SF50 Limitations / Memory Items Flashcards

(57 cards)

1
Q

Engine Manufacturer and Model

A

Williams International FJ33-5A

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2
Q

Engine Thrust Rating

A

1846 lb

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3
Q

Usable Fuel

A

296 gallons

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4
Q

Approved Fuels

A

Jet A, Jet A-1, JP-8

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5
Q

Total Oil Quantity

A

3 Quarts

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6
Q

Oil Quantity to Full Line

A

2.2 Quarts

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7
Q

Amount of Usable IPS Fluid

A

3.0 Gallons

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8
Q

Minimum IPS Fluid Dispatch Quantity

A

1.0 Gallon

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9
Q

Maximum Gross Takeoff Weight

A

6000 lb

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10
Q

Maximum Landing Weight

A

5550 lb

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11
Q

Maximum Ramp Weight

A

6040 lb

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12
Q

Maximum Zero Fuel Weight

A

4900 lb

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13
Q

Maximum Baggage Compartment Weight

A

300 lb

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14
Q

Maximum Cargo Extend Weight

A

40 lb

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15
Q

Maximum Tailwind for Takeoff or Landing

A

10 knots

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16
Q

Operating Maneuvering Speed (Vo)

A

150 KIAS

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17
Q

Maximum Operating Speed (Vmo)

A

250 KIAS

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18
Q

Maximum Mach Number

A

0.53 Mach

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19
Q

Maximum Flaps 50% Extended Speed

A

190 KIAS

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20
Q

Maximum Flaps 100% Extended Speed

A

150 KIAS

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21
Q

Maximum Landing Gear Extension Speed

A

210 KIAS

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22
Q

Maximum Landing Gear Retraction Speed

A

150 KIAS

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23
Q

Maximum Operating Speed with Gear Extended

24
Q

Maximum Allowable Fuel Imbalance

A

15 US Gallons

25
Maximum Fuel Temperature
122F / 50C
26
Minimum Fuel Temperature
-40F / -40C
27
Recommended Fueling Increment per wing
75 Gallons per side
28
Approved Oils
Mobile Jet II / Mobile 254
29
Minimum Oil Temperature for Engine Start
-40F / -40C
30
External Power Cart Settings for Starting
28V and 800-1000A
31
Maximum Duration for Takeoff Thrust
5 Minutes (2 Minutes Recommended)
32
Maximum Tailwind for Engine Start
15 Knots
33
Maximum Crosswind for Engine Start
25 Knots
34
Starter/Generator Duty Cycle Limits
30 seconds on / 30 seconds off (check for pooling fuel) 30 seconds on / 5 minutes off 30 seconds on / 30 minutes off
35
Maximum Demonstrated Crosswind with Flaps 50%
18 knots
36
Maximum Demonstrated Crosswind with Flaps 100%
16 knots
37
Maximum Airport Elevation
10,000 ft MSL
38
Maximum Operating Altitude
FL310
39
Minimum Airport Elevation
-1000 ft MSL
40
Maximum Cabin Pressure Differential
G2 - 7.1 PSI G1 - 6.8 PSI
41
Minimum Takeoff Temperature
-40F / -40C
42
Maximum Takeoff Temperature
122F / 50C
43
Minimum Operating Temperature (up to 20,000')
-65F / -54C
44
Minimum Operating Temperature (up to 31,000)
-82F / -63C
45
Maximum Engine IPS Operating Temperature
50F / 10C
46
Maximum Operating Temperature
122F / 50C
47
Approved Flap Setting(s) for Takeoff
50%
48
Approved Flap Setting(s) for Approach and Landing
UP, 50%, 100%
49
Landing Gear Cycle Limits
8 Cycles in 32 Minutes 10 Seconds between Cycles Cycle = 2 motions (up down up / down up down)
50
Minimum Airspeed in Icing Conditions with flaps and hear UP
160 KIAS
51
Flap position when holding in icing conditions
UP
52
Maximum flap deflection with ice accretions
50%
53
Maximum duty cycle for Windshield MAX Mode
50% - up to 10 seconds on 10 seconds off
54
IPS Fluid Endurance Limits with Minimum Dispatch Quantity
NORM - 90 minutes HIGH - 45 minutes
55
Minimum Autopilot Engagement Speeds: 100% / 50% / UP Flaps
85 KIAS / 95 KIAS / 105 KIAS
56
Maximum Autopilot Speeds: Flaps 100% / Flaps 50% / Clean / Landing Gear Down
150 KIAS / 190 KIAS / 250 KIAS (0.53mach) / 210 KIAS
57
When must the autopilot be disconnected on an approach to landing
Visual - 1000' AGL Non-Precision Approach - Higher of MDA or 400' AGL Precision Approach - Higher of DA or 200' AGL