Performance

Question 1

514. According to airworthiness, what is the maximum number of passager seats on a A
320-200 :
145
180
220

Answer 1

180

Question 2

515. 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.

Answer 2

At 100 ft and at least 5 seconds after LIFT-OFF.

Question 3

516. What is the maximum speed for the landing gear retraction ?
     250 kt
     220 kt
     280 kt

Answer 3

220 kt

Question 4

517. 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

Answer 4

280 kt / M 0.67

Question 5

518. The maximum altitude to extend the speed brakes is :
     FL 250
     No limitation
     FL 200

Answer 5

No limitation

Question 6

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

Answer 6

160 ft AGL

Question 7

520. 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.

Answer 7

MDA or 500 ft AGL.

Question 8

521. LFPG 27L - WIND = 180/31 kt.
     TAKE OFF and LANDING are allowed
     TAKE OFF is prohibited
     TAKE OFF is allowed but LANDING is prohibited

Answer 8

TAKE OFF and LANDING are allowed

Question 9

522. The maximun brake temperature for TAKE-OFF is :
     300°C BRAKE FAN OFF
     250°C BRAKE FAN ON
     150°C BRAKE FAN OFF

Answer 9

300°C BRAKE FAN OFF

Question 10

523. 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.

Answer 10

Either by pushing the armed mode P/B or by pressing firmly the brake pedals.

Question 11

524. 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

Answer 11

959 PSI

Question 12

525. 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

Answer 12

You can accept one jump seat

Question 13

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

Answer 13

At least 60 minutes

Question 14

527. APU can be started :
     Up to FL 390
     Up to FL 250
     Only on ground

Answer 14

Up to FL 390

Question 15

528. The APU START LIMITATION with only batteries is :
     Up to FL 390
     Up to FL 250
     Only on ground

Answer 15

Up to FL 250

Question 16

529. In case of engine failure during TAKE-OFF, TOGA THRUST can be set for :
     5 minutes
     10 minutes
     Unlimited time

Answer 16

10 minutes

Question 17

530. 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

Answer 17

15 minutes to allow starter cooling before attempting a new start

Question 18

531. 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

Answer 18

Maximum REVERSE should not be used below 70 kt except in emergency

Question 19

532. FL 190, APU GEN ON, APU AIR BLEED can support :
     1 PACK
     2 PACKS
     APU cannot support AIR CONDITIONNING

Answer 19

1 PACK

Question 20

533. WING ANTI-ICING supplied by APU AIR BLEED is :
     Allowed.
     Not allowed.
     Technically impossible

Answer 20

Not allowed.

Question 21

534. 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

Answer 21

Immediately

Question 22

535. 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

Answer 22

Reduced TAKE OFF THRUST is not allowed

Question 23

536. 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

Answer 23

Is not permitted

Question 24

537. 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

Answer 24

Start-up is not allowed

Question 25

538. 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

Answer 25

Pilot has to use ENG ANTI ICE

Question 26

539. 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

Answer 26

ENG ANTI ICE is not required

Question 27

540. 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

Answer 27

OAT < 10°C and visibility less than 1600 m

Question 28

541. 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

Answer 28

OAT < 10°C and water patches on runway

Question 29

42. IGN START must be used for TAKE-OFF when : Runway is wet Heavy rain or severe turbulences are expected Icing conditions are encountered

Answer 29

Heavy rain or severe turbulences are expected

Question 30

543. 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

Answer 30

ENG ANTI ICE is not required if SAT < - 40°C

Question 31

544. 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

Answer 31

Extended flight in icing conditions should be avoided

Question 32

545. In flight, the maximum fuel unbalance is : 530 kg between inner tanks 530 kg between both wings 530 kg between outer tanks

Answer 32

530 kg between outer tanks

Question 33

546. 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

Answer 33

Simultaneously if the fuel load exceeds the wing tanks capacity

Question 34

547. 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

Answer 34

There is only an EXCESS CABIN ALT alarm

Question 35

548. 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

Answer 35

It is permitted, according to MEL conditions

Question 36

549. 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

Answer 36

There is a technical procedure to check T.O. CONFIG (MEMO ECAM INOP)

Question 37

550. 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

Answer 37

If the engine failure procedure is completed before reaching 1000 ft AGL and DH is limited to 50 ft

Question 38

551. 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

Answer 38

EGT MAX is 725° and FADEC does not control overlimit

Question 39

552. 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

Answer 39

No, in any case

Question 40

553. 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

Answer 40

No, and the aircraft continues to descent according to the selected rate of descent

Question 41

``` 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 ```

Answer 41

SPD / VS / HDG

Question 42

555. Normal electrical power being available, APU may be started up : 25000 ft or lower 10000 ft or lower Throughout the normal flight envelope

Answer 42

Throughout the normal flight envelope

Question 43

556. The MAX SPEED at which the L/G may be extended is : 260 kts 250 kts 240 kts

Answer 43

250 kts

Question 44

557. The maximum speed to use the windshield wipers is : 200 kts 250 kts 230 kts

Answer 44

230 kts

Question 45

558. What is the MAX TIRE speed ? 205 kts 195 kts 185 kts

Answer 45

195 kts