Cirrus SR 22 Flashcards

1
Q

V Rotate

A

73 KIAS

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2
Q

Vx

A

88 KIAS

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3
Q

Vy

A

108 KIAS

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4
Q

Vglide

A

92 KIAS

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5
Q

Vfe

A

50% 150 KIAS

100% 110 KIAS

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6
Q

VFinal

A

Clean 90-95 KIAS
Flaps 50% 85 - 90 KIAS
Flaps 100% 80 - 85 KIAS

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7
Q

V final - Short Field

A

79 KIAS

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8
Q

Vs

A

74 KIAS

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9
Q

Vso

A

64 KIAS

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10
Q

Vne

A

205 KIAS

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11
Q

FLT Plan CRZ

A

KIAS

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12
Q

CCTs - Down wind

A

D/Wind
PWR 35% - 100 KIAS
ABEAM THRESHOLD
PWR 20% - Flaps 50%

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13
Q

CCTs - Base

A

PWR 20 - 30 %

Flaps 100% - 90 KIAS

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14
Q

PWR Settings Descent

A

RPM

Mix

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15
Q

PWR Settings Final

A

30% - Flaps 100 - 85 KIAS

80 KIAS Short Final

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16
Q

Fuel Capacity

usable

A

350 Ltr

92 USG

17
Q

Burn Rate

A

A050 / 55%
Best Power - 50 Ltr/Hr (13.1 USG) - 155 KIAS
Best Eco - 45 Ltr/Hr (11.3 USG) - 153 KIAS

65% Best Power - 60 Ltrs/Hr (15.4 USG) - 166 KIAS

18
Q

Engine

A

IO 550-N

19
Q

Engine Power

A

310 SHP

20
Q

Weights

A

MTOW 1633 Kgs (3600 ibs)
MZFW 1542 Kgs (3400 lbs)
Baggage 59 Kgs (130 lbs)

21
Q

Max Useful load - Full Fuel

A

314 Kgs

22
Q

What is Vpd

A

CAPS deployment speed

140 KIAS

23
Q

Vno

A

176 KIAS

24
Q

Va

A

140 KIAS @ 3000 lbs (1365 Kgs)

25
Q

Max Operating ALT

A

FL 175

17,500’

26
Q

Max Fuel Imbalance

A

10USG (38 Ltrs)

27
Q

Max X/wind

A

21 Kts

28
Q

Min oil Temp for Runups

A

100 deg F (38 deg C)

29
Q

Start Cycle

A

10 s crank

20 cool down

30
Q

Alternator 1 rating

A

100 AMPs

28 V

31
Q

Alternator 2 rating

A

70AMPs
28.75 V
*

32
Q

Battery 1

A

10 AMP/Hr

24 V

33
Q

Battery 2

A

7 AMP/Hr

24 V

34
Q

Main Distribution BUS 1

A
Landing Light
MAIN BUS 3
A/C Bus 1
A/C BUS 2
ESS buses (through main dist bus 1)
35
Q

Main Distribution BUS 2

A
Powered By ALT 2
Powers
ESS BUS's 1 & 2 ( through the MCU)
Non ESS BUS
Main BUS 1
Main BUS 2
36
Q

What is the job of the MCU

Master Control Unit

A

MCU is located on the left firewall.
- controls ALT 1, ALT 2, starter, landing light, external power & power generation functions.
- Provides voltage regulation ALT 1 & ALT 2 ,
- external power reverse polarity protection,
- alternator overvoltage protection,
- Systems health annunciations
- Power is distributed to the airplane circuit panel buses through Main and Essential buses in the MCU.
The Main distribution buses are interconnected by an 80-amp fuse and a diode.
The diode prevents ALT 2 from feeding the Main distribution Bus 1. Additionally, since ALT 2 Bus voltage is slightly higher than ALT 1 voltage, bus separation is further assured

37
Q

Leaning -

Best Power

A

Rich Of Peak
75% Power or Less
Lean until 1st Cylinder then enrichen by 75 deg F
High CHT - richen mixture (more Fuel)

38
Q

Leaning

Best Economy

A

Lean Of Peak
65% or Less
Lean until last Cylinder then keep leaning 50 Deg F
Hgh CHT - lean further (Less Fuel)

39
Q

CAPs HGT

A

600 AGL (SR22) - 500 AGL (SR20)