Boldface Ops Limits Flashcards
Engine Fire During Ground OperationS
THROTTLES - CUTOFF
Engine Fire During Flight
If engine fire switchlight remains illuminated, L or R FIRE DET FAIL illuminates, fire warning test fails, or fire conditions persist:
THROTTLE IDLE
THROTTLE - CUTOFF
ENGINE FIRE SWITCH - PUSH
BOTTLE ARMED SWITCH - PUSH
Smoke Or Fumes In Aircraft
OXYGEN MASKS - DON / 100%
Pitch Trim/Roll Trim/Rudder Trim Runaway
TRIM INT & A/P DISENGAGE SWITCH - PUSH AND HOLD
Low Cabin Pressure
OXYGEN MASKS - DON / 100%
Engine:
Thrust Setting: Takeoff
Time Limit (Minutes):
5 (1)
Engine:
Thrust Setting: Maximum Continuous
Time Limit (Minutes):
Continuous
Engine:
Thrust Setting: Idle
Time Limit (Minutes):
Continuous
Engine:
Thrust Setting: Takeoff
Maximum Observed ITT degrees C:
700
Engine:
Thrust Setting: Maximum Continuous
Maximum Observed ITT degrees C:
680
Engine:
Thrust Setting: Idle
Maximum Observed ITT degrees C:
580
Engine:
Thrust Setting: Starting (4)
Maximum Observed ITT degrees C:
550 - 600 4 SEC
600 - 700 2 SEC
700 - 720 1 SEC
Engine:
Thrust Setting: Transient
Maximum Observed ITT degrees C:
(720 2 SEC Max)
Engine:
Thrust Setting: Takeoff
N2%:
96
Engine:
Thrust Setting: Miximum Continuous
N2%:
96
Engine:
Thrust Setting: Idle
N2%:
52 (Min)
Engine:
Thrust Setting: Transient
N2%:
96
Engine:
Thrust Setting: Takeoff
N1%:
104
Engine:
Thrust Setting: Maximum Continuous
N1%:
104
Engine:
Thrust Setting: Transient
N1%:
106
Engine:
Thrust Setting: Takeoff
Oil Pressure (2) PSI:
60 to 83
Engine:
Thrust Setting: Maximum Continuous
Oil Pressure (2) PSI:
60 to 83
Engine:
Thrust Setting: Idle
Oil Pressure (2) PSI:
40 (Min)
Engine:
Thrust Setting: Transient
Oil Pressure (2) PSI:
95 for 90 SEC
Engine:
Thrust Setting: Takeoff
OilTemperature (degrees C):
10 to 121
Engine:
Thrust Setting: Maximum Continuous
OilTemperature (degrees C):
10 to 121
Engine:
Thrust Setting: Idle
OilTemperature (degrees C):
-40 to 121
Engine:
Thrust Setting: Starting
OilTemperature (degrees C):
-40 (Min)
Engine:
Thrust Setting: Transient
OilTemperature (degrees C):
135 (Max) (15 MIN Max)
(2) Normal Flight: Normal oil pressure is ___ to ___ PSI at N2 speeds above ___%. Oil pressure below ___ PSIis 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
(3) Under cold starting conditions, oil pressure between ___ PSI and ___ PSI is limited to ___ seconds.
83
95
90
(4) The ITT during ground starts should normally not exceed ___ degrees C.
550
Normal hydraulic pressure ___ to ___ PSI
1350 to 1550
Normal nitrogen pressure ___ to ___ PSI
1350 to 1650
Normal oxygen pressure ___ to ___ PSI
1600 to 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 Wieght ___ lbs
15,700
Extend flaps to 10 degrees ___ KIAS
200
Extend flaps >10 degrees ___ KIAS
170
Flaps extended > 10 degrees ___ KIAS
165
Aircraft if 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 ___ degrees C OAT/SAT
10
Do not operate surface anti-ice systems in flight at ram air temperatures above ___ degrees C.
10
To ensure proper wing anti-ice operations, the throttles must be kept at ___% N2 minimum.
70
