David's SF50 Vision Jet Flashcards

(54 cards)

1
Q

Max Ramp Weight

A

6040lbs

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2
Q

Max Takeoff Weight

A

6000 lbs

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3
Q

Max Landing Weight

A

5550 lbs

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4
Q

Max Zero Fuel Weight

A

4900 lbs

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5
Q

Max Aft Baggage Compartment

A

300 lbs

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6
Q

Max Cargo X-Tend Compartment

A

40 lbs

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7
Q

Min temp oil temp

A

-40F/C

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8
Q

Min start temp

A

-40F/C

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9
Q

EPU Voltage and Amperage requirements

A

28V and 800-1000 amps

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10
Q

Max tailwind for start

A

15 knots

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11
Q

Max crosswind for start

A

25 knots

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12
Q

Inflight air start and less than 18,000ft Speed

A

120-200 knots

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13
Q

Starter Limits

A

30 seconds on per attempt

1st Attempt - 30 seconds Off
2nd Attempt - 5 minutes Off
3rd Attempt - 30 minutes Off

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14
Q

Approved fuel types

A

Jet-A, Jet A-1, JP-8

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15
Q

Maximum Fuel

A

296 gallons

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16
Q

Maximum allowable fuel imbalance

A

15 gallons

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17
Q

Min fuel temp

A

-40F/C

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18
Q

Max fuel temp

A

122F/50C

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19
Q

Gallons increments when refueling

A

75 gallons

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20
Q

Type of engine and capable thrust

A

Williams FJ33-5A

1846lbs thrust, uninstalled, sea level, temp of 60F

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21
Q

Approved oil

A

Mobile Jet II / Mobile 254

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22
Q

Max oil quantity

23
Q

Amount of oil to full line

24
Q

Maximum tailwind

25
Maximum demonstrated crosswind
18 knots - Flaps 50% 16 knots - Flaps 100%
26
Maximum airport elevation
10,000 ft
27
Minimum airport elevation
-1,000 ft
28
Minimum Takeoff temperature
-40C/F
29
Takeoff flaps
50%
30
Maximum Takeoff temperature
50C/122F
31
Vmo/Mmo
250knots/.53 Mach
32
Vo
150 knots
33
Maximum time in T/O Thrust
5 minutes
34
Maximum operating altitude
FL310
35
Min operating temp at FL310
-63C/-82F
36
Min operating temp at FL200
-54C/-65F
37
Cool down after high energy event
30 minute
38
Vfe - 50%, 100%
190 knots - Flaps 50% 150 knots - Flaps 100%
39
Vlo- Extend
210 knots
40
Vlo - Retract
150 knots
41
Vle
210 knots
42
Maximum cabin pressure differential
7.1 psi
43
Minimum Autopilot engagement speeds
85 knots - Flaps 100% 95 knots - Flaps 50% 105 knots - Flaps Up
44
Minimum autopilot engagement altitude
400’ AGL
45
Minimum altitude for autopilot use
1,000ft AGL - visual approaches DA/MDA - Instrument approaches
46
Usable IPS fluid
3.0 gal
47
Minimum IPS fluid dispatch quantity into icing conditions
1.0 gal
48
Minimum windshield IPS temp
-30C/--22F
49
Minimum wing/stab IPS Temp
-40C/F
50
Minimum airspeed in icing conditions
160 knots
51
Maximum flap deflection with ice accretion
50% Flaps
52
Max duty cycle for windshield IPS
10 seconds on, 10 seconds off
53
How long before departure is tactile inspection required?
5 minutes
54
Maximum time for probe heat on ground
5 minutes