My lesson

 0    26 schede    cyberbloney
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emergency engine shut down on the ground
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PCL - OFF; FIREWALL SHUTOFF HANDLE - PULL
abort
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PCL - IDLE; BRAKES - AS REQUIRED
engine failure immediately after takeoff (sufficient runway remaining straight ahead)
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AIRSPEED - 110 KNOTS (MINIMUM); PCL - AS REQUIRED; EMER LDG GR HANDLE - PULL (AS REQUIRED)
engine failure during flight
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ZOOM/GLIDE - 125 KNOTS; PCL - OFF; INTERCEPT ELP
immediate airstart (PMU NORM)
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PCL - OFF; STARTER SWITCH - AUTO/RESET; PCL - IDLE, ABOVE 13% N1
Uncommanded power changes/ loss of power/ uncommanded propeller feather
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PCL - MID RANGE; PMU SWITCH - OFF; PROP SYS CIRCUIT BREAKER (left front console) - PULL, IF NP STABLE BELOW 40%
inadvertent departure from controlled flight
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PCL - IDLE; CONTROLS - NEUTRAL; ALTITUDE - CHECK
Fire in flight if fire is confirmed
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PCL - OFF; FIREWALL SHUTOFF HANDLE - PULL
OBOGS inoperative
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GREEN RING - PULL (AS REQUIRED)
eject
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EJECTION HANDLE - PULL
engine maximum torque takeoff/max
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100%
engine maximum torque transient
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131% (20 seconds)
engine torque indicative of a system malfunction
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102%
engine maximum ITT idle
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750 °c
engine maximum ITT takeoff/max
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820 °c
engine maximum ITT transient
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870 °c (up to 20 seconds)
engine N1 idle ground
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60 to 61%
engine N1 idle flight
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67% min
engine NP idle
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46 to 50%
engine takeoff/max
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100% (100% +- 2% PMU off)
engine NP avoid stabilized ground operations from
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62 to 80% NP
engine oil pressure takeoff/max
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90 to 120 PSI
engine oil pressure aerobatucs/spins
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40 to 130 PSI
engine oil pressure aerobatic/spins (idle)
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15 to 40 PSI (5 sec)
engine oil temp takeoff/max
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10 to 105 °c
engine oil temp transient
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106 to 110 °c (10 minutes)
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