Ground School Flashcards

(47 cards)

1
Q

What are bold face drills

A

Actions to be performed immediately

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2
Q

What is as required

A

Pliot required to state condition, setting or reading of the system

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3
Q

What is land as soon as practicable

A

Land at nearest airfield safely and expect practical assistance for your ac type

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4
Q

Land as soon as possible

A

Land at the nearest suitable airfield and be prepared to force Land immediately

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5
Q

What are cautions

A

If not observed may result in damage to ac or its equipment

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6
Q

What are warnings

A

If not observeday result in injury, loss of life or loss of aircraft

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7
Q

What is max take off weight

A

Aerobatic 1440kg
Utility 1515kg

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8
Q

What is Vo

A

Max manoeuvre speed
Aerobatic 164kts
Utility 143 kts

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9
Q

What is VLOE

A

Max speed for landing gear operation
182 kts

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10
Q

What is VLE

A

Max speed with landing gear extended
182kts

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11
Q

What is VLOR

A

Max speed for landing gear operation during retraction
137kts

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12
Q

What is VFE

A

Max speed with flaps extended
114 kts

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13
Q

What is VFE-T/O

A

Max speed with flaps in take off position
151kts

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14
Q

What is VMO

A

Max operating speed
238kts
Mmo is max mach no which is 0.45

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15
Q

What is N1

A

Speed of engine
Measured as a percentage

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16
Q

What is N2

A

Speed of propellor

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17
Q

What is TOT

A

Turbine Outlet Tenperature

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18
Q

What is the usable fuel capacity

A

275kg

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19
Q

Max crosswind at takeoff

20
Q

Climb speed up to 50ft

21
Q

What is best rate of climb speed

22
Q

What is final approach and landing speed

23
Q

Elevator

A

Longitudinal control but lateral axis
Pull back moves elevator up reduces lift and so tail drops

24
Q

Aileron

A

Lateral control but longitudinal axis
When column moved left the left aileron goes up creating less lift and banking ac left

25
Rudder
Yaw control about the normal axis When left rudder pedal pushed the rudder moves left creating more lift and pushing nose left
26
Flaps
Have take off, land and full setting Increase lift for low speeds but increase drag
27
Components of the electrical system
Battery External power connector Starter/ generator Busbar
28
Battery
24V - 28Ah Used to Start engine when external power not available
29
What are the 5 busbars
Hot battery bus (vital) Battery bus Main bus Avionics bus 1 Avionics bus 2
30
Where is each busbar CBs located
Battery bus (essential) - right bottom row and second half of top row, and inbetween MFD Main bus (non essential) - left side bottom row Avionic bus 1 - first half of top right row and 2 on top left Avionics bus 2 - top left row
31
How can battery operation be started
Battery power or external power
32
When does VOLT warning appear
29V
33
Where is lighting switches located
Left side
34
What are the different external lights
Anti collision strobe lights Navigation lights Combined taxy and landing lights Gear down light
35
What fuels does prefect use
AVTUR (black and white) F24, F35 and F34 AVTAG (black and green, AVGAS and AVTUR) F40 AVCAT (black and yellow) F44
36
Where are the fuel switches
Middle left
37
What positions can the fuel selector valve be
Left - fuel from collector tank Off - no fuel can pass Emergency transfer - fuel from RH tank
38
Explain the fuel system
Fuel is taken from LH tank to collector tank by 2 jet pumps A flop tube take fuel from collector tank to the engine via the main pump to a filter and then a de aerator
39
Fuel specifications
Collector tank capacity is 16.8kg Max usable capacity is 275kg Max inbalance is 45kg
40
Warnings
F LOW LEVEL - collector tank below half F PRESS - under 12psi so stby pump on
41
What does the power lever do
Black, control turbine from 58% N1 to max power
42
What is the condition lever
Red one, starts and stops the engine and feathers the prop
43
What are the engine indications
N1 - engine rpm in %RPM, max is 105% N2 - propellor rpm, max 2130 rom Turbine outlet temperature TOT Torque TO - in percentage Oil pressure - low is 35 to 90 psi and max is 130/150 Oil temp - high is 82 to 107
44
What is included in the engine ignition system
Electrical power supply Ignition exciter unit Spark igniter Spark igniter lead Electrical switches
45
Where are the icing controls
Left of top right switches
46
Where are the venting controls
2 switches on far right Ventilation lever on far left Bleed air knob In middle
47
When does the following malfunctions show LOW OIL PRESSURE INTAKE HEAT FAIL BLEED TEMP ENGINE POWER EXCEEDANCE OIL CHIP BETA
LOW OIL PRESSURE - below 35psi INTAKE HEAT FAIL - anti icing not working BLEED TEMP - too high ENGINE POWER EXCEEDANCE - 111% TRQ or 899°C OIL CHIP - metal particle detected BETA - prop in negative pitch so in reverse