David's SF50 Vision Jet Flashcards
Max Ramp Weight
6040lbs
Max Takeoff Weight
6000 lbs
Max Landing Weight
5550 lbs
Max Zero Fuel Weight
4900 lbs
Max Aft Baggage Compartment
300 lbs
Max Cargo X-Tend Compartment
40 lbs
Min temp oil temp
-40F/C
Min start temp
-40F/C
EPU Voltage and Amperage requirements
28V and 800-1000 amps
Max tailwind for start
15 knots
Max crosswind for start
25 knots
Inflight air start and less than 18,000ft Speed
120-200 knots
Starter Limits
30 seconds on per attempt
1st Attempt - 30 seconds Off
2nd Attempt - 5 minutes Off
3rd Attempt - 30 minutes Off
Approved fuel types
Jet-A, Jet A-1, JP-8
Maximum Fuel
296 gallons
Maximum allowable fuel imbalance
15 gallons
Min fuel temp
-40F/C
Max fuel temp
122F/50C
Gallons increments when refueling
75 gallons
Type of engine and capable thrust
Williams FJ33-5A
1846lbs thrust, uninstalled, sea level, temp of 60F
Approved oil
Mobile Jet II / Mobile 254
Max oil quantity
3 quarts
Amount of oil to full line
2.2 quarts
Maximum tailwind
10 knots
Maximum demonstrated crosswind
18 knots - Flaps 50%
16 knots - Flaps 100%
Maximum airport elevation
10,000 ft
Minimum airport elevation
-1,000 ft
Minimum Takeoff temperature
-40C/F
Takeoff flaps
50%
Maximum Takeoff temperature
50C/122F
Vmo/Mmo
250knots/.53 Mach
Vo
150 knots
Maximum time in T/O Thrust
5 minutes
Maximum operating altitude
FL310
Min operating temp at FL310
-63C/-82F
Min operating temp at FL200
-54C/-65F
Cool down after high energy event
30 minute
Vfe - 50%, 100%
190 knots - Flaps 50%
150 knots - Flaps 100%
Vlo- Extend
210 knots
Vlo - Retract
150 knots
Vle
210 knots
Maximum cabin pressure differential
7.1 psi
Minimum Autopilot engagement speeds
85 knots - Flaps 100%
95 knots - Flaps 50%
105 knots - Flaps Up
Minimum autopilot engagement altitude
400’ AGL
Minimum altitude for autopilot use
1,000ft AGL - visual approaches
DA/MDA - Instrument approaches
Usable IPS fluid
3.0 gal
Minimum IPS fluid dispatch quantity into icing conditions
1.0 gal
Minimum windshield IPS temp
-30C/–22F
Minimum wing/stab IPS Temp
-40C/F
Minimum airspeed in icing conditions
160 knots
Maximum flap deflection with ice accretion
50% Flaps
Max duty cycle for windshield IPS
10 seconds on, 10 seconds off
How long before departure is tactile inspection required?
5 minutes
Maximum time for probe heat on ground
5 minutes