LIMITATIONS

Question 1

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS
- Clean configuration
- Other configurations

Answer 1

-1 g to +2.5 g
0 g to 2 g

Question 2

OPERATIONAL PARAMETERS
Runway slope (mean)

Answer 2

±3 %

Question 3

OPERATIONAL PARAMETERS
PASSENGER AND CARGO DOORS OPERATION

Answer 3

‐ The maximum wind for passenger door operation is 65 kt
‐ The maximum wind for FWD and AFT cargo door operation is 40 kt (or 50 kt, if the aircraft nose
is into the wind, or if the FWD and AFT cargo doors are on the leeward side)
‐ The FWD and AFT cargo doors must be closed before the wind speed exceeds 65 kt.

Question 4

OPERATIONAL PARAMETERS
NOMINAL RUNWAY WIDTH

Answer 4

45 m

Question 5

OPERATIONAL PARAMETERS
MINIMAL RUNWAY WIDTH

Answer 5

30 m

Question 6

COCKPIT WINDOW OPEN MAXIMUM SPEED

Answer 6

200 kt

Question 7

MAXIMUM OPERATING SPEED VMO/MMO

Answer 7

350 kt/M 0.82

Question 8

MAXIMUM SPEEDS WITH THE LANDING GEAR EXTENDED

Answer 8

Maximum speed with the landing gear extended (VLE)…………………………………………..280 kt /M 0.67
Maximum speed at which the landing gear may be extended (VLO extension) …………. 250 kt /M 0.60
Maximum speed at which the landing gear may be retracted (VLO retraction) ………….. 220 kt /M 0.54

Question 9

MAXIMUM TIRE SPEED

Answer 9

195 kt

Question 10

TAXI SPEED
When the takeoff weight is higher than 76 000 kg (167 550 lb):

Answer 10

CAUTION Do not exceed a taxi speed of 20 kt during a turn.

Question 11

WIPERS MAXIMUM OPERATING SPEED

Answer 11

230 kt
Note: This limitation is applicable when the wipers are sweeping. It is not applicable if the wipers
are not sweeping for any reasons.

Question 12

With passengers on board, it is not recommended to exceed ___ without air conditioning supply. The lack of fresh air supply will significantly reduce the cabin’s air quality.

Answer 12

20 min

Question 13

CABIN PRESSURE
Maximum positive differential pressure

Answer 13

9.0 PSI

Question 14

CABIN PRESSURE
Maximum negative differential pressure

Answer 14

-1.0 PSI

Question 15

CABIN PRESSURE
Safety relief valve setting

Answer 15

8.6 PSI

Question 16

AUTOPILOT FUNCTION
The autopilot can be used with the following minimum values:
At takeoff

Answer 16

100 ft AGL and at least 5 s after liftoff

Question 17

AUTOPILOT FUNCTION
The autopilot can be used with the following minimum values:
In approach with FINAL APP, V/S or FPA mode

Answer 17

250 ft AGL

Question 18

AUTOPILOT FUNCTION
The autopilot can be used with the following minimum values:
ILS approach when CAT1 is displayed on the FMA

Answer 18

160 ft AGL

Question 19

AUTOPILOT FUNCTION
The autopilot can be used with the following minimum values:
In all other phases

Answer 19

500 ft AGL

The AP or FD in OP DES or DES mode can be used in approach. However, its use is only permitted if the FCU selected altitude is set to, or above, the higher of the two: MDA/MDH or 500 ft AGL.

Question 20

FLIGHT MANAGEMENT FUNCTION
DEGRADED SITUATION
If GPS PRIMARY LOST  is displayed on the ND and MCDU, the navigation accuracy remains sufficient for RNP operations provided that,

Answer 20

the RNP value is checked or entered on the MCDU and HIGH ACCURACY is displayed.

Question 21

AUTOMATIC APPROACH, LANDING AND ROLLOUT

MAXIMUM WIND CONDITIONS FOR ILS

Answer 21

Headwind : 30 kt
Tailwind : 10 kt
Crosswind : 20 kt (15 kt for automatic rollout with OEI)

If the tower reports a surface wind that exceeds the limitations, only CAT I automatic approach without autoland can be performed.

Question 22

AUTOMATIC APPROACH, LANDING AND ROLLOUT
AUTOMATIC LANDING
- ILS autoland are approved in CONF ___
- With a glide slope angle between ___
- With an airport elevation at or below ___
- With aircraft weight below ___
- Automatic landing is not allowed below ___

Answer 22

• 3 and CONF FULL
• (-2.5 ° and -3.25 °)
• 9 200 ft
• the maximum landing weight
• (-2 000 ft pressure altitude.)

Question 23

LIMITATIONS
AUXILIARY POWER UNIT
APU START

Answer 23

After three consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt.

Question 24

LIMITATIONS
AUXILIARY POWER UNIT
ROTOR SPEED Maximum N speed

Answer 24

107 %

Question 25

APU START/SHUTDOWN DURING REFUELING/DEFUELING During refuel/defuel procedures, APU starts or shutdown are permitted with the following restrictions:

Answer 25

‐ If the APU failed to start or following an automatic APU shutdown, do not start the APU ‐ If a fuel spill occurs, perform a normal APU shutdown.

Question 26

APU BLEED Max altitude to assist engine start

Answer 26

20 000 ft

Question 27

OIL TEMPERATURE Maximum temperature

Answer 27

151 °C

Question 28

OIL TEMPERATURE Minimum starting temperature

Answer 28

-40 °C

Question 29

OIL TEMPERATURE Minimum temperature before takeoff

Answer 29

52 °C

Question 30

OIL QUANTITY (Minimum) OAT at or above -30 °C

Answer 30

14 qt

Question 31

OIL QUANTITY (Minimum) OAT below -30 °C

Answer 31

16.5 qt

Question 32

MINIMUM OIL PRESSURE

Answer 32

65 PSI

Question 33

MAXIMUM OIL PRESSURE

Answer 33

270 PSI

Question 34

LIMITATIONS ENGINES STARTER

Answer 34

‐ A standard automatic start that includes up to two start attempts, is considered one cycle ‐ For ground starts (automatic or manual), a 35 s pause is required between successive cycles ‐ A 15 min cooling period is required, subsequent to three failed cycles, or 15 min of continuous or cumulated crank ‐ The starter must not be run when N2 is above 20 %.

Question 35

LIMITATIONS ENGINES REVERSE THRUST

Answer 35

- Selection of the reverse thrust is prohibited in flight. - Backing the aircraft with reverse thrust is not permitted. - Maximum reverse should not be used below 70 kt. Idle reverse is permitted down to aircraft stop.

Question 36

REDUCED THRUST TAKEOFF FLEX TAKEOFF TFLEX cannot be:

Answer 36

‐ Higher than TMAXFLEX, equal to ISA + 50 °C. ‐ Lower than the flat temperature (TREF). ‐ Lower than the actual OAT.

Question 37

CROSSWIND OPERATION ON GROUND ENGINE START The engine is able to start in crosswind up to

Answer 37

35 kt.

Question 38

SOFT GO-AROUND The use of GA SOFT mode is prohibited with

Answer 38

one engine inoperative

Question 39

Maximum operating altitude with slats and/or flaps extended

Answer 39

20 000 ft

Question 40

DEFINITION OF ICING CONDITIONS Icing conditions exist when the OAT (on ground or after takeoff) or the TAT (in flight) is

Answer 40

at or below 10 °C and visible moisture in any form is present (such as clouds, fog with visibility of 1 sm (1 600 m) or less, rain, snow, sleet or ice crystals). operating on ramps, taxiways or runways where surface snow, standing water or slush may be ingested by the engines, or freeze on engines, nacelles or engine sensor probes.

Question 41

BRAKE TEMPERATURE Maximum brake temperature for takeoff (brake fans off)

Answer 41

300 °C

Question 42

TAXI WITH DEFLATED OR DAMAGED TIRES If maximum one tire per gear is deflated (consider three gears) Maximum taxi speed during turn

Answer 42

7 kt

Question 43

TAXI WITH DEFLATED OR DAMAGED TIRES If two tires are deflated on the same main gear (maximum one main gear) Maximum taxi speed

Answer 43

3 kt

Question 44

TAXI WITH DEFLATED OR DAMAGED TIRES For the nosewheel steering (NWS) angle Maximum NWS angle

Answer 44

30 °

Question 45

TAXI WITH DEFLATED OR DAMAGED TIRES In addition, if tire damage is suspected, the flight crew must ask for

Answer 45

aircraft inspection prior to vacate the runway or taxi. If the ground crew suspects that a tire burst may damage the landing gear, maintenance action is due.

Question 46

BACF abbreviation

Answer 46

BRAKING ACTION COMPUTATION FUNCTION

Question 47

BACF The BACF results should not be used in the case of:

Answer 47

- Any failure impacting aircraft performance during landing (brakes, engines, aerodynamics...) or, - Runways with an average slope greater than 1 % (uphill or downhill).

Question 48

LIMITATIONS ENGINES THRUST SETTING/EGT LIMITS Takeoff and Go-around - All engines operative - One engine inoperative

Answer 48

Time Limit - 5 min - 10 min EGT Limit 1 083 °C

Question 49

LIMITATIONS ENGINES THRUST SETTING/EGT LIMITS Maximum Continuous Thrust (MCT)

Answer 49

EGT Limit 1 043 °C

Question 50

LIMITATIONS ENGINES THRUST SETTING/EGT LIMITS Starting

Answer 50

EGT Limit 1 083 °C