Master Question File Flashcards
1
Q
Where can the crash axe be found?
A
In the flight compartment step
AOH V1 pg. 2-11
2
Q
The following emergency equipment is located with the crash axe:
A
Protective breathing equipment and fire extinguisher
AOH V1 pg. 2-11
3
Q
What is the maximum takeoff weight?
A
30,843 lbs
AOH V1 pg. 5-2
4
Q
What is the maximum landing weight?
A
29,167 lbs
AOH V1 pg. 5-2
5
Q
What is the maximum speed for Flaps 12*?
A
200 KIAS
AOH V1 pg. 5-14
6
Q
What is the maximum speed for Flaps 32*?
A
160 KIAS
AOH V1 pg. 5-14
7
Q
What is the Maximum allowable ITT on an engine start?
A
950
AOH V1 pg. 5-15
8
Q
What is the maximum tailwind component for takeoff and landing?
A
10 kts
AOH V1 pg. 5-38
9
Q
You will get a fuel asymmetry indication when your fuel imbalance exceeds…
A
210 lbs
AOH V1 pg. 5-19
10
Q
The APU shall not be started above ______ft pressure altitude.
A
20,000
AOH V1 pg. 5-17
11
Q
Maximum Altitude for ECS Single Pack Operations is ________?
A
25,000 ft
AOH V1 pg. 5-32
12
Q
The pressurization systems maximum differential pressure is _______?
A
6.9 psi
AOH V1 5-32
13
Q
The pressurization systems maximum differential pressure for Landing is _______?
A
0.4 psi
AOH V1 pg. 5-32
14
Q
Maximum altitude with flaps extended is ________?
A
18,000 ft MSL
AOH V1 pg. 5-36
15
Q
Maximum altitude for landing gear operation is _______?
A
18,000 ft MSL
AOH V1 pg. 5-36
16
Q
Flights above 27,000 ft are limited to less than _____ hours.
A
3
AOH V2 pg. 5-38
17
Q
Maximum demonstrated crosswind for takeoff/landing-Dry runway ____ Wet runway____
A
21 kt and 21 kt
AOH V1 pg. 5-38
18
Q
After landing on unpaved runways do not select reverse bellow _____ KIAS to avoid foreign object ingestion/damage.
A
55
AOH V1 pg. 5-39
19
Q
The propeller de-icing system must be activated during all ground and flight operations when icing conditions exist.
A
True
AOH V1 pg. 5-46
20
Q
The maximum holding airspeed is _____ kts.
A
175
AOH V1 pg. 6-10
21
Q
What is the minimum flight weight of the C-146A?
A
20,724 lbs
AOH V2.1 pg. 8-1
22
Q
What is the maximum operating altitude?
A
FL310
AOH V2.1 pg. 8-1
23
Q
The number of plug type emergency exist in the passenger compartment is:
A
2
AOH V2.1 pg. 8-1
24
Q
What is the wheel base for the C-146A?
A
10 ft 7 inches
AOH V2.1 pg. 8-2 (Aircraft Overview)
25
Up to _______ emergency exist are in the passenger compartment
four
| AOH V2.1 pg. 8-4
26
All cabin doors can be used as:
Emergency exits
| AOH V2.1 pg. 8-4
27
The purpose of the ELPMP in the feeder tank is:
To provide fuel pressure for starting and act as a backup for the jet booster pumps.
AOH V2.1 pg. 8-12
28
When the flight crew presses the EMG CALL button on the crew station:
The EMG button in the flight deck flashes on indicate an emergency call
AOH V2.1 pg. 8-217
29
Which aircraft components are the primary suppliers of DC current in normal operations?
2 starter/generators and 2 24V, 42hn lead-acid batteries
| AOH V2.1 pg. 8-257/8-264
30
Under normal flight condition DC power is generated by:
Two DC starter/generators
| AOH V2.1 pg. 8-257/8-264
31
What is the function of the TRU?
To convert AC power to DC power
| AOH V2.1 pg. 8-268
32
When DC external power is connected:
The two batteries and the two starter generators are automatically disconnected
AOH V2.1 pg. 8-274
33
In the wings tanks, the following pumps are installed:
Electrical boost pumps and jet pumps
| AOH V2.1 pg. 8-524
34
The APU normally draws fuel from:
The RH wing tank group
| AOH V2.1 pg. 8-524
35
Fuel transfer between the inner and outer tanks to the feeder tank is accomplished by:
Jet transfer pumps
| AOH V2.1 pg. 8-524
36
The purpose of the jet transfer pumps is:
To keep the feeder tank full
| AOH V2.1 pg. 8-524
37
It is possible to transfer fuel from one tank group to the other:
On the ground from the refuel/defuel panel
| AOH V2.1 pg. 8-566
38
Fuel quantity is indicated on:
```
On EICAS main page, fuel sys page, and the RMU
By magna sticks
On the refuel/defuel panel
AKA all of the above
AOH V2.1 pg. 8-527, 8-593, 8-530
```
39
If a malfunction occurs in either sensing element loop or its associated wiring, the:
LOOP FAIL indicators of fire warning extinguisher panel comes on
AOH V2.1 pg. 8-321
40
Verification of the fired bottle discharge can be assured:
By the white DIS light in the squib push-button
| AOH V2.1 pg. 8-320 (fig 8-142)
41
When an engine fire is indicated, the control unit produces a fire signal which causes:
Aural warning on the loud speakers and headphones sounds.
The LH,RH ENG fire field on the red warning panel illuminates
The ENG LH fire light/switch illuminates
AKA all of the above
AOH V2.1 pg. 8-329
42
Discharging the fire bottle is accomplished:
By pushing the squib push-button after the squib has been armed
AOH V2.1 pg. 8-320 (fig 8-142)
43
The engine fire extinguishing system:
Has four extinguishing bottles, two for each engine
| AOH V2.1 pg. 8-318
44
They hydraulic system consist of:
Main, standby, auxiliary
| AOH V2.1 pg. 8-605
45
The power source for the hydraulic main pump is:
AC variable power
| AOH V2.1 pg. 8-614
46
The power source for standby pump is:
DC 28 V
| AOH V2.1 pg. 8-640
47
Hydraulic consumers are:
Landing gear, main brake, E/P brake, nose wheel steering, wing flaps, roll spoilers, and ground spoilers
AOH V2.1 pg. 8-607
48
The standby pump switch selection during normal operation is:
AUTO
| AOH V2.1 pg. 8-644
49
The standby pump in the auto mode will switch on:
If the system pressure drops bellow 1958 psi
| AOH V2.1 pg. 8-646, 8-650
50
The accumulators are used by:
Main system, normal brakes and E/P brakes
| AOH V2.1 pg. 8-624, 8-658
51
With the standby hydraulic selector on the control panel selected with the MAN position:
The DC pump runs continuously
| AOH V2.1 pg. 8-650
52
The hydraulically operated flight controls are:
The flaps and roll spoilers
| AOH V2.1 pg. 8-607
53
Flaps are:
Electrically controlled and hydraulically operated
| AOH V2.1 pg. 8-440
54
The emergency brake system uses supply pressure from:
The main hydraulic system and/or the E/P brake accumulator
| AOH V2.1 pg. 8-507, 8-658
55
In order to extend the gear during an abnormal gear extension, the manual selector valve must be:
In the landing gear emergency extension position
| AOH V2.1 pg. 8-659
56
What is the total fuel capacity (manual)?
7531 lbs
| AOH V2.1 pg. 8-532
57
How is an impending fuel imbalance notification indicated?
A blue advisory CAS message
| AOH V2.1 pg. 8-597
58
Which of the following will not trigger a T/O CONF warning?
Ground Spoilers armed
| AOH V2.1 pg. 8-941
59
A caution is presented by a:
Single chime, a message on the CAS field, and an indication (when applicable) on the system page
AOH V2.1 pg. 8-928
60
Four stairway lights, integrated into the stairs of the crew/passenger entrance door, are activated by:
The STAIR switch on the loadmaster's panel
| AOH V2.2 pg. 8-1094
61
The emergency lights can be activated:
Automatically if the main aircraft power supply fails
Manually be a switch on the loadmaster's panel
AKA both a & b
AOH V2.2 pg. 8-1096
62
External emergency lights are located:
Adjacent to the emergency exit doors
| AOH V2.2 pg. 8-1100
63
What is the power source when the cargo lighting system is set to TIMER?
Battery voltage via the DC HOT BUS 1
| AOH V2.2 pg. 8-1076
64
The oxygen system consists of:
An oxygen bottle system for crew and passengers
| AOH V2.2 pg. 8-1295
65
When the cockpit oxygen masks are used:
The microphone control must be switched over on the audio control panel
AOH V2.2 pg. 8-1308
66
The crew oxygen masks are equipped with:
Manual selector with Normal, 100%, and Emergency settings
| AOH V2.2 pg. 8-1307
67
The purpose of the PAX SUPPLY guarded pushbutton on the overhead panel is:
To switch off the passenger oxygen system when desired
| AOH V2.2 pg. 8-1316
68
The oxygen bottle quantity can be checked:
On the CPCS/Oxygen system page
| AOH V2.2 pg. 8-1319
69
The oxygen supply for the passengers is made available by the:
```
Altitude switch
Manual drop-out switch
Separation valve
AKA all of the above
AOH V2.2 pg. 8-1310
```
70
What are the conditions necessary to supply oxygen to the passengers?
Solenoid valve open, cabin altitude above 10,000'
| AOH V2.2 pg. 8-1301, 8-1311
71
The dropout oxygen masks are activated automatically by an altitude switch if the aircraft suffers decompression with a cabin altitude greater than _________. When the aircraft descends bellow ________ the oxygen supply to the dropout units is stopped:
13,800 ft +- 700 ft; 10,000 ft
| AOH V2.2 pg. 8-1311
72
To prevent smoke or fumes entering the mask or smoke goggles:
Select EMER on demand regulator
| AOH V2.2 pg. 8-1307, 8-1309
73
The function of the X-Bleed valve is:
To supply bleed air to both packs from one engine
To supply bleed air to both packs from the APU
AKA both a and c
AOH V2.2 pg. 8-1351
74
Which systems are supplied by bleed air?
The de-icing system
Then air conditioning system
AKA both a and b
AOH V2.2 pg. 8-1334, 8-1335
75
A bleed air leak is indicated on:
The EICAS system page
| AOH V2.2 pg. 8-1348
76
The gust lock is designed to protect:
The elevators and ailerons
| AOH V2.2 pg. 8-1628
77
What is the main purpose of the condition levers?
To set the required propeller RPM
| AOH V2.2 pg. 8-1511
78
What positions/ranges are there for the condition levers?
Fuel off, feather, min, high taxi, maximum (not placated)
| AOH V2.2 pg. 8-1515
79
APU is ready to accept electrical and/or bleed air loads is indicated by?
READY TO LOAD on the APU system page
| AOH V2.2 pg. 8-1440 (Table 8-125)
80
If an APU OVERSPEED is displayed on the APU system page, the following will happen:
The APU will shut down both in flight and on ground
| AOH V2.2 pg. 8-1440 (Table 8-125)
81
When the APU master switch/light is pressed and the ON caption comes on the following occurs:
Electrical power (28vDC) is supplied to the START switch/light and to the APUT electronic control unit (ECU)
APU fuel shut-off valve moves to the open position
AKA both a and b
AOH V2.2 pg. 8-1392
82
Maintain a _____ circle of safety from all parts of the aircraft except when authorized in certain loading, unloading, or fueling operations.
10 feet
| AOH V4 pg. 11-9
83
When vehicles are left unattended on the flight line you must:
```
Install chocks (when near an aircraft)
Turn off the ignition
Leave key in ignition
Place transmission in low gear or "park" position
AKA all of the above
AOH V4 pg. 11-09
```
84
There are two ________ in emergency exit passenger hatches in the cabin, one in the front of the cabin on the right side directly opposite from the crew/passenger door and one on the left side just aft of the trailing edge of the wing.
20x35.8 in
| AOH V4 pg. 11-109
85
The cargo door dimensions are
55.1x36.2 in
| AOH V4 pg. 11-109
86
The service door dimensions are:
49.2x20 in
| AOH V4 pg. 11-109
87
A single seat weights ______ and a double seat weights ________.
19.8 lbs and 34.4 lbs
| AOH V4 pg. 13-13
88
Each double-deck litter rack assembly weighs ______.
133 lbs
| AOH V4 pg.13-13
89
A minimum of _______ turn on the spool must be maintained to prevent the strap from coming unsecure.
1/2
| AOH V4 pg. 11-125
90
The green marks on the cargo floor seat tracks indicate ____________.
Cargo hold down attachment points
| AOH V4 pg. 11-91
91
When the fuel load is unknown, load plan for a ______ percent of mean aerodynamic chord (MAC) zero fuel.
21-40
| AOH V4 pg. 11-108
92
What is the formula for PSI of a wheeled load?
wheel load/pad area = psi
| AOH V4 pg. 11-123
93
Configuration One allows for ________ passengers.
27
| AOH V4 pg. 13-4
94
Configuration two allows for ________ passengers.
15 plus four litters or 21 plus two litters
| AOH V4 pg. 13-5
95
Configuration three allows for _______ passengers.
18
| AOH V4 pg. 13-6
96
Configuration four allows for _______ passengers.
12 plus two litters
| AOH V4 pg. 13-6
97
Configuration five allows for ________ passengers.
4
| AOH V4 pg. 13-7
98
_________ indicate(s) a mandatory requirement.
"Must", "Will" and "Shall"
| AFSOCI 11-2C-146A V3 (ISG), pg. 2 para 1.3.1
99
________ indicates a recommended procedure.
Should
| AFSOCI 11-2C-146A V3 (ISG), pg. 2 para 1.3.2
100
________ indicates an acceptable or suggested means of accomplishment.
May
| AFSOCI 11-2C-146A V3 (ISG), pg. 2 para 1.3.3
101
_______ indicates operating procedures, techniques, etc., which will result in personal injury or loss of life if not carefully followed.
WARNING
| AFSOCI 11-2C-146A V3 (ISG), pg. 2 PARA 1.3.4
102
_______ indicates operating procedures, techniques, etc., which will result in damage to equipment if not carefully followed.
CAUTION
| AFSOCI 11-2C-146A V3 (ISG), pg. 2 para 1.3.5
103
_______ indicates operating procedures, techniques, etc., which are essential to emphasis.
NOTE
| AFSOCI 11-2C-146A V3 (ISG), pg. 2 para 1.3.6
104
A minimum of one additional pilot or one loadmaster is required when carrying more than _____ passengers.
10
| AFSOCI 11-2C-146A V3 (ISG), pg. 7 para 3.2.1
105
Crewmembers occupying a primary crew position will have seat belts fastened ________.
At all times
| AFSOCI 11-2C-146A V3 (ISG), pg. 11 para 5.3.1
106
Floor loading is authorized to support dedicated __________ during contingencies, exercises, or training.
Special operations forces team members or liter medical patients
AFSOCI 11-2C-146A V3 (ISG), pg. 11 para 5.3.3
107
Accomplish alternate passenger restraints by one of the following methods in descending order of preference:
Seatbelts or snap links attached to tie-down rings on the cabin floor.
Five thousand (5000) pound tie-down straps
AKA a and b
AFSOCI 11-2C-146A V3 (ISG), pg. 11 para 5.3.3.2
108
Aircrew will complete before landing checklist no lower than:
200 ft AGL
| AFSOCI 11-2C-146A V3 (ISG), pg. 11 para 5.1.4
109
Taxi width. Minimum width for all operations ________.
22 feet
| AFSOCI 11-2C-146A V3 (ISG), pg. 13 para 5.7.2.1
110
Without wing walkers, avoid taxi obstructions by at least ______ feet.
25
| AFSOCI 11-2C-146A V3 (ISG), pg. 12 para 5.6.1
111
With wing walkers, avoid taxi obstruction by at least _____ feet.
10
| AFSOCI 11-2C-146A V3 (ISG), pg. 12 para 5.6.1
112
Runway width. Minimum width for normal operations is ________.
35 feet
| AFSOCI 11-2C-146A V3 (ISG), pg. 13 para 5.7.2.2
113
Identification tags should be worn around the neck or carried in a flight suit pocket. If identification tags are not carried, member will carry a military issue _______.
Identification card
| AFSOCI 11-2C-146A V3 (ISG), pg. 20 para 6.2.3
114
A _______ are required on ALL flights.
Headset and operable flashlight
| AFSOCI 11-2C-146A V3 (ISG), pg. 20 para 6.2.6
115
Crew members will remove ___________ before performing aircrew duties.
Rings and scarves
| AFSOCI 11-2C-146A V3 (ISG), pg. 20 para 6.2.4
116
Each crew member is required to carry an EFB with current publications. Crews will ensure paper backup copies of required in-flight publications are carried unless approved for paperless cockpit transition.
True
| AFSOCI 11-2C-146A V3 (ISG), pg. 21 para 6.4.3
117
Passenger Briefings. Prior to each flight, the loadmaster will ensure that all passengers are briefed.
Prior to each flight
| AFSOCI 11-2C-146A V3 (ISG), pg. 23 para 6.11.2
118
Minimum Fuel is _____ pounds and Emergency Fuel is 250 pounds.
450
| AFSOCI 11-2C-146A V3 (ISG), pg. 24 para 6.18.6
119
Anti-exposure suits for the aircrew will be readily available during any preplanned overwater flights which are beyond power off gliding distance from land and the water temperature is _____ Fahrenheit (F)/(16*C) or less.
60
| AFSOCI 11-2C-146A V3 (ISG), pg. 28 para 6.28.3
120
_______ accept hazardous materials unless proper documentation, certification, and identification of cargo are provided.
Do not
| AFSOCI 11-2C-146A V3 (ISG), pg. 34 para 6.50.2
121
If an armed crew member must leave the crew en route, transfer the weapon to another authorized crew member using _______.
AF Form 1297, Temporary issue Receipt
| AFSOCI 11-2C-146A V3 (ISG), pg. 40 para 7.5.1
122
Due to the sensitivity of weapons in foreign countries, crews will keep their weapons
Inside the aircraft and out of sight of foreign nations
| AFSOCI 11-2C-146A V3 (ISG), pg. 40 para 7.5.3.1
123
Weapons need not be ________ before being placed in the gun box.
Unloaded
| AFSOCI 11-2C-146A V3 (ISG), pg. 40 para 7.5.4
124
If individuals must clear their weapons before boarding the aircraft, and access to clearing barrel/facilities is limited, as a minimum, direct them to : move to a safe, clear area at least _____ feet from any aircraft, equipment, or personnel before upholstering/unslinging their weapons.
50
| AFSOCI 11-2C-146A V3 (ISG), pg. 41 para 7.6.2.1.1
125
Passengers may be anti-hijack inspected at the aircraft by ________ if no passenger processing facility exist.
The aircrew
| AFSOCI 11-2C-146A V3 (ISG), pg. 41 para 7.6.1
126
Loadmasters in-flight duties include but not limited to ____________.
airspeeds, altitudes, headings, TCAS, monitoring systems
| AFSOCI 11-2C-146A V3 (ISG), pg. 42 para 8.1.3
127
Load aircraft in such a manner that emergency exits are available as follows: Emergency Exits and Safety Aisles: At least ______ cabin emergency exits is unobstructed.
One
| AFSOCI 11-2C-146A V3 (ISG), pg. 42 para 8.3.1
128
Access to the rear of the aircraft and entry into cargo or baggage areas, or emergency exits must be maintained without exception. No less then __________ space will be provided.
30 inch by 14 inch
| AFSOCI 11-2C-146A V3 (ISG), pg. 42 para 8.3.3
129
________ passengers to lounge on or tamper with equipment, cargo, or baggage.
Do not allow
| AFSOCI 11-2C-146A V3 (ISG), pg. 43 para 8.6.2
130
Ensure ________ remains covered during the entire mission when passengers are on board and ensure passengers are denied access to this equipment.
Classified equipment
| AFSOCI 11-2C-146A V3 (ISG), pg. 43 para 8.6.3
131
__________ with quick release is authorized as restraint for specific SOF operations.
Pig tails
| AFSOCI 11-2C-146A V3 (ISG), pg. 43 para 8.6.4
132
Cellular phones must be turned off and stowed from the time ________ clear of the runway after landing.
the aircraft leaves parking its parking spot
| AFI 11-202 V3, para 2.9.1
133
When shipping Hazardous Cargo who is ultimately responsible?
The pilot in command
| AFI 11-202 V3, para 2.12
134
Supplemental oxygen must be used by all persons while above _______ ft MSL.
14,000
| AFI 11-202 V3, para para 6.4.1.3
135
Individuals suspected of DCS should be administered and remain on _________ (using tight-fitting mask or equivalent) until evaluated by competent aviation medical authority.
100% oxygen
| AFI 11-202 V3, para 6.4.4
136
An alert crew will not remain in alert status for more then ____ consecutive ____ hour periods.
2, 72
| AFI 11-202 V3 AFSOC Sup 1, para 9.5.9
137
Landing lights will be illuminated bellow _______ ft.
10,000 ft MSL
| AFI 11-202 V3 para 5.20.5.1
138
If the autopilot is not operational or its use is denied for more than 4 hours (8 hours augmented), the FDP will be ______ hours (16 hours augmented).
12
| AFI 11-202 V3 AFSOC Sup 1, para 9.7.7.5
139
Post mission crew rest is computed at the rate of _____ hour off for each _____ hours off-station, up to 96 hours.
1, 3
| AFI 11-202 V3 AFSOC Sup 1, para 9.8.9.1
140
Aircrew members will not fly within 72 hours after donating blood, plasma or bone marrow. The flying unit commander must approve donation of blood, plasma or bone marrow by aircrew members.
True
| AFI 11-202 V3, para 9.11.3.3
141
Aircrew members will not fly within ____ hours of consuming alcohol or while impaired by its after effects.
12
| AFI 11-202 V3, para 9.11.3.4
142
What MUST the shipper provide on the Shipper's Declaration of Dangerous Goods when transporting hazardous material?
24-hr emergency response phone number
| AFMAN 24-204 pg. 13
143
HAZMAT. What are "P" codes?
Passenger Eligibility codes
| AFMAN 24-204 pg. 14
144
What is a Chapter 3 Movement?
Tactical, contingency, or emergency airlift
| AFMAN 24-204 pg. 18
145
A Shipper's Declaration for Dangerous Goods is not required for Chapter 3 movement.
True
| AFMAN 24-204 pg. 20
146
In the absence of an Air Cargo Manifest, the ______________ form may serve as a shipping paper.
Shipper's Declaration for Dangerous Goods
| AFMAN 24-204 pg. 39
147
What mark on the segregation table indicates that articles may not be loaded, transported, or stored together unless separated by a distance of 88 inches in all directions?
O
AFMAN 24-204 pg. 453
148
What mark on the segregation table indicates that articles must not be loaded, transported, or store together?
X
| AFMAN 24-204 pg. 543
