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60 Cards in this Set
- Front
- Back
Takeoff, Time Limit
|
5min
|
|
Takeoff, Miximum Observed ITT
|
700
|
|
Takeoff, N2%
|
96
|
|
Takeoff, N1%
|
104
|
|
Takeoff, Oil Pressure PSI
|
60 to 83
|
|
Takeoff, Oil Temperature
|
10 to 121
|
|
Maximum Continuous, Time Limit
|
Continuous
|
|
Maximum Continuous, Miximum observed ITT
|
680
|
|
Maximum Continuous, N2
|
96
|
|
Maximum Continuous, N1
|
104
|
|
Maximum Continuous, Oil Pressure psi
|
60 to 83
|
|
Maximum Continuous, Oil Temperature
|
10 to 121
|
|
Idle, Time limit
|
Continuous
|
|
Idle, Maximum Observed ITT
|
580
|
|
Idle, N2
|
52 (min)
|
|
Idle, Oil Pressure psi
|
40 (min)
|
|
Idle, Oil Temperature
|
-40 to 121
|
|
Transient, Maximum Observed ITT
|
720 2sec Max
|
|
Transient, N2
|
96
|
|
Transient, N1
|
106
|
|
Transient, Oil Pressure psi
|
95 for
90 sec |
|
Transient, Oil Temperature
|
135 (max)
15min max |
|
Starting, Maximum Observed ITT
|
550 - 600 4 sec
600 - 700 2 sec 700 - 720 1 sec |
|
NOTES:
(1) Time limit starts when throttle first advanced |
for take off thrust.
|
|
NOTES:
(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 (undesirable) 40 (unsafe) |
|
NOTES:
(3) Under cold starting conditions, oil pressure between ___ psi and ___ psi is limited to ___ seconds. |
83
95 90 |
|
NOTES:
(4) The ITT during ground starts should normally not exceed ___ C |
550
|
|
Starter/Generator Limitations
Ground - Max for each generator ___ amps |
280
|
|
Starter/Generator Limitations
Flight - Both generators operating Up to 41,000ft ___ amps |
280
|
|
Starter/Generator Limitations
Flight - One generator operating Up to 32,500 ft ___ amps |
400
|
|
Starter/Generator Limitations
Flight - One generator operating 32,500ft - 41,000ft ___ amps |
280
|
|
Starter/Generator Limitations
Min battery voltage for battery start ___ volts DC |
22
|
|
Starter/Generator Limitations
Max generator load prior to starting second engine ___ amps |
150
|
|
Starter/Generator Limitations
Motoring of the starter is limited to 1st crank ___ sec then ___ min cooling 2nd crank ___ sec then ___ min cooling 3rd crank ___ sec then ___ min cooling |
1st crank 30 sec then 5 min cooling
2nd crank 30 sec then 15 min cooling 3rd crank 30 sec then 60 min cooling |
|
Airspeed & Mach Limitations
Extend flaps to 10 degrees ___ KIAS |
200
|
|
Airspeed & Mach Limitations
Extend flaps >10 degrees ___ KIAS |
170
|
|
Airspeed & Mach Limitations
Flaps extended > 10 degrees ___ KIAS |
165
|
|
Airspeed & Mach Limitations
Aircraft is limited to ___ KIAS or ___ MACH whichever is less |
330
.78 |
|
Airspeed & Mach Limitations
Landing gear/lights ___ KIAS/FL ___ |
200
200 |
|
Airspeed & Mach Limitations
Wipers ___ KIAS |
200
|
|
Airspeed & Mach Limitations
Tire ___ Knots GS |
165
|
|
Enroute Limitations
Max Operating Altitude |
FL410
|
|
Enroute Limitations
Yaw damper required operable for flight above |
FL280
|
|
Enroute Limitations
Do not use autopilot below ___ft AGL |
200
|
|
Fuel Limitations
Min/Max Fuel Temperature |
-40C/50C
|
|
Fuel Limitations
Emergency Fuel/Minimum Fuel |
300lbs/500lbs
|
|
Fuel Limitations
Max Fuel Imbalance - T.O/Touch & Go |
100lbs
|
|
Fuel Limitations
Max Fuel Imbalance - Flight |
300lbs
|
|
Fuel Limitations
Max Fuel Imbalance - Landing |
300lbs
|
|
Fuel Limitations
Fuel crossfeed with 2 engines operating is limited to level flight when less than ___lbs of fuel remains in the wing tank supplying fuel. |
600
|
|
Takeoff & Landing Limitations
Max Tailwind |
10 Knots
|
|
Takeoff & Landing Limitations
Max Crosswind (Dry) |
25 Knots
|
|
Takeoff & Landing Limitations
Max Crosswind (Wet) |
15 Knots
|
|
Takeoff & Landing Limitations
Max Crosswind (Icy) |
10 Knots
|
|
Weight Limitations
Max Takeoff Weight |
16,100lbs
|
|
Weight Limitations
Max Landing Weight |
15,700
|
|
Anti-Ice Limitations
Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above ___C OAT/SAT |
10
|
|
Anti-Ice Limitations
Reduce throttles below ___ N1 prior to turning on engine or wing anti-ice. |
90
|
|
Anti-Ice Limitations
Do not operate surface anti-ice systems inflight at ram air temperatures above ___C |
10
|
|
Anti-Ice Limitations
To ensure proper wing anti-ice operation, the throttles must be kept at ___% N2 minimum |
70
|