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66 Cards in this Set
- Front
- Back
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MAX Ramp Weight
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18078
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MAX T/O Weight
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17968
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MAX Landing Weight
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16865
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MAX Zero Fuel Weight
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13999
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What must be done if landing is performed below -40C?
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Report to maintenance
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Vlo
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250
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Vle
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250
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Vmc for T/O
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97kias
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Vmc for Landing (no ice)
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86kias
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Vmc for Landing (icing conditions)
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95kias
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Mmo
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0.78 Mach
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Vmo
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320kias
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Vo
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205
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Vfe Flaps 1
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180
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Vfe Flaps 2 or 3
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170
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MAX Altitude for Flaps Extended
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18000ft.
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MAX Tire Ground Speed
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182
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Positive Load Factor Limit Flap 0
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3.00 g
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Positive Load Factor Limit Flap Extended
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2.00 g
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Forward Baggage Limit
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110 lb
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Lavatory Cabinet Limit
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33 lb
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Aft Baggage Limit
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463 lb
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Runway Slope
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-2% TO +2%
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MAX T/O and Landing Tailwind Component
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10kt
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How often must the hydraulic accumulator precharge be checked?
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15 concsecutive calender days or before the next flight, whichever occurs last
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When must the stall warning and protection system be tested?
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Prior to each flight
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Minimum Battery Voltage for Engine Start
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24v
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Minimum GPU voltage for battery charging
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27v
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MAX Generator Load on Ground
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330A each
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Max Generator Load in Flight
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390A each
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MAX Usable Fuel Quantiity per Tank
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2676lb / 399.4 US gal
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Unusable Fuel Quantity per Tank
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24.2lb / 3.70 US gal
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MAX Fuel Capacity
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5401lb / 806.2 US gal
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MAX Fuel Imbalance
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220lb
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With the associated ejector pump inoperative what does unusable fuel increase to?
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44lb / 6.6 US gal
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MIN Fuel Tank Temp
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-37C
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MAX Fuel Tank Temp on ground
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52C
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MAX Fuel Tank Temp in Flight
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80C
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XFEED Valve operation
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XFEED Knob must be set to OFF during T/O and LAND
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What are the engines on a Phenom 300?
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Two Pratt & Whitney Canada PW535E
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MAX ITT
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725C
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MAX ITT Time Limit
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10 Min
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Takeoff ITT
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700C
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Takeoff Time Limit
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5 Min
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MAX Continuous ITT
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680C
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MAX Climb ITT
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680C
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Starting ITT
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765C for 5 sec
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Transient ITT
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765C for 20 sec
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Static takeoff power application on ground is limited to crosswind components up to...
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18kt
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Starter Limits
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1 - 60 sec
2 - 60 sec 3 - 15 min 4 - 30 min |
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What is needed for air conditioner operation on ground?
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GPU or one engine generator must be on
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MAX Differential Pressure
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8.4psi
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MAX Differential Overpressure
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8.6psi
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MAX Differental Negative Pressure
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-0.3psi
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MAX Differential Pressure for T/O and LAND
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0.2psi
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MAX T/O and Landing Altitude in icing conditions
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10,000'
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Minimum Airspeed WINGSTAB Inhibited (flaps and gear up)
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165kias
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Minimum Airspeed WINGSTAB Uninhibited (flaps and gear up)
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150kias
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MAX Altitude for Operations in Icing AEO
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45000'
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MAX Altitude for Operations in Icing OEI
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15000'
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Wing Inspection Light
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Must be operative prior to flight into known or forcast icing conditions at night
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Minium AP Engagement Height (dual engine)
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600'
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Minimum AP Engagement Height (single engine)
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1000'
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Minimum AP Use Height (dual engine)
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195'
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Minimum AP Use Height (single engine)
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220'
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AP Altitude Loss (manuevering/cruise)
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160'
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