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80 Cards in this Set

  • Front
  • Back

Max Ramp Weight and Taxi weight

53250 lbs

Max TO Weight

53000 lbs

Max Landing Weight

47000 lbs

Max Zero Fuel Weight

44000 lbs

Minimum flight weight

30000 lbs

Max Cargo in cargo compartment

3500 lbs

Max Turbulent Air Speed

280 KIAS or M 0.75 whichever is lower

Maximum Operating speed

M 0.85 or 335 KIAS (can be lower depending of pressure altitude)

Max Differential for pressurization

8.7 PSI

Max Negative differential pressure

-0.5 PSI

Maximum Differential pressure for taxi, take off and landing

0.1 PSI

Minimum Cabin Altitude while in manual mode

-1500 ft

Maximum altitude for single pack operation

25000 ft

Autopilot engaged prohibited at what altitude for visual or non-precision approaches

400 ft AGL

Autopilot engaged prohibited at what altitude for precision app (ILS/PAR)

80 ft AGL

Autopilot engaged at what minimum altitude

600 ft AGL

On a SCDA what is the span for the descent angle allowed

Not less than 2.9 degrees and not more than 3.5 degrees

Max Load on Main AC Generator from 0 to 35000 ft

30 kVA

Max Load on Main AC Generator above 35000 ft

25 kVA

Max Load on APU AC Generator from 0 to 37000 ft

30 kVA

Max Load on APU AC Generator above 37000 ft

APU Operation not permitted

Max continuous load on each TRU in flight

100 AMPS

Max time permissible with DC power only on the ground

5 minutes (to protect flight deck CRT display)

Maximum Airspeed with ADG deployed

Vmo or Mmo

Max altitude for Slats/flaps operations

15000 ft

Flaps 8 Vfo

200 KIAS

Flaps 20 Vfo

200 KIAS

Flaps 30 Vfo

185 KIAS

Flaps 45 Vfo

170 KIAS

Minimum altitude for use of flight spoilers

300 ft AGL

Flight spoilers must not be extended in flight at airspeeds below applicable minimum speed book Landing speed (Vref) for Flaps setting, plus how many knots ?

17 KIAS

Left and right main tank quantity

4760 lbs

Centre tank fuel quantity

4998 lbs

Total fuel quantity

14518 lbs

Minimum engine fuel temperature for takeoff

5 degrees Celsius

Takeoff with a fuel load in excess of 500 lbs in the centre tank is not permitted unless:

.Each main tank is above 4400lbs or,


.Each wing tank is above 2000lbs; and,


.the allowable zero fuel weight is reduced by the weight of the fuel in the center tank in excess of 500lbs; and,


.the centre of gravity in this config is verified to be within the allowable CG envelope.

Max fuel imbalance between main tanks

800 lbs

Minimum fuel in each main wing tank for go around (assuming a max of 10° nose up)

450 lbs

Can the powered crossflow and gravity crossflow be ON for Takeoff ?

NO !

Normal HYD system pressure

2800 PSI to 3200 PSI

Normal HYD system quantity

45% to 85%

How are the L&R 10TH stage bleed valve on take off and landing if Wing anti ice is NORM and Cowl anti ice is ON ?

They must be closed !

Max speed with windshield wipers

220 KIAS

Anti Ice requirement on ground

Anti Ice requirement in flight

What are the condition to have the CAS Message : Bleed Misconfig during an approach and it's acceptable

. Ceiling at arrival airport above 3000 AGL


. Icing conditions do not exist for landing or go around


. The WING and COWL anti ice is selected OFF prior to landing

Max operating speed for gear extension

250 KIAS

Max operating speed with gear down and locked

250 KIAS

Max operating speed for gear retraction

200 KIAS

Tire speed limit

182 knots Ground speed

Minimum brake cooling time between landing stop or reject take off and a subsequent take off ?

15 minutes

Starter limits

1 / 1 minute / 10 sec off


2 / 1 minute / 10 sec off


3 / 1 minute / 5 min off


4 and subsequent / 1 minute / 5 min off

N2 limit for starter cut out ?

55 % N2

Max ITT to go from Shut off to Idle

120 ° C or less on ground


90 ° C for airborne starts

Minimum idle oil pressure

25 PSI

Minimum oil pressure at takeoff power

45 PSI

Max continuous oil pressure

115 PSI

How long can oil pressure be greater than 115 PSi ?

10 min and engine must be at idle until back to normal range

Max oil consumption per engine ?

189 Cubic centimeter per hour (6.4 ounces per hour / 0.05 US Gallons per hour)

When do we need Continuous Ignition ?

Normal value for N1 reverser at IDLE ?

25% to 30% N1

When can we not use reduced trust ?

APU Max operating altitude

37000 ft

Max Altitude for APU starting

30000 ft

Minimum temperature on the ground to start a cold soaked APU ?

-40°C

Max altitude for Air conditioning use from APU

15000 ft

APU bleed extraction for engine start in flight max altitude ?

13000 ft

Limitations when APU door is not closed or in an unknown position

Max 300 KIAS


APU must remain ON

Maximum pressure altitude for take off and landing

10000 ft

Maximum operating altitude

41000 ft

Maximum ambient air temperature for take off and landing

50° C

Minimum ambient air temperature for take off

-40°C

Max Crosswind for Dry/ Damp runway

27 kts

Max Crosswind for Wet runway

22 kts

Max Crosswind for Contaminated and or slippery runway

15 kts

Max Crosswind for CAT II/III app

13 kts

Max headwind for CAT II/III app

19 kts

Max tailwind for CAT II/III app

10 kts

Minimum useable runway width for takeoff and landing

98 ft (30m)

Maximum depths of contaminants covering the useable area of the runway are :