Ground School Flashcards
What are bold face drills
Actions to be performed immediately
What is as required
Pliot required to state condition, setting or reading of the system
What is land as soon as practicable
Land at nearest airfield safely and expect practical assistance for your ac type
Land as soon as possible
Land at the nearest suitable airfield and be prepared to force Land immediately
What are cautions
If not observed may result in damage to ac or its equipment
What are warnings
If not observeday result in injury, loss of life or loss of aircraft
What is max take off weight
Aerobatic 1440kg
Utility 1515kg
What is Vo
Max manoeuvre speed
Aerobatic 164kts
Utility 143 kts
What is VLOE
Max speed for landing gear operation
182 kts
What is VLE
Max speed with landing gear extended
182kts
What is VLOR
Max speed for landing gear operation during retraction
137kts
What is VFE
Max speed with flaps extended
114 kts
What is VFE-T/O
Max speed with flaps in take off position
151kts
What is VMO
Max operating speed
238kts
Mmo is max mach no which is 0.45
What is N1
Speed of engine
Measured as a percentage
What is N2
Speed of propellor
What is TOT
Turbine Outlet Tenperature
What is the usable fuel capacity
275kg
Max crosswind at takeoff
25kts
Climb speed up to 50ft
78kts
What is best rate of climb speed
116kts
What is final approach and landing speed
85 kts
Elevator
Longitudinal control but lateral axis
Pull back moves elevator up reduces lift and so tail drops
Aileron
Lateral control but longitudinal axis
When column moved left the left aileron goes up creating less lift and banking ac left
Rudder
Yaw control about the normal axis
When left rudder pedal pushed the rudder moves left creating more lift and pushing nose left
Flaps
Have take off, land and full setting
Increase lift for low speeds but increase drag
Components of the electrical system
Battery
External power connector
Starter/ generator
Busbar
Battery
24V - 28Ah
Used to Start engine when external power not available
What are the 5 busbars
Hot battery bus (vital)
Battery bus
Main bus
Avionics bus 1
Avionics bus 2
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
How can battery operation be started
Battery power or external power
When does VOLT warning appear
29V
Where is lighting switches located
Left side
What are the different external lights
Anti collision strobe lights
Navigation lights
Combined taxy and landing lights
Gear down light
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
Where are the fuel switches
Middle left
What positions can the fuel selector valve be
Left - fuel from collector tank
Off - no fuel can pass
Emergency transfer - fuel from RH tank
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
Fuel specifications
Collector tank capacity is 16.8kg
Max usable capacity is 275kg
Max inbalance is 45kg
Warnings
F LOW LEVEL - collector tank below half
F PRESS - under 12psi so stby pump on
What does the power lever do
Black, control turbine from 58% N1 to max power
What is the condition lever
Red one, starts and stops the engine and feathers the prop
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
What is included in the engine ignition system
Electrical power supply
Ignition exciter unit
Spark igniter
Spark igniter lead
Electrical switches
Where are the icing controls
Left of top right switches
Where are the venting controls
2 switches on far right
Ventilation lever on far left
Bleed air knob In middle
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
