BOLDFACE
Eject
EJECTION HANDLE - PULL
<32> Physiological Symptoms
BOS PUSH MAN - PRESS ON
MAX TORQUE
TAKEOFF/MAX - ___
TRANSIENT - ___ TO ___ (___ SECONDS)
TORQUE ABOVE ____ in indicative of a system malfunction
MAX TORQUE
TAKEOFF/MAX - 100%
TRANSIENT - 101 TO 107% (5 SECONDS)
TORQUE ABOVE 107% in indicative of a system malfunction
Intentional Spin Entry
Minimum Altitude for Entry ____ Feet MSL
minimum Cloud Clearance ____ Feet above clouds
Intentional Spin Entry
Minimum Altitude for Entry 13,500 Feet MSL
minimum Cloud Clearance 7,000 Feet above clouds
Pressurization
Normal Above 18,000 Ft MSL ____ +- ___ PSI
Over pressurization Safety Valve Opens ____ PSI
Pressurization
Normal Above 18,000 Ft MSL 3.6 +- 0.2 PSI
Over pressurization Safety Valve Opens 4.0 PSI
Emergency Engine Shutdown on the Ground
PCL - OFF
FIREWALL SHUTOFF HANDLE - PULL
ABORT
PCL - IDLE
BRAKES - AS REQUIRED
Max ITT
Idle ___
Takeoff/Mac ___
Transient ___ to ___ (___ seconds)
750
820
821 to 870 (20 Seconds)
Airspeed Limitations
Max Airspeed Gear/Flaps ____ KIAS
Max Operating Speed ___ KIAS or ___ Mach
Full rudder deflection above ___ KIAS will exceed the limits of the rudder control system
Airspeed Limitations
Max Airspeed Gear/Flaps 150 KIAS
Max Operating Speed 316 KIAS or .67 Mach
Full rudder deflection above 150 KIAS will exceed the limits of the rudder control system
Fuel
Normal recovery Fuel ___ Pounds
Minimum Fuel ___ Pounds (___ Pounds SOLO)
Emergency Fuel ___ Pounds
Minimum Fuel for Aerobatics ___ Pounds per side
Fuel
Normal recovery Fuel 200 Pounds
Minimum Fuel 150 Pounds (200 Pounds SOLO)
Emergency Fuel 100 Pounds
Minimum Fuel for Aerobatics 150 Pounds per side
Inadvertent Departure From Controlled Flight
PCL - IDLE
CONTROLS - NEUTRAL
ALTITUDE - CHECK
Fire In Flight, If Fire Is confirmed
PCL - OFF
FIREWALL SHUTOFF HANDLE - PULL
N1
Idle ___ to ___ Ground, ___ Flight
Np
Idle ___ to ___
Takeoff/max ___ (___ +- ___ PMU OFF)
Avoid stabilized ground ops from ___ to ___ Np
N1
Idle 60% to 61% Ground, 67% Flight
Np
Idle 46 to 50%
Takeoff/max 100% (100% +- 2% PMU OFF)
Avoid stabilized ground ops from 62 to 80% Np
Starting Limits
Starter Limit : ___ Seconds
Wait ___ Sec, ___ Min, ___ Min, ___ Min after each start/motoring attempt
Max ITT ___ to ___ C for ___ Sec
Max Oil Pressure ___ PSI
Min Oil Temp ____ C
Min Battery Voltage ____ V
Starting Limits
Starter Limit : 20 Seconds
Wait 30 Sec, 2 Min, 5 Min, 30 Min after each start/motoring attempt
Max ITT 871 to 1,000 C for 5 Sec
Max Oil Pressure 200 PSI
Min Oil Temp -40 C
Min Battery Voltage 23.5 V
Runway
Minimum Landing Distance Available (LDA) ____ Feet or heavy weight flaps ___ landing ground roll plus ___ feet, whichever is greater
Minimum Runway Width ____ Feet
Runway
Minimum Landing Distance Available (LDA) 4,000 Feet or heavy weight flaps up landing ground roll plus 500 feet, whichever is greater
Minimum Runway Width 75 Feet
IMMEDIATE AIRSTART (PMU NORM)
PCL - OFF
STARTER SWITCH - AUTO/RESET
PCL - IDLE, ABOVE 13% N1
Engine Failure Immediately After Takeoff (Sufficient Runway remaining Straight Ahead)
PCL - OFF
EMER LDG GR HANDLE - PULL (AS REQUIRED)
Oil Temp
Takeoff/Max ___ to ___ C
Transient ___ to ___ C (___ Min)
Fuel Flow
All Phases of Flight ___ PPH
Oil Temp
Takeoff/Max 10 to 105 C
Transient 106 to 110 C (10 Min)
Fuel Flow
All Phases of Flight 799 PPH
Winds - Maximum Crosswinds
Dry Runway ___ Knots
Wet Runway ___ Knots
Icy Runway ___ Knots
Touch-and-Go ___ Knots
Formation Takeoff/landing ___ Knots
Maximum Tailwind Component for Takeoff ___ Knots
Maximum Wind with Canopy Open ___ Knots
Winds - Maximum Crosswinds
Dry Runway 25 Knots
Wet Runway 10 Knots
Icy Runway 5 Knots
Touch-and-Go 20 Knots
Formation Takeoff/landing 15 Knots
Maximum Tailwind Component for Takeoff 10 Knots
Maximum Wind with Canopy Open 40 Knots
Acceleration Limits
Symmetric Clean ____ to ____ G's
Symmetric Gear/Flaps ____ to ____ G's
Asymmetric Clean ____ to ____ G's
Asymmetric Gear/Flaps ____ to ____ G's
Acceleration Limits
Symmetric Clean -3.5 to 7 G's
Symmetric Gear/Flaps 0 to 2.5 G's
Asymmetric Clean -1.0 to 4.7 G's
Asymmetric Gear/Flaps 0 to 2.0 G's
<30> OBOGS Failure / Overtemp / Physiological Symptoms / <32> OXY CRIT Annunciator
GREEN RING - PULL (AS REQUIRED)
DESCENT BELOW 10,000 FEET - INITIATE
OBOGS SUPPLY LEVER - OFF (BOTH)
Uncommanded Power Changes / Loss of Power / Uncommanded Propellor Feather
PCL - MID RANGE
PMU SWITCH - OFF
PROP SYS CIRCUIT BREAKER (LEFT FRONT CONSOLE) - PULL, IF Np STABLE BELOW 40%
Oil Pressure
Takeoff/Max ___ to ___ PSI
Aerobatics/Spins ___ to ___ PSI
Aerobatics/Spins (Idle) ___ to ___ PSI
Oil Pressure
Takeoff/Max 90 to 120 PSI
Aerobatics/Spins 40 to 130 PSI
Aerobatics/Spins (Idle) 15 to 40 PSI
Prohibited Maneuvers
____ Stalls
____ Spins
Aggravated ____
Spins with the PCL ____
Spins with ____, ____ or ____ extended
Spins below ___ feet pressure alt
Spins above ____ Feet Pressure Alt
Abrupt ____ Maneuvers
Aerobatic maneuvers, spins or stalls with greater than ___ pounds fuel imbalance
____ Slides
Prohibited Maneuvers
Inverted Stalls
Inverted Spins
Aggravated Spins past 2 turns
Spins with the PCL Above Idle
Spins with Landing Gear, Flaps or Speed Brake extended
Spins below 10,000 feet pressure alt
Spins above 22,000 Feet Pressure Alt
Abrupt Cross-Controlled (Snap) Maneuvers
Aerobatic maneuvers, spins or stalls with greater than 50 pounds fuel imbalance
Tail Slides
Icing
Max Icing Band ____ Feet
Max Icing Type ____
Temperature
Ground operations is limited to ambient temperatures of ____ to ____ C
Icing
Max Icing Band 5,000 Feet
Max Icing Type light rime
Temperature
Ground operations is limited to ambient temperatures of -23 to 43 C