Load factor limitation clean

Enviornmental envelope in flight

Load Factor other than clean configuration

Enviornmental envelope for takeoff and landing

Enviornmental envelope minimum TAT

Runway slope (Mean)

Minimum runway width

The flight crew applies specific procedure for runway + shoulders is less than___ metes wide (input number only)

The techinique of turn on a runway or turn pad is not permitted

Maximum certified crosswind at takeoff (gust included)

Maximum certified crosswind at landing (gust included)

Maximum tailwind at takeoff

Maximum tailwind at landing (if the airport pressure altitude is at, or below 8000ft)

Maximum tailwind at landing (if the airport pressure altitude is ABOVE 8000ft)

Meximum wind for cabin door operation

Maximum wind for cabin door operation if the aircraft nose is oriented into the wind

Maximum wind for CARGO door operation is 40kt, maximum wind is 50k if the aircraft nose is oriented into the wind or if the CARGO door is____

The cabin and cargo door must be closed before the wind reaches

Cockpit window maximum opening / closing speed

Operating the cockpit window is NOT possible with____

Maximum flaps / slats speeds of configuration 1, 1+F, 2, 3 and full (write only the numbers in sequence separated by a space)

Maximum operating speed VMO (type only numbers)

Maximum operating speed MMO

Maximum speed with the landing gear extended VLE

Maximum speed with the landing gear operating VLO

Maximum speed for landing gear gravity extension VLE/VLO

Maximum tire speed (maximum ground speed)

VMCL and VMCL2 for both models

Windshield wipers maximum speed

Maximum taxi weight for all variants

Maximum takeoff weight for all variants

Maximum landing weight

Maximum zero fuel weight all variants

Minimum weight

Takeoff with both packs off is prohibited

______ when APU supplies bleed air

The airflow from the LP ground carts must not exceed

Cabin pressure maximum positive / negative differential pressure

Minimum height for the use of autopilot at takeoff

Minimum height for the use of autopilot in Non-precision approach

An internal PRIM logic prevents the autopilot from engaging ______

Minimum height for the use of autopilot circling approach

Minimum height for use of autopilot ILS Approach with APPR1 displayed on FMA

Minimum height for use of Autopilot after a manual go around

Minimum height for the use of Autopilot ALL OTHER PHASES

The AP or FD in OP DES or DES mode can be used in approach

All AP/FD modes may be used with or without autothrust, except if specified.

Autothrust may be used with, or without AP/FD, __________

Maximum headwind for automatic approach, landing and rollout.

Maximum crosswind for automatic approach, landing and rollout

Maximum tailwind at automatic landing landing if the airport pressure altitude is below 8000ft

Maximum tailwind at automatic landing if the pressure altitude is above 8000ft

Wind limitation is based on the wind reported by…

GLS cathegory 1 minimum decision height

ILS CAT II Minumum decision height

If the flight crew performs an automatic approach without autoland (CAT II), the autopilot must be disengaged no later than…

ILS CAT III FAIL PASSIVE minumum decision height

ILS CAT III FAIL OPERATIONAL Alert height

ILS CAT III FAIL OPERATIONAL Minimum RVR

ONE ENGINE INOPERATIVE Automatic approach and automatic landing are approved in __________, if engine out procedures are completed before reaching 1 000 ft in approach.

TWO ENGINES INOP OPPOSITE SIDE, Automatic approach and automatic landing are approved in _______, if engine out procedures are completed before reaching 1 000 ft in approach.

CAT IIIB Operation is NOT authorized on contaminated runways

GLS CAT I, ILS CAT II or III automatic landing has been demonstrated

During the APU start, the flight crew must wait ____s after setting the APU MASTER SW pb-sw to ON, before setting the APU START pb to ON. These XXs correspond to the time the ______ when the APU MASTER SW pb-sw is set to ON.

In the case of an aborted APU start or APU shutdown, the flight crew must wait ____ before a new start attempt. This 60 s period is due to the ______ after an aborted APU start or APU shutdown.

After three consecutive APU start attempts, the flight crew must wait _____ before a new start attempt. This 60 min period is to allow ____________.

APU maximum N1/N2 rotor speeds

APU maximum indicated EGT

Maximum EGT for APU start

Maximum aircraft speed for APU operation

In the case of all engine failure, APU con operate

(APU) On ground…

In flight, up to______ft, only one APU generator can operate.

Use of APU bleed air for WAI ______

EA Thrust setting / EGT limits TOGA, MCT, Starting on ground, Starting in flight

RR Thrust setting / EGT limits TOGA, MCT, Starting in ground, Starting in flight

EA OIL temperature Maximum, starting, prior to takeoff, minumum pressure

EA minimum oil quantity

RR Oil temperature, Maximum, Minimum starting, Minimum before TO

EA starter limitation

RR Starter limitation

Reverser thrust limitations

Takeoff at reduced thrust is not allowed on contaminated runways.

The flex temperature must not be:

The use of the GA Soft mode (soft go-around function) is prohibited on airport with missed approach gradient greater than…

Maximum operating altitude with flaps/slats extended

JET A fuel specification freezing point.

JET A1 fuel specification freezing point.

JP5 fuel specification freezing point.

JP8 fuel specification freezing point.

TS-1 fuel specification freezing point.

RP-3 fuel specification freezing point.

Maximum fuel temperature

Maximum Allowed Wing Imbalance at Takeoff, in Flight , and Landing FEED TANKS (1 vs 4; 2 vs 3)

Maximum Allowed Wing Imbalance at Takeoff, in Flight , and Landing INNER TANKS (L vs R)

Maximum Allowed Wing Imbalance at Takeoff, in Flight , and Landing MID TANKS (L vs R)

Maximum Allowed Wing Imbalance at Takeoff, in Flight , and Landing OUTER TANKS (L vs R)

Minimum fuel quantity before pushback