 125C. VREF + 20; VREF + 20; 140D. VREF; VREF + 10; 135

A

D. VREF; VREF + 10; 135

42
Q

(With ISR Mod) The Left Escape hatch is blocked by OP1 rack and is not accessible as an emergency exit.Ref: Pilot Operating Handbook-ISR Supplement Para: Pg: 31A. TrueB. False

A

A. True

43
Q

Turret Limitations: For ground operations where the temperature is above 35°C (95°F), restrict operations to a duty cycle of _____ on, _____ off. If ground operations are approaching maximum limit time, verify Turret Power Switch (on Left Side SO avionics rack) is off. [Note: This is a situation where there is no airflow over the turret. The system does not have a self contained cooling system and is dependent on slipstream for cooling.]Ref: MX-15Di Designator System Para: Pg: 9A. 1 hour; 4 hoursB. 30 minutes; 45 minutesC. 2 hours; 2 hoursD. 45 minutes; 30 minutes

A

A. 1 hour; 4 hours

44
Q

(With ISR Mod) The laser illuminator is non-eye safe and may result in serious eye damage (including blindness) and/or skin damage to any ground personnel, flight crew or any other observers (including other aircraft).Ref: Pilot Operating Handbook-ISR Supplement Para: Pg: N-6A. TrueB. False

A

A. True

45
Q

Keep turret powered. There are no mechanical locks to keep the turret in the stowed position while powered down.Ref: Pilot Operating Handbook-ISR Supplement Para: Pg: N-2A. TrueB. False

A

A. True

46
Q

Do not take off if fuel quantity gages indicate in yellow arc or indicate less than 265 pounds of fuel in each wing systemRef: Pilot’s Operating Handbook Para: Pg: 2-11A. TrueB. False

A

A. True

47
Q

Fuel Reserve: For turbine-powered aircraft use fuel consumption rates that provide maximum endurance at 10,000 ft. Mean Sea Level (MSL).Ref: AFI 11-202V3 ACCSUP Para: 2.4.4.2A. TrueB. False

A

A. True

48
Q

In order to increase awareness on potential conflicts with other aircraft, aircrews will brief the following special subject on every sortie:Ref: AFI 11-202V3 ACCSUP Para: 2.7.3.1A. Radar/visual search responsibilities for departure, en route, recovery and high density traffic areasB. mid-air collision avoidance (from other military aircraft and/or civilian aircraft)C. Both A and BD. None of the above

A

C. Both A and B

49
Q

In the absence of other MAJCOM guidance, USAF aircrews shall consider as mountainous: those areas defined in 14 CFR 95.11 for CONUS, Alaska, Hawaii, and Puerto Rico. For all other areas of operation, use ______________ to define the location of mountainous terrain.Ref: AFI 11-202V3 ACCSUP Pg: 20 Chap: 2 Para: 2.11.A. 100 ft surface elevation change over a ½ NM distanceB. 200 ft surface elevation change over a 1 NM distanceC. 300 ft surface elevation change over a ½ NM distanceD. 500 ft surface elevation change over a ½ NM distance

A

D. 500 ft surface elevation change over a ½ NM distance

50
Q

Pilots shall always ensure ________________ prior to commencing an RNAV procedure (departure, arrival, or approach) using any MAJCOM-approved RNAV equipment.Ref: AFI 11-202V3 ACCSUP Para: 2.16.4.3.1A. Ceiling and visibility are 1500/3 and clear of cloudsB. Landing checklist is completedC. RAIM availabilityD. clearance to land

A

C. RAIM availability

51
Q

The ________ is responsible for ensuring that the aircraft is not operated in a careless, reckless, or irresponsible manner that could endanger life or property.Ref: AFI 11-202V3 ACCSUP Para: 5.1.1A. PilotB. Senior ranking officerC. Operations Group Commander (OG/CC)D. PIC

A

D. PIC

52
Q

A person shall not act as a crewmember of an aircraft:Ref: AFI 11-202V3 ACCSUP Para: 5.1.4A. While under the influence of alcohol or its after-effectsB. While using, or while under the influence of, any substance that affects the crewmembers ability to safely perform assigned dutiesC. While self-medicating (unless approval granted IAW AFI 48-123)D. All of the above

A

D. All of the above

53
Q

Pilots operating in VMC, under IFR or VFR, and operating under radar control are not required to see and avoid other traffic, terrain, and obstacles.Ref: AFI 11-202V3 ACCSUP Para: 5.4A. TrueB. False

A

B. False

54
Q

Use of tobacco products aboard any ACC aircraft, aircraft under ACC oversight, or within RPA ground control stations including the control element __________.Ref: AFI 11-202V3 ACCSUP Para: 5.23A. is prohibitedB. must be authorized by the PICC. Is only authorized with WG/CC approvalD. Is prohibited below 10,000 ft MSL

A

A. is prohibited

55
Q

Avoid thunderstorm activity by any means available by at least:Ref: AFI 11-202V3 ACCSUP Para: 5.26.3A. 20 NM laterally at or above FL 230B. 10 NM laterally below FL 230C. Both A and BD. Neither A or B

A

C. Both A and B

56
Q

Pilots shall not deviate from an ATC clearance in response to a Resolution Advisory (RA).Ref: AFI 11-202V3 ACCSUP Para: 5.27.1.3A. TrueB. False

A

B. False

57
Q

The supplemental electric heater must be off for at least _____ minutes prior to and during engine start.Ref: Pilot’s Operating Handbook Para: Pg: 2-18A. 1B. 2C. 3D. 4

A

B. 2

58
Q

During day/VMC flight, terrain warnings _____________.Ref: AFI 11-202V3 ACCSUP Para: 5.28A. Must be followedB. Need not be followed if the TAWS/EGPWS has previously given erroneous indicationsC. Need not be followed if the pilot can verify the warning is false by visual contact with the terrain/obstacleD. Caused by an error in the TAWS/EGPWS system can be corrected by pulling the TAWS/EGPWS circuit breaker

A

C. Need not be followed if the pilot can verify the warning is false by visual contact with the terrain/obstacle

59
Q

Weather for the ETA (+/- 1 hour) at destination or recovery base must be __________ for the aircraft concerned.Ref: AFI 11-202V3 ACCSUP Para: 8.6.3A. At or below the lowest compatible published landing minimumsB. At or above the lowest compatible published landing minimumsC. above the lowest compatible published landing minimumsD. below the lowest compatible published landing minimums

A

B. At or above the lowest compatible published landing minimums

60
Q

An alternate is required when the worst weather (TEMPO or prevailing) at the ETA (+/- 1 hour) for the point of intended landing (or each point of intended landing on a stopover flight plan) does not permit a VFR descent from the MIA and is less than:Ref: AFI 11-202V3 ACCSUP Para: 8.7.1.1A. A ceiling of 2,000 ft and a visibility of 3 SMsB. A ceiling of 2,000 ft and a visibility of 2 SMsC. A ceiling of 3,000 ft and a visibility of 2 SMsD. A ceiling of 3,000 ft and a visibility of 3 SMs

A

A. A ceiling of 2,000 ft and a visibility of 3 SMs

61
Q

Compute fuel requirements using a fuel reserve as prescribed in AFI 11-202v3, paragraph 2.4.4, from __________________. Include fuel for 30 minutes holding at the destination fix, plus fuel for the penetration and landing.Ref: AFI 11-202V3 ACCSUP Para: 8.7.3.3A. Takeoff to over the destination fixB. Departure to the first point of intended landingC. Takeoff to the first point of intended landingD. Departure to over the destination fix.

A

D. Departure to over the destination fix.

62
Q

Pilots shall not begin an en route descent, arrival, or published approach if the destination’s weather is below the required approach minimums.Ref: AFI 11-202V3 ACCSUP Para: 8.17.1A. TrueB. False

A

A. True

63
Q

The maximum Flight Duty Period (FDP) for training flights is ____ hours.Ref: AFI 11-2-MC-12 Vol 3 Pg: 13 Chap: 3 Para: 3.6.2.A. 10B. 12C. 14D. 16

A

C. 14

64
Q

The minimum crew required to fly the MC-12W is _______________.Ref: AFI 11-2-MC-12 Vol 3 Para: 3.2A. One AC and one copilot (CP)B. One MC, one copilot (CP), one Sensor Operator (SO), and one COC. One ACD. None of the above

A

A. One AC and one copilot (CP)

65
Q

During training missions, pilot in-flight seat swaps may be accomplished only with a qualified pilot at the flight controls and above 1,000 feet Above Ground Level (AGL).Ref: AFI 11-2-MC-12 Vol 3 Para: 5.2.1A. TrueB. False

A

A. True

66
Q

Minimum runway width is ___ feet.Ref: AFI 11-2-MC-12 Vol 3 Pg: 21 Chap: 5 Para: 5.9.1.A. 50B. 60C. 65D. 75

A

B. 60

67
Q

Minimum runway length for touch and go landings is ______ or TOFL, whichever is greater.Ref: AFI 11-2-MC-12 Vol 3 Para: 5.9.4A. 4,000 feetB. 5,000 feetC. 6,000 feetD. 8,000 feet

A

C. 6,000 feet

68
Q

The autopilot minimum engage height after takeoff is ________.Ref: Pilot’s Operating Handbook Para: Pg: 2-20A. 79 feet AGLB. 79 feet MSLC. 400 feet AGLD. 400 feet MSL

A

C. 400 feet AGL

69
Q

With an RCR of 10, the maximum crosswind component for takeoff and landing is _____ knots.Ref: AFI 11-2-MC-12 Vol 3 Para: Table 5.5A. 10B. 15C. 20D. 25

A

C. 20

70
Q

Before departure, the _____________ will be set for emergency return.Ref: AFI 11-2-MC-12 Vol 3 Para: 5.13A. Primary ATC radioB. SquawkC. Radar AltimeterD. Primary navigation source

A

C. Radar Altimeter

71
Q

Crewmembers will accomplish FENCE checks on all operational missions. FENCE stands for:Ref: AFI 11-2-MC-12 Vol 3 Para: 5.15A. Fire Control, Emissions, Navigation, Communication, EmergencyB. Frequency, Electronics, Navigation, Communication, EmergencyC. Fuel, Electronics, Navigation, Coordinates, EmergencyD. Frequency, Emissions, NORDO, Communications, Electronics

A

A. Fire Control, Emissions, Navigation, Communication, Emergency

72
Q

Maintain at least ____ NM separation from heavy rain showersRef: AFI 11-2-MC-12 Vol 3 Para: 6.19.4.3.2A. 3B. 4C. 5D. 6

A

C. 5

73
Q

The MC-12W is a Category “C” aircraft. If approach speeds exceed 120 KIAS, use Category “D” approach minimums. If approach speeds exceed 140 KIAS, use Category “E” approach minimums.Ref: AFI 11-2-MC-12 Vol 3 Para: 6.34.1A. TrueB. False

A

B. False

74
Q

Only a crew member or properly trained ground personnel should close and lock the Airstair Door and Cargo Door (if installed).Ref: Pilot Operating Handbook-Liberty 9+ POH Supp Para: Pg: 15A. TrueB. False

A

A. True

75
Q

The autopilot minimum use height during approach is ________.Ref: Pilot’s Operating Handbook Para: Pg: 2-20A. 160 feet AGLB. 160 feet MSLC. 79 feet MSLD. 79 feet AGL

A

D. 79 feet AGL

76
Q

VNAV altitudes must be displayed on the MFD map page or CDU (center console display) LEGS page when utilizing VNAV for flight guidance.Ref: Pilot’s Operating Handbook Para: Pg: 2-25A. TrueB. False

A

A. True

MQT (2 decks)

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