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Cirrus > SF50 Limitations / Memory Items > Flashcards

SF50 Limitations / Memory Items Flashcards

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

A

210 KIAS

24
Q

Maximum Allowable Fuel Imbalance

A

15 US Gallons

25
Q

Maximum Fuel Temperature

A

122F / 50C

26
Q

Minimum Fuel Temperature

A

-40F / -40C

27
Q

Recommended Fueling Increment per wing

A

75 Gallons per side

28
Q

Approved Oils

A

Mobile Jet II / Mobile 254

29
Q

Minimum Oil Temperature for Engine Start

A

-40F / -40C

30
Q

External Power Cart Settings for Starting

A

28V and 800-1000A

31
Q

Maximum Duration for Takeoff Thrust

A

5 Minutes (2 Minutes Recommended)

32
Q

Maximum Tailwind for Engine Start

A

15 Knots

33
Q

Maximum Crosswind for Engine Start

A

25 Knots

34
Q

Starter/Generator Duty Cycle Limits

A

30 seconds on / 30 seconds off (check for pooling fuel)
30 seconds on / 5 minutes off
30 seconds on / 30 minutes off

35
Q

Maximum Demonstrated Crosswind with Flaps 50%

A

18 knots

36
Q

Maximum Demonstrated Crosswind with Flaps 100%

A

16 knots

37
Q

Maximum Airport Elevation

A

10,000 ft MSL

38
Q

Maximum Operating Altitude

A

FL310

39
Q

Minimum Airport Elevation

A

-1000 ft MSL

40
Q

Maximum Cabin Pressure Differential

A

G2 - 7.1 PSI
G1 - 6.8 PSI

41
Q

Minimum Takeoff Temperature

A

-40F / -40C

42
Q

Maximum Takeoff Temperature

A

122F / 50C

43
Q

Minimum Operating Temperature (up to 20,000’)

A

-65F / -54C

44
Q

Minimum Operating Temperature (up to 31,000)

A

-82F / -63C

45
Q

Maximum Engine IPS Operating Temperature

A

50F / 10C

46
Q

Maximum Operating Temperature

A

122F / 50C

47
Q

Approved Flap Setting(s) for Takeoff

A

50%

48
Q

Approved Flap Setting(s) for Approach and Landing

A

UP, 50%, 100%

49
Q

Landing Gear Cycle Limits

A

8 Cycles in 32 Minutes
10 Seconds between Cycles
Cycle = 2 motions (up down up / down up down)

50
Q

Minimum Airspeed in Icing Conditions with flaps and hear UP

A

160 KIAS

51
Q

Flap position when holding in icing conditions

A

UP

52
Q

Maximum flap deflection with ice accretions

A

50%

53
Q

Maximum duty cycle for Windshield MAX Mode

A

50% - up to 10 seconds on 10 seconds off

54
Q

IPS Fluid Endurance Limits with Minimum Dispatch Quantity

A

NORM - 90 minutes
HIGH - 45 minutes

55
Q

Minimum Autopilot Engagement Speeds: 100% / 50% / UP Flaps

A

85 KIAS / 95 KIAS / 105 KIAS

56
Q

Maximum Autopilot Speeds: Flaps 100% / Flaps 50% / Clean / Landing Gear Down

A

150 KIAS / 190 KIAS / 250 KIAS (0.53mach) / 210 KIAS

57
Q

When must the autopilot be disconnected on an approach to landing

A

Visual - 1000’ AGL
Non-Precision Approach - Higher of MDA or 400’ AGL
Precision Approach - Higher of DA or 200’ AGL

Cirrus (3 decks)

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