LOAD MQF 2015 Flashcards

1
Q

Where can the crash axe be found?

A

In the Floor Step

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2
Q

The following emergency equipment is located with the crash axe:

A

Portable Breathing Equipment & Fire Exinguisher

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3
Q

What is the maximum takeoff weight?

A

30,843 lb

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4
Q

What is the maximum ramp weight?

A

31,019 lbs

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5
Q

What is the maximum zero fuel weight?

A

27,800 lbs

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6
Q

What is the maximum landing weight?

A

29,167 lbs

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7
Q

What is the minimum flight weight?

A

20,724 lbs

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8
Q

Cargo area floor limitation for 75 lb/ft2?

A

FS 602 to FS 705

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9
Q

Cargo area floor limitation configuration 3 and 4, for 82 lb/ft2?

A

FS 457 to FS 602

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10
Q

Cargo area floor limitation configuration 5, for 82 lb/ft2?

A

FS 298 to FS 602

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11
Q

With MAX Takeoff weight of 30,843 lb, Center of Gravity Limitation will be _____ to _____ during Takeoff and landing.

A

22.5% to 40%

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12
Q

What is the maximum speed for Flaps 12?

A

200 KIAS

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13
Q

What is the maximum speed for Flaps 20?

A

180 KIAS

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14
Q

What is the maximum speed for Flaps 32?

A

160 KIAS

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15
Q

What is the maximum landing gear operating speed (VLE=VLO)?

A

200 KIAS

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16
Q

What is the maximum tire speed, (ground speed)?

A

165 KTS

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17
Q

Engine operating limitations for max takeoff power?

A

100% at 100%

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18
Q

Engine operating limitations for max takeoff TQ?

A

1

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19
Q

Engine operating limitations for max takeoff ITT?

A

800

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20
Q

Engine operating limitations for transient TQ up to 20 seconds?

A

120

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21
Q

Engine operating limitations for starting ITT from 8500C to 9500C is limited to seconds.

A

5

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22
Q

Engine operating limitations for transient ITT up to 8500C is limited to seconds.

A

20

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23
Q

Engine operating limitations for transient TQ up to ____ is limited to 20 seconds.

A

1.2

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24
Q

__________ lever movements from MIN to MAX in less than 2 seconds are prohibited.

A

CONDITION

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25
Q

The APU shall not be started above _____ ft pressure altitude.

A

20000

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26
Q

A restart of the APU is allowed only after a complete roll down of the APU: ____ minutes after the APU MASTER button is selected off.

A

2

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27
Q

Maximum allowable inflight fuel imbalance between contents of left and right wing tank group: _____ lb.

A

210

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28
Q

Maximum fueling pressure: _____ psi.

A

50

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29
Q

Maximum defueling pressure: _____ psi.

A

(-)10

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30
Q

Total fuel quantity for automatic pressure refueling is?

A

7300 lbs

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31
Q

Total fuel quantity for gravity or manual pressure refueling is?

A

7531 lbs

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32
Q

Maximum altitude for ECS single pack operation is?

A

25,000 ft MSL

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33
Q

Maximum differential pressure is?

A

6.9 psi

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34
Q

Maximum differential pressure for landing is?

A

.40 psi

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35
Q

What is the flap setting for takeoff?

A

12

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36
Q

What is the maximum altitude with flaps extended?

A

18,000 ft MSL

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37
Q

_______ is prohibited if the BRK TEMP HIGH CAUTION message is displayed on the EICAS

A

Takeoff

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38
Q

Maximum Operating Altitude: _____ ft pressure altitude.

A

31000

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39
Q

Flights above 27,000 ft are limited to less than ___ hours.

A

3

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40
Q

Maximum altitude for takeoff and landing: ______ ft.

A

12000

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41
Q

Maximum demonstrated crosswind for takeoff/landing - Dry runway: ___ kt, Wet runway: ___.

A

21 & 21

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42
Q

Maximum tailwind for takeoff/landing - Dry runway: ___ kt, Wet runway: ___ kt.

A

10 & 10

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43
Q

Maximum demonstrated wind for taxiing: ___ kt.

A

40

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44
Q

Aircraft, which are to be parked outdoors for long periods or with current or predicted winds of more than ____ KT, must be moored to prevent damage during storms

A

30

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45
Q

Takeoff and landing with the Environmental Control System (ECS) flow mode set to _____ is prohibited if the ECS is fed by engine bleed air.

A

HIGH

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46
Q

These color codes are used on the displays, EICAS page, and different system pages:

A

Red: Operation limit / Amber: Caution range / White/Green: Normal Operating Range

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47
Q

Provide a minimum of _____ hours (except ARC at home station and U-28) from arrival at aircraft to stations time for crew members to complete preflight duties, unless preflight duties have been accomplished.

A

2

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48
Q

Spectacles. Crewmembers that require corrective spectacles while performing aircrew duties ______ only use Air Force-provided spectacles (T-1). Crewmembers must also carry a spare set of clear Air Force-provided spectacles while performing aircrew duties (T-1)

A

MUST

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49
Q

Flashlights (N/A for UAS). Each crewmember must have an operable flashlight for _______ operations (T-2).

A

NIGHT

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50
Q

Tobacco use in all forms, including electronic nicotine delivery systems, is _______ on all aircraft (T-0).

A

PROHIBITED

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51
Q

Crewmembers must occupy their _______ from takeoff to landing unless absence is normal in the performance of crew duties or in connection with physiological needs (T-0).

A

ASSIGNED DUTY STATIONS

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52
Q

In the absence of MAJCOM guidance, aircrew of fixed-wing aircraft shall minimize non- ssential cockpit conversations and other extraneous activities which could interfere with flight duties when below ______ ft. MSL, during critical phases of flight, and during all taxi operations.

A

10000

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53
Q

Without supplemental oxygen: Flight time between _____ and _____ ft. MSL is unrestricted, but shall not exceed 1 hour if any portion of the flight is conducted in IMC, at night (with or without NVDs), while employing weapons, conducting airdrop, air-refueling, or if performing high-g maneuvers.

A

10,000 / 12,500

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54
Q

Without supplemental oxygen: Flight time between _____ and _____ ft. MSL shall not exceed 30 minutes.

A

12,500 / 14,000

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55
Q

Individuals suspected of DCS shall be administered and remain on _________ (using tight-fitting mask or equivalent) until evaluated by an aviation medical authority (T-1).

A

100% OXYGEN

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56
Q

If anyone on the aircraft experiences _______ symptoms, descend immediately to the lowest practical altitude and land at a suitable location to obtain medical assistance (T-1).

A

HYPOXIA

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57
Q

If equipped, landing lights should be turned on when takeoff clearance is received, when commencing takeoff roll at an airport without an operating control tower, or when operating below ______ ft. MSL within normal MDS-specific operating procedures.

A

10000

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58
Q

List passengers on a DD Form _____, Passenger Manifest, or a MAJCOM-approved form (T-0). File the manifest and crew list with the flight plan, the passenger service facility, or other responsible agency (T-0). Notify C2 prior to departure if there is a passenger manifest (or crew list) change (T-1).

A

2131

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59
Q

In the absence of MDS-specific guidance, _______ without the availability to in-flight refuel, operated for extended periods over large bodies of water or desolate land areas (outside gliding distance to a suitable landing site) shall calculate and plot on a navigational chart an ETP to a suitable alternate for that mission leg.

A

MULTI ENGINE AIRCRAFT

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60
Q

______ takeoff with ice, snow, frost, or other contamination adhering to the wings, control surfaces, propellers, engine inlets, or other critical surfaces of the aircraft, unless authorized by the flight manual (T-2).

A

Do not

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61
Q

A thin coating of _____ is permitted on the fuselage, provided the lettering and/or paint lines are visible.

A

FROST

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62
Q

Do not takeoff where ________ or other ________ are producing hail, strong winds, gust fronts, heavy rain, lightning, wind shear, or microbursts (T-1).

A

THUNDERSTORMS, HAZARDOUS CONDITIONS

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63
Q

Do not turn after a takeoff until at least _____ ft. above the Departure End of the Runway (DER) elevation, at a safe airspeed, and past the end of the runway (if visible) unless specifically cleared by the controlling agency, required by a published procedure, or when executing a closed pattern (T-0).

A

400

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64
Q

Crew Complement. The ______ crew complement for flight operations is two pilots and one loadmaster.

A

MINIMUM

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65
Q

The basic FDP is _____ hours providing no training events or maintenance ground runs are accomplished after _____ hours. Fully qualified and current crew members must occupy duty stations past _____ hours.

A

16/12/12

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66
Q

The ______ is the approval authority for operations with degraded equipment within the guidelines of the aircraft Minimum Equipment List (MEL) and Minimum Equipment Subsystems List (MESL). Operating outside of the aircraft MEL or MESL guidelines requires Group/CC or COMAFSOF approval.

A

PIC

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67
Q

Before Landing Checklists. Aircrew will complete the Before Landing Checklist no lower than _____ feet (ft) Above Ground Level (AGL). Aircraft will be established on final, wings level, with a controlled rate of descent in a position to execute a safe landing no lower than ______ .

A

200/100

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68
Q

All crew members will be at their duty stations during all ____, ____, ____ and ____.

A

Takeoffs, departures, approaches, and landings

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69
Q

The loadmaster?s primary duty station is the _______ for critical phases of flight. The AC may assign an alternate duty station for abnormal situations.

A

JUMP SEAT

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70
Q

Crew members occupying a primary crew position will have seat belts _____ at all times.

A

Fastened

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71
Q

Floor loading is authorized to support dedicated special operations forces team members or liter medical patients during , , or .

A

Contingencies, exercises, or training

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72
Q

Without wing walkers, avoid taxi obstructions by at least ______ ft.

A

25

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73
Q

With wing walkers, avoid taxi obstructions by at least ______ ft.

A

10

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74
Q

Do not taxi aircraft closer than _____ ft to any obstacle.

A

10

75
Q

A minimum of ft of runway is required for Flaps 20 touch-and-go landings.

A

6000

76
Q

A minimum of _____ ft of runway is required for zero-flap or Flaps 32 touch-and-go landings.

A

7000

77
Q

Any crew member will immediately advise the PF when observing unannounced heading deviations greater than ___ degrees, airspeed deviations of ___ knots, altitude deviations of ___ ft during approach or ___ ft while en route, or potential terrain or obstruction problems and no attempt is being made by the PF to correct the deviation.

A

10, 10, 100 & 200

78
Q

Engines Running Onload or Offload (ERO). The ____ will direct all onloading or offloading operations using pre-briefed signals. Other qualified crew members may assist the operation; however, the PIC and loadmaster retains overall responsibility for the operation.

A

Loadmaster

79
Q

Engines Running Onload or Offload (ERO). Passengers will be escorted by the ÿÿÿÿÿÿÿÿÿÿÿÿÿÿÿÿwhen enplaning or deplaning.

A

Loadmaster

80
Q

_________ worn will consist of casual slacks or cargo pants, collared shirts, shoes or hiking boots.

A

CIVILIAN CLOTHING

81
Q

All aircrew members _____ have flight gloves readily available during all flights.

A

Will

82
Q

Foreign Object Damage (FOD) Hazards. Aircrew will not wear wigs, hairpieces, rings, scarves, ornaments, pins, hair clips or fasteners, or earrings in the aircraft or on the flight line. Crew members _____ remove rings and scarves before performing aircrew duties.

A

Will

83
Q

Carry a headset and operable flashlight on _____ flights.

A

All

84
Q

All crew members will carry and preflight their own _____ prior to flight for missions using NVG’s.

A

NVG’S

85
Q

Passenger Briefings. Prior to each flight, the _____ will ensure that all passengers are briefed.

A

Loadmaster

86
Q

Any mission planned when the lunar illumination is forecast to be less than _____ during the mission will require an additional level of Operational Risk Management (ORM), as determined by unit supplement.

A

0.1

87
Q

_______ lbs of fuel remaining during day VFR or night VFR conditions when using NVGs.

A

600

88
Q

lbs of fuel remaining during night VFR conditions when not using NVGs or IFR conditions.

A

900

89
Q

Land with no less than ______ pounds of fuel on board.

A

450

90
Q

Minimum Fuel is ______ pounds and Emergency Fuel is pounds.

A

450/250

91
Q

A copy of each mission?s ______ will be maintained at the squadron or operations center (as applicable) and carried with the aircrew.

A

WEIGHT & BALANCE

92
Q

For en route stops, weight and balance need not be recomputed provided the ________ has not changed.

A

ZERO FUEL WEIGHT

93
Q

Review the __________ before applying power to the aircraft or operating aircraft systems.

A

AIRCRAFT MAINTENANCE FORMS

94
Q

Anytime the APU is running, at least ______ or maintainer will remain within the immediate vicinity of the APU fire suppression control panel in order to adequately hear the APU fire bell.

A

one crew member

95
Q

Crew members will wear ______ when operating aft of the 3-9 line while the APU is operating.

A

HEARING PROTECTION

96
Q

Eye protection _____ be used during refueling operations.

A

Will

97
Q

The loadmaster _____ backup the PNF with the QRH checklist reading/actions as directed, visual confirmation of the memory items, and scanning of engines/passenger compartment.

A

Will

98
Q

The ______ is the primary crew member responsible for fighting fires in the cabin/cargo area

A

Loadmaster

99
Q

If any crew member calls ?________?, the PF will immediately apply power to establish a climb that clears all obstacles. Minimum altitude for overflight of aircraft, equipment, or personnel on the runway is 500 ft AGL.

A

GO-AROUND

100
Q

The ______ will perform servicing when maintenance personnel are not available. When executing refueling operations, loadmasters will wear gloves and eye protection.

A

Loadmaster

101
Q

______ will ensure the aircraft is clean, stow publications, deposit trash in proper receptacles, and account for all personal equipment before leaving the aircraft.

A

ALL CREW MEMBERS

102
Q

The AC and the LM will complete a ________ to determine any changes from their pre-mission inspection (i.e., bird strike).

A

POST MISSION WALK AROUND

103
Q

Mission Radios.________ leave the aircraft unattended with crypto loaded into the mission radios.

A

DO NOT

104
Q

will not permit the inspection of their aircraft by officials of any foreign government. If requested to do so, the PIC and crew will deny access and seek aid from the senior AFSOC or USAF representative or US Embassy or consulate within the host nation.

A

PIC

105
Q

Cargo Documentation: _____ accept hazardous materials unless proper documentation, certification, and identification of cargo are provided.

A

Do not

106
Q

The aircraft should be : _______ during all off-station missions remaining overnight.

A

Locked

107
Q

Due to the sensitivity of ______ in foreign countries, crews will keep their weapons inside the aircraft and out of sight of foreign nationals, even if the FCG allows them to be carried outside the aircraft.

A

WEAPONS

108
Q

Weapons need not be _______ before being placed in the gun box.

A

UNLOADED

109
Q

Loadmaster in-flight duties also include backing up the _____ on radio traffic, assigned altitude/heading/airspeeds, altimeter settings, Traffic Collision Avoidance System (TCAS) alerts, monitoring systems and periodically accomplishing an interior/exterior scan.

A

Pilots

110
Q

The loadmaster is responsible for, supervises, performs, and/or participates in the following: _________________.

A

Perform and or read checklists initiated by the PF or PNF.

111
Q

Load aircraft in such a manner that emergency exits are available as follows: At least ÿÿÿÿÿÿÿÿcabin emergency exit is unobstructed.

A

One

112
Q

Access to the rear of the aircraft and entry into cargo or baggage areas, or emergency exits ÿÿÿÿÿÿÿÿÿÿ be maintained without exception. No less than 30 inch by 14 inch space will be provided.

A

Must

113
Q

________ allow passengers to lounge on or tamper with equipment, cargo, or baggage.

A

Do not

114
Q

Customs, Immigration, and Agriculture require certain forms for ________. The loadmaster will ensure that required forms are contained in the aircraft mission kit.

A

BORDER CLEARANCE

115
Q

Mission permitting, fueling the aircraft in excess of _____ pounds the night prior should be avoided when practical. Thermal expansion overnight sometimes results in excessive venting. Consider this in your mission planning.

A

6500

116
Q

Loadmasters not current in an event must fly with an Instructor _____ to regain currency. For Loadmasters not current in NVG operations only, an Instructor Pilot may fulfill this requirement.

A

Loadmaster

117
Q

Crewmembers _____ change between military uniforms and civilian attire during any single flight duty period (FDP).

A

Will not

118
Q

Crewmembers will not mix ______ issue clothing items and civilian attire (such as boots, belts, or jackets).

A

MILITARY

119
Q

The Aircraft Commander _____ be notified if any crew member must arrive more than 30 minutes prior to the normal show time.

A

Should

120
Q

Emergency Ground Evacuation. Conditions permitting, the primary emergency exit for both crew and passengers will be the

A

Crew entrance door

121
Q

When directed, the _____ should initiate the evacuation of all passengers through the selected emergency exit. The flight crew should be notified by the Loadmaster of the selected exit and any hazards or issues.

A

Loadmaster

122
Q

A rally point will should be established ____ at a ____ angle away from the aircraft centerline on the side exited.

A

300 FT / 45 DEGREE

123
Q

When all personnel are accounted for, determine if it is necessary to ______separation from the aircraft.

A

Increase

124
Q

Prior to conducting reverse operations the _____ will conduct a thorough reverse taxi briefing using the 524 SOS IFG.

A

Loadmaster

125
Q

The _______ will conduct mission communications, as directed by the Aircraft Commander, and relay pertinent information to the pilots when necessary.

A

LOADMASTER

126
Q

The loadmasters ______ provide torque call-outs starting at 70% TQ.

A

Will

127
Q

The loadmasters will announce ?_______? over the interphone when the engine torque reaches either 100% TQ or the green torque markers, whichever is lower. The PNF will verbally acknowledge the call. This restriction does not apply to enhanced field performance operations.

A

TORQUE

128
Q

Full stop landings and touch and go landings are limited to a maximum of _____ per flight hour.

A

10

129
Q

Unless considerations dictate otherwise, the Pilot?s TCAS should be placed in _______ and the Copilot?s TCAS will be in _______.

A

ABOVE / BELOW

130
Q

After landing, the Loadmasters ______ remain seated until the aircraft has taxied clear of the runway, at which point the Loadmaster may leave the jump seat to perform duties for the After Landing Checklist.

A

Will

131
Q

NVG Operations. The first crew member to positively identify an airfield of intended landing should notify the remaining crew by stating ?________? Subsequent crew members identifying the airfield should also state ?airfield in sight,? and confirm with the first crew member using clock position and approximate distance.

A

AIRFIELD IN SIGHT

132
Q

Any time the aircraft will be _________ by U.S. military or diplomatic personnel, the aircraft will have all emergency exits pinned and the cargo door will be locked or secured with a strap to prohibit entry.

A

UNATTENDED

133
Q

If the ______ cannot be secured with an approved lock, tamper-evident seals should be utilized. Tamper evident tape or distinctive numbered seals satisfy this requirement.

A

crew entry door

134
Q

Maximum weight limit of the aircraft mounted safe is ____ lbs. and lock boxes will not be used to store liquids of any kind.

A

20

135
Q

Weapons ______ be stored in the aircraft lock box or kept in a holster on the crew member at all times.

A

Will

136
Q

Maintain a _____ ft circle of safety from all parts of the aircraft except when authorized in certain loading, unloading, or fueling operations. In these cases, always post guides (spotters) and place wheel chocks in position to prevent the vehicle from backing into the aircraft.

A

10

137
Q

Vehicles must not be driven towards the aircraft when within ft.

A

25

138
Q

Base fire marshals prohibit smoking on flight lines, on aprons, in hangars, or on aircraft parking areas except in designated areas. At no time is smoking allowed within ft of an aircraft, fuel tanks, fueling operations, or any flammable substance storage facility.

A

50

139
Q

Do not use any radios on an aircraft that is being fueled. Do not transmit on a high frequency (HF) radio when fueling operations are being performed within ft of the aircraft.

A

200

140
Q

Aircrew must conduct HAZMAT transportation IAW _______.

A

AFMAN 24-204

141
Q

Performing Routine Steward?s Duties: As the most ____ crewmember during the flight, your conduct reflects upon the whole crew. So act as if the whole crew?s image depends on your actions.

A

VISIBLE

142
Q

MEASUREMENTS AND CONVERSIONS: = PSF.

A

PSI x 144 = PSF

143
Q

MEASUREMENTS AND CONVERSIONS: =50 PSI.

A

3.45 Bar = 50 Psi

144
Q

CARGO SHALL ONLY BE ATTACHED TO SEAT TRACKS AT THE PAINTED ÿÿÿÿÿÿÿÿÿÿÿÿÿÿÿÿÿÿLOCATIONS.

A

GREEN

145
Q

1 maximum allowable loading: 75 lb/ft2, lb total.

A

771

146
Q

The cargo door dimensions are: .

A

55.1in x 36.2in

147
Q

The service door dimensions are: .

A

49.2in x 20in

148
Q

The passenger/crew door dimensions are: .

A

66.9in x 30.2in

149
Q

The dimensions of the two emergency exit hatches are: .

A

35.8in x 20in

150
Q

Pounds per square inch (psi) is derived by ______ the weight of an item by the area bearing on the cargo floor, in square inches (in2).

A

DIVIDING

151
Q

USE ANY TYPE OF LEVER OR MECHANICAL MEANS TO ASSIST HAND RATCHETING OF THE STRAPS.

A

DO NOT

152
Q

A MINIMUM OF ____ TURNS ON THE SPOOL MUST BE MAINTAINED TO PREVENT THE STRAP FROM COMING UNSECURe

A

«

153
Q

The _____ include a continuous and permanent record of aircraft weight, moment, and CG position. This is sometimes referred to as Chart C.

A

AIRCRAFT FORMS

154
Q

What is the WAM formula?

A

Weight x Arm = Moment

155
Q

Configuration one consists of ______ passenger seats and approximately 294 ft3 of cargo space.

A

27

156
Q

Configuration 2 consists of two options, each providing approximately 294 ft3 of cargo space. Option 2A consists of passenger seats plus four litters. Option 2B replaces one litter rack assembly with three rows of dual seats ( seats and 2 litters).

A

15/21

157
Q

Configuration 3 consists of ____ passenger seats and approximately 470 ft3 of cargo space.

A

18

158
Q

Configuration 4 consists of up to _____ passenger seats, two litters, and approx. 470 ft3 of cargo space.

A

12

159
Q

Configuration 5 consists of_____ passenger seats and approximately 971 ft3 of cargo space aft of the smoke barrier at FS 298.

A

4

160
Q

BLOCK 20 TWO-WAY COMMUNICATION SYSTEM: The aft most plug may be used for reverse taxi operations by the loadmaster. All three plugs in the ceiling are tied to the _________ ICS system.

A

OBSERVER’S

161
Q

The C-146A utility seats are similar to commercial aviation-style seats. A single seat weighs lb and a double seat weighs lb.

A

19.8/34.4

162
Q

A folded single seat has a weight bearing capacity of lbs.

A

150

163
Q

A folded double seat has a weight bearing capacity of lbs.

A

200

164
Q

A double litter stacking system weighs ____ lbs.

A

133

165
Q

Aisle clearance at its smallest point is _____ in.

A

20.7

166
Q

[Block 20] Two IV hangars are provided for the litter patients. They are placarded ?For IV Use Only? and have a _ lb IV bag maximum limit.

A

5

167
Q

[Block 20] The medical bag together with its contents is limited to lb.

A

100

168
Q

The APU bleed air is fed into the cross-bleed line through a check valve and supplies the ECS . The APU bleed air supply is controlled by an APU BLEED switch/light located on the ECS control panel.

A

Packs

169
Q

The ACP?s are divided into two groups: ______ & _____ ACP 1,2 and 5 are in the Flight Deck Group; ACP?s 3,4 and 6 are in the Cabin Group

A

FLIGHT DECK / CABIN

170
Q

The flight controls consists of the following components and subsystems:

A

Ailerons and Trim Tab, Rubber and Trim Tab, Elevator and Trim Tab, Flaps, Ground Spoilers, Gust Locks and Damper, Stall Warning and Prevention.

171
Q

Fuel transfer within each tank group is made by ______ pumps in the inner and the outer wing tanks. These pumps supply fuel to the feeder tank to keep in in the full state during aircraft operation. outer wing tanks. These pumps supply fuel to the feeder tank to keep in in the full state during aircraft operation.

A

jet transfer

172
Q

When the left or right electrical booster pump (ELPMP) ______ button is in normal mode (dark), the electrical booster pump is triggered to activate automatically if there is a failure in the jet booster pump (JETPMP).

A

AUTO

173
Q

_fuel is taken from the right wing tank group, via the tapping in the main engine cross-feed pipeline.

A

APU

174
Q

A system of float-operated manual magnetic indicators (magna-sticks) can be used on the ground when no _power is available to determine the quantity of fuel in the tanks.

A

Electrical

175
Q

The fuel system receives electrical power from the 28 VDC ESSENTIAL BUS, DC HOT BUS 2, 28 VDC BUS 1, and 28 VDC BUS 2. The circuit breakers of the fuel system are installed on the circuit breaker panel in the flight compartment.

A

Overhead

176
Q

The left and right wing tank groups can be gravity refueled through a ________ with lockable cap in the inner fuel tank.

A

FILLER WELL

177
Q

The ______ valves allow the fuel to flow from the inner and the outer tanks into the feeder tank. They do not permit the fuel to flow back again.

A

Flapper

178
Q

There are ______ drain valves in each fuel tank group. The drain valves are provided for draining condensed water and fuel samples.

A

5

179
Q

The inner and outer tanks of each wing tank group are vented to the atmosphere by the following components:

A

Main Vent Line, Vent Float Valves, Vent Tank, Flush Inlet and Overboard Vent Line.

180
Q

The aircraft hydraulic system consists of the following four:

A

Main Hydraulic System, Standby Hydraulic System, Auxiliary System, Indicating System.

181
Q

The main system supplies hydraulic pressure to the following consumers:

A

Landing Gear, Main Landing Gear Wheel Brakes, Emergency and Parking Brake, Trailing Edge Flaps, Nose Wheel Steering, Roll Spoilers, Ground Spoilers.

182
Q

The ______ are externally bonded into a recessed portion of the leading edges on the wing and the vertical and horizontal stabilizer.

A

DE-ICER BOOTS

183
Q

The propeller de-icing system prevents or eliminates ice formation on the propellers. This is done by ____ heating de-icer boots on each blade.

A

Electrically