You may prefer our related Brainscape-certified flashcards:
1
Q

Top speed ISA see level

A

99 kts

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2
Q

Cruise speed 1000ft ISA 4000 RPM

A

59 kts

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3
Q

4600 rpm

A

80 kts

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4
Q

4800 rpm

A

84 kts

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5
Q

5000 rpm

A

87 kts

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6
Q

Range - 30 min reserve, 4000 rpm, 1000 ft isa

A

530 nm

981 km

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7
Q

Vx

A

49 kts

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8
Q

Vy

A

53 kts

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9
Q

Vs 600 kg

A

42 kts

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10
Q

Vs0

A

33 kts

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11
Q

Duration max power

A

5 min

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12
Q

Rpm max power

A

5800 rpm

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13
Q

Landing gear psi

A

22.7 psi

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14
Q

Max revs with no time limit

A

5500 rpm

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15
Q

2 fuels

A

95 RON

AVgas 100LL

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16
Q

Max EGT

A

950 C

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17
Q

Minimum idle rpm

A

1400

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18
Q

Max coolant temp

A

120 C

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19
Q

Max oil

A

130 C

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20
Q

Min oil

A

50C

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21
Q

Normal oil pressure above 3500 rpm

A

2 - 5 bar

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22
Q

Type of oil

A

any automotive oil of API classification “SG” or higher

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23
Q

Oil capacity

A

3 L

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24
Q

Wingspan

A

9548 mm

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25
Q

Length

A

6232 mm

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26
Q

Height

A

2476 mm

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27
Q

Fuel lines lead to the…

A

Sediment separator

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28
Q

Sediment separator leads to…

A

Coarse filter

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29
Q

Coarse filter leads to…

A

Main fuel pump

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30
Q

Main fuel pump leads to…

A

Aux fuel pump and

Return valve

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31
Q

Aux fuel pump to …

A

Fine filter

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32
Q

Fine filter to…

A

Pressure sensor and

Rail injectors of cylinders 1 and 3

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33
Q

Rail injectors fuel goes via the

A

Rod

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34
Q

Rail injectors of 1 and 3 goes to

A

Rail injectors of cylinders 3 and 4

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35
Q

Fuel from rail injectors 3 and 4 goes to

A

The pressure regulator

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36
Q

Fuel from pressure regulator goes via the

A

Low pressure fuel return line

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37
Q

Fuel from the pressure regulator goes to the

A

T junction

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38
Q

Fuel ? Are in the fuel caps

A

Vent tubes

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39
Q

Fuel vent tubes are in the

A

Inlet caps

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40
Q

The fuel valves control what

A

Fuel line and return line

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41
Q

Fuel can be drained via the

A

Drain valve

42
Q

Both fuel pumps have capacity of

A

120 L per hour

43
Q

It is/not recommended to have both fuel valves open?

A

Not

44
Q

If both fuel valves are open…

A

Fuel will escape out of the vent tube of one tank

45
Q

If air gets in the fuel line the engine will stop for

A

Several dozen seconds (? A minute)

46
Q

Fuel pressure absolute

A

4.5 bar minimum

47
Q

Fuel pressure relative to intake manifold

A

2.8 to 3.2 bar

48
Q

The elevator control system linkage has two xxxxx and three xxxxxx

A

Bellcranks

Pushrods

49
Q

The rear pushrod is supported by

A

Rollers

50
Q

The elevator is connected to the third pushrod by the xxxxxxx

A

Elevator arm

51
Q

The elevator angles of deflection are

A

Up 25 degrees pm 1 and down 15 deg pm 1

52
Q

The elevator trim is controlled by the

A

Elevator trim control lever

53
Q

The elevator control tab is held in place …

A

By friction… wheel

54
Q

The trim tab cable runs to the ….

A

Trim tab control arm

55
Q

The trim tab cable is in xxxxx at each end

A

Conduit

56
Q

The trim tab control arm runs through two …

A

Fairleads

57
Q

The elevator trim tab is hinged on a

A

Wire acting as a torsion spring

58
Q

The deflection of the elevator trim is ….

A

22 deg pm 1

59
Q

Each pedal shaft is hinged on a …

A

Lower fuselage beam

60
Q

Each pedal shaft has two ….

A

Arms

61
Q

The rudder pedal is attached to the rudder xxxxxx by a yyyyy

A

Control arm

Cable

62
Q

The rudder pedal arms are attached to the nose wheel xxxxx by a yyyyy

A

Control arm

Rod

63
Q

The rudder cables run via xxxxxx on frames yyyyy and zzzzz. They run via a xxxxx on the yyyyy

A

Pulleys
Frames 3 and 4
A fairlead
The pilot seat beam and frame

64
Q

The pedal shaft arms are attached to the cable by

A

Turnbuckles

65
Q

The rudder is deflected xxxx degrees yyyyy in its zzzzz position

A

Three degrees
Right
Neutral

66
Q

The rudder deflection is xxxxx degrees

A

25 pm 1

67
Q

Roll control force is transferred to the

A

Central control shaft

68
Q

The roll-control central controll shaft has NUMBER xxxxx that connect to NUMBER yyyyyy

A

Two
Bellcranks
Two
Control rods

69
Q

Roll control forces go from the push rods to the xxxxx

A

Flaperon control shafts

70
Q

The flaperon control shafts connect laterally to a

A

Cardin joint

71
Q

The flaperon control shafts attach medially to a xxxxx on the aaaaa bbbbb ccccc

A

Trunion
Flap
Control
Rod

72
Q

A aaaaa at the bbbbb end of the ccccc limits the deflection of the flaperons as ailerons

A

Stop
Front
Central control shaft

73
Q

The flaperons maximum deflection is aaaaa degrees up and bbbbb degrees down, as an airleron

A

20 pm 1

13 pm 1

74
Q

The flap lever is connected to the aaaaa by bbbbb.

A

Flap shaft

Arms and linkage

75
Q

The flap lever is held in place by a aaaaa with bbbbb.

A

Stopper block

Three slots

76
Q

The aaaaa of the flap lever goes into the Bbbbb of the stopper block

A

Locking pin

Fixing slot

77
Q

Deflection angles of the flaperons, as flaps is aaaaa

A

First 10 deg pm 1

Second 20 deg pm 1

78
Q

The throttle lever is located

A

Central console

79
Q

The throttle lever moves the

A

Cable

80
Q

The throttle cable is in a

A

Bowden cable sheath

81
Q

The throttle cable moves the

A

Throttle valve arm

82
Q

The throttle valve arm is located

A

Just media to the air filter, and a little to the right of the midline.

83
Q

The throttle cable sheath has an aaaaa at the bbbbb

A

Adjustable stop

Throttle valve housing bracket

84
Q

The throttle valve cable has a aaaaa at bbbbb located ccccc

A

Fixed stop
The throttle lever unit
Low and forward in the centre console

85
Q

The tension in the throttle cable is maintained by the aaaaa, which holds the bbbbb

A

Throttle return spring

Throttle full open

86
Q

The brake master cylinder is attached to X located at Y

A

X extension tank

Y firewall

87
Q

To use the park brake 1 then 2

A

1 park brake on on console

2 press and release the brakes

88
Q

The park brakes are located ….

A

In the wheels

89
Q

The warning lights are for…

A

Lanes A and B.

90
Q

The switches are, L to R

A

Landing lights
Navigation lights
Strobe lights
Intercom

91
Q

The four lower switches, l to r

A

Lane a
Lane b
Fuel pump ?
Fuel pump ?

92
Q

The trim tab indicator is located

A

Between the banks of switches

93
Q

Switches are on if they are X

Which is Y compared to Australian switches

A

Up

Different

94
Q

The emergency power switch is located

A

Above and between the fuel gauges

95
Q

The static pressure opening is located

A

Below the pitot tube

96
Q

Preflight for pitot tube

A

Remove the cover
Inspect both openings
Inspect tubes

97
Q

The battery switch is located X

And is switched off when Y

A

Under pilots seat

End of the day (flight)

98
Q

Master switch does not supply (3)

A

Engine, battery and extra stuff

99
Q

Emergency power switch switches on

A

Emergency power when neither generator is working (? How different to the master switch)

100
Q

Vine

A

124 kt

100
Q

Va

Max maneuvering speed

A

Va 101 kts

101
Q

Ve

Flap extension speed

A

Ve flap extension speed 80 kts