Baron Flashcards

1
Q

What type of engine does it have?

A

2 x IO-520-C
Fuel injected
Air cooled
6 cylinder

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2
Q

What is the horsepower and RPM?

A

285HP @ 2700RPM

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3
Q

Take off power setting

A

Full throttle & 2700RPM

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4
Q

Max OEI power setting

A

Full throttle & 2700RPM

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5
Q

Cruise climb power setting

A

25” & 2500RPM

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6
Q

Max cruise power setting

A

24.5” & 2500RPM

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7
Q

What fuel is permitted?

A

100LL (blue) preferred

100 (green) is also approved

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8
Q

Fuel capacity

A

106USG total

100USG usable

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9
Q

Oil capacity

A

12 quarts per engine

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10
Q

Max ramp weight

A

5324lbs

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11
Q

MTOW

A

5300lbs

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12
Q

MLW

A

5300lbs

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13
Q

Max cabin baggage

A

400lbs

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14
Q

Max aft baggage

A

120lbs

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15
Q

Max nose baggage

A

300lbs

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16
Q

Vne

A

223kts

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17
Q

Vno

A

195kts

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18
Q

Va

A

156kts

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19
Q

Vfe 15

A

152kts

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20
Q

Vfe 30

A

122kts

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21
Q

Vlo/le

A

152kts

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22
Q

Vmca

A

79kts

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23
Q

Vy OEI

A

99kts

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24
Q

Max CHT

A

460˚F

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25
Q

Max oil temperature

A

240˚F

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26
Q

Min take off oil temperature

A

75˚F

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27
Q

Normal oil pressure range

A

30-100psi

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28
Q

Starter operation limits

A

Do not operate starter continuously for more than 30 seconds

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29
Q

Max g load clean

A

4.2g

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30
Q

Max g load dirty

A

2g

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31
Q

Vx

A

86kts

32
Q

Vy

A

101kts

33
Q

Vx OEI

A

96kts

34
Q

Minimum Voei intentional

A

84kts

35
Q

Vcruise climb

A

130kts

36
Q

Vga climb

A

88kts

37
Q

Vapp

A

88kts

38
Q

Vapp flapless

A

96kts

39
Q

Vb

A

156kts

40
Q

Max demonstrated xwc

A

22kts

41
Q

Start procedure

A
Throttle 1/2"
Props full fine
Mixture rich
Aux fuel pump high until pressure stabilises
Engage starter
42
Q

After start checks

A

@ 1000-1200RPM
Oil pressure 25psi within 30 seconds
Alternator on
T’s and P’s check

43
Q

Run ups/Before take off checks

A
Belts secure
Park brake set
Aux fuel pumps off (>32˚C on low)
Check instruments
Check fuel
Mixture rich
Set 2200RPM
Cycle props and check for RPM drop and small oil pressure drop
Check loadmeters
Set 1700RPM
Magneto check (150 max drop, 50 max difference)
Set 1500RPM
Props feather check (stop before 500RPM drop)
Set idle
Electric trim check
Trim set
Flaps set
Flight controls full and free
Hatches closed and locked
Park brake release
44
Q

Max performance climb procedure

A

Full throttle & 2700RPM
Mixture lean to appropriate fuel flow
Cowl flaps open
101kts

45
Q

Cruise climb procedure

A

25” & 2500RPM
Mixture lean to appropriate fuel flow
Cowl flaps as required to maintain temperature
130kts

46
Q

Various cruise procedures

A
Max - 24.5" & 2500RPM
Recommended - 24" or 21" & 2300RPM
Economy - 20.5" & 2100RPM
Lean as required
Cowl flaps as required
47
Q

Leaning procedure

A

Lean until temperature peaks then starts to decrease
Richen until 25˚ rich of peak
For best power richen until 100˚ rich of peak

48
Q

Descent procedure

A
Set altimeter
Cowl flaps closed
Windshield defroster as required
Power as required (avoid prolonged idling and low CHT)
Recommended smooth 170kts
49
Q

Before landing procedure

A
Belts and harnesses secure
Fuel selector valves on
Aux fuel pumps off (or low if >32˚c)
Cowl flaps as required
Mixture rich
Flaps 15˚
Gear down
Flaps 30˚
Vapp
Pitch fine
50
Q

Go around procedure

A
Pitch fine
Power max
88kts
Flaps 0˚
Gear up
Cowl flaps as required
51
Q

After landing procedure

A
Lights as required
Flaps up
Trim reset
Cowl flaps open
Aux fuel pumps as required
52
Q

Shutdown procedure

A
Park brake set
Pitch full fine
Set 1000RPM
Aux fuel pumps off
Electrical/avionics off
Mixture ICO
Ignition off
Battery/alternator off
Controls locked
53
Q

EF during take off

A

Throttles closed

Max braking

54
Q

EFATO/during flight

A
Gear up
Flap up
Identify with throttle
Feather prop
Power as required on live
99kts until obstacles cleared
Secure inoperative engine
Electrical load monitor
55
Q

Securing engine procedure

A
Mixture ICO
Fuel selector off
Aux fuel pump off
Ignition off
Alternator off
Cowl flap closed
56
Q

Engine fire on the ground

A
Mixture ICO
Crank
Fuel selector valves off
Battery/alternator off
Use fire extinguisher
57
Q

Engine fire in flight

A
Fuel selector valve off
Mixture ICO
Feather prop
Aux fuel pump off
Ignition off
Alternator off
58
Q

Emergency descent

A
2700RPM
Throttles closed
152kts
Gear down
Flaps 15˚
59
Q

Glide procedure

A

Feather props
Flaps up
Gear up
Cowl flaps closed

60
Q

Glide ratio

A

2NM for every 1000ft @ 120kts

61
Q

OEI landing

A
When assured of reaching field
Gear down
Flap 15˚
90kts
800fpm
When no possibility of go around
Flaps 30˚
62
Q

OEI go around

A
Do not attempt after full flap
Max power
Gear up
Flap 0˚
99kts
63
Q

Crossfeed operation

A

Operating aux fuel pump low
Inoperative fuel selector off
Operating crossfeed
Operating aux fuel pump low/as required

64
Q

Electrical smoke/fire

A
Battery/alternator off
Oxygen as required
All electrical switches off
Battery/alternator on
Essentials on
Isolate defective equipment
Turn off cabin heat
Push in cabin air control
Open storm window if required
65
Q

Unscheduled electric elevator trim

A
Maintain attitude manually
Pitch trim switch in appropriate direction
Pitch trim switch off
Pitch trim CB pull
Retrim manually
66
Q

Spin recovery

A
Control column full forward
Full opposite rudder
Idle power
When spin stopped
Neutral controls
Smooth pullout
67
Q

Landing gear light meanings

A

3 green - down and locked
Red - in transit/intermediate position
Lights out - up and locked

68
Q

Landing gear warning horn meaning

A

Either or both throttles are too low with gear up

If operating OEI can cancel horn by advancing inoperative throttle

69
Q

Where is the brake hydraulic fluid reservoir?

A

In the nose baggage compartment

70
Q

Fail condition of the props if oil pressure is lost?

A

Towards coarse i.e. closer to feather

71
Q

Aux fuel pump use

A

High - stabilising fuel pressure before start and providing max engine performance should an engine driven pump fail (provides more than injector system is capable of accepting so only use if engine driven pump has failed)
Low - for use during ground operation and take off/climb in high temperatures

72
Q

Minimum fuel for take off

A

13USG per side

73
Q

Battery

A

17 amp
24V
Lead acid
Beneath nose baggage compartment

74
Q

Alternator

A

50 amp

24V

75
Q

Oxygen location and nominal pressure for full supply

A

Forward baggage compartment

1850psi for full pressure

76
Q

Gear strut expectation

A

3-4” nose gear

3” main gear