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TAKEOFF: Time Limit (minutes)
5 min
-
MAX CONTINUOUS: Time Limit (minutes)
Continuous
-
IDLE: Time Limit (minutes)
Continuous
-
TAKEOFF: Max Observed ITT oC
700
-
MAX CONTINUOUS: Max Observed ITT oC
680
-
IDLE: Max Observed ITT oC
580
-
STARTING: Max Observed ITT oC
- 550 - 600 (4 sec)
- 600 - 700 (2 sec)
- 700 - 720 (1 sec)
-
TRANSIENT: Max Observed ITT oC
720 (2 sec Max)
-
-
-
-
-
-
-
-
TAKEOFF: Oil Pressure (PSI)
60 to 83
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MAX CONTINUOUS: Oil Pressure (PSI)
60 to 83
-
IDLE: Oil Pressure (PSI)
40
-
TRANSIENT: Oil Pressure (PSI)
95 for 90 sec
-
TAKEOFF: Oil Temperature (oC)
10 to 121
-
MAX CONTINOUS: Oil Temperature (oC)
10 to 121
-
IDLE: Oil Temperature (oC)
-40 to 121
-
STARTING: Oil Temperature (oC)
-40
-
TRANSIENT: Oil Temperature (oC)
135 (Max) (15 min Max)
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Note (1): Time limit starts when throttles first advanced for takeoff thrust
-
Note (2): Normal flight: Normal oil pressure is __ to __psi at N2 speeds above __%. Oil pressure below __psi is undesirable and should be tolerated only for the safe recovery of the flight, preferably at reduced power setting. Oil pressure below __psi is unsafe.
60; 83; 60; 60; 40
-
Note (3): Under cold starting conditions, oil pressure between __psi and __psi is limited to __ seconds.
83; 95; 90
-
Note (4): The ITT during ground starts should normally not exceed ___oC.
550
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GROUND - Max for each generator
280 amps
-
FLIGHT - Both generators operating
Up to 41,000 ft -- 280 amps
-
FLIGHT - One generator operating
Up to 32,500 ft -- 400 amps
-
FLIGHT - One generator operating
32,500 ft - 41,000 ft -- 280 amps
-
Min battery voltage for battery start
22 volts DC
-
Max generator load prior to starting second engine
150 amps
-
Motoring of the starter is limited to:
- 1st crank: 30 sec then 5 min cooling
- 2nd crank: 30 sec then 15 min cooling
- 3rd crank: 30 sec then 60 min cooling
-
Extend flaps to 10 degrees
200 KIAS
-
Extend flaps >10 degrees
170 KIAS
-
Flaps extended >10 degrees
165 KIAS
-
Aircraft is limited to
330 KIAS or .78 MACH, whichever is less
-
Landing gear/lights
200 KIAS / FL200
-
Wipers (airspeed limits)
200 KIAS
-
Tire (airspeed limits)
165 knots GS
-
Min / Max Fuel Temperature
-40 oC / 50 oC
-
Emergency Fuel / Minimum Fuel
300 lbs / 500 lbs
-
Max Fuel Imbalance - T.O. / Touch & Go
100 lbs
-
Max Fuel Imbalance - FLIGHT
300 lbs
-
Max Fuel Imbalance - LANDING
300 lbs
-
Fuel crossfeed with 2 engines operating is limited to level flight when less than ___lbs of fuel remaining in the wing tank supplying fuel
600
-
-
Max Crosswind (Dry)
25 knots
-
Max Crosswind (Wet)
15 knots
-
Max Crosswind (Icy)
10 knots
-
Max Takeoff Weight
16,100 lbs
-
Max Landing Weight
15,700 lbs
-
Max Operating Altitude
FL410
-
Yaw damper required operable for flight above
FL280
-
Do not use autopilot below
200 ft AGL
-
Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above
10 oC OAT/SAT
-
Reduce throttles below ___ N1, prior to turning on engine or wing anti-ice.
90
-
Do not operate surface anti-ice systems inflight at ram air temperatures above ___oC
10
-
To ensure proper wing anti-ice operation, the throttles must be kept at __% N2 minimum
70
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