Ops Limits Flashcards
Thrust Setting: Takeoff: Time Limit
5 (1) Time limit starts when throttles first advanced for takeoff thrust
Thrust Setting: Takeoff: Maximum Observed ITT
700
Thrust Setting: Takeoff: N2 %
96
Thrust Setting: Takeoff: N1 %
104
Thrust Setting: Takeoff: Oil Pressure (PSI)
60 to 83
Thrust Setting: Takeoff: Oil Temperature (C)
10 to 121
Thrust Setting: Max Continuous: Time Limit
Continuous
Thrust Setting: Max Continuous: Max Observed ITT (C)
680
Thrust Setting: Max Continuous: N2 %
96
Thrust Setting: Max Continuous: N1 %
104
Thrust Setting: Max Continuous: Oil Pressure (PSI)
60 to 83
Thrust Setting: Max Continuous: Oil Temp (C)
10 to 121
Thrust Setting: Idle: Time Limit
Continuous
Thrust Setting: Idle: Max Observed ITT (C)
580
Thrust Setting: Idle: N2 %
52 (Min)
Thrust Setting: Idle: Oil Pressure (PSI)
40 (Min)
Thrust Setting: Idle: Oil Temperature (C)
-40 to 121
Thrust Setting: Starting: Max Observed ITT (C)
550 - 600 4 SEC
600 - 700 2 SEC
700 - 720 1 SEC
Thrust Setting: Starting: Oil Temperature (C)
-40 (Min)
Thrust Setting: Transient: Max Observed ITT (C)
(720 2 SEC Max)
Thrust Setting: Transient: N2 %
96
Thrust Setting: Transient: N1 %
106
Thrust Setting: Transient: Oil Pressure (PSI)
95 for 90 SEC
Thrust Setting: Transient: Oil Temperature (C)
135 (Max)
15 MIN Max
Normal flight: Normal oil pressure is…
60 to 83 PSI at N2 speeds above 60%.
Oil pressure below ___ PSI is undesirable and …
60 PSI; … should be tolerated only for the safe recovery of the flight.
Oil pressure between ___ PSI and ___ PSI is limited to ___ 90 seconds.
83; 95; 90
The ITT during ground starts should normally not exceed ___ C
550
Normal hydraulic pressure
1350 to 1550 PSI
Normal nitrogen pressure
1350 to 1650 PSI
Normal oxygen pressure
1600 to 1850 PSI
Min battery voltage for battery start
22 volts
Max gen load prior to starting second engine
150 amps
Motoring of the starter is limited to:
First, 30 seconds then 5 minutes cooling.
Second, 30 seconds then 15 minutes cooling.
Third, 30 seconds then 60 minutes of cooling.
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 with less than ___ lbs of fuel remains in the wing tank supplying fuel.
600
Max Ramp Weight
16,300 lbs
Max Takeoff Weight
16,100 lbs
Max Landing Weight
15,700 lbs
Extend flaps to 10 degrees
200 KIAS
Extend flaps > 10 degrees
170 KIAS
Flaps extended > 10 degrees
165 KIAS
Aircraft is limited to ___ KIAS or ___ MACH, whichever is less
330; .78
Landing Gear/Lights ___ KIAS / FL ___
200; 200
Wipers
200 KIAS
Tire
165 Knots GS
Max Tailwind
10 Knots
Max Crosswind (Dry)
25 Knots
Max Crosswind (Wet)
15 Knots
Max Crosswind (Icy)
10 Knots
Max Operating Altitude
FL410
Yaw Damper required operable for flight above
FL280
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
