Performance Flashcards
1
Q
514. According to airworthiness, what is the maximum number of passager seats on a A 320-200 : 145 180 220
A
180
2
Q
- After TAKE OFF, pilot can engage AP :
At 30 ft.
5 seconds after LIFT-OFF.
At 100 ft and at least 5 seconds after LIFT-OFF.
A
At 100 ft and at least 5 seconds after LIFT-OFF.
3
Q
- What is the maximum speed for the landing gear retraction ?
250 kt
220 kt
280 kt
A
220 kt
4
Q
- In normal operation, what is the maximum speed with landing gear extended ?
280 kt / M 0.67
250 kt / M 0.67
220 kt / M 0.60
A
280 kt / M 0.67
5
Q
- The maximum altitude to extend the speed brakes is :
FL 250
No limitation
FL 200
A
No limitation
6
Q
519. Minimum usable altitude for AP during an ILS approach with CAT 1 displayed on FMA is : 160 ft AGL MDA When flare is displayed on FMA
A
160 ft AGL
7
Q
- On A320 the use of AP or FD in OPEN DES or DES MODES is not permitted in
approach unless the FCU altitude is set at or above :
No restriction
1500 ft.
MDA or 500 ft AGL.
A
MDA or 500 ft AGL.
8
Q
- LFPG 27L - WIND = 180/31 kt.
TAKE OFF and LANDING are allowed
TAKE OFF is prohibited
TAKE OFF is allowed but LANDING is prohibited
A
TAKE OFF and LANDING are allowed
9
Q
- The maximun brake temperature for TAKE-OFF is :
300°C BRAKE FAN OFF
250°C BRAKE FAN ON
150°C BRAKE FAN OFF
A
300°C BRAKE FAN OFF
10
Q
- The pilot can disengage AUTO BRAKES system :
Only by pressing firmly the brake pedals.
Only by pushing the armed mode P/B.
Either by pushing the armed mode P/B or by pressing firmly the brake pedals.
A
Either by pushing the armed mode P/B or by pressing firmly the brake pedals.
11
Q
- During preflight check on a A320-200, external temperature 17°C, cabine temperature
23°C, 1 observer is expected in cockpit, the minimum crew oxygen bottle pressure has
to be :
1425 PSI
731 PSI
959 PSI
A
959 PSI
12
Q
- During PREFLIGHT on a A320-200, external temperature 17°C, cabine temperature
23°C, the flight crew oxygen pressure is 1000 PSI :
You can accept one jump seat
You can accept two jump seats
This is the minimum pressure for PEQ 2
A
You can accept one jump seat
13
Q
526. After 3 APU STARTER CYCLES separated by 1 minute COOL DOWN, you have to wait : At least 60 minutes At least 15 minutes Mechanical check has to be performed
A
At least 60 minutes
14
Q
- APU can be started :
Up to FL 390
Up to FL 250
Only on ground
A
Up to FL 390
15
Q
- The APU START LIMITATION with only batteries is :
Up to FL 390
Up to FL 250
Only on ground
A
Up to FL 250
16
Q
- In case of engine failure during TAKE-OFF, TOGA THRUST can be set for :
5 minutes
10 minutes
Unlimited time
A
10 minutes
17
Q
- If after 4 consecutive engine start cycles of 2 mn, start up is not completed, pilot has to
wait :
15 minutes to allow starter cooling before attempting a new start
20 seconds to allow starter relubrification
No delay is required
A
15 minutes to allow starter cooling before attempting a new start
18
Q
- REVERSE THRUST can be used :
To back track the aircraft
IDLE REVERSE is allowed to stop the aircraft in normal operation
Maximum REVERSE should not be used below 70 kt except in emergency
A
Maximum REVERSE should not be used below 70 kt except in emergency
19
Q
- FL 190, APU GEN ON, APU AIR BLEED can support :
1 PACK
2 PACKS
APU cannot support AIR CONDITIONNING
A
1 PACK
20
Q
- WING ANTI-ICING supplied by APU AIR BLEED is :
Allowed.
Not allowed.
Technically impossible
A
Not allowed.
21
Q
- After one unsuccessful APU START UP, a new start can be performed :
Immediately
After a 1 minute cooling period
After a 2 minute cooling period
A
Immediately
22
Q
- On contamined runways :
Reduced TAKE OFF THRUST is allowed
Reduced TAKE OFF is allowed but FLEX TEMP must be reduced by 4°C
Reduced TAKE OFF THRUST is not allowed
A
Reduced TAKE OFF THRUST is not allowed
23
Q
- When items are affecting performance at take-off (like THRUST REVERSERS
inoperative), TAKE-OFF with reduced THRUST :
Is permitted without any restriction
Is not permitted
Is permitted on dry runways only
A
Is not permitted
24
Q
- During preflight check in winter at MOSCOW, the ECAM ENG OIL T° is - 45°C :
Start-up is not allowed
There is no oil temperature limitation for start-up
Start-up may be performed
A
Start-up is not allowed
25
Q
- During DESCENT, flying under IMC conditions, TAT = +5°C :
Pilot has not to use ENG ANTI ICE
Pilot has to use ENG ANTI ICE
Before using ANTI ICE, pilot can wait ice emergence
A
Pilot has to use ENG ANTI ICE
26
Q
- Flying FL 390, SAT = - 50°C, entering cirrus clouds :
ENG ANTI ICE is required
ENG ANTI ICE is not required
ENG ANTI ICE is not allowed at FL 390
A
ENG ANTI ICE is not required
27
Q
- On ground, A/C is under icing conditions when :
OAT < 10°C
OAT < 10°C and visibility less than 1600 m
Visibility less than 1600 m
A
OAT < 10°C and visibility less than 1600 m
28
Q
- On ground, A/C is under icing conditions when :
OAT < 10°C
OAT < 10°C and water patches on runway
OAT < 10°C and ceiling below 200 ft
A
OAT < 10°C and water patches on runway
29
Q
- IGN START must be used for TAKE-OFF when :
Runway is wet
Heavy rain or severe turbulences are expected
Icing conditions are encountered
A
Heavy rain or severe turbulences are expected
30
Q
- During CLIMB, IMC CONDITIONS, TAT - 30°C :
ENG ANTI ICE is required
ENG ANTI ICE is required if SAT < - 40°C
ENG ANTI ICE is not required if SAT < - 40°C
A
ENG ANTI ICE is not required if SAT < - 40°C
31
Q
- Extended flight in icing conditions with the SLATS extended :
Is permitted because SLATS are deiced
Is not permitted
Extended flight in icing conditions should be avoided
A
Extended flight in icing conditions should be avoided
32
Q
- In flight, the maximum fuel unbalance is :
530 kg between inner tanks
530 kg between both wings
530 kg between outer tanks
A
530 kg between outer tanks
33
Q
- On A320-200, tanks must be emptied as follows :
Central tanks then wing tanks
Wing tank then central tanks
Simultaneously if the fuel load exceeds the wing tanks capacity
A
Simultaneously if the fuel load exceeds the wing tanks capacity
34
Q
- The cabin altitude reaches 9550 ft :
There is no alarm
There is an EXCESS CABIN ALT alarm and “FASTEN SEAT BELTS” illuminates
There is only an EXCESS CABIN ALT alarm
A
There is only an EXCESS CABIN ALT alarm
35
Q
- Crew want to TAKE-OFF without FD :
It is permitted with this aircraft
It is permitted without any restriction
It is permitted, according to MEL conditions
A
It is permitted, according to MEL conditions
36
Q
- When pressing T.O. CONFIG P/B for TAKE-OFF, T.O. CONFIG TEST remains BLUE
on ECAM TAKE-OFF CHECK LIST.
Pilot cannot check if TAKE OFF conditions are correct
There is a technical procedure to check T.O. CONFIG (MEMO ECAM INOP)
QRH CHECK LIST has to be performed
A
There is a technical procedure to check T.O. CONFIG (MEMO ECAM INOP)
37
Q
- An AUTOLAND procedure can be conducted with one engine failure :
Without any restriction
If the engine failure procedure is completed before reaching 1000 ft AGL and DH is
limited to 50 ft
There is no AUTOLAND procedure allowed with 1 engine out
A
If the engine failure procedure is completed before reaching 1000 ft AGL and DH is
limited to 50 ft
38
Q
- When starting the engine in flight :
EGT MAX is 725° and FADEC controls the overlimit
EGT MAX is 950° and FADEC does not control the overlimit
EGT MAX is 725° and FADEC does not control overlimit
A
EGT MAX is 725° and FADEC does not control overlimit
39
Q
- A localizer (ILS without G/S) approach can be performed in full MANAGED mode :
Yes, provided the approach exists in DATA BASE, and is performed with AP
No, in any case
Yes, provided the approach exists in DATA BASE and the navigation accuracy is
HIGH
A
No, in any case
40
Q
- When a VOR approach is performed in SELECTED MODE, with AP ON, the AP
disconnects automatically when reaching MDA minus 50 ft :
Yes, in any case
No, and the aircraft automatically levels OFF
No, and the aircraft continues to descent according to the selected rate of descent
A
No, and the aircraft continues to descent according to the selected rate of descent
41
Q
554. In descent, with the FMA reading SPD / DES / NAV, if the HDG KNOB on FCU is pulled, the FMA will turn to : SPD / DES / HDG THR IDLE / OPEN DES / HDG SPD / VS / HDG
A
SPD / VS / HDG
42
Q
- Normal electrical power being available, APU may be started up :
25000 ft or lower
10000 ft or lower
Throughout the normal flight envelope
A
Throughout the normal flight envelope
43
Q
- The MAX SPEED at which the L/G may be extended is :
260 kts
250 kts
240 kts
A
250 kts
44
Q
- The maximum speed to use the windshield wipers is :
200 kts
250 kts
230 kts
A
230 kts
45
Q
- What is the MAX TIRE speed ?
205 kts
195 kts
185 kts
A
195 kts
