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102 Cards in this Set
- Front
- Back
Maximum 90 degree crosswind for takeoff and landing? |
27kts |
|
Maximum 90 degree crosswind for landing from a cat 2 approach? |
15kts |
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Maximum headwind for landing from a cat 2 approach? |
16kts |
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Maximum tailwind for takeoff and landing? |
10kts |
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Maximum Operating Altitude in the 200? |
36,000ft |
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Maximum Operating Altitude 700/900 |
41,000ft |
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Maximum Taxi/Ramp Weight 701 |
75,250 lbs |
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Maximum Taxi and Ramp Weight 900 |
85,000 lbs |
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Maximum Takeoff Weight 701 |
75,000 lbs |
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Maximum Takeoff Weight 900 |
84,500 lbs |
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Maximum Landing Weight 701 |
67,000 lbs |
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Maximum Landing Weight 900 |
75,100 lbs |
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Maximum Zero Fuel Weight 701 |
62,300 lbs |
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Maximum Zero Fuel Weight 900 |
70,750 lbs |
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Turbulence Penetration Speed |
280 KIAS/.75M whichever is lower |
|
Max Gear Extension Speed |
220 KIAS |
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Maximum Gear Extended Speed |
220 KIAS |
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Maximum Gear Retraction Speed |
200 KIAS |
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Maximum Speed for Windshield Wiper Operation |
220 KIAS |
|
Flaps 1 speed 701/900 |
230 KIAS |
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Flaps 8 Speed |
230 KIAS |
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Flaps 20 Speed |
220 KIAS |
|
Flaps 30 Speed |
185 KIAS |
|
Flaps 45 Speed |
170 KIAS |
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During Taxi or Takeoff when would you only activate Cowl Anti-Ice? |
Ground contamination or visible moisture with an OAT 10°c or below. |
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During Takeoff when would you activate both Wing and Cowl Anti-Ice systems? |
With ground contamination or visible moisture with an OAT 5°c or below. |
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In flight what conditions would require the use of only Cowl Anti-Ice? |
Visible moisture from TAT 10°c to SAT -40°c and an airspeed greater than or equal to 230 KIAS. |
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In flight what conditions would require the use of both Wing and Cowl Anti-Ice systems? |
Visible moisture from TAT 10°c to SAT -40°c and an airspeed less than 230 KIAS. |
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If the Ice Annunciation illuminates what is the response? |
Wing and Cowl Anti-Ice systems on. |
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What does a red engine EICAS message signify? |
Maximum and minimum limitations. |
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What does an Amber engine EICAS message indicate? |
Caution range |
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What does a green engine EICAS message indicate? |
Normal operating range. |
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When are there no limitations on applying TOGA thrust due to wind direction? |
Wind within 30° of the nose, or more than 30° with a wind speed less than 5 kts |
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When may you only apply 75% N1 before brake release on takeoff? |
Wind more than 30° off the nose between 5 kts and 30 kts. |
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When may you only apply idle/taxi thrust before brake release on takeoff? |
Wind more than 30° off the nose with a windspeed greater than 30 kts. |
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Engine start crank limits first start. |
90 seconds on 10 off. 7/9 60 seconds on 10 off. 2 |
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Engine start crank limits second start. |
90 seconds on then 10 seconds off. 7/9 60 seconds on then 10 seconds off. 2 |
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Engine start crank limits third and subsequent starts. |
90 seconds on 5 minutes off 7/9 60 seconds on 5 minutes off 2 |
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Minimum oil pressure for takeoff |
45 psi |
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Max fuel imbalance for takeoff 701/900 |
300 lbs |
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Max fuel imbalance all phases other than takeoff 701/900 |
800 lbs |
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Maximum fuel quantity in pounds 701/900 |
19,594 lbs |
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What must the ITT be below for all ground starts? |
120°c |
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Bleed air extraction for air conditioning from the APU is not permitted |
At or above 25,000 ft |
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Which engines may be started using the APU as the bleed source? |
Each engine may be started using the APU |
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What is the APU starter motor duty cycle? |
No more than 3 starts/start attempts in 1 hour with 2 minutes between each cranking attempt. |
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If the APU door is not closed, or the position is unknown what precautions must be taken? |
Airspeed limited to 220 KIAS (300 KIAS in the 200), or the APU must remain in operation. |
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What is ground contamination? |
Runways, ramps, or taxiways with surface snow, ice, slush, or standing water. |
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What is visible moisture? |
Visible moisture or precipitation in any form (including fog with vis 1sm or less) is present in flight or below 400 ft agl for takeoff. |
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Do not hold in icing conditions with... |
Slats/flaps extended |
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When must a tactile check be performed? |
OAT 10°c or less Bulk fuel 0°c or less Atmospheric conditions conducive for frost Ice and frost may continue to adhere to wing surfaces even at temps above 10°c |
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Max itt of thrust lever from shut-off to idle? |
120°c or less |
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After starting the engines do not exceed... |
75% N1 for 2 minutes or until engine indicators are in the green, whichever is longer. |
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Operate all engines at or near idle for... |
2 minutes prior to shutdown |
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Min oil pressure for takeoff? |
45 PSI |
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When must continuous Ignition be used? |
Takeoff/landing on contaminated runway
Takeoff with crosswind >15kts
Flight through moderate or heavier intensity rain
Flight through moderate or greater turbulence
Flight in vicinity of thunderstorm |
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Maximum single pack altitude 701 |
31,000ft |
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Max altitude single pack 900 |
25,000ft |
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Minimum autopilot engagement altitude under normal circumstances? |
600ft |
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Minimum auto pilot engagement altitude on a non precision and precision approach respectively? |
400 ft / 80 ft |
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What auto pilot mode is prohibited during approach? |
Speed |
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Maximum slats/flaps extension altitude? |
15,000ft |
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Enroute use of slats/flaps |
Is prohibited |
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Minimum altitude for flight spoiler deployment? |
1,000ft agl |
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Minimum speed for flight spoilers? |
Ref +17kts |
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Minimum brake cooling time after a RTO |
15 minutes and all BTMS must indicate green and not be increasing |
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Max time for taxi light operation while stationary? |
No longer than 10 minutes |
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Draw the RVSM required equipment list. |
|
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How much fuel may be in the center tank during Takeoff? |
500 lbs unless there is at least 4,400 lbs in each wing tank. |
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Maximum runway slope |
2% takeoff or landing |
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Max temp for takeoff |
ISA +35 |
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Minimum temperature |
-40°c |
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Max windshield failed non parked speed |
250 KIAS |
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Tire Limit Ground Speed |
700/200-182kts 900-195kts |
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Max cruise Mach in RVSM airspace |
.82 mach |
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Max altitude to start the APU? |
37,000ft |
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Max APU running altitude |
41,000ft |
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Permissible AC electric load |
40 kVA |
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Max load on each TRU |
120 amps |
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Max itt for a 200/700/900 ground start. |
120°c |
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What conditions would be considered cold soaked? |
-30°c or below for more than 8 hours |
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What are the cold soak starting procedures? |
Motor engines for 60 seconds and verify fan rotation. Thrust reversers must be actuated until stow and deploy cycles are 2 seconds or less. |
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Max continuous oil temperature |
155°c |
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Dry motor cycle limits |
First: 90 seconds on 5 minutes off Second and subsequent: 30 seconds on 5 minutes off |
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When would you not use FLEX takeoff? |
Anti-skid inop Contaminated runway Airplane has been de-iced Wing or Cowl Anti-Ice in use Any windshear/downdraft warnings Engine cannot create full thrust When a departure calls for full thrust
|
|
Engine fuel temp must be at least what temperature for takeoff? |
5°c |
|
Contaminated runway landing is prohibited when |
Standing water more than .75 inches Slush or wet snow is more than .88 inches Dry snow more than 3.75 inches |
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Max pressure altitude for takeoff and landing |
8,000ft |
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Maneuvering limit load factors |
Flaps up: -1 to 2.5 Flaps down: 0 to 2 |
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Max pressure differential during ground ops? |
.1psi |
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Max pressure differential at touchdown? |
1.0psi |
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Do not exceed what cabin Altitude when In manual mode? |
-1,500ft |
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Max altitude to use APU to start the engines? |
21,000ft |
|
What time limit is applied to the usage of normal takeoff power and maximum power? |
Limited to 5 minutes |
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APR power usage single engine is limited to |
10 minutes |
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APR power is prohibited |
Above 7,500ft |
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Max itt for airstart |
90° |
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In flight starter cranking limits |
2 minutes on 10 seconds off Then 1 minute on 5 minutes off |
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After deploying thrust reversers |
Do not attempt a go around |
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Turning radius of 700 |
75ft |
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Min fuel per wing tank for a go around |
600lbs 7/9 450lbs 2 |
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Cat 2 approaches not allowed when braking action is less than |
Fair |