*Memory Limitations

Question 1

A*Nominal Runway Width
Minimal Runway Width

Answer 1

148 ft
100 ft

Question 2

*Max Demonstrated X-wind

Answer 2

38 kts (gust included)

Question 3

*Max Tailwind for Take Off or Landing

Answer 3

10 kts.

Question 4

*Max Tire Speed

Answer 4

195 kts (ground speed)

Question 5

*Windshield Wipers in Use

Answer 5

Max Speed 230

Question 6

*Cockpit Window Open

Answer 6

200 kts

Question 7

*Auto Pilot Function

(8)

Answer 7

T/Off……..100 ft/5sec after lift-off.

NPA (FINAL APP, NAV FPA, NAV V/S, TRK FPA, HDG V/S). 250 AGL

ILS Cat 1 displayed. 160AGL
ILS Cat 1 (Cat3 single/dual) 50’ below DA
Circling App. 500 ft
Manual Go-Around 100 ft
All other phases 500 ft

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 8

*Non Precision Approaches with Engine Out (319 only)

(3)

Answer 8

If one engine is inoperative, it is not permitted to use the autopilot to perform NPA in FINAL APP, NAV V/S, NAV/FPA,
only FD use is permitted.

Question 9

*Max Operating Altitude with Flaps/Slats Extended

Answer 9

20,000 ft.

Question 10

*Minimum Fuel Qty for Take Off

Answer 10

3300 lbs
The ECAM alerts that are related to fuel low level in the wing tanks (FUEL WING TK LO LVL, etc.) must not appear for take off.

Question 11

*Max Brake Temp for Takeoff (fans off)

Answer 11

300 C

Question 12

*APU Starter Limitation

Answer 12

After 3 consecutive APU start attempts, the flight crew must wait 60 mins before a new start attempt.

Question 13

*Thrust Settings/EGT Limits

Answer 13

T-OFF and Go Around 5 mins, 10 mins if OEI

MCT Not limited

Question 14

*Oil Temperature Limitations

Answer 14

Min starting temp -40 C
Min temp for takeoff -10 C

Question 15

*Min Oil Qty

Answer 15

9.5 Qts + 0.5 qts consumption for every flight hour.

Question 16

*Engine Starter Limitations

Answer 16

-A standard automatic start that includes up to 3 attempts is considered 1 cycle.
For ground starts a pause between cycles is 20 secs.
-Cooling period subsequent of 4 failed cycles: 15 mins
-No running engagement of the starter, when N2 is above 20%.

Question 17

*Reverse Thrust Limitations

Answer 17

Not during flight
Not allowed to back up the airplane
Max reverse should not be used below 70 kts. Idle reverse is permitted down to aircraft stop.

Question 18

*Turbulent air penetration speed

Answer 18

Vra. 0.76/275
Vra below 10,000’ 250

Question 19

*Take off limitations on contaminated runways

Answer 19

Not recommended on

1-water on top of compacted snow
2-Dry or wet snow over ice.

Not permitted when conditions reported as 0-NIL

Question 20

*APU Startup/Shutdown during refueling/defueling.

Answer 20

During refuel/defuel procedures, APU starts or shutdowns are permitted provided:
-If the APU fails to start or following an automatic shutdown, do not start the APU.
-If a fuel spill occurs, perform a normal APU shutdown.

Question 21

*Fuel imbalance at Take Off (in flight/landing)

Answer 21

If the quantity difference of the outer or inner wing fuel tanks on one side is greater than 800 lbs (1500 lbs, for inflight/landing), refer to the table located in the FCOM limitations.

Question 22

*APU Bleed use with HP Air Start Unit

Answer 22

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit, at the same time, to prevent any adverse effect on the Bleed Air System.

Question 23

*Packs use with LP Air Conditioning Unit

Answer 23

The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time, to prevent any adverse effect on the Air Conditioning System.

Question 24

*RNAV Approach

Answer 24

An RNAV (RNP) approach may be performed, with GPS PRIMARY not available, only if the radio navaid coverage supports the RNP value and HIGH accuracy is displayed on the MCDU with the specified RNP, and an operational approval is obtained.
An RNAV (GNSS) approach may be performed provided that the GPS PRIMARY is available.

Question 25

*Definition of Icing Conditions

Answer 25

-Icing conditions exist when the OAT (on ground or after takeoff) or the TAT (in flight) is at or below 10 deg. C and visible moisture in any form is present (such as clouds, fog with visibility of 1 SM (1600m) or less, rain, snow, sleet or ice crystals).
-Icing conditions also exist when the OAT on the ground and for takeoff is at or below 10 deg. C and 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 sensors probes.