Brainscape's Knowledge GenomeTM


Top Flashcards (Certified)
All Flashcards

Global Express > Oral Exam > Flashcards

Oral Exam Flashcards

1
Q

Max Taxi/Ramp Weight

A

98,250 lb

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

Max Takeoff

A

98,000 lb

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

Max Landing

A

78,600 lb

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

Max Zero Fuel

A

56,000 lb

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

What do you do for takeoffs or forced landings near bodies of water?

A

At weights above max landing, outflow valve #2 must be closed and one air conditioning pack must be shut down for takeoff and landing

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

Where is outflow #2 located?

A

Rear of aircraft

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

Why do you need to shut down one AC pack when outflow #2 is off?

A

Since you reduced the outflow by 1/2, you must reduce the inflow by 1/2

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

Max airport pressure altitude takeoff and landing?

A

10,000 PA

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

Max operation altitude

A

FL510

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

Max OAT takeoff/landing

A

+50C (122F)

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

Min OAT takeoff/landing

A

-40C

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

Cowl Anti-Ice - what mode do you need to be in for takeoff? Why?

A

Takeoff in auto is prohibited, because anti-ice is inhibited on the ground and to 400’ AGL after takeoff

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

Cowl Anti-Ice - when must anti ice be on?

A

Anti-Ice on OAT 10C (50F) or below, visible moisture in any form is present such as fog with vis less than 1 mile
Must also be on OAT 10C or below when operating on runways, ramps, taxiways where surface snow, ice, standing water, or slush is present

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

Cowl Anti-Ice - in flight operation

A

Must be on when in icing conditions or when ICE is annunciated by the ice detection system (visible moisture with TAT less than 10C)

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

Wing Anti-Ice - when must anti ice be on?

A

Must be on for takeoff when the OAT is 5C (41F) or below and visible moisture in any form is present, visibility of 1 mile, runway is contaminated
When Type II or Type IV anti icing fluids have been applied, the wing anti ice system must be selected On, if required, just prior to thrust increase for takeoff

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

Wing Anti-Ice - inflight operations

A

Must be on when in icing conditions or when ICE is annunciated by the ice detection system
Must be on when icing conditions exist in flight at a TAT of 10C or below and visible moisture, except when the SAT is -40C or below

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

Is there any limitation for holding in icing conditions?

A

Do not hold in icing conditions with the slats extended

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

What is the minimum engine speed for flight in icing conditions?

A

76% N1

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

What are the maximum runway slops?

A

+/-2%

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

What is the Max tailwind for takeoff and landing?

A

10kts

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

What is the Max tailwind for engine start?

A

20kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

What is the tailwind start procedure?

A

EICAS indications of N1 rotation: crank engine for 30sec, then select auto start, followed by selecting the ENG RUN switch to run (pause between AUTO and ENG RUN switch)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

What is the taxi procedure when winds exceed 20kts?

A

Do not exceed idle thrust for taxi

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

What is the procedure for takeoff when crosswind component exceeds 20kts?

A

Do not exceed 66% N1 below 30 KIAS (due to possible compressor stall)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
How much additional runway is required for a rolling start?
1000 ft
26
How much additional runway is required for a crosswind rolling takeoff flaps 16? Flaps 6?
Flaps 16 - 1500 ft Flaps 6 - 1700 ft
27
Engine?
BR700-710A-20
28
Start ITT
GND - 700C AIR - 850C
29
Engine Idle
58.0% N1 (minimum)
30
Engine takeoff
99.6 N2, 102.0 N1, 900 ITT
31
Static ground run in the range of _ to _ is prohibited
66% - 80% N1 Acceleration and deceleration through this range is permitted. Not applicable to reverse thrust
32
Reverse thrust
70.0 N1 (30 secs)
33
Min Oil Temp - Start
-40C
34
Min acceleration above idle
20C
35
Max Oil Temp
160C
36
Min Oil Pressure (continue flight)
35 PSI
37
Shut Down Oil Pressure
25 PSI
38
When is operation of oil replenishment system prohibited?
When OAT is -12C or less (engines can be reoiled 5-45 min, APU 30 min per mx manual)
39
What are the starter cranking limits?
3 consecutive engine start cycles of 3 mins with a 15 sec cooling between cycles. After 3 attempts, 15 min cool down is required. Dry motoring/cranking are the same as engine start and is preformed with the ENG RUN switches OFF
40
Starter Re-engage Max N2
42% N2
41
Useable fuel - main tanks
15,050 lb/wing
42
Usable fuel - center tank
11,150 lb
43
Usable fuel - aft tank
2,300 lb
44
Total usable fuel
43,550 lb
45
Max fuel imbalance during flight
1,100 lb
46
Max fuel imbalance on ground
<19,450 - 1,100 lb >20,250 - 600 lb
47
How does fuel get loaded?
Wings, Aft, Center
48
What is the engine fuel burn sequence?
Winds to 93%, then from the center tank into the wings to 97%, then to the wings to 5,500 lb, then aft tank transfer to wings
49
When do the DC aux pumps come on automatically?
Engine and APU starting Wing to wing transfer When AC pump fails During takeoff and landing with the engine on and at least one of the following: flaps >0, landing gear down (in flight), low wing fuel condition of 600 lb/wing
50
When does the auto fuel transfer come on?
400 lb fuel imbalance
51
Does the auto fuel transfer continue to work with an AC pump failure?
No
52
How would you transfer fuel after an AC pump fails?
Use the wing transfer switch on the overhead
53
When would you use fuel crossfeed?
1) during single engine operations 2) cross feed open and shut off the pumps on the “light side of the A/C, so the heavy side can feed both engines”
54
How to close the engine feed SOVs?
The fuel shut off valves are commandeered closed when the fire handle is pulled (HOSOV in the fuel metering unit are commanded closed with the ENG RUN switch)
55
What is the normal fuel Temp for takeoff?
5-43C (takeoff with the engine fuel <5C is prohibited, takeoff with the tank bulk fuel Temp >43C is prohibited)
56
When must fuel cross feed be off?
Takeoff and landing
57
When must fuel recirc be on and off?
Must be off for takeoff and initial climb to FL340 and must be off when the bulk fuel temp is >0C. Must turn on if fuel temp reaches -25C
58
Max operating speeds, <8000/>8000
<8000 - 300 KIAS >8000 - 340 KIAS
59
Max Mach - FL300-350
.89 M
60
Max Mach - FL350-410
.88 M
61
Max Mach - FL470
.858 M (linear decrease to FL510)
62
Max Mach - FL510
.842 M
63
Slats out speed
225 KIAS
64
Flaps 6 speed
210 KIAS
65
Flaps 16 speed
210 KIAS
66
Flaps 30 speed
185 KIAS
67
Max flap/slat altitude
18,000 ft
68
Landing gear Vle
200 KIAS
69
Landing gear Vlo
250 KIAS
70
Max altitude for landing gear extension
20,000 ft
71
Tire speed limit
183 KIAS
72
Max turbulence penetration speed
300 KIAS/.80 M Whichever is lower
73
Vmcg
80 KIAS
74
Vmca
86 KIAS
75
How many generators are there?
5 total 4 - 40KVA variable frequency generators, 115 VAC, 324-596 HZ (variable frequency) 1 - 45KVA (GND)/40KVA (AIR) constant frequency APU GEN, 115 VAC, 400 HZ
76
The generators power what buses?
Each generator power is respective bus (GEN 1/AC BUS 1, etc) AC ESS BUS is powered through AC BUS 4 by GEN 4 (also RAT powers AC ESS BUS)
77
If all other power is lost, the RAT supplies power to what bus?
The RAT will provide power to the AC ESS BUS until airspeed is reduced to <147kts, then the electrical load is shed in favor of hydraulics
78
How is DC power created for the equipment requiring DC power?
There are 4 150 amp transformer rectifier units, which convert AC power to DC power and send the DC current to the DCPC and the SPDAs
79
What buses are DC?
DC BUS 1, 2, DC ESS, BATT BUS, DC EMER BUS
80
What significant equipment is in the DC emergency bus?
Fire protection
81
What are the main ship batteries?
Avionics battery - 24 volt, 25 amp APU battery - 25.2 volt, 42 amp
82
Can the AC batteries be charged by external DC power?
No, battery chargers are powered by the main AC buses
83
Can you start the APU using external DC power?
Yes. External DC provides power to the APU BATT direct bus
84
External AC power which buses?
Powers all AC buses, 1/2/3/4 which also powers AC ESS
85
What is the temp for pack discharge in manual mode?
The packs must be kept between 5-60C
86
Operation in temp manual mode?
One pack must be selected off
87
Max relief pressure differential?
10.02 PSI
88
Max diff taxi/takeoff/landing?
0.1 PSI
89
Max AUX pressure system altitude?
41,000 ft
90
Max altitude for yaw damp disengaged?
FL410
91
Min altitude for autopilot engage?
400’ AGL
92
Min altitude for autopilot disengage?
Precision App - 50’ Non-Precision App - 400’ AGL
93
Flight spoilers must be retracted?
Below 300’ AGL
94
APU Max rpm?
106%
95
APU Max start EGT?
1038C
96
Max APU EGT normal ops?
732C
97
APU Max operating altitude?
FL450
98
APU Max starting altitude?
FL370
99
APU min temp for ground start?
-40C
100
APU Max electrical load
45KVA GND, 40KVA AIR
101
Above FL370, if APU is powering a bus what must be done?
The associated hydraulic pump must be selected off
102
APU Max altitude for bleed extraction?
FL300
103
When must auto throttles be engaged?
Prior to 60 KIAS
104
When is use of auto throttles prohibited?
When landing flaps is less than 30
105
What happens when a fire handle is pulled?
1) fuel sov closes 2) hydraulic sov closes 3) bleed (HOV, PRV) sov closes 4) VFG is tripped 5) ignition is canceled 6) FIDEX control unit is armed 7) turning the handle discharges the fire bottle
106
What is the minimum paved surface width for a 180 turn?
68 ft
107
Thrust reversers limitations
Not to be selected in flight Touch and go after deployment is prohibited Use fire power back is prohibited
108
FADEC
Controls: thrust management, fuel metering, fuel and oil temp, bleed valves, start valves and igniters, partial thrust reversers
109
What does the EMER switch on the audio panel do?
When pressed, the microphone is connected directly to the on side VHF (COMM) transceiver and the audio is connected directly to the airline’s headphone. This mode disables all other audio control unit modes. Used in panel failure
110
RAT
9Kva, 115-200 VAC Auto deploys with no delay: -N2 on both engines <35% and all AC power lost -loss of all AC power and flaps/slats >0 -manually deployed Auto reply with 14 sec delay: -loss of all AC power airborne and slats/flaps 0
111
Gravity Refueling
Total - 38,850lbs Wings - 13,850 Center - 11,150 Aft - N/A
112
Fire detection system - engine
Three dual loop sensing elements: accessory gearbox, engine core, fixed cowl
113
Fire detection system - APU
Three dual loop sensing elements: APU educator, right APU compartment hatch, along strut supporting APU
114
Auto ground start abort occurs:
1) N2 speed not greater than it equal to 15% within 120 secs 2) idle speed has not been achieved within 120 secs HPSOV opens 3) starter cutout has not occurred within 180 secs of the SAV open 4) ITT exceeds the ground starting limit of 700C after light off and during acceleration
115
Auto air start abort:
1) crew selects ENG RUN switch to off 2) N2 speed not greater or equal to 15% within 60 secs 3) idle speed not achieved within 600 secs after HPSOV opens 4) starter cutout has not occurred within 180 secs of the SAV open
116
Hydraulic Accumulators
System 2/3 - 500PSI RAT - 1000PSI
117
Hydraulic system capacity
System 1 - 6.7 gals System 2 - 8.25 gals System 3 - 14 gals
118
Rudder travel limiter- flaps down
Airspeed less than 155kts, +/-37 degrees
119
Rudder travel limiter- flaps up
Airspeed less than 155kts, +/-25 degrees
120
Brake control unit (BCU) provides:
Gear retract braking, anti skid, locked wheel protection
121
Electric anti icing provided for:
Pitot static probes, ice detectors, TAT probes, heater/brake temp monitoring units, AOA vanes
122
Hydraulic B pumps will come on in AUTO:
-associated primary pump drops below 1800psi in flight (primary pump failure) -slats or flaps are not at 0 and at least one VFG is operating

Global Express (4 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2025 Bold Learning Solutions. Terms and Conditions