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
Max oil temperature
240˚F
26
Min take off oil temperature
75˚F
27
Normal oil pressure range
30-100psi
28
Starter operation limits
Do not operate starter continuously for more than 30 seconds
29
Max g load clean
4.2g
30
Max g load dirty
2g
31
Vx
86kts
32
Vy
101kts
33
Vx OEI
96kts
34
Minimum Voei intentional
84kts
35
Vcruise climb
130kts
36
Vga climb
88kts
37
Vapp
88kts
38
Vapp flapless
96kts
39
Vb
156kts
40
Max demonstrated xwc
22kts
41
Start procedure
``` Throttle 1/2" Props full fine Mixture rich Aux fuel pump high until pressure stabilises Engage starter ```
42
After start checks
@ 1000-1200RPM Oil pressure 25psi within 30 seconds Alternator on T's and P's check
43
Run ups/Before take off checks
``` 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
Max performance climb procedure
Full throttle & 2700RPM Mixture lean to appropriate fuel flow Cowl flaps open 101kts
45
Cruise climb procedure
25" & 2500RPM Mixture lean to appropriate fuel flow Cowl flaps as required to maintain temperature 130kts
46
Various cruise procedures
``` Max - 24.5" & 2500RPM Recommended - 24" or 21" & 2300RPM Economy - 20.5" & 2100RPM Lean as required Cowl flaps as required ```
47
Leaning procedure
Lean until temperature peaks then starts to decrease Richen until 25˚ rich of peak For best power richen until 100˚ rich of peak
48
Descent procedure
``` Set altimeter Cowl flaps closed Windshield defroster as required Power as required (avoid prolonged idling and low CHT) Recommended smooth 170kts ```
49
Before landing procedure
``` 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
Go around procedure
``` Pitch fine Power max 88kts Flaps 0˚ Gear up Cowl flaps as required ```
51
After landing procedure
``` Lights as required Flaps up Trim reset Cowl flaps open Aux fuel pumps as required ```
52
Shutdown procedure
``` 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
EF during take off
Throttles closed | Max braking
54
EFATO/during flight
``` 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
Securing engine procedure
``` Mixture ICO Fuel selector off Aux fuel pump off Ignition off Alternator off Cowl flap closed ```
56
Engine fire on the ground
``` Mixture ICO Crank Fuel selector valves off Battery/alternator off Use fire extinguisher ```
57
Engine fire in flight
``` Fuel selector valve off Mixture ICO Feather prop Aux fuel pump off Ignition off Alternator off ```
58
Emergency descent
``` 2700RPM Throttles closed 152kts Gear down Flaps 15˚ ```
59
Glide procedure
Feather props Flaps up Gear up Cowl flaps closed
60
Glide ratio
2NM for every 1000ft @ 120kts
61
OEI landing
``` When assured of reaching field Gear down Flap 15˚ 90kts 800fpm When no possibility of go around Flaps 30˚ ```
62
OEI go around
``` Do not attempt after full flap Max power Gear up Flap 0˚ 99kts ```
63
Crossfeed operation
Operating aux fuel pump low Inoperative fuel selector off Operating crossfeed Operating aux fuel pump low/as required
64
Electrical smoke/fire
``` 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
Unscheduled electric elevator trim
``` Maintain attitude manually Pitch trim switch in appropriate direction Pitch trim switch off Pitch trim CB pull Retrim manually ```
66
Spin recovery
``` Control column full forward Full opposite rudder Idle power When spin stopped Neutral controls Smooth pullout ```
67
Landing gear light meanings
3 green - down and locked Red - in transit/intermediate position Lights out - up and locked
68
Landing gear warning horn meaning
Either or both throttles are too low with gear up | If operating OEI can cancel horn by advancing inoperative throttle
69
Where is the brake hydraulic fluid reservoir?
In the nose baggage compartment
70
Fail condition of the props if oil pressure is lost?
Towards coarse i.e. closer to feather
71
Aux fuel pump use
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
Minimum fuel for take off
13USG per side
73
Battery
17 amp 24V Lead acid Beneath nose baggage compartment
74
Alternator
50 amp | 24V
75
Oxygen location and nominal pressure for full supply
Forward baggage compartment | 1850psi for full pressure
76
Gear strut expectation
3-4" nose gear | 3" main gear