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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
Amount of oil to full line
2.2 quarts
26
Maximum tailwind
10 knots
27
Maximum demonstrated crosswind
18 knots - Flaps 50% | 16 knots - Flaps 100%
28
Maximum airport elevation
10,000ft
29
Minimum airport elevation
-1,000 ft
30
Minimum Takeoff temperature
-40C/F
31
Maximum Takeoff temperature
50C/122F
32
Vmo/Mmo
250knots/.53 Mach
33
Vo
150 knots
34
Maximum time in T/O Thrust
5 minutes
35
Maximum operating altitude
FL280
36
Min operating temp at FL280
-61C/-77F
37
Min operating temp at FL200
-54C/-65F
38
Cool down after high energy event
30 minute
39
Flight Load Limits
``` +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
Vfe - 50%, 100%
190 knots - Flaps 50% | 150 knots - Flaps 100%
41
Vlo- Extend
210 knots
42
Vlo - Retract
150 knots
43
Vle
210 knots
44
Maximum cabin pressure differential
6.4 psi
45
Min landing gear operating temp
-40C/F
46
Maximum gear cycles Rest period between cycles
8 gear cycles per 30 minutes 10 seconds
47
Generator 1 voltage and Current
27.8V, 270A
48
Generator 2 Voltage and Amp
28.7V, 72A
49
CABIN ALTITUDE Warning Altitude
10,000ft
50
Minimum Autopilot engagement speeds
85 knots - Flaps 100% 95 knots - Flaps 50% 105 knots - Flaps Up
51
Minimum autopilot engagement altitude
400’ AGL
52
Minimum altitude for autopilot use
1,000ft AGL - visual approaches | DA/MDA - Instrument approaches
53
Usable IPS fluid
3.0 gal
54
Minimum IPS fluid dispatch quantity into icing conditions
1.0 gal
55
Minimum windshield IPS temp
-30F/-34C
56
Minimum wing/stab IPS Temp
-40C/F
57
Minimum airspeed in icing conditions
160 knots
58
Maximum flap deflection with ice accretion
50% Flaps
59
Max duty cycle for windshield IPS
10 seconds on, 10 seconds off
60
How long before departure is tactile inspection required?
5 minutes
61
Maximum time for probe heat on ground
5 minutes

SF50 Vision Jet (2 decks)

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