Takeoff Time Limit (Minutes)
5
Maximum Continuous Time Limit (Minutes)
Continuous
Idle Time Limit (Minutes)
Continuous
Takeoff Maximum Observed ITT deg C
700
Maximum Continuous Observed ITT deg C
680
To ensure proper wing anti-ice operation, the throttles must be kept at _____ %
N2
minimum.
70
Starting Maximum Observed ITT deg C
-
SEC
-
SEC
-
SEC
550 - 600 4 SEC
600 - 700 2 SEC
700 - 720 1 SEC
Transient Maximum Observed ITT deg C
(
SEC Max
)
(720 2 SEC Max)
Takeoff N2%
96
Maximum Continuous N2%
96
Idle N2% (
Min
)
52
Transient N2%
96
Takeoff N1%
104
Maximum Continuous N1%
104
Transient N1%
106
Takeoff Oil Presssure PSI
60 to 83
Maximum Continuous Oil Pressure PSI
60 to 83
Idle Oil Pressure PSI (
Min
)
40 (Min)
Transient Oil Pressure PSI
for
SEC
95, 90
Takeoff Oil Temperature (deg C)
10 to 121
Maximum Continuous Oil Temperature (deg C)
10 to 121
Idle Oil Temperature (deg C)
-40 to 121
Starting Oil Temperature (deg C) (
Min
)
-40
Transient Oil Temperature (deg C)
(
Max
)
(
MIN Max
)
135 (Max)
15 (MIN Max)
Normal Flight: Normal Oil pressure is _____ to _____PSI at N2 speeds above _____%. Oil pressure below _____PSI is undesireable and should be tolerated only for the safe recovery of the flight, preferably at reduced power setting. Oil pressure below _____
60, 83, 60, 60, 40
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
lbs
ency Fuel / Minimum Fuel _____ *lbs* / _____ *lbs*
300, 500
Transient Maximum Observed ITT deg C
(
SEC Max
)
(720 2 SEC Max)
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 _____
deg C
OAT/SAT
10
To ensure proper wing anti-ice operation, the throttles must be kept at _____ %
N1
minimum.
70