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63 Cards in this Set
- Front
- Back
Shaft Horsepower
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850
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Oil
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14.5 Quarts total capacity (9.2 Drain and refill Capacity)
Site gauge for reference only. When below green check stick. |
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Max weights
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Landing 9,000
Ramp 9,100 (actually 9097) Takeoff 9,062 |
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Max continuous power
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2232 ft/lbs @ 2,000 RPM 770 C or 101.6%np
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Takeoff power
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800 C for 5 minutes
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Total useable fuel
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332 Gal (166/side)
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Vne
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175
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Va
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112/143 min/max (basic speeds for Va during skydive ops)
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Vfe 0-10 degrees
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175
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Vfe 10-20 degrees
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150
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Vfe 20-full
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125
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Torque limitations
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2232 ft/lbs for most operations
2750 max transient (No more than 5 seconds) 1100 when < 1600 RPM For "max" operations (max t/o, max climb, max cruise,) +/- 40 torque indication is allowed |
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Np limitations
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2,000 most operations
1,050 idle 2,205 transient |
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Ng limitations
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101.6 most operations
103.9 transient for 10 seconds |
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Max idle T5
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750
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Max reverse T5 Ng Np
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750 88 1900
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Max start T5
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1000 (850-100 for no more than 5 seconds)
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Max takeoff T5
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800
770-800 no more than 5 minutes |
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Oil temp limitations
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0-99 for most operations
55C min for takeoff |
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Oil pressure limits
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Normal in flight = 100-135 @ 60-70C
Idle = min of 60 85 is min when at high power @ 60-70C 60-85 in flight = emergency and 1100 torque limited < 60 = emergency, either use minimum power or shutdown and feather |
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Recommended oil temp before takeoff
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55
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Max OAT for ground ops
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53C (Fuuck that ****!)
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Airspeed engine failure flaps up
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100
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Max fuel imbalance
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200 lbs
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Airspeed engine failure flaps full
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80
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Engine failure during takeoff
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1. POWERLever.......................... BETARANGE
2. Brakes...................................... APPLY IF GOING TO OVERRUN Condition lever OFF Fuel Shutoff PULL Fuel selectors OFF Battery OFF |
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Engine failure immediately after takeoff
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Airspeed 85
Prop FEATHER Condition lever OFF Fuel shutoff OFF Fuel selectors OFF Battery OFF |
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Engine failure
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Airspeed 100 knots
Power IDLE Prop FEATHER Condition lever OFF Boost pump OFF Fuel shutoff OFF Ignition NORMAL Standby elec power OFF Electrical load SHED |
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Engine flameout
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> 50% Ng Power IDLE Ignition ON
<50% Ng Condition lever CUTOFF (try air restart) |
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Forced landing NO POWER
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1. Seats, Seat Belts, Shoulder Harnesses . . . . . . . SECURE
2. Airspeed........100KIAS(flapsUP) 80 KIAS (flaps FULL) 3. POWERLever .................................. IDLE 4. PROPRPMLever........................... FEATHER 5. FUELCONDITIONLever.......................CUTOFF 6. FUELBOOSTSwitch............................. OFF 7. IGNITIONSwitch .............................. NORM 8. STBYALTPWRSwitch ........................... OFF 9. NonessentialEquipment........................... OFF 10. FUELSHUTOFFKnob...................... PULLOFF 11. FUEL TANK SELECTORS . . . . . OFF (warning horn will sound) 12.WINGFLAPSHandle.. A/R (FULLrecommended) 13. CrewDoors...........UNLATCHPRIORTOTOUCHDOWN 14. GENERATOR Switch . . . . . . . . . . . . TRIP 15. BATTERYSwitch ........... OFF(whenlandingisassured) 16. Touchdown....................... SLIGHTLYTAILLOW 17. Brakes............................... APPLYHEAVILY |
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Engine fire in flight
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1. POWERLever.................................. IDLE
2. PROPRPMLever........................... FEATHER 3. FUELCONDITIONLever ...................... CUTOFF 4. FUELSHUTOFFKnob...................... PULLOFF 5. CABIN HEAT...... OFF 6. ForwardSideVents ........................... CLOSE 7. OverheadVents................................ OPEN 8. VENTAIRFANS.................................. ON 9. WINGFLAPSHandle........................20°-FULL 10.Airspeed ................................ 80-85KIAS 11.ForcedLanding............................. EXECUTE |
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Electrical fire in flight
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1. STBYALTPWRSwitch........................... OFF
2. GENERATORSwitch............................ TRIP 3. BATTERYSwitch................................ OFF 4. Vents ........................ CLOSED(toavoiddrafts) a. ForwardSideVents ....................... CLOSE b. OverheadVents........................... CLOSE c. VENTAIRFANS............................. OFF 5. BLEEDAIRHEATSwitch ......................... OFF 6. FireExtinguisher ................................ USE |
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Cabin fire
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1. STBYALTPWRSwitch...........................OFF
2. GENERATORSwitch............................ TRIP 3. BATTERYSwitch................................OFF 4. Vents......................... CLOSED(toavoiddrafts) a. ForwardSideVents ........................ CLOSE b. OverheadVents........................... CLOSE c. VENTAIRFANS .............................OFF 5. BLEEDAIRHEATSwitch..........................OFF 6. FireExtinguisher................. ACTIVATE(ifavailable) |
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Wing fire
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1. PITOT/STATICHEATSwitch....................... OFF
2. STALLHEATSwitch ............................. OFF 3. STROBESwitch................................. OFF 4. NAVSwitch .................................... OFF 5. LDGandTAXI/RECOGSwitches................... OFF 6. FUELQUANTITYCircuitBreakers .................. OFF (second row, third breaker from front and third row third breaker from front) 7. RADARR/TCircuitBreaker(ifinstalled)............. PULL (AVN BUS 1, second row, sixth breaker from left side) 8. VENTAIRFANS ................................ OFF 9. AIRCONDITIONING(ifinstalled) ................... OFF |
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Engine fire during start
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Condition lever OFF
Boost pump OFF MOTOR>>>>>>> IF FIRE CONTINUES Starter OFF Fuel shutoff PULL Battery OFF EVACUATE AND EXTINGUISH |
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Pitch trim failure
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1. ControlWheel........................... GRIPFIRMLY
2. AP/TRIMDISCButton.......................... PRESS (high elevator control forces possible) 3. ELEVATOR TRIM . . . . . . . . RETRIM (using manual trim wheel) NOTE Actuate each half of the pilot and copilot Manual Electric Pitch Trim Switches separately to make sure trim does not actuate with only one half switch. IF Red PTRIM CAS MESSAGE CLEARS Procedure complete IF Red PTRM MESSAGE REMAINS 4. Autopilot ........................ DONOTRE-ENGAGE |
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Fuel flow interruption to reservoir
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1. FUELTANKSELECTORS.................... BOTHON
2. IGNITIONSwitch............................. ON 3. FUELBOOSTSwitch............................. ON 4. If Red RSVR FUEL LOW CAS MSG remains and there is usable fuel in the wing tanks: a. Carefully monitor engine indications and Amber FUEL PRESS LOW CAS MSG for signs of fuel starvation. b. Land as soon as possible and determine cause of Red RSVR FUEL LOW warning. |
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Trim tabs
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Aileron- 1 tab on right side (servo)
Elevator- 2 tabs |
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Spoilers
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Disrupt airflow over corresponding flap for increased maneuverability at slow speeds. Spoilers are extended after 5 degrees of aileron travel has been reached.
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OIL PRESS LOW (RED)
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Indicates engine oil pressure is less than 40 psi.
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VOLTAGE LOW (RED)
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Indicates electrical system bus voltage is less than 24.5 volts and power is being supplied from the battery.
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VOLTAGE HIGH (RED)
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Indicates electrical system bus voltage is greater than 32.0 volts.
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RSVR FUEL LOW (RED)
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reservoir is less than 1/2 full and 3-9 minutes of fuel is left
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FUEL SELECT OFF (RED)
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Indicates left and right fuel selectors are both OFF at any time, or left fuel selector is OFF when right tank is low, or right fuel selector is OFF when the left tank is low; or that either left or right selectors are OFF when starter switch is ON. It can also indicate that the FUEL SEL WARN circuit breaker has been pulled.
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FUEL PRESS LOW (AMBER)
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<4.75 psi
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ITT sensing
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Done by 8 Chromel/alumel probes located near the power turbine stator vanes.
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Chip detectors
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1 under reduction gear case
1 under accessory gear case |
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Battery start procedure (abridged)
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Bat - On
Bus volts - 24 min E power lev - norm Boost pump on- looking for Aux pump light on and low pressure light off. Starter switch on- observe start light on, Ng 14% min, oil pressure up Condition lever - Low idle (min FF 50pph) 1000C max temp (850-1000 for 5 seconds) Ng 50% min Start switch off - Check light off Fuel boost switch normal Avionics etc. - On |
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Aux start procedure (abridged)
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External power switch - BUS
Voltmeter - 24-28.5 Bat switch - On External power switch - Starter Boost pump - On and observe necessary lights Starter switch on - lights, 14% min, oil... Con lever - Low Idle observe 50pph min, 1000C max Ng 50% stabilized Start switch - Off / lights off External power switch - Off Boost switch - Norm / lights off Avionics etc. .. |
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Condition lever
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Low idle = 58-61%
High idle = 68-71% |
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Engine instruments
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LED's
None = Normal Constant red = exceeding limit Flashing red fast = Transducer signal failed Flashing red slow = Instrument has failed |
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Torque indicator
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Electrically powered 28VDC
Measures torque difference between different sides of the gearbox and transmits electrically in ft/lbs |
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Oil pressure gauge
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Electrically powered 28VDC
Measured at upper right truss tube and signal sent and converted to psi |
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Torque limiter
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At 2410 ft/lbs Py air is bled off to reduce fuel flow and reduce torque
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Starter/generator time limitations
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Batt: 30 on 30 off, 30 on 30 off, 30 on 30 min.
Ext: 20 on 120 off, 20 on 120 off, 20 on 60 min. |
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Prop overspeed governor
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TEST = 1750 +- 50
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Aux fuel pump
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In 'normal' will turn on when fuel manifold pressure drops below 4.75 psi
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Stby power rating
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75 amps
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Stby power setup
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Gen fail/off
stby power on stby avionics power on avionics bus tie on avionics 1 & 2 off maintain @ or below 75 amps |
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starter/generator output and cutoff start-gen
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28V 200 amp
Cuts out during start after 47% |
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Fuel quantity transmitters
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8
4 in each tank float |
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When does standby power come on?
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When bus voltage drops below 27.5V
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Prop overspeed governor tests @
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1750 +- 50
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