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90 Cards in this Set
- Front
- Back
Take off decision speed
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V1
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Takeoff safety speed
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V2
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Climb speed
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V35
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Maneuvering speed
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Va
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Landing approach climb speed
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Vapp (1.3 Vs1)
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Single engine enroute climb speed
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Venr
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Maximum flap extended speed
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Vfe
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Maximum landing gear extended speed
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Vle
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Maximum landing gear operating speed
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Vlo
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Minimum airspeed in flight at which directional control can be maintained
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Vmc 83 knots flaps zero
76 knots flaps 15 |
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minimum airspeed on the ground at which directional control can be maintained with one engine suddengly inoperative using only aerodynamic controls
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Vmcg, 79 knots
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Maximum Operating Limit Speed
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Vmo or Mmo
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Rotation speed
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Vr
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Airspeed equal to the landing 50 foot point with flaps in landing position and landing gear extended (1.3 Vso)
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Vref
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stalling speed or minimum steady flight speed in the landing configuration
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Vso
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stalling speed or the minimum steady flight speed obtained in a specified configuration
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Vs1
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Best Angle of Climb speed (multiengine, flaps15)
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Vx 124 knots
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Best Rate of climb speed, (multiengine flaps 15)
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Vy 191 knots
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Maximum ramp weight
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12,625
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Maximum takeoff weight
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12,500
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Maximum Landing Weight
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11,525 pounds
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Maximum Zero Fuel Weight
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9,700 pounds
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Engine type
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Williams FJ44-3A-24
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Engine start maximum tailwind
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12 knots
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Engine start maximum crosswind
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16 knots
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Starting: maximum time to light-off
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10 seconds
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Minimum engine oil temperature
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-40C
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Maximum airport elevation for a ground battery start
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10,000 feet
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Maximum airport elevation for ground external power start
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10,000 feet
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Minimum voltage for battery start
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24 volts
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Minimum/Maximum Power Current Capacity for start
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800/1000 amps
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Start cycle limitations
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three engine starts in 30 minutes
three cycles of operation with a 60-second rest between cycles |
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Maximum time for pitot heat on ground
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2 minutes
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Maximum generator current on ground
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200 amps
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Ground operation greater than 75% N2with engine, wing or windshield anti-ice on
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2 minutes
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Windshield Ice Protection Fluid
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Isopropyl alcohol
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Hydraulic Fluid
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MIL-PRF-83282
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Fuel boost pumps on when....
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Fuel Low Level lights illuminate (approximately 220 pounds or less)
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Approved oils
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Mobile Jet II
Mbil 254 |
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Maximum speeds
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Mmo .737 (above FL290)
Vmo 278 KIAS between 8,000 and 29,000 Vmo 260 KIAS below 8,000 |
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Maximum Turbulent Air Penetration Speed
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180 KIAS
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Vfe flaps 15
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200 KIAS
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Vfe flaps 35
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161 KIAS
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Vfe ground flaps 60
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140 KIAS
Intentional selection of ground flaps in flight is prohibited |
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Vle
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200 KIAS
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Vlo extending
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200 KIAS
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Vlo retracting
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200 KIAS
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Vsb (maximum speed speed break operation)
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no limit
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Maximum Autopilot Speed
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278 KIAS or .737 Mach
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Maximum Altitude for Take Off
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10,000 feet
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Maximum Tailwind for Take-off and Landing
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10 knots
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Minimum Temperature for take-off
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-54 C
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Maximum fuel imbalance
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200 pounds (but 600 pounds has been demonstrated)
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Minimum cabin temperature prior to take-off
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0 C (because of the oxygen masks)
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Maximum tire speed
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165 KIAS
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Maximum operating altitude
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45,000 feet
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Maximum generator current
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300 amps to 41,000 feet
250 amps above 41,000 feet |
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Maximum altitude to extend flaps or gear
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18,000 feet
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Load factors
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Flaps up: -1.52 G to +3.6G at 12,500 pounds
Flaps 15 to 35: 0 to +2 G at 12,500 pounds |
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Normal cabin pressurization
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0 to 8.9 PSI
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N1 redline
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102.9%
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ITT redline
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1001C
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ITT redline one engine running
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878C
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N2 redline
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100.8%
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Oil temp redline
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149C
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Oil pressure redline
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22 psi
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Autopilot minimum altitude ILS
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70 feet
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Autopilot minimum altitude non-precision
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240 feet
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Autopilot minimum altitude cruise
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1,000 feet
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Which mode for a VOR approach?
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Approach mode
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Icing conditions exist when the RAT
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is +10C or below and visible moisture is present
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Minimum speed for flight in icing conditions (except approach and landing)
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160 KIAS
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What position should the flaps be in during icing conditions? (except approach and landing?)
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zero degrees, flaps up
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Minimum N2 speed for effective wing anti-icing
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80% N2
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Minimum temperature for operation of tail decing boots
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-35C RAT
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Kinds of Equipment for single pilot operations
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1. Operating autopilot
2. Headset/microphone 3. FAA approved abbreviated checklist 4. Accessible charts |
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Engine failure below V1
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Brakes-as required
Throttles-idle Speed brakes-extend |
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Engine failure above V1
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1. Maintain directional control
2. Accelerate to Vr 3. Rotate at Vr 4. Landing gear up 5. Wing X/Flow switch if anti ice is on 6. AT 1500 AGL retract flaps at V2+10 and accelerate to Venr |
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Engine failure during final approach
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1. Thrust-increase as required
2. Airspeed Vapp 3. Flaps-take-off and approach |
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Engine Fire
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1. Throttle on affected engine to idle
IF LIGHT REMAINS ON 2. Engine fire switch, lift cover and push 3. Either bottle illuminated BOTTLE ARMED light-push |
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Engine restart-two engines
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1. L/R Boost switches-BOTH ON
2. Throttle-OFF, then IDLE 3. If altitude allows, INCREASE AIRSPEED TO 230 KIAS |
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Electrical fire or smoke
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1. Oxygen Masks -DON and EMER
2. Microphone select switches-MIC OXY MASK |
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Environmental system smoke or odor
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1. Oxygen Masks-DON and EMER
2. Microphone select switches-MIC OXY MASK |
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Smoke removal
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1. Oxygen Masks-DON and EMER
2. Microphone select switches-MIC OXY MASK |
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Cabin Altitude Light
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1. Oxygen Masks DON and 100% OXYGEN
2. Microphone select switches-MIC OXY MASK 3. Emergency Descent-AS REQUIRED 4. Passenger Oxygen-Make sure passengers are receiving oxygen |
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Emergency Descent
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1. AP TRIM DISC button-press and release
2. Throttles-IDLE 3. Speed brakes-EXTEND 4. Airplane pitch attitude-INITIALLY TARGET 20 DEGREE PITCH DOWN |
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Battery Overtemp
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1. Volt/Amp-Note
2. Battery switch-EMER 3. Volt/Amp-Note |
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Autopilot malfunction
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1. AP TRIM DISC Button-Press and Release
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Electric Elevator Trim Runaway
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1. AP TRIM DISC Button-Press and Release
2. Throttles-As required 3. Speed brakes-As required 4. Manual Elevator Trim-As required 5. PITCH TRIM Circuit Breaker (L Panel) Pull |
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Emergency Evacuation
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1. Parking brake-set
2. Throttles-both off 3. L/R Engine Fire Switches-Both press 4, Illuminated Bottle Armed buttons-push 5. Battery switch-off 6. ELT-On 7. Escape route-choose best |