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David's SF50 Vision Jet > David's SF50 Vision Jet > Flashcards

David's SF50 Vision Jet Flashcards

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

A

3 quarts

23
Q

Amount of oil to full line

A

2.2 quarts

24
Q

Maximum tailwind

A

10 knots

25
Q

Maximum demonstrated crosswind

A

18 knots - Flaps 50%
16 knots - Flaps 100%

26
Q

Maximum airport elevation

A

10,000 ft

27
Q

Minimum airport elevation

A

-1,000 ft

28
Q

Minimum Takeoff temperature

A

-40C/F

29
Q

Takeoff flaps

A

50%

30
Q

Maximum Takeoff temperature

A

50C/122F

31
Q

Vmo/Mmo

A

250knots/.53 Mach

32
Q

Vo

A

150 knots

33
Q

Maximum time in T/O Thrust

A

5 minutes

34
Q

Maximum operating altitude

A

FL310

35
Q

Min operating temp at FL310

A

-63C/-82F

36
Q

Min operating temp at FL200

A

-54C/-65F

37
Q

Cool down after high energy event

A

30 minute

38
Q

Vfe - 50%, 100%

A

190 knots - Flaps 50%
150 knots - Flaps 100%

39
Q

Vlo- Extend

A

210 knots

40
Q

Vlo - Retract

A

150 knots

41
Q

Vle

A

210 knots

42
Q

Maximum cabin pressure differential

A

7.1 psi

43
Q

Minimum Autopilot engagement speeds

A

85 knots - Flaps 100%
95 knots - Flaps 50%
105 knots - Flaps Up

44
Q

Minimum autopilot engagement altitude

A

400’ AGL

45
Q

Minimum altitude for autopilot use

A

1,000ft AGL - visual approaches
DA/MDA - Instrument approaches

46
Q

Usable IPS fluid

A

3.0 gal

47
Q

Minimum IPS fluid dispatch quantity into icing conditions

A

1.0 gal

48
Q

Minimum windshield IPS temp

A

-30C/–22F

49
Q

Minimum wing/stab IPS Temp

A

-40C/F

50
Q

Minimum airspeed in icing conditions

A

160 knots

51
Q

Maximum flap deflection with ice accretion

A

50% Flaps

52
Q

Max duty cycle for windshield IPS

A

10 seconds on, 10 seconds off

53
Q

How long before departure is tactile inspection required?

A

5 minutes

54
Q

Maximum time for probe heat on ground

A

5 minutes

David's SF50 Vision Jet (2 decks)

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