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56 Cards in this Set

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