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SF50 Vision Jet > Limitations > Flashcards

Limitations 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

40lbs

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7
Q

Min Oil Temp

A

-40F/-40C

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8
Q

Min temp for battery 1 start

A

0F/-18C

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9
Q

Min voltage for battery 1 start

A

23.5 Volts

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10
Q

Min temp for EPU Start

A

-40F/C

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11
Q

EPU Voltage and Amperage requirements

A

28V and 800-1000 amps

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12
Q

Max tailwind for start

A

15 knots

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13
Q

Max crosswind for start

A

25 knots

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14
Q

Inflight air start and less than 18,000ft Speed

A

120-200 knots

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15
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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16
Q

Approved fuel types

A

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

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17
Q

Maximum Fuel

A

296 gallons

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18
Q

Maximum allowable fuel imbalance

A

15 gallons

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19
Q

Min fuel temp

A

-40F/C

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20
Q

Max fuel temp

A

122F/50C

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21
Q

Gallons increments when refueling

A

75 gallons

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22
Q

Type of engine and capable thrust

A

Williams FJ33-5A

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

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23
Q

Approved oil

A

Mobile Jet II / Mobile 254

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24
Q

Max oil quantity

A

3 quarts

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25
Q

Amount of oil to full line

A

2.2 quarts

26
Q

Maximum tailwind

A

10 knots

27
Q

Maximum demonstrated crosswind

A

18 knots - Flaps 50%

16 knots - Flaps 100%

28
Q

Maximum airport elevation

A

10,000ft

29
Q

Minimum airport elevation

A

-1,000 ft

30
Q

Minimum Takeoff temperature

A

-40C/F

31
Q

Maximum Takeoff temperature

A

50C/122F

32
Q

Vmo/Mmo

A

250knots/.53 Mach

33
Q

Vo

A

150 knots

34
Q

Maximum time in T/O Thrust

A

5 minutes

35
Q

Maximum operating altitude

A

FL280

36
Q

Min operating temp at FL280

A

-61C/-77F

37
Q

Min operating temp at FL200

A

-54C/-65F

38
Q

Cool down after high energy event

A

30 minute

39
Q

Flight Load Limits

A 
\+3.6g, -1.5g    Flaps Up, any Weight
\+1.9g, 0g          Flaps 50%, any weight
\+1.9g, 0g          Flaps 100%, any weight
\+3.6g, -1.5g    Vle 
\+2g, 0g             Vlo
40
Q

Vfe - 50%, 100%

A

190 knots - Flaps 50%

150 knots - Flaps 100%

41
Q

Vlo- Extend

A

210 knots

42
Q

Vlo - Retract

A

150 knots

43
Q

Vle

A

210 knots

44
Q

Maximum cabin pressure differential

A

6.4 psi

45
Q

Min landing gear operating temp

A

-40C/F

46
Q

Maximum gear cycles

Rest period between cycles

A

8 gear cycles per 30 minutes

10 seconds

47
Q

Generator 1 voltage and Current

A

27.8V, 270A

48
Q

Generator 2 Voltage and Amp

A

28.7V, 72A

49
Q

CABIN ALTITUDE Warning Altitude

A

10,000ft

50
Q

Minimum Autopilot engagement speeds

A

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

51
Q

Minimum autopilot engagement altitude

A

400’ AGL

52
Q

Minimum altitude for autopilot use

A

1,000ft AGL - visual approaches

DA/MDA - Instrument approaches

53
Q

Usable IPS fluid

A

3.0 gal

54
Q

Minimum IPS fluid dispatch quantity into icing conditions

A

1.0 gal

55
Q

Minimum windshield IPS temp

A

-30F/-34C

56
Q

Minimum wing/stab IPS Temp

A

-40C/F

57
Q

Minimum airspeed in icing conditions

A

160 knots

58
Q

Maximum flap deflection with ice accretion

A

50% Flaps

59
Q

Max duty cycle for windshield IPS

A

10 seconds on, 10 seconds off

60
Q

How long before departure is tactile inspection required?

A

5 minutes

61
Q

Maximum time for probe heat on ground

A

5 minutes

SF50 Vision Jet (2 decks)

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