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Cirrus SR20 G6 > General > Flashcards

General Flashcards

1
Q

What Type of Engine is in the G6?

A 
Lycoming IO-390-C3B6
215Hp @ 2700rpm
4 cylinder
Horizontally Opposed
Air Cooled
Normally Aspirated
Direct Drive
Fuel Injected
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2
Q

Propeller

A

Hartzell 74”
Constant Speed
Aluminum-alloy
Three-Blade Prop

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3
Q

Fuel Capacity Usable/Unusable

A

58.5 Gallons Total
Total Usable 56 Gallons

29.3 per tank
28 usable per tank

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4
Q

Maximum Certificated Weight

A

3150Ibs

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5
Q

Vo Definition

A

Operating Maneuvering speed is the maximum speed at which application of full control movement will not overstress the aircraft.

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6
Q

Vpd definition

A

Maximum Demonstrated parachute deployment speed at which parachute deployment has been demonstrated.

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7
Q

Vs 50% Definition

A

Stalling speed is minimum steady flight speed at which the aircraft is controllable with 50% flaps.

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8
Q

Vso Definition

A

Stalling Speed is the minimum steady flight speed at which the aircraft is controllable in the landing configuration (100%) at the most unfavorable weight and balance.

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9
Q

MCP definition

A

Maximum continuous Power is the maximum power that can be used continuously.

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10
Q

Vne Speed

A

201 KIAS

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11
Q

Vno Speed

A

164 KIAS

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12
Q

Vo Speed

A

3150 ibs 133 IAS
Operating maneuvering speed is the maximum speed at which full control travel may be used. Below this speed the airplane stalls before limit loads are reached. Above this speed, full control movements can damage the aircraft.

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13
Q

Vfe Speed

A

50% Flaps 150 IAS

100% Flaps 110 IAS

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14
Q

Vpd Speed

A

133 KIAS

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15
Q

White Ark Speed range

A

62-110 IAS
Lower limit is the most adverse stall speed in the landing configuration. Upper limit is the maximum speed permissible with flaps extended.

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16
Q

Green Arc Speed Range

A

71-164 IAS

17
Q

Yellow Arc

A

164-201 IAS

18
Q

Red Line

19
Q

Maximum Takeoff Weight

20
Q

Maximum Landing Weight

21
Q

Maximum Weight in baggage Compartment

22
Q

Maximum Allowable Fuel Imbalance

A

7.5 Gallons

23
Q

Maximum Takeoff Altitude

24
Q

Maximum operating Altitude

25
Q

Maneuvering Speed

A

3150 Ibs 133 IAS
2700 Ibs 123 IAS
2300 Ibs 114 IAS

26
Q

Best Glide Speeds

A

3150 Ibs 100 IAS

2600 Ibs 92 IAS

27
Q

Partial flap ldg

A

Flaps up 89 Ias
Flaps 50% 83 IAS
Flaps 100% 78 IAS

28
Q

Normal FLaps 50% takeoff speed

29
Q

Short Field Flaps 50% TO Speed

30
Q

Obstacle Clearance Flaps 50% Speed

31
Q

Normal Enroute Climb Flaps Up Vy

32
Q

Enroute Climb Flaps Up Normal Vy @ 10,000ft

33
Q

Short Field Flaps 100% Speed

34
Q

Go Around Flaps 50% Speed

35
Q

Max recommended Turbulent Air Penetration Speed

A

3150 IB 133 IAS
2700 IB 123 IAS
2300 IB 114 IAs

36
Q

Max Demonstrated Crosswind Velocity

37
Q

Flap design

A

Single SLotted Flaps

38
Q

How is the Wing powered?

A

28 VDC through the 10-amp Flaps circuit breaker on the NOn Ess Bus

Cirrus SR20 G6 (9 decks)

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