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21 Cards in this Set
- Front
- Back
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AB Start
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Condition lever............................Fuel Off
Ignition switch............................Hold Off (Starter Continue engaged) Starter............................Off (after 20 seconds) Ignition Switch ............................Release Caution: Do not release the ignition switch prior to securing the starter |
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Emergency Engine Shutdown
Emergency Exit |
Emergency Engine Shut Down
Condition Lever............................Fuel Off Emergency Fuel shutoff handle............................pull Note: After the emergency fuel shutoff handle is pulled do not reset on the ground until the cause of the shutdown is determined and corrected. Emergency Exit Canopy............................Open (Emergency open, as required) Battery............................Off Harness. cords, mask............................Release Parachute............................Unfastened Aircraft............................Evacuate Warning: If the aircraft is evacuated on the ground while wearing the parachute with the lanyard connected, the parachute will deploy, possibly inflating and dragging the pilot in windy conditions. Should a postcrash fire occur, this can be extremely hazardous because the pilot may be dragged into the fireball. |
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Fire on the ground
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Starter............................Off (as required)
Emergency Engine Shutdown............................Execute Emergency Exit............................Execute Caution: Do not attempt engine restart until the cause of the fire is determined and corrected. |
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Abnormal ITT During shutdown
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Emergency engine shutdown............................Execute
Ignition switch............................Hold Off Starter............................On (monitor for normal shutdown) Starter............................Off Emergency Exit............................Execute |
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Brake Failure
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Aircraft............................Stop, using other cockpit brakes
Aircraft............................Maintain directional control and stop aircraft utilizing Beta, rudder, and remaining brakes Aircraft............................Do not taxi or shutdown until wheels are chocked Emergency engine shutdown............................Execute Emergency exit............................Execute Warning: Simultaneous actuation of the same brake pedal in both cockpits may cause the shuttle valve to neutralize, causing loss of braking effectiveness. Note: Pumping the brakes may restore enough braking action to stop or better control the aircraft. If the brakes in one cockpit fail the brakes in the other cockpit may still function normally. Warning: The aircraft will initially accelerate until propeller reaches full feather position. |
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Aborting Takeoff
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PCL............................Full Beta
Wheelbrakes............................As Required Canopy............................Emergency Open Emergency Engine Shutdown............................Execute Emergency Exit............................Execute Warning: Simultaneous actuation of the same brake pedal in both cockpits may cause the shuttle valve to neutralize, causing loss of braking effectiveness. Note: When maximum braking is required, lower the nosewheel to the deck before applying the brakes. For maximum braking, use a single, smooth application of the brakes with constantly increasing pedal pressure as speed is lost. Use as much braking pressure as possible without sliding the tires. BETA is not available with an engine failure. |
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Tire Failure on Takeoff Roll
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Aborting takeoff............................Execute
Landing Gear............................Remain Down Note: If landing gear/wheel departs the aircraft, consideration may be given to leaving the landing gear down and performing the landing with Nosegear retracted, or landing with one main gear retracted procedures as follows. |
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Roll Back
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Condition Lever............................Full Increase RPM
EPL............................Advance to desired power setting EPL............................disconnect Engine Failure............................Execute Warning: A generator which fails with extreme heat could possibly lead to a loss of useful power situation in which the emergency power lever (EPL) may not be effective. The close proximity of the generator to the FCU can cause the fuel with the FCU to vapor-lock, inhibiting fuel flow through the FCU. Caution: Binding of the EPL cable may occur when the aircraft is operating in freezing temperatures. Note: When using EPL maintain N1 above 65 percent to improve engine response and ensure generator stays on line. Warning: When the engine is so underpowered that high rates of descent occur, any delay in feathering the propeller may result in insufficient altitude to reach a suitable landing site. It is not recommended to delay feathering the propeller in the landing configuration below landing patter altitude. Note: If resultant power is sufficient to maintain a rate of descent less that the feathered condition (600 to 800 fpm clean), consideration should be given to allowing the engine to operate until the field is made. Caution: Use of Beta is not recommended when performing a landing using the manual fuel control system. If the use of BETA is required, ensure the EPL is in the idle range or disconnect before selecting BETA with the PCL. |
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Compressor Stalls
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PCL............................ Slowly retard to just below stall threshold to clear stall
Cockpit environmental control............................Full forward PCL............................slowly advance (as required) Engine Failure............................Execute PEL............................Execute Warning: Avoid unnecessary PCL movement. Advancing the PCL may result in further compressor stalls and engine flameout. Retarding the PCL further may limit maximum power available. Warning: Use of manual fuel control will only aggravate compressor stalls and could lead to flameout. Warning: When the engine is so underpowered that high rates of descent occur any delay in feathering the propeller may result in insufficient altitued to reach a suitable landing site. Note: If the situation permits, record the altitude, OAT, maximum ITT, and duration of compressor stall. If resultant power is sufficient to maintain a rate of descent less that the feathered condition (600 to 800 fpm clean), consideration should be given to allowing the engine to operate until the field is made. |
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Engine Failure
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Flying speed............................maintain (100 KIAS minimum)
Landing gear and flaps............................Up Engine instruments............................Check Condition Lever............................Feather (as required) Landing site............................Select Harness............................Locked Airstart............................Perform (if situation permits) No landing site available and altitude permits............................Bail Out Emergency Engine Shutdown............................Execute Mayday/7700............................Broadcast ELP............................intercept Gear and Flaps............................As required Canopy............................Emergency Open Battery switch............................Off Warning: If N1 and ITT indicate a rollback condition (FCU stuck at minimum flow), execute the Fuel Control Stuck at Minimum Flow (Rollback) procedure. If application of power results in compressor stalls (possible compressor bleed valve malfunction/failure), execute Compressor Stalls procedure. Note: Dirt and loose objects propelled by the air-blast may restrict visibility. Note: Consideration should be given to leaving the battery on at night. |
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Airstart
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PCL............................Idle
Emergency fuel shutoff handle............................Down Standby fuel pump switch............................On Starter............................On N1 and ITT............................Monitor for start indications Starter............................Off (when ITT peaks or no indications of start) Standby fuel pump............................Off (if start unsuccessful) Condition lever............................Full Increase PCL............................Advance (as required) PEL............................Execute Autoignition............................On Note: If an airstart is attempted and unsuccessful, sufficient battery power may not be available to lower the flaps or gear electrically. |
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Tire Failure on Takeoff Roll
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Aborting takeoff............................Execute
Landing Gear............................Remain Down Note: If landing gear/wheel departs the aircraft, consideration may be given to leaving the landing gear down and performing the landing with Nosegear retracted, or landing with one main gear retracted procedures as follows. |
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Roll Back
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Condition Lever............................Full Increase RPM
EPL............................Advance to desired power setting EPL............................disconnect Engine Failure............................Execute Warning: A generator which fails with extreme heat could possibly lead to a loss of useful power situation in which the emergency power lever (EPL) may not be effective. The close proximity of the generator to the FCU can cause the fuel with the FCU to vapor-lock, inhibiting fuel flow through the FCU. Caution: Binding of the EPL cable may occur when the aircraft is operating in freezing temperatures. Note: When using EPL maintain N1 above 65 percent to improve engine response and ensure generator stays on line. Warning: When the engine is so underpowered that high rates of descent occur, any delay in feathering the propeller may result in insufficient altitude to reach a suitable landing site. It is not recommended to delay feathering the propeller in the landing configuration below landing patter altitude. Note: If resultant power is sufficient to maintain a rate of descent less that the feathered condition (600 to 800 fpm clean), consideration should be given to allowing the engine to operate until the field is made. Caution: Use of Beta is not recommended when performing a landing using the manual fuel control system. If the use of BETA is required, ensure the EPL is in the idle range or disconnect before selecting BETA with the PCL. |
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Compressor Stalls
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PCL............................ Slowly retard to just below stall threshold to clear stall
Cockpit environmental control............................Full forward PCL............................slowly advance (as required) Engine Failure............................Execute PEL............................Execute Warning: Avoid unnecessary PCL movement. Advancing the PCL may result in further compressor stalls and engine flameout. Retarding the PCL further may limit maximum power available. Warning: Use of manual fuel control will only aggravate compressor stalls and could lead to flameout. Warning: When the engine is so underpowered that high rates of descent occur any delay in feathering the propeller may result in insufficient altitued to reach a suitable landing site. Note: If the situation permits, record the altitude, OAT, maximum ITT, and duration of compressor stall. If resultant power is sufficient to maintain a rate of descent less that the feathered condition (600 to 800 fpm clean), consideration should be given to allowing the engine to operate until the field is made. |
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Engine Failure
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Flying speed............................maintain (100 KIAS minimum)
Landing gear and flaps............................Up Engine instruments............................Check Condition Lever............................Feather (as required) Landing site............................Select Harness............................Locked Airstart............................Perform (if situation permits) No landing site available and altitude permits............................Bail Out Emergency Engine Shutdown............................Execute Mayday/7700............................Broadcast ELP............................intercept Gear and Flaps............................As required Canopy............................Emergency Open Battery switch............................Off Warning: If N1 and ITT indicate a rollback condition (FCU stuck at minimum flow), execute the Fuel Control Stuck at Minimum Flow (Rollback) procedure. If application of power results in compressor stalls (possible compressor bleed valve malfunction/failure), execute Compressor Stalls procedure. Note: Dirt and loose objects propelled by the air-blast may restrict visibility. Note: Consideration should be given to leaving the battery on at night. |
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Airstart
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PCL............................Idle
Emergency fuel shutoff handle............................Down Standby fuel pump switch............................On Starter............................On N1 and ITT............................Monitor for start indications Starter............................Off (when ITT peaks or no indications of start) Standby fuel pump............................Off (if start unsuccessful) Condition lever............................Full Increase PCL............................Advance (as required) PEL............................Execute Autoignition............................On Note: If an airstart is attempted and unsuccessful, sufficient battery power may not be available to lower the flaps or gear electrically. |
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PEL
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Nearest Suitable runway......................select
Aircraft......................Climb at 100 KIAS or accelerate to a position within dead engine glide distance of the runway Landing gear and flaps......................up as appropriate aircraft and engine instruments......................check ELP......................intercept Warning: If established on any portion of the emergency landing pattern, and able to safely land the aircraft, ensure landing gear is down, remain on the ELP and land. Maneuvering off the ELP in an attempt to reenter at a higher altitude may preclude the possibility of reaching a suitable landing site if an engine failure occurs. Should engine failure occur at low altitude (below 2500 feet AGL and before established on the ELP), any delay in transitioning to engine failure procedures may result in high rates of descent and/or inability to reach a suitable landing site. Note: In the landing environment, the nearest suitable runway may include runway remaining during climbout. |
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Uncontrollable High Power
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PEL......................Execute
Warning: Certain failures can cause wide power surges from maximum to as low as minimum fuel flow. Engagement of the EPL in this case will have no effect on the high end of the power fluctuations, but may raise the low end of the surges, thus reducing the magnitude of the fluctuations. Caution: When retarding the condition lever do not hesitate in the feather detent because high power from the engine with the propeller in feather may cause severe airframe vibration and very high torque applied to the propeller and reduction gearbox. Note: Altitude permitting, the pilot may elect to shut down the engine with the emergency fuel shutoff handle. The engine may continue running for as long as 30 seconds after the handle is pulled. |
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Engine Fire In flight
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Fire......................Confirm
Emergency engine shutdown......................Execute Cockpit environmental control/aft cockpit outside air......................Off Bailout......................Execute Engine Failure......................Execute PEL......................Execute Note: Under varying conditions of altitude, fire, smoke, or fumes, the pilot has the option of using 100-percent oxygen, opening canopy, and/or closing the oxygen cylinder valve as dictated by judgement. |
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Electrical/Unknown Origin Fire
VMC |
Battery and generator switches......................Off
100 percent Oxygen......................Don (as required) Airspeed......................Reduce (as required) Cockpit environmental control/aft cockpit outside air......................Off Engine Fire......................Execute Land as soon as possible. Note: Under varying conditions of altitude, fire, smoke, or fumes, the pilot has the option of using 100-percent oxygen, opening canopy, and/or closing the oxygen cylinder valve as dictated by judgement. Note: Should the pilot elect to initiate an emergency landing with the electrical power secured, additional consideration should be given to the landing approach; allow additional time to handcrank the landing gear down and plan for a no flap landing with maximum runway length, since BETA will not be available. |
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Electrical/Unknown Origin Fire
IMC |
Utility Buss switches......................Off
All other nonessential equipment......................Off 100 percent Oxygen......................Don (as required) Airspeed......................Reduce (as required) Cockpit environmental control/aft cockpit outside air......................Off Bailout (altitude permitting) Land as soon as possible. Note: The following items when securing the utility bus switches: Oil pressure and temperature, flap power and position indicator, RMI compass and cards, NACWS CDU's and TRC, transponder, VOR, TACAN, GPS, fuel quantity, BETA release, utility lights, console lights, console flood lights, instrument flood lights, vent blowers, scavenge pump, prop test, condenser blower, AC clutch, and avionics cooling fan. Note: Under varying conditions of altitude, fire, smoke, or fumes, the pilot has the option of using 100-percent oxygen, opening canopy, and/or closing the oxygen cylinder valve as dictated by judgement. Note: If landing with utility buss switches secured, addition consideration should be given to the landing approach. Plan for a no-flap landing using maximum runway length since BETA will not be available. |
