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127 Cards in this Set
- Front
- Back
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Max Taxi and Ramp Wt
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48,300
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Max Take Off Wt
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48,200
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Max Landing Wt
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38,000
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Max Zero Fuel Wt
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32,000
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Min Flight Wt
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26,000
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Min Operating Empty Wt
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22,150
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Max Landing Wt May be Limited at airports that is above what elevation
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10,000
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Max Airport Pressure Altitude for Takeoff and Landing
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10,000
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Max Operating Altitude
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41,000
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Max Ambient Operating Temp for takeoff
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+35c
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Min Ambient Operating Temp for Takeoff
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-40c
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At Altituds above 25000 feet, one pilot must wear a
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Safety Harness
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Is Take Off Permitted with any frost on any surface
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No
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What conditions demand a tactile inspection of the plane for frost
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Outside Temp is 5c or less
Temp of wing cannot be determined Visible Moisture Water Present OAT and Dewpoint are within 3c Atmospheric Conditions are Conducive to Frost Formation |
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When must Cowl Anti Ice Be on for ground operations
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When OAC is 10c or les and there is visible moisture (fog, visibility of less than one mile, rain, sleet, Ice Crystals)
Or on runways or ramps with standing water, ice, snow, slush. |
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When must Cowl Anti Ice be on in flight
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Icing conditions must be at or below 10c and not less than -40c
It must be on above 22000ft when Ice is detected by the Ice dection system and when Icing conditions exists and the Ice detections system is Inop, Cowl Anti Ice should be on when Icing conditions exists or Ice is detected by the Ice detections systme. |
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When must Wing Anti Ice be On for ground operations
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When OAC is 5c or less and there is visible moisture (fog, visibility of less than one mile, rain, sleet, Ice Crystals)
Or on runways or ramps with standing water, ice, snow, slush. If type 2,3 or 4 anti ice solutions have been applied, the wing anti ice must only be selected on just prior takeoff thrust has been applied. |
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When Must Wing Anti Ice be used In flight
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Icing conditions must be at or below 10c and not less than -40c
It must be on above 22000ft when Ice is detected by the Ice dection system and when Icing conditions exists and the Ice detections system is Inop, Anti Ice should be on when Icing conditions exists or Ice is detected by the Ice detections systme. |
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When must the Wing and Cowl Anti Ice be on during Super Cooled Large Droplet Icing
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Operation is Prohibitied
Indicated by side window icing must exit these conditions Wing and Cowl Anti Ice must be on |
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What are the Min and Max Runway Slopes
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+2
-2 |
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What is the Max Tailwind for takeoff and landing
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10 kts
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What is the Max Glidepath Angle for ans approach
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4 degrees
3.5 degrees at an airport with an elevation of 7000 feet or more |
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Min number of flight crew
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one Pilot and one Co Pilot
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Max Occupants
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22 or the The max number approved for the airplane configuration
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Max Cross Wind
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24 knots OR
With 3.00mm or .125 inches of standing moisture and a co efficient of braking of .3 10 knots .4 15 knots .5 24 knots Or an contaminated runwat is 10 knots. Operations with a braking coefficient of less than .3 is prohibited. |
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What are the Engines
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General Electric
CF34-3B |
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N1 Normal Range
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0 to 98.5
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N1 Max or red
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98.6
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ITT APR not Operating, normal range
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0 to 900 for first 2 mins
0 to 884 for second 3 mins |
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ITT APR Operating, Normal range
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0 to 928 first 2 mins
0 to 900 second 3 mins |
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ITT Max Continous Thrust
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900
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Max N2 percent RPM
Wing anti Ice on and off |
99.3
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N2 Percent RPM Caution Range
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0 to 77.9
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N2 Percent RPM Normal Range
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Wing Anti Ice on 78 to 99.2
Wing Anti Ice Off 0 to 99.2 |
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Max Oil Temp
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163c
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Oil Temp Caution Range
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155c to 162c
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Oil Temp Normal Range
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-40c to 154c
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Min Oil Pressure psi
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25psi
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Oil Pressure Caution Range
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116 to 156psi
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Oil Pressure Normal Range
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26 to 115psi
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Engine operating limits for Start
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N2 20 percent rpm
N1 ITT 903 for up to 50 seconds |
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Engine operating limits for Acceleration
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N2
N1 ITT 930 for up to 5 seconds |
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Engine operating limits for Max Continous
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N2 99.2 percent rmp
N1 98.6 ITT 899 |
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Engine Operating Limits for
Normal Takeoff |
N2 98.3
N1 96.2 ITT 884 for 5 mins 900 for 2 mins out of 5 total transient |
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Engine Operating Limits for
Max Takeoff (APR Operating) |
N2 99.4 percent rpm
N1 98.6 ITT 899 for 5 min 928 for 2 mins of 5 mins total transient time |
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above what altitude must one airconditioning pack or cowl anti ice be selected on for each engine
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40,000 ft
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What is the definition of cold soaked
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-30 or below for 8 hours or more
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When the plane is cold soked, what must you do before starting
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Motor each engine for 60 seconds before starting and Thrust Reversers must be actuated until they deploy and stow in 5 secs or less.
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Oil Temp Min for starting
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-40c
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Oil Temp Max Continous
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+155c
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Oil Temp Max Permissable
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+163c for 15 mins max
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Oil Pressure Min Steady state Idle
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25 psi
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Oil Pressure Min Take Off
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45 psi
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Oil Pressure Max Continous
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110 psi
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Oil Pressure Max Transient after cold start
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115 psi which is the transmitter limit (10 mins max)
Engine must remain at Idle until oil pressure returns to normal. |
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When must continous Engine Ignition be used
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take off and landing on contaminated runways
take off and landings in high crosswinds flight through moderate or heavier continous rain flight through moderate or heavier turbulence flight in the vicinity of Thunder Storms |
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When must APR be verified functional
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when using apr numbers for takeoff
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Must APR be selected off if you get an APR INOP messange on EICAS
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Yes and APR off numbers must be used for takeoff
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Starter Cranking Limits
Starter must not be used if N2 rpm exceeds |
55 percent
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Starter Cranking Limits Normal
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3 consecutive engine starts with 5 minutes cooling between starts
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Starter Cranking Limits
At Initiation of thrust lever movement between Cut Off and Idle, ITT must be |
Ground Start 120c or less
Air Start 90c or less |
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What are the Dry Motoring Starter Limits
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1rst Cycle 90 seconds followed by 5 minutes off
2nd and Subsequent 30 seconds followed by 5 minutes off |
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When can a engine relight be performed
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Only when within the performance envelope
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Max Fuel inbalance between the main tanks on
Ground |
400lbs
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Max Fuel inbalance between the main tanks in flight
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800lbs
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Max Fuel inbalance between main tanks or landing
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400lbs
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Max Fuel in left and right main
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4860lbs each
9720 total |
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Max Fuel in Aux Tank
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7168lbs
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Max fuel in Tail Tank
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3112lbs
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Total Usable Fuel with all tanks full
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20000lbs
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Takeoff with up to 500lbs fuel in the aux tank is allowed as long as each wing contains
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1500lbs
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What is the Min Fuel Quantity for go around
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500lbs per wing, assuming the nose up pitch is not more than 10 degrees.
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Min fuel temp for takeoff
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5c
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Can Fuel Transfer be on for takeoff
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no
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What position must the flaps be in for fuel jettison
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0 degrees
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Is fuel jettison prohibited when lightning exists
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yes
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What is the Max Oil Consumption
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6.4 ounces per hour
0.05 gallons per hour |
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When must the oil level be checked
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between 15 minutes to two hours after the engines have been shut down. If beyond those limits the engine must be motored.Max refill limit is 2 quarts without dry motoring the engine
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What apu
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36-150 or gtcp-36-100(e)
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At what rpm will the apu shut down
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36-150 107 percent
gtcp-36-100(e) 110 percent |
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Max APU EGT
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731c
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Min ambient temp for Cold Soaked Start
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-40c
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What are the APU starter limits when starting on Batterys
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3 attempts of not more than 30 seconds continous cranking
Followed by a 20 minute rest time. Followed by 2 more attempts of not more than 15 seconds cranking. If no start, no further attempts may be attempted. |
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What are the APU starter limits when using a ground power.
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2 Start attempts of not more than 15 seconds cranking, followed by a 20 minute rest period. Followed by 2 more attempts of not more than 15 seconds cranking.
If APU does not start, no further attempts may be made. |
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APU Max EGT
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974c
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What constitutes an APU hung start
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36-150 If not more than 30 percent after 60 secs of cranking.
GTCP-36-100(E),below 60 percent for max of 20 seconds. between 60 to 95 percent for max of 10 seconds |
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In flght start of the APU gauranteed up to what altitude.
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36-150 20000ft
GTCP-36-100(E) 15000ft, but demonstrated up to 20000ft |
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Bleed Air extraction from the APU is not permitted above what Altitude
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36-150 15000ft
GTCP-36-100(E) 14500ft and bleed air extraction is not permitted inflight whenever standby electrical power is required from the APU |
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What is the Max APU Generator load in flight
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36-150 30kVA
GTCP-36-100(E) use of APU generator may not be used unless both engine driven generators are offline. |
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Mmo
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.85 or not more than .83 in RVSM airspace
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Vmo
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300kts to 348kts depending on altitude
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Vfe
20 30 45 |
231
197 189 |
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Vlo
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197
.6 |
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Vle
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250
.7 |
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Max Gear Extended Altitude
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20000ft
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Tire Limit Speed
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182
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Max Speed with ADG deployed
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250
When Operationally Necessary 330 for 12 minutes 348 for 4 minutes 215 for flight test or pilot training |
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Turbulence Penetration Speed
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280
.75 |
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Load Factors
Flaps Up Flaps Down |
-1.0 to 2.5 g
0.0 to 2.0 |
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Are Side Slips allowed
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no
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Max relief differential pressure
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9.2 psi
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Max negative differential pressure
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-0.5
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Max defferential during taxi, takeoff, and landing
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0.2
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Min autopilot engage altitude after takeoff
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320ft AGL
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Min autopilot use height for visual and non-precision approaches
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320ft AGL
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Min autopilot use height for precision approaches with glideslope angle of 3.5 degrees or less
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80ft AGL
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Min autopilot altitude use for precision approach with glidepath angle between 3.6 and 4.7 is
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160ft AGL
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Max IDG Generator Load
Below 35000ft Above 35000ft |
30kVA
25kVA |
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Max load on each TRU is
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100 amp
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Are use of flaps allowed in flight
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no
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Flight with flaps extended is prohibited above what altitude
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15500ft
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Min Altitude with flight spoilers extended
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300ft
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Min speed for flight spoiler extension
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Vref +10kts
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Must both stick shacker and pushers be on for all phases of flight
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yes
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When is stll protection test indicator used
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Only for System testing
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Are Thrust Reversers approved for flight
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No, for ground use only
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Are Thrust Reversers approved for go arounds
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No, for full stop only
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Can you takeoff with any TR icon or caution alert message shown on EICAS
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no
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During landing what N1 are you limited to when below 60kts
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60 percent
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Max demonstrated crosswind with TR deployed
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24kts, this was demonstrated on a dry runway and is considered limiting
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When must taxi lights be selected off
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when stationary for more than 10 minutes
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How do you determine amount of time to cool the brakes between takeoffs
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Ref performance section for wheel brake cooling
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What must be accomplished if a fusible plug releases on the wheels
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The wheels , brakes, tires and the antiskid speed sensors must be inspected before the next takeoff.
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Are pilots authorized to deviate from ATC clearance in order to comply with an resolution advisory (RA) command.
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Yes, The pilots shall inform ATC of the deviation from the ATC clearance following the response to the RA
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May Evasive Maneuvers be made solely on information presented on the traffic display
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no
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What modes has the transponder been demonstrated in
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Mode A and C and TCAS functions
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What is the Configuration Deviation List (CDL).
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Allows operation with certain secondary airframe and/or necelle missing must be in accordance with the AFM as amended by the CDL
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