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56 Cards in this Set
- Front
- Back
Takeoff max observed ITT (C) and time limit
|
700, 5 min
|
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Max continuous ITT
|
680
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Max continuous N2
|
96
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Max continuous N1
|
104
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Max takeoff N1
|
104
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Max takeoff N2
|
96
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Oil pressure for takeoff
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60 to 83
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Oil temperature for takeoff
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10 to 121
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Continuous oil pressure
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60 to 83
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Continuous oil temperature
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10 to 121
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Idle maximum ITT
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580
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Idle minimum N2
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52
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Idle minimum oil pressure
|
40
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Idle minimum oil temperature
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-40 to 121
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Starting maximum ITT
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550 - 600 4 SEC
600 - 700 2 SEC 700 - 720 1 SEC |
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Transient maximum ITT
|
720 2 SEC Max
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Transient maximum N2
|
96
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Transient maximum N1
|
106
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Transient maximum oil pressure
|
95 for 90 SEC
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Transient oil temperature
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135 (Max) (15 MIN Max)
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Normal Flight: Normal oil pressure is ____ to ____ PSI at N2 speeds above ____ %.
|
60, 83, 60
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Oil pressure below ____ PSI is undesirable and should be tolerated only for the safe recovery of the flight, preferably at reduced power setting.
|
60
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Oil pressure below ____ PSI is unsafe.
|
40
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Under cold starting conditions, oil pressure between ____ PSI and ____ PSI is limited to ____ seconds.
|
83, 95, 90
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The ITT during ground starts should normally not exceed ____ °C.
|
550
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Normal hydraulic pressure ____ to ____ PSI
|
1350, 1550
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Normal nitrogen pressure ____to ____ PSI
|
1350, 1650
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Normal oxygen pressure ____ to ____ PSI
|
1600, 1850
|
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Min battery voltage for battery start ____ volts
|
22
|
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Max gen load prior to starting second engine ____ amps
|
150
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Motoring of the starter is limited to:
First, ____ seconds then ____ minutes cooling. Second, ____ seconds then ____ minutes cooling. Third, ____ seconds then ____ minutes cooling. |
30, 5
30, 15 30, 60 |
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Emergency Fuel / Minimum Fuel ____ lbs / ____ lbs
|
300, 500
|
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Maximum Fuel Imbalance – T.O./Touch & Go ____ lbs
|
100
|
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Max Fuel Imbalance – Flight ____ lbs
|
300
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Max Fuel Imbalance – Landing ____ lbs
|
300
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Fuel crossfeed with 2 engines operating is limited to level flight with less than ____ lbs of fuel remains in the wing tank supplying fuel.
|
600
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Max Ramp Weight ____ lbs
|
16,300
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Max Takeoff Weight ____ lbs
|
16,100
|
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Max Landing Weight ____ lbs
|
15,700
|
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Extend flaps to 10 degrees ____ KIAS
|
200
|
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Extend flaps > 10 degrees ____ KIAS
|
170
|
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Flaps extended > 10 degrees ____ KIAS
|
165
|
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Aircraft is limited to ____ KIAS or ____ MACH, whichever is less.
|
330, .78
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Landing Gear/Lights ____ KIAS / FL ____
|
200, 200
|
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Wipers ____ KIAS
|
200
|
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Tire ____ Knots GS
|
165
|
|
Max Tailwind ____Knots
|
10
|
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Max Crosswind (Dry) ____ Knots
|
25
|
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Max Crosswind (Wet) ____ Knots
|
15
|
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Max Crosswind (Icy) ____ Knots
|
10
|
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Max Operating Altitude FL ____
|
410
|
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Yaw Damper required operable for flight above FL ____
|
280
|
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Do not use autopilot below ____ FT AGL
|
200
|
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Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above ____ °C OAT/SAT.
|
10
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Do not operate surface anti-ice systems in flight at ram air temperatures above ____ °C.
|
10
|
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To ensure proper wing anti-ice operation, the throttles must be kept at ____ % N2 minimum.
|
70
|