BOLDFACE and Ops Limits Flashcards
Emergency Engine Shutdown on the Ground
PCL - OFF
FIREWALL SHUTOFF HANDLE - PULL
Abort
PCL - IDLE
BRAKES - AS REQUIRED
Engine Failure Immediately After Takeoff
(Sufficient Runway Remaining Straight Ahead)
AIRSPEED - 110 KNOTS (MINIMUM)
PCL - OFF
EMER LDG GR HANDLE - PULL (AS REQUIRED)
Engine Failure During Flight
ZOOM/GLIDE - 125 KNOTS (MINIMUM)
PCL - OFF
INTERCEPT ELP
Immediate Airstart (PMU NORM)
PCL - OFF
STARTER SWITCH - AUTO/RESET
PCL - IDLE, ABOVE 13% N1
Uncommanded Power Changes
Loss of Power
Uncommanded Propeller Feather
PCL - MID RANGE
PMU SWITCH - OFF
PROP SYS CIRCUIT BREAKER - PULL, IF NP STABLE BELOW 40%
Inadvertent Departure From Controlled Flight
PCL - IDLE
CONTROLS - NEUTRAL
ALTITUDE - CHECK
Fire In Flight
PCL - OFF
FIREWALL SHUTOFF HANDLE - PULL
OBOGS Failure/ Overtemp/ Physio Symptoms
GREEN RING - PULL (AS REQUIRED)
DESCENT BELOW 10,000 FEET MSL - INITIATE
OBOGS SUPPLY LEVER - OFF
Eject
EJECTION HANDLE - PULL
Maximum Torque
Takeoff/Max ______%
100
Maximum Torque
Transient _________% (_____ Seconds)
132, 20
Maximum Torque
Torque above ___% is indicative of sys malfunction
102
Maximum ITT
Idle ____ *C
750
Maximum ITT
Takeoff/Max ___*C
820
Maximum ITT
Transient ___ to ___ *C (___ Seconds)
821, 870, 20
N1
Idle ___ to ___% Ground, ___% (Min) Flight
60, 61, 67
NP
Idle ___ to ___%
46, 50
NP
Takeoff/Max ___%,(___% +/- ___% PMU off)
100, 100, 2
NP
Avoid stabilized ground operations from ___ to ___ % Np
62, 80
Oil Pressure
Takeoff/ Max ___ to ___ PSI
90, 120
Oil Pressure
Aerobatics/Spins ___ to ___ PSI
40, 130
Oil Pressure
Aerobatics/Spins (Idle) ___ to ___ PSI (___ Sec)
15, 40, 5
Oil Temp
Takeoff/Max ___ to ___ *C
10, 105
Oil Temp
Transient ___ to ___ *C (___ Min)
106, 110, 10
All phases of flight ___ PPH
799
- _________ Stalls
Inverted
- _________ Spins
Inverted
- Aggravated ___________________
spins past 2 turns
- Spins with the PCL ____________
above idle
- Spins with the _______,_______, or ______ extended
landing gear, flaps, speed brake
- Spins with the _________
PMU off
- Spins below _______ feet pressure altitude
10,000
- Spins above ________ feet pressure altitude
22,000
- Abrupt _________ maneuvers
cross-controlled (snap)
- Aerobatic maneuvers, spins, or stalls with greater than _____ pounds fuel imbalance
50
- _______ Slides
Tail
Max airspeed Gear and/or Flaps _______KIAS
150
Max operating Speed _______KIAS or ________ mach
316, 0.67
Full rudder deflection above _____ KIAS will exceed the limits of the rudder control system.
150
Starter limit: ______ Seconds
20
Wait ___ Sec, ___ Min, ___Min, ___ Min after each start/motoring attempt
30, 2, 5, 30
Maximum ITT___ to ___ *C for ___ Sec (Do not Attempt Restart)
871, 1,000, 5
Maximum Oil Pressure ___ PSI
200
Minimum Oil Temperature ___ *C
-40
Minimum Batter Voltage ___V
23.5
Normal Above 18,000 Ft MSL ___ +/- ___ PSI
3.6, 0.2
Overpressurization Safety Valve Opens ___ PSI
4.0
Normal Recovery Fuel ___ Pounds
200
Minimum Fuel ___ Pounds (___ Pounds Solo)
150, 200
Emergency Fuel ____ Pounds
100
Minimum Fuel for Aerobatics ___ Pounds per side
150
Minimum landing distance available (LDA) ___ feet, or heavy weight flaps ___ landing distance plus ___ feet, whichever is greater
4,000, up, 500
Minimum Runway width ____ Feet
75
Maximum Crosswinds
Dry Runway ___ Knots
25
Maximum Crosswinds
Wet Runway ___ Knots
10
Maximum Crosswinds
Icy Runway ___ Knots
5
Maximum Crosswinds
Touch and Go ___ Knots
20
Maximum Crosswinds
Formation Takeoff/ Landing ___ Knots
15
Maximum Crosswinds
Maximum tailwind component for takeoff ___ knots
10
Maximum wind with canopy open ___ Knots
40
Symmetric clean ___ to ___ Gs
-3.5, 7.0
Symmetric Gear/ Flaps ___ to ___ Gs
0, 2.5
Asymmetric Clean ___ to ___ Gs
-1.0, 4.7
Asymmetric Gear/Flaps ___ to ___ Gs
0, 2.0
Minimum altitude for entry ____ Feet MSL
13,500
Minimum cloud clearance ____ feet above clouds
7,000
Maximum Icing Band ____ Feet
5,000
Maximum Icing type ____
Light Rime
Ground Operation is limited to ambient temperatures of ___ to ___ *C
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