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80 Cards in this Set
- Front
- Back
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Max Ramp Weight and Taxi weight |
53250 lbs |
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Max TO Weight |
53000 lbs |
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Max Landing Weight |
47000 lbs |
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Max Zero Fuel Weight |
44000 lbs |
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Minimum flight weight |
30000 lbs |
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Max Cargo in cargo compartment |
3500 lbs |
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Max Turbulent Air Speed |
280 KIAS or M 0.75 whichever is lower |
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Maximum Operating speed |
M 0.85 or 335 KIAS (can be lower depending of pressure altitude) |
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Max Differential for pressurization |
8.7 PSI |
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Max Negative differential pressure |
-0.5 PSI |
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Maximum Differential pressure for taxi, take off and landing |
0.1 PSI |
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Minimum Cabin Altitude while in manual mode |
-1500 ft |
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Maximum altitude for single pack operation |
25000 ft |
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Autopilot engaged prohibited at what altitude for visual or non-precision approaches |
400 ft AGL |
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Autopilot engaged prohibited at what altitude for precision app (ILS/PAR) |
80 ft AGL |
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Autopilot engaged at what minimum altitude |
600 ft AGL |
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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 |
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Max Load on Main AC Generator from 0 to 35000 ft |
30 kVA |
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Max Load on Main AC Generator above 35000 ft |
25 kVA |
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Max Load on APU AC Generator from 0 to 37000 ft |
30 kVA |
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Max Load on APU AC Generator above 37000 ft |
APU Operation not permitted |
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Max continuous load on each TRU in flight |
100 AMPS |
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Max time permissible with DC power only on the ground |
5 minutes (to protect flight deck CRT display) |
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Maximum Airspeed with ADG deployed |
Vmo or Mmo |
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Max altitude for Slats/flaps operations |
15000 ft |
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Flaps 8 Vfo |
200 KIAS |
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Flaps 20 Vfo |
200 KIAS |
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Flaps 30 Vfo |
185 KIAS |
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Flaps 45 Vfo |
170 KIAS |
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Minimum altitude for use of flight spoilers |
300 ft AGL |
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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 |
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Left and right main tank quantity |
4760 lbs |
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Centre tank fuel quantity |
4998 lbs |
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Total fuel quantity |
14518 lbs |
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Minimum engine fuel temperature for takeoff |
5 degrees Celsius |
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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. |
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Max fuel imbalance between main tanks |
800 lbs |
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Minimum fuel in each main wing tank for go around (assuming a max of 10° nose up) |
450 lbs |
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Can the powered crossflow and gravity crossflow be ON for Takeoff ? |
NO ! |
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Normal HYD system pressure |
2800 PSI to 3200 PSI |
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Normal HYD system quantity |
45% to 85% |
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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 ! |
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Max speed with windshield wipers |
220 KIAS |
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Anti Ice requirement on ground |
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Anti Ice requirement in flight |
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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 |
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Max operating speed for gear extension |
250 KIAS |
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Max operating speed with gear down and locked |
250 KIAS |
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Max operating speed for gear retraction |
200 KIAS |
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Tire speed limit |
182 knots Ground speed |
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Minimum brake cooling time between landing stop or reject take off and a subsequent take off ? |
15 minutes |
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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 |
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N2 limit for starter cut out ? |
55 % N2 |
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Max ITT to go from Shut off to Idle |
120 ° C or less on ground 90 ° C for airborne starts |
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Minimum idle oil pressure |
25 PSI |
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Minimum oil pressure at takeoff power |
45 PSI |
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Max continuous oil pressure |
115 PSI |
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How long can oil pressure be greater than 115 PSi ? |
10 min and engine must be at idle until back to normal range |
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Max oil consumption per engine ? |
189 Cubic centimeter per hour (6.4 ounces per hour / 0.05 US Gallons per hour) |
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When do we need Continuous Ignition ? |
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Normal value for N1 reverser at IDLE ? |
25% to 30% N1 |
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When can we not use reduced trust ? |
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APU Max operating altitude |
37000 ft |
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Max Altitude for APU starting |
30000 ft |
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Minimum temperature on the ground to start a cold soaked APU ? |
-40°C |
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Max altitude for Air conditioning use from APU |
15000 ft |
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APU bleed extraction for engine start in flight max altitude ? |
13000 ft |
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Limitations when APU door is not closed or in an unknown position |
Max 300 KIAS APU must remain ON |
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Maximum pressure altitude for take off and landing |
10000 ft |
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Maximum operating altitude |
41000 ft |
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Maximum ambient air temperature for take off and landing |
50° C |
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Minimum ambient air temperature for take off |
-40°C |
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Max Crosswind for Dry/ Damp runway |
27 kts |
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Max Crosswind for Wet runway |
22 kts |
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Max Crosswind for Contaminated and or slippery runway |
15 kts |
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Max Crosswind for CAT II/III app |
13 kts |
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Max headwind for CAT II/III app |
19 kts |
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Max tailwind for CAT II/III app |
10 kts |
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Minimum useable runway width for takeoff and landing |
98 ft (30m) |
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Maximum depths of contaminants covering the useable area of the runway are : |
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