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Systems Study Questions Flashcards

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1
Q

What are the dimensions of the A321?

(Length, Wingspan, Height)

Aircraft General

A
  • Length = 146’
  • Wingspan = 117’ 5”
  • Height = 38’ 7”

Aircraft General

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2
Q

What is the minimum pavement width required for 180° turn?

Aircraft General

A

93’, recommended 99’

Aircraft General

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3
Q

What are the unpressurized areas of the A321?

Aircraft General

A
  • Radome
  • Nosegear Bay
  • Air Conditioning Comp (e.g. Packs)
  • Main Gear Bay
  • Tail cone

(5)

Aircraft General

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4
Q

Where is the VHF 2 antenna located?

Rea

Aircraft General

A

Rear lower fuselage

Aircraft General

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5
Q

Where are the GPS antennas located?

Aircraft General

A

Upper forward fuselage

Aircraft General

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6
Q

Where are the HF antennas located?

Aircraft General

A

Mid vertical stabalizer

Aircraft General

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7
Q

What is the maximum takeoff weight for the A321?

Aircraft General

A

206,132 lbs

Aircraft General

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8
Q

What is the maximum landing weight of the A321?

Aircraft General

A

174,606 lbs

Aircraft General

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9
Q

How many cabin exits are there on the A321?

Doors

A

8

Doors

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10
Q

How does the opening of the passenger doors differ from the cabin emergency exits during slide deployment?

Doors

A

Passenger doors drive full open and do not hesitate in opening for slide inflation. Cabin emergency exits have intermediate opening to prevent passengers exiting during slide inflation - this can be manually overridden.

Doors

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11
Q

What happes to the cockpit door if electrical power is lost?

Doors

A

The door is unlocked but remains closed.

Doors

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12
Q

What would a strike light illuminated on the upper overhead panel indicate?

Doors

A

An illuminated light indicated there is a fault with the corresponding system.

Doors

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13
Q

The cockpit window handle must have what color band showing to indicate the window is locked shut.

Doors

A

Red

Doors

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14
Q

What does a WHITE slide indication on the ECAM DOORS page indicate?

Doors

A

The slide is armed.

Doors

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15
Q

Where is the slide located for the cabin emergency exits?

Doors

A

Below the floor.

Doors

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16
Q

Where is the manual slide deployment located for the passenger doors? Cabin emergency exits?

Doors

A
  • Passenger doors = floor right side
  • Cabin emergency exits = in the door jamb upper right side

Doors

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17
Q

What is the only cockpit light that will work when batteries are supplying electrical power?

Lights

A

FP Dome Light

Lights

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18
Q

How do you tell a NAV or STROBE light is reaching the end of its service life.

Lights

A

A blue LED will blink

Lights

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19
Q

Cabin signs will automatically illuminate at what cabin altitude.

Lights

A

11,300’ ±350’

Lights

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20
Q

What is the required Emergency equipment?

Equipment

A
  • R - Ropes
  • A - Axe
  • M - Masks
  • P PBE
  • A - AVSAX
  • G - Gloves
  • E - Extinguishers
  • F - Flashlights
  • V - Vests

Equipment

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21
Q

Where is the fire extinguisher located?

Equipment

A

Behind the FO - all the fire fighting equipment is by the FO.

Equipment

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22
Q

Where are the life jackets for the 3rd and 4th occupant located?

Equipment

A

Below their associated seats.

Equipment

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23
Q

Pressing a switch in is normally associated with turning the switch ____?

Equipment

A

On

Equipment

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24
Q

What do 2 dots on a pushbutton indicate?

Equipment

A

That portion of the switch is not used.

Equipment

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25
Where is Circuit Breaker Panel 49VU located? ## Footnote Equipment
Overhead Panel ## Footnote Equipment
26
What does "=" throughout the PFD indicate? | (Green "=") ## Footnote Indicating & Recording
"Normal Law" limit or protection available. ## Footnote Indicating & Recording
27
Can the flight crew manually start the DFDR? ## Footnote Indicating & Recording
Yes, by pressing the GND CTL switch. Normal procedure on the ground before the Before Start Checklist to ensure the checklist is recorded. ## Footnote Indicating & Recording
28
Instead of airspeed, the BUSS uses ____. For altitude information, the BUSS uses altitude from ____. ## Footnote Indicating & Recording
- AOA - GPS ## Footnote Indicating & Recording
29
Which DUs will automatically switch in the event of a failure? ## Footnote Indicating & Recording
- PFD → ND - E/WD → SD | (3 total screens switch) ## Footnote Indicating & Recording
30
What on screen indication would you get if DMC 1 fails? ## Footnote Indicating & Recording
Captain-side screen would indicate "invalid data", the ECAM would flash on then off. ## Footnote Indicating & Recording
31
How do the DMCs reconfigure if DMC1 fails? Does anything happen to the screens when DMC 1 fails? What does the crew need to do? ## Footnote Indicating & Recording
- DMC 2 automatically takes over to display information on the ECAM. - CA screens will shut off and the ECAM will "blink" - The crew needs to select EIS DMC to CAPT 3 to allow the CA's screens to use DMC 3. ## Footnote Indicating & Recording
32
What is the difference between level 1, 2, and 3 ECAM warinings/cautions? ## Footnote Indicating & Recording
- 3 has CRC (Continuous Repetative Chime) - 2 has SC (Single Chime) - 1 has no chime ## Footnote Indicating & Recording
33
How would you identify a Primary Failure? ## Footnote Indicating & Recording
A box around the item | (on the ECAM) ## Footnote Indicating & Recording
34
How long does the Cabin Oxygen System supply oxygen for? ## Footnote Oxygen
15 mins ## Footnote Oxygen
35
The masks for the Cabin Oxygen System will automatically drop at what cabin altitude? ## Footnote Oxygen
14,000' (+250', -750') | (13,250'-14,250') ## Footnote Oxygen
36
How long does the PBE supply oxygen for? ## Footnote Oxygen
15 mins ## Footnote Oxygen
37
When does the Quick Don Mask automatically provide overpressure oxygen supply? ## Footnote Oxygen
30,000' ## Footnote Oxygen
38
The ENG generators supply ____ kVA of ____ power. ## Footnote Electrical
- 90 kVA - AC ## Footnote Electrical
39
What is the generator priority? ## Footnote Electrical
1. GEN 1/2 (onside, offside) 2. External Power 3. APU | Technically, offside genis #4 as it will only pwr off-side busses last. ## Footnote Electrical
40
How is the emergency generator powered? ## Footnote Electrical
BLUE Hydraulic System ## Footnote Electrical
41
Can the entire electrical network be powered by a single ENG generator? ## Footnote Electrical
No, the GALLEY BUS is shed. | Technically it **can**, but it doesn't due to auto shed. ## Footnote Electrical
42
What is the difference between the Emergency Configuration and the Smoke Configuration? ## Footnote Electrical
The Smoke Configuration is a configuration purposefully entered by the crew to identify the source of smoke. The fuel pumps are connected upstream of the GEN 1 line connector. ## Footnote Electrical
43
What is the required voltage for the batteries prior to APU start. ## Footnote Electrical
25.5V ## Footnote Electrical
44
How do you recharge the batteries? ## Footnote Electrical
- Batt pushbuttons on, aircraft connected to EXT PWR, 20 mins. - Batt Pushbuttons off to display how much charge the batteries have. ## Footnote Electrical
45
What does FAULT indicate on the EMER ELEC PWR Panel? ## Footnote Electrical
The EMER GEN is not supplying power. ## Footnote Electrical
46
What fuel pumps normally deliver fuel to the APU? ## Footnote APU
- Left tank pumps. - If pressure is insufficient or during start, the APU has its own fuel pump. ## Footnote APU
47
What switches do you push to start the APU? ## Footnote APU
MASTER, START ## Footnote APU
48
After using bleed air you go to shut off the APU, does the APU shut down immediately? ## Footnote APU
No, it undergoes a cooling period for 60-120 secs and teh shutdown process can be stopped by pressing MASTER. ## Footnote APU
49
What switches do you press to shutdown the APU? ## Footnote APU
After turning off the bleed air, press MASTER. ## Footnote APU
50
When securing the aircraft, what must the aircrew do before turning off the batteries? ## Footnote APU
Wait until the APU flap is fully closed before switching off the batteries. (about 2 mins after APU AVAIL light goes out) | (FLAP OPEN indication on ECAM APU PAGE is removed) ## Footnote APU
51
What stage air is the normal source for engine bleed air? ## Footnote Pneumatic
IP (Intermediate Stage) air ## Footnote Pneumatic
52
When would the BMC switch to HP air? ## Footnote Pneumatic
When the BMC senses IP air is unable to provide 65 ±15 psi. Generally low engine power settings. ## Footnote Pneumatic
53
What would a FAULT light on the overhead AIR COND panel indicate? ## Footnote Pneumatic
- Overheat - Overpressure - Leak - Incorrect valve position ## Footnote Pneumatic
54
____ bleed has priority over ____ bleed air. ## Footnote Pneumatic
APU, Engine ## Footnote Pneumatic
55
Air conditioning valves are ____ operated, ____ controlled, and fail ____. ## Footnote Air Conditioning
- Pneumatically - Electrically - Closed ## Footnote Air Conditioning
56
When will the packs automatically deliver NORM pressure? ## Footnote Air Conditioning
When LO is selected and the ACSC determines the system is unable to meet the cooling demands requested. ## Footnote Air Conditioning
57
When will the packs automatically deliever HI pressure? ## Footnote Air Conditioning
- Single Pack operation - APU is the source of bleed air ## Footnote Air Conditioning
58
When do the cabin pressure controllers switch? ## Footnote Pressurization
- By cycling the MODE SEL switch to manual and back to auto - 70 secs after landing ## Footnote Pressurization
59
How many motors are on the Outflow Valve? ## Footnote Pressurization
- 3 motors - 2 automatic AC faster motors - 1 manual DC slower motor ## Footnote Pressurization
60
Seatbelt signs will automatically come on when cabin altitude reaches what value? ## Footnote Pressurization
11,300' ± 350' ## Footnote Pressurization
60
Cabin altitude for the following: - Cockpit masks Overpress - Outflow Valve Closes - Masks drop - Cabin signs come on - "__CAB PR__ EXCESS CAB ALT" ECAM Warning - ADV (boxed) - Normal ## Footnote Pressurization
- Cockpit masks Overpress - 30,000' - Outflow Valve Closes - 15,000' - Masks drop - 14,000 (-750' +250')...(13,250'-14,250') - Cabin signs come on - 11,300' (±350') - "_CAB PR_ EXCESS CAB ALT" ECAM Warning - 9,550' - ADV (boxed) - 8,800' - Normal - ≤ 8,000' ## Footnote Pressurization
61
What are the 3 systems that are ventilated? ## Footnote Ventilation
- Battery - Lavatory/Galley - Avionics ## Footnote Ventilation
62
When is the Avionics System in the open configuration on the ground? ## Footnote Ventilation
When the skin temperature is above the threshold. ## Footnote Ventilation
63
When is the Avionics System in the intermediate configuration in the air? ## Footnote Ventilation
When the skin temperature is above the threshold. ## Footnote Ventilation
64
What portion of the wing is heated with bleed air? ## Footnote Ice & Rain Protection
3 outboard slats ## Footnote Ice & Rain Protection
65
Wing anti-ice valves fail ____? ## Footnote Ice & Rain Protection
Closed ## Footnote Ice & Rain Protection
66
Engine Anti-ice valves fail ____? ## Footnote Ice & Rain Protection
Open ## Footnote Ice & Rain Protection
67
How do you perform the APU fire test on a cold dark airplane, what indications should you see? ## Footnote Fire Protection
- Batt 1 & 2 pushbuttons - On - Press the TEST button - APU FIRE push button and SQUIB/DISCHARGE switch should illuminate. ## Footnote Fire Protection
68
What indications would you see for a successful APU and Engine Fire test with AC power ## Footnote Fire Protection
- APU - CRC - 4 lights - ECAM - ENG - CRC - 6 lights - ECAM ## Footnote Fire Protection
69
What indication would you have for smoke detected in the avionics bay? ## Footnote Fire Protection
- SC - 5 lights - ECAM | Smoke in Avionics Bay ## Footnote Fire Protection
70
What indication does the crew have to identify when a fire has gone out? ## Footnote Fire Protection
- The associated FIRE pushbutton will no longer be illuminated. - There is no way to tell if a cargo fire has gone out (HALON will trigger smoke detectors.) ## Footnote Fire Protection
71
How many extinguishing bottles per engine? APU? Cargo? ## Footnote Fire Protection
- 2 per engine - 1 for APU - 2 shared for both cargo compartments ## Footnote Fire Protection
72
How long does AGENT 1 take to discharge | Cargo Fire Extinguisher ## Footnote Fire Protection
60 seconds ## Footnote Fire Protection
73
On the Cargo Smoke Panel, when does the DISCH AGENT 2 light illuminate? | Cargo Fire Extinguisher ## Footnote Fire Protection
60 mins after discharging AGENT 1 ## Footnote Fire Protection
74
How long does AGENT 2 take to discharge? | Cargo Fire Extinguisher ## Footnote Fire Protection
140 mins ## Footnote Fire Protection
75
How much total fire protection do we have? | Cargo Fire Extinguisher ## Footnote Fire Protection
200 mins (60 mins from AGENT 1, 140 mins from AGENT 2) ## Footnote Fire Protection
76
What hydraulic system are the ____ on? - Normal Brakes - Alternate Brakes - Parking Brake - NWS - EMER GEN - MLG ## Footnote Hydraulics
- Normal Brakes - GREEN - Alternate Brakes - YELLOW - Parking Brake - YELLOW - NWS - YELLOW - EMER GEN - BLUE - MLG - YELLOW ## Footnote Hydraulics
77
What hydraulic systems contain electric pumps. ## Footnote Hydraulics
BLUE and YELLOW ## Footnote Hydraulics
78
When does the BLUE electric pump operate? YELLOW? ## Footnote Hydraulics
- BLUE - After engine start - YELLOW - When manually selected or for cargo door operations ## Footnote Hydraulics
79
Hydraulic Pumps provide ____ psi except the RAT which provides ____ psi? ## Footnote Hydraulics
- Hyd pumps = 3,000 psi - RAT = 2,500 psi ## Footnote Hydraulics
80
When will the PTU operate? ## Footnote Hydraulics
When differential pressure of at least 500 psi witht the parking brake released. | PTU Operate ## Footnote Hydraulics
81
What are the only 2 mechanically controlled flight surfaces? ## Footnote Flight Controls
1. Rudder 2. Pitch Trim ## Footnote Flight Controls
82
How many flight control computers are there? ## Footnote Flight Controls
**7** (3 SECs, 2 ELACs, and 2 FACs) - FAC = Flight Augmentation Computer - ELAC = Elevator Aileron Computer - SEC = Spoiler Elevator Computer Also: - 2 FCDC - Flight Control Data Concentrator (collect info from ELAC, SEC and send to CFDS and EIS). ## Footnote Flight Controls
83
In the event a sidestick malfunctions, how would a pilot takeover control and deactivate the other sidestick? ## Footnote Flight Controls
Press and hold the sidestick priority button for 40 seconds. (Control can be regained if the opposite side stick priority pushbutton is pressed.) ## Footnote Flight Controls
84
Looking at the PFD, how would you be able to identify: - Normal Law? - Alternate Law? - Direct Law? - Mechanical Law? ## Footnote Flight Controls
- Normal Law - Green "=" - Alternate Law - Amber "x" - Direct Law - Amber "USE MAN PITCH TRIM" - Mechanical Law - Red "MAN PITCH TRIM ONLY" ## Footnote Flight Controls
85
What happens in Alternate Law when the gear is extended. ## Footnote Flight Controls
It goes into Direct Law. ## Footnote Flight Controls
86
At what fuel value would a LO LVL indication be displayed? ## Footnote Fuel
1,650 lbs in the associated wing. ## Footnote Fuel
87
How does fuel get from an ACT to the Center Tank? ## Footnote Fuel
When the hi level sensor in the center tank has been dry for 10 mins, the FLSCU modulates valves and the ACT transfer pump to take fuel from the ACT to the center tank. ## Footnote Fuel
88
How does fuel get from the center tank to the wing tanks? ## Footnote Fuel
After 550 lbs of fuel is burned from the wing tank, the XFR valve is opened to allow the jet pumps to suck fuel from the center tank into the wings. ## Footnote Fuel
89
How does fuel get from the Wing Tanks into the engine? ## Footnote Fuel
2 fuel pumps per wing. ## Footnote Fuel
90
What are the 3 times the FD will automatically engage? ## Footnote Auto Flight
- FMGC power-up - TCAS event - Go Around ## Footnote Auto Flight
91
What does --FD2 indicate? ## Footnote Auto Flight
FD 1 is off. ## Footnote Auto Flight
92
Managed guidance is achieved by ____ knobs, selected guidance is achieved by ____ knobs. ## Footnote Auto Flight
- Pushing - Pulling ## Footnote Auto Flight
93
Where is AP, FD, and A/THR engagement displayed? ## Footnote Auto Flight
5th column of the FMA. ## Footnote Auto Flight
94
Which RMP works in the EMER ELEC configuration? ## Footnote Communications
RMP 1 ## Footnote Communications
95
How can you erase the CVR? ## Footnote Communications
When the aircraft is on the ground and the parking brake is on, press the ERASE button for 2 seconds. ## Footnote Communications
96
The Landing Gear panel attains information from which LGCIU? ## Footnote Landing Gear
LGCIU 1 ## Footnote Landing Gear
97
The brake pressure gauge on the main console shows pressure for which system? ## Footnote Landing Gear
Alternate Braking, Yellow System ## Footnote Landing Gear
98
Which statement below is correct regarding antenna location? ## Footnote B
HF1 & HF 2 antennas are on vertical stab. ## Footnote B
99
In pitch alternate law, the flight mode changes to direct law when ____. ## Footnote B
The landing gear is lowered. ## Footnote B
100
In the hydraulic system, the priority valves ____. ## Footnote B
Cut-off hydralic power to heavy load user systems if hydraulic pressure in a system gets low. ## Footnote B
101
When the PTU is operating, solid green arrows to the left indicate ____. ## Footnote B
The YELLOW system is powering the GREEN system. ## Footnote B
102
For full lift augmentation, each wing has ____ leading edge slat surfaces and ____ trailing edge flap surfaces. ## Footnote B
- 5 - 2 ## Footnote B
103
Is it possible to move hydralic fluid from GREEN to YELLOW or YELLOW to GREEN system? ## Footnote B
No ## Footnote B
104
There is one ____ in each hydraulic system, which assists in maintaining a constant pressure during normal operation. ## Footnote B
Accumulator ## Footnote B
105
Normally, DMC 2 supplies data to ____. ## Footnote B
- FO PFD & ND ## Footnote B
106
In case of loss of electrical power supply, the engine anti-ice valves: ## Footnote B
Open ## Footnote B
107
A primary failure is the failure of ____. ## Footnote B
a system or item that causes the loss of use of other systems or items of equipment that depend on it. ## Footnote B
108
The temperature of each aircraft zone is optimized by what means? ## Footnote B
TRIM AIR valve ## Footnote B
109
The PACK FLOW selector is set to NORM and yet the ECAM display shows PACK FLOW to be HI. How is this possible? ## Footnote B
- Single Pack Operation - **APU supplying bleed air** ## Footnote B
110
The air conditioned supply of air is distributed into ____ independent, automatically controlled zones. ## Footnote B
3 ## Footnote B
111
The air conditioning system is controlled automatically by 2 ____. ## Footnote B
Air Conditioning System Controllers ## Footnote B
112
Having manually set the LDG ELEV, the cabin altitude is: ## Footnote B
Still controlled automatically through the outflow valve. ## Footnote B
113
The safety valves are: ## Footnote B
Fully automatic and cannot be controlled manually. ## Footnote B
114
The ____ contolled trim air valves add hot pneumatic air to the conditioned air of the mixer unit.. ## Footnote B
Electronically ## Footnote B
115
The MODE SEL pb-sw in MAN mode allows you to use the MAN V/S CTL in order to: ## Footnote B
Manually adjust the outflow valve. ## Footnote B
116
The avionics ventilation close-circuit configuration operates on the ground when the skin temperature is below the on-ground threshold, or when the thrust levers are set to take-off power or when the aircraft is in flight with the skin temperature below the in flight threshold. ## Footnote B
True ## Footnote B
117
When landing elevation is set to auto, the landing elevation is sent to the controler from the: ## Footnote B
FMGS ## Footnote B
118
Which RMP operates in EMER ELEC CONFIG? ## Footnote B
1 ## Footnote B
119
The PARK BRK system is supplied by: ## Footnote B
The YELLOW hydraulic system or accumulator pressure, through the Parking Brake Control Valve. ## Footnote B
120
When the slide arming lever is in the ARMED position, opening the door from the outside disarms the door and escape slide. ## Footnote B
True ## Footnote B
121
Hydraulic pressure to the landing gear is supplied up to: ## Footnote B
260 kts ## Footnote B
122
On the ECAM WHEEL page, an amber arc appears on one wheel indication meaning the brake temperature is above: ## Footnote B
300° ## Footnote B
123
The red arrow near the landing gear lever illuminates when? ## Footnote B
The landing gear is not down when the aircraft is in the landing configuration. ## Footnote B
124
The flight crew's portable oxygen system (smoke hood) is serviceable as long as the yellow indicator on the case is not broken. The hood should work satisfactorily for at least: ## Footnote B
15 minutes ## Footnote B
125
If the cabin altitude goes above ____, the FASTEN SEAT BELT, EXIT and NO SMOKING signs come on, regardless of the SEAT BELTS and NO SMOKING switches. ## Footnote B
11,300' (±350') ft ## Footnote B
126
When in normal law during the flare, pitch inputs to the stick command: ## Footnote B
Direct stick to elevator control ## Footnote B
127
After 3 APU starter motor duty cycles, the crew must wait: ## Footnote B
60 minutes before attempting 3 more cycles ## Footnote B
128
In flight, if the flap WTBs (wing tip brakes) are on, the pilot cannot operate the flaps or slats. ## Footnote B
False ## Footnote B
129
In ____ guidance the display window assosciated with that moide displays dashes, and the white dot next to the window illuminates. ## Footnote B
Managed ## Footnote B
130
The engine and APU fire protection system includes: ## Footnote B
- 2 extinguisher bottes for each engine - 1 extinguisher bottle for the APU ## Footnote B
131
All flight control surfaces are ____ controlled and ____ actuated. ## Footnote B
- Electrically controlled - Hydraulically actuated ## Footnote B
132
By moving the MAN V/S CTR to the UP position: ## Footnote B
The cabin altitude is raised by opening the Outflow Valve. ## Footnote B
133
Bank angle protection ____ provided in alternate control law. ## Footnote B
Is not ## Footnote B
134
In normal law during landing, the THS is frozen at: ## Footnote B
100 ft ## Footnote B
135
Fuel for the APU is normally available from the: ## Footnote B
Left side tank pumps. ## Footnote B
136
Why are ALT and G/S on the smae line of the FMA but in different colors (magenta/blue)? ## Footnote B
ALT and G/S are in armed mode, but ALT has a constraint. ## Footnote B
137
The blue LOC is an armed mode. ## Footnote B
True ## Footnote B
138
According to this display (SPD on FMC is --- with white dot) ## Footnote B
Speed is managed by the FM. ## Footnote B
139
ATC cleared you to FL 150. What selections should you make to ensure the aircraft complies with the contraints? ## Footnote B
Dial in the new cleared level FL150 ## Footnote B
140
The FMS Landing System (FLS) allows the crew to fly non-precision approaches such as VOR, LOC, or RNAV that are stored in the Flight Managment (FM) with a glideslope and localizer type aid. ## Footnote B
True ## Footnote B
141
During a LOC FMS Landing System (FLS) approach the FMA veritcal and lateral indication will be: ## Footnote B
F-G/S and LOC ## Footnote B
142
In case of RMP 2 failure, VHF 2 is lost. ## Footnote B
False ## Footnote B
143
If the battery voltages are below the minimum, how do you charge them? ## Footnote B
Check that the BAT pushbuttons are on and switch the External Power on. ## Footnote B
144
What does the blue EXT PWR ON light mean? ## Footnote B
External Power is supplying the aircraft's electrical system. ## Footnote B
145
After IDG disconnection why do you get a GALLEY SHED indication on the SD? ## Footnote B
It is a reminder that the main galley has been shed automatically due to a single engine driven generator condition. ## Footnote B
146
You want to open the cabin door. While lifting the control handle the white light comes on. What does this mean. ## Footnote B
The slide is still armed. ## Footnote B
147
If the oxygen masks fail to deploy automatically they:
can be manually deployed by pressing the MASK MAN ON pb on the overhead panel.
148
While carrying out the APU FIRE test on battery power only you see the indications of half the APU FIRE pb lit up and the SQUIB and FAULT lights lit; is this successful. ## Footnote B
Yes ## Footnote B
149
According to the following indications; Amber ENG 1 LOOP B: ## Footnote B
One fire detection loop for Engine 1 has failed. Fire detection for both engines is still available. ## Footnote B
150
The DISCH AGENT2 amber light comes on ____ after AGENT 1 is discharged. ## Footnote B
60 minutes ## Footnote B
151
The message WING TIP BRK ON appears on the E/WD. What does it mean? ## Footnote B
A hydraulic device lockes the flaps in their present position. ## Footnote B
152
Give the scenario displayed at right (Spoiler 3s amber with left having up arrow) what will happen next? ## Footnote B
The left SPLR 3 will be retracted by aerodynamic force, the right SPLR 3 will be inhibited to prevent asymmetry. ## Footnote B
153
According to the indications (4 green "=" on PFD) which flight control law is active? ## Footnote B
Normal ## Footnote B
154
According to the indications (4 amber "x" on PFD, amber USE MAN PITCH TRIM) which flight control law is active? ## Footnote B
Direct ## Footnote B
155
Given indications (4 green "=" on PFD, 25° AOB), without any side stick inputs: ## Footnote B
The aircraft's attitude will stay constant ## Footnote B
156
According to the indications (3° NU, 0° AOB, Airspeed on top of red band at 120 kts), if the side stick is held full back: ## Footnote B
The High Angle of Attack protection will override the side stick input and pitch will be reduced to maintain 120 knots. ## Footnote B
157
The YELLOW hydraulic system may be powered by: ## Footnote B
- Engine 2 Hydraulic Pump - YELLOW Electric Pump - PTU - Hand pump for cargo door ## Footnote B
158
In normal law, what indicates bank angle limit ## Footnote B
Green "=" ## Footnote B
159
What does an amber line across the last two digits of the fuel mean? ## Footnote B
The fuel quantity indication is inaccurate. ## Footnote B
160
When will the FLSCU open the XFR valves to transfer fuel from the center tank to a wing tank. ## Footnote B
When the engines have burned 550 lbs of wing tank fuel. ## Footnote B
161
The APU fuel system: ## Footnote B
Obtains fuel from the left wing tank via the left side fuel pumps or, if needed, the APU fuel pump. ## Footnote B
162
During start up, when is the BLUE hydraulic system presurized? ## Footnote B
Automatically after the first engine start. ## Footnote B
163
What activates the PTU and how does it work? ## Footnote B
The PTU enables the GREEN and YELLOW systems to pressurize each other when the differential pressure is greater than 500 psi. ## Footnote B
164
The Engine Anti-Ice system: ## Footnote B
is controlled manually by the pilot ## Footnote B
165
What does the green arrow at the bottom of the STATUS page at right indicate? ## Footnote B
It means that there is more STATUS information to be seen. ## Footnote B
166
The upper Display Unit (DU) has failed. You want to see the DOOR/OXY page on the lower DU. How would you do this? ## Footnote B
Pres and hold the DOOR key on the ECP. ## Footnote B
167
Both ECAM Display Units (DU) have failed, How would you get the ECAM E/WD page to appear on the CA's ND? ## Footnote B
Move the ECAM/ND XFR to CAPT. ## Footnote B
168
How can the NAV ILS 2 FAULT be restored from being an cancelled caution: ## Footnote B
By pressing and holding the RCL key for more than 3 seconds. ## Footnote B
169
At what speed can the slats be safely retracted. ## Footnote B
"S" Speed (191 kts in picture) ## Footnote B
170
What is the meaning of a cyan 9000 at top of altitude scale. ## Footnote B
FCU Selected altitude ## Footnote B
171
What indicated aircraft track on heading tape? ## Footnote B
Green diamond (156° in example) ## Footnote B
172
What does the NW STRG DISC memo (green) mean? ## Footnote B
The NWS has been disconnected by the ground crew. ## Footnote B
173
How do you interpret LDG GEAR Panel red nose gear with (WHEEL page) 5 green triangles with 1 red triangle on left nose gear? ## Footnote B
All gear are down and locked as detected by LGCIU 2. | One green triangle is enough to confirm that the gear is down and locked ## Footnote B
174
You have performed the L/G GRAVITY EXTENSION procedure; LDG GEAR panel has 3 green triangles, WHEEL page has 6 green triangles and 3 amber doors. ## Footnote B
The gear is in the down and locked position ## Footnote B
175
When set to TA/RA, the TCAS system provides traffic and resolution advisories on ## Footnote B
other aircraft with an active transponder only. ## Footnote B
176
You are performing a NAV ACCUR check. Does ACCUR HIGH satisfy you? (RNP 2.0, ANP 0.06NM) ## Footnote B
Yes, raw data and FMGS position are the same or the difference is within acceptable limits. ## Footnote B
177
There are two triangles for each gear on the ECAM WHEEL page; what do they represent? ## Footnote B
Each triangle represents the gear position detected by one of the two LGCIUs. ## Footnote B
178
You have pulled down a passenger mask. What is its standard oxygen generator effective time of use once activated? ## Footnote B
15 minutes ## Footnote B
179
With the oxygen crew supply switched off, which ECAM indication would you see? ## Footnote B
Amber CKPT OXY ## Footnote B
180
What is the maximum demonstrated crosswind for the A321 ## Footnote B
38 kts ## Footnote B
181
The cockpit's fixed oxygen system ## Footnote B
Two sub-systems; one that supplies oxygen to the Captain and 3rd occupant, and a separate one that supplies oxygen to the FO and 4th occupant. ## Footnote B
182
What is the maximum altitude to use the APU for air cond/press (dual pack)? ## Footnote B
15,000 ft ## Footnote B
183
According to the indications (APU Bleed Air switch on, XBleed switch in AUTO, APU Bleed valve open, XBleed open, Eng Bleed valves closed) which source is providing the bleed air. ## Footnote B
The engines are not running, the APU is supplying the bleed air. ## Footnote B
184
What is the simplest way to bring the APU back online (APU AVAIL light on pb and ECAM). ## Footnote B
Turn the MASTER SW back on. ## Footnote B
185
According to the indications (APU Bleed Air switch OFF, XBleed switch in AUTO, APU Bleed valve closed, XBleed closed, Eng Bleed valves open, 0 psi on both) which source is providing the bleed air. ## Footnote B
No bleed air is being supplied. ## Footnote B
186
According to the ECAM APU page (AVAIL, APU Bleed Valve open, 35 psi; APU gen 0%) ## Footnote B
The APU is running and available. It is providing bleed air only. ## Footnote B
187
What does the white SLIDE indication mean on the ECAM DOOR/OXY page? ## Footnote B
The slide is armed. ## Footnote B
188
An amber cargo door on the ECAM DOOR/OXY page means that it is inoperative. ## Footnote B
False ## Footnote B
189
You are about to takeoff. You have not inserted a FLEX temperature. Can you still takeoff? ## Footnote B
Yes, but only using the TO/GA detent. ## Footnote B
190
You are performing a takeoff with the thrust levers at the FLEX position. The A/THR is now active. ## Footnote B
False ## Footnote B
191
You are at the start of descent and a green N1 arc is displayed showing the new thrust demand. When does this happen? ## Footnote B
Whenever there is a power change with auto-thrust engaged. ## Footnote B
192
A few seconds after selecting reverse, the amber REV indication changes to green. What does this mean? ## Footnote B
The reversers are now fully deployed. ## Footnote B
193
After ____ engine start cycles a ____ minute cooling period is required. ## Footnote B
- 3 - 15 ## Footnote B
194
The FADEC controls and monitors the ignition starting system according to: ## Footnote B
- The position of the ENG MODE Selector - The position of the ENG MASTER sw - The aircraft status (flight or ground) - (**All of these**) ## Footnote B
195
What is Alpha-Floor protection? ## Footnote B
It is a function of the flight control laws to prevent the aircraft from stalling. ## Footnote B
196
The A321 principle aircraft dimensions are: | Wingspan, Length, Height ## Footnote B
- Wingspan: 117' 5" - Length: 146' - Height: 38' 7" ## Footnote B
197
The A321 has eight cabin doors; four passenger doors and 4 emergency doors. The emergency doors are used for: ## Footnote B
Emergency exit use only. ## Footnote B
198
Turn Coordination is available up to what AOB in Normal mode. ## Footnote A
Up to 67° AOB ## Footnote A
199
- AOB Limits: - Normal Law - Full sidestick - No sidestick - High Speed protection - Full sidestick - No sidestick ## Footnote A
- Normal Mode - Full sidestick - 67° - No sidestick - returns 33° - High Speed protection - Full sidestick - returns to 45° - No sidestick - returns to 0° ## Footnote A
200
Is there Pitch Attitude protection in Alternate Law? ## Footnote A
No ## Footnote A
201
What pressure causes HYD LO PR message? ## Footnote A
1,450 psi | (FCOM mentions 1,750 with a note about 1,450; 1,450 answers question.) ## Footnote A
202
Windshield wiper speed limit ## Footnote A
230 kts ## Footnote A
203
- When do the following appear? - Red Cabin Altitude warning - Cabin Alt advisory? - How is the advisory displayed? - Cabin signs - Masks drop ## Footnote A
- Red Cabin Altitude warning - 9,550' - Cabin Alt advisory? - 8,800' - How is the advisory displayed? - Flashing Green - Cabin signs - 11,300' ±350' - Masks drop - 14,000' (+250', -750') ## Footnote A
204
If the Outflow Valve is in MAN MODE, will the DITCHING and RAM AIR pbs move the Outflow Valve? ## Footnote A
No, they rely on the AC motors to move it. ## Footnote A
205
Will the ventilation system remain in Open configuration on takeoff. ## Footnote A
No, it closes with thrust levers forward for FOD protection. ## Footnote A
206
- What do the colors on FMA mean? - Green - White in 5th column ## Footnote A
- Green = Active - White (in 5th Column) = Active ## Footnote A
207
Which areas have extinguishing vs just detection. ## Footnote A
If galley and lav grouped together, the Avionics compartment is only one with detection and not extinguishing. ## Footnote A
208
When does the FUEL USED on the ECAM reset to zero. ## Footnote A
At first engine start. ## Footnote A
209
When do LO FUEL messages come on ## Footnote A
< 1,650 lbs ## Footnote A
210
If see STS on ECAM after engine shutdown, what does that mean. ## Footnote A
STATUS messages for maintenance ## Footnote A
211
How do you find the EMER CANC messages from previous flight ## Footnote A
Press RCL for 3 seconds on preflight | SD Page - Bottom Left, "Cancelled Cautions" ## Footnote A
212
What do amber "=" mean on the airspeed tape? ## Footnote A
VFENext | (Once below, can take next flaps) ## Footnote A
213
When do Auto-Brakes activate? ## Footnote A
When spoilers deploy. ## Footnote A
214
What does a white "GRD" with triangle mean on the ECAM BLEED page ## Footnote A
Aircraft is on the ground | A/C meets parameters for GND AIR, one of those is being on the ground ## Footnote A
215
- When does A/THR arm on takeoff? - When does it activate? - What range does it operate? - 2EO? - 1EO? ## Footnote A
- Arms when THR LVR set to FLX or TOGA - Activates when THR LVR pulled to CL - Operates in flight: - 2EO - IDLE-CL - 1EO - IDLE-MCT ## Footnote A
216
Is it normal for the landing gear doors to turn amber on the ECAM WHEELS page during landing gear transit? ## Footnote A
Yes ## Footnote A

A321Neo (5 decks)

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