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66 Cards in this Set
- Front
- Back
MAX Ramp Weight
|
18078
|
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MAX T/O Weight
|
17968
|
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MAX Landing Weight
|
16865
|
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MAX Zero Fuel Weight
|
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
|
250
|
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Vle
|
250
|
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Vmc for T/O
|
97kias
|
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Vmc for Landing (no ice)
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86kias
|
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Vmc for Landing (icing conditions)
|
95kias
|
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Mmo
|
0.78 Mach
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Vmo
|
320kias
|
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Vo
|
205
|
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Vfe Flaps 1
|
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
|
3.00 g
|
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Positive Load Factor Limit Flap Extended
|
2.00 g
|
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Forward Baggage Limit
|
110 lb
|
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Lavatory Cabinet Limit
|
33 lb
|
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Aft Baggage Limit
|
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
|
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
|
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?
|
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?
|
Two Pratt & Whitney Canada PW535E
|
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MAX ITT
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725C
|
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MAX ITT Time Limit
|
10 Min
|
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Takeoff ITT
|
700C
|
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Takeoff Time Limit
|
5 Min
|
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MAX Continuous ITT
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680C
|
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MAX Climb ITT
|
680C
|
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Starting ITT
|
765C for 5 sec
|
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Transient ITT
|
765C for 20 sec
|
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Static takeoff power application on ground is limited to crosswind components up to...
|
18kt
|
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Starter Limits
|
1 - 60 sec
2 - 60 sec 3 - 15 min 4 - 30 min |
|
What is needed for air conditioner operation on ground?
|
GPU or one engine generator must be on
|
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MAX Differential Pressure
|
8.4psi
|
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MAX Differential Overpressure
|
8.6psi
|
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MAX Differental Negative Pressure
|
-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
|
10,000'
|
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Minimum Airspeed WINGSTAB Inhibited (flaps and gear up)
|
165kias
|
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Minimum Airspeed WINGSTAB Uninhibited (flaps and gear up)
|
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
|
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)
|
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)
|
220'
|
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AP Altitude Loss (manuevering/cruise)
|
160'
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