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63 Cards in this Set
- Front
- Back
Thrust setting Takeoff
|
5 min
|
|
Thrust setting Maximum Continuous
|
CONT
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Thrust setting IDLE
|
CONT
|
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Thrust setting Takeoff Maximum Observed ITT
|
700
|
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Maximum Continuous Thrust Setting at Maximum Observed ITT
|
680
|
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Thrust setting IDLE at Maximum Observed ITT
|
580
|
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Thrust setting Takeoff N2%
|
96
|
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Maximum Continuous Thrust Setting N2%
|
96
|
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Thrust setting IDLE N2%
|
52 (min)
|
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Thrust setting Transient N2%
|
96
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Starting Maximum Observed ITT
|
550 - 600 4 sec
600 - 700 2 sec 700 - 720 1 sec |
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Takeoff N1%
|
104
|
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Maximum Continuous N1%
|
104
|
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Takeoff Oil Pressure (PSI)
|
60 - 83
|
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Maximum Continuous Oil Pressure(PSI)
|
60 - 83
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IDLE Oil Pressure (PSI)
|
40 (min)
|
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Transient Maximum Observed ITT
|
720 - 2 sec Max
|
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Transient Oil Pressure (PSI)
|
95 for 90 sec
|
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Takeoff Oil Temperature
|
10 - 121
|
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Maximum Continuous Oil Temperature
|
10 - 121
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IDLE Oil Temperature
|
-40 - 121
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Starting Oil Temperature
|
-40
|
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Transient Oil Temperature
|
135 for 15 min
|
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Normal Flight Oil Pressure
|
60 - 83 at N2 speeds above 60.
|
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Oil Pressure below __ is unsafe
|
40
|
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Oil Pressure below ___ psi is undesirable
|
60
|
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Under cold starting conditions, oil pressure between __ and __ psi limit for __ sec
|
83 and 95 psi for 90 sec
|
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ITT during ground start should not normally exceed ___
|
550 C
|
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Ground Max for each generator
|
280 amps
|
|
Flight - both generators operating up to 41,000
|
280
|
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Flight - one generator operating up to 32500
|
400
|
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Flight One generator operating 32500 - 41000
|
280
|
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Min battery volts for battery start
|
22 DC
|
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Max Generator load prior to starting second engine
|
150 amps
|
|
Extend flaps to 10 degrees
|
200 knots
|
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Extend flaps >10 degrees
|
170 knots
|
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Flaps extended >10 degrees
|
165 knots
|
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Aircraft is limited to (speed)
|
330 KIAS / .78MACH
|
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Landing gear/lights
|
200KIAS / FL200
|
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Max Tailwind
|
10 knots
|
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Max Crosswind (Dry)
|
25 knots
|
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Max Crosswind (Wet)
|
15 knots
|
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Max Crosswind (Ice)
|
10 knots
|
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Max Operating Altitude
|
FL410
|
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Yaw damper required operable for flight above
|
FL280
|
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Do not use autopilot below
|
200 ft AGL
|
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To ensure proper wing anti-ice operations, the throttles must be kept at ___% N2 minimum
|
70
|
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Do not operate surface anti-ice systems inflight at ram air temperature above __
|
10C
|
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Reduce throttles below ____ N1 prior to turning on engine or wing anti-ice
|
90
|
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Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperature above ____C OAT/SAT
|
10
|
|
Max Takeoff Weight
|
16,100 lbs
|
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Max Landing Weight
|
15,700lbs
|
|
Fuel crossfeed with 2 engines operating is limited to level flight when less than ____ lbs of fuel remains in the wing tank supplying fuel
|
600
|
|
Max Fuel Imbalance - Landing
|
300 lbs
|
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Max Fuel Imbalance - Flight
|
300 lbs
|
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Max Fuel Imbalance - T.O. / Touch & Go
|
100 lbs
|
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Emergency Fuel / Minimum Fuel
|
300 lbs / 500 lbs
|
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Min/Max Fuel Temperature
|
-40 / 50 C
|
|
Motoring Starter Limit 1st Crank
|
30 sec then 5 min cooling
|
|
Motoring Starter Limit 2nd Crank
|
30 Sec then 15 min cooling
|
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Motoring Starter Limit 3rd Crank
|
30 Sec then 60 min cooling
|
|
Wipers (Speed)
|
200 KIAS
|
|
Tire (speed)
|
165 Knots GS
|