PPL Oral - Aircraft Systems (General & Specific to DA 40NG) Flashcards
Objective: To obtain an in depth understanding of how aircraft systems work generally, with a heavy focus on the DA40 NG (229 cards)
1
Q
What are the 3 primary flight control surfaces and what do they do?
A
- Ailerons (Roll about the longitudinal axis)
- Elevator (Pitch about the lateral axis)
- Rudder (Yaw about the vertical axis)
2
Q
What is Trim and what is it for?
A
- Small, adjustable, hinged surfaces on the aileron, rudder, or elevator (most common).
- Used for fine tuning of controls to relieve pressure on the controls to maintain a specific AIRSPEED.
3
Q
What flight controls are operated via Cable connections on the DA 40NG?
A
- Rudder
- Pitch Trim Tab
4
Q
What flight controls are operated via Pushrod connections on the DA 40NG?
A
- Ailerons
- Elevator
- Flaps (electronic)
5
Q
How are the flaps operated on the DA 40NG?
A
Electronically actuated, mechanically interconnected pushrods
6
Q
What are flaps and what are they for?
A
- Lift generating devices that increase lift by extending the chord line of the wing, thereby increasing AOA. Flaps are moveable panels on the inboard trailing edge of the wings
- When lowered, they increase lift and drag, enabling us to make a steeper descent without a large increase in airspeed
7
Q
What type of landing gear does the DA 40NG have?
A
1.Fixed Tricycle gear
2. Steel spring strut Main Gear
3. Free-castering Nose Wheel
8
Q
Describe the Break System diagram for the DA 40NG.
A
DRAW IT OUT!
(at least do so in your head)
9
Q
How does the breaking action occur on the DA 40NG?
A
Hydraulic fluid provides pressure to break disks and pads which squeez the wheel and the resutling friction causes the plane to stop.
10
Q
If it can be said that the right seat breaks work, what conclusion can be made about the left seat breaks and why?
In the DA40 NG
A
- If the Right seat breaks work then you know the Left seat breaks work also.
- This is because the the breaks lines run from the Left THROUGH the right. (The left seat breaks are connected to the rest of the system through the right seat breaks)
11
Q
What effect on performance does NOT having Wheel Fairings installed on the DA 40NG have?
A
- It increases drag and reduces our True Airspeed by 4%
- It decreases our glide distance
12
Q
Normally, what color is Hydraulic fluid?
A
Red or pinkish
13
Q
How do you steer the DA 40NG on the ground?
A
- Differential toe breaking at low speeds.
- Rudder at high speeds
14
Q
What are the specific things you need to know a about the DA 40NG engine?
There are 11 total, get at least 8.
A
- NAME: Austro E4-A
- 165 Horsepower
- Four Cylinder
- Inline
- Common Rail Direct Fuel Injection
- Dual Digital Engine Control (2 ECUs)
- Vibration damper isolates engine from prop
- Its Turbo Charged
- Liquid cooled
- It has glow plugs instead of spark plugs
- Gearbox equipped. Ratio = 1:1.69
Get at least 7 of theses correct
15
Q
How long can you set the power to 100% in the DA 40NG?
A
5 mins max.
16
Q
What is Max continuous power (generally and specifically)
A
- The power setting at which the engine is designed to operate continuously
- It is 92% (2100 RPM) in the DA 40NG
17
Q
What are the four cycles of an internal combustion engine?
A
- Intake (air and fuel)
- Compression
- Ignition/combustion (power stroke)
- Exhaust
18
Q
How does combustion happen in the DA 40NG?
A
Combustions occurs by high compression in the cylinders
19
Q
What is unique about the Austro E4-A compared to most GA aircraft?
A
- Its a Turbo-Diesel
- Its liquid cooled
- It uses Jet fuel
20
Q
What does a Carburetor do?
A
Ads fuel to the air intake, providing the fuel/air mixture needed to induce combustion
21
Q
How does Carburetor heat work?
A
Opening the Carb Heat valve allows hot, unfiltered air from around the engine to enter the air intake just before running through the Carburetor
22
Q
What effect will Carb Heat have on your engine?
A
Carb Heat will result in a loss of engine power (up to 15%) due to the fact that warm air is less dense than cool air.
23
Q
What does the Throttle do in the DA 40NG?
A
Adjusts engine power/load through…
- Mixture
- Prop pitch
- RPM
All done automatically through the ECUs
24
Q
What does Mixture control do?
The DA40 NG does not have a mixture control knob
A
Regulates the fuel to air ratio
DA 40 NG: The fuel/air mixture is controlled automatically by the ECUs
25
What is a lean Mixture?
Less fuel is being introduced into the engine
26
What is a Rich Mixture?
More fuel is being introduced into the engine
27
Why, if unchanged, will the mixture become too rich at higher altitudes?
Because air is less dense at higher altitudes, resulting in an excessively rich mixture.
28
What are Glow Plugs?
1. Devices used to heat up the cylinder in a diesel engine to a point at which combustion can freely occur
29
What are the advantages of having Magnetos AND multiple Spark Plugs per cylinder?
1. Increased safety, redundancy in case of failure
2. More complete and even combustion will improve performance
30
What type of fuel system does the DA 40NG have?
Electrical and engine powered fuel pump common rail injection system
31
Describe the Fuel Schematic for the DA 40NG
DRAW IT OUT!
(at least in your head)
32
How fast does the fuel flow through our fuel lines in the following scenarios?
1. Fuel Pump switch set to ON
2. Fuel Pumps Off
1. Fuel Pumps on = 60-63 gal PER HOUR (up to 71gph according to the diamond slideshow)
2. Fuel Pumps Off = 45 gal PER HOUR
33
Approximately how fast does our Fuel Transfer Pump transfer fuel between tanks?
At about 1gal PER MIN or 60 gal per hour
34
When the Fuel Selector Valve is on Normal, which fuel tank is the engine running on?
The left wing tank
35
How many fuel pumps does our aircraft have?
There are 4:
1. High pressure engine driven fuel pump
2. ECU A fuel pump
3. ECU B fuel pump
4. Fuel Transfer Pump
36
Will you be able to transfer fuel from the Right tank to the Left (main tank) tank if the Fuel Transfer Pump is broken?
Yes
1. By turning the fuel selector valve to Emergency
2. Now the engine will draw fuel from the Right tank and the excess will flow into the Left tank
37
Which tank is our Main fuel Tank?
The Left wing fuel tank
38
What happens when the fuel selector valve is switched to Emergency?
1. Engine will use fuel from the Right tank
2. Excess fuel gets dumped into the Left tank and will overflow eventually
39
How much fuel can each tank hold?
19.5 gal
40
What is our max indicated fuel?
28 gal total, 14 gal per tank
41
What is our max Usable Fuel?
39 gal
42
What is our full fuel amount?
41 gal (39 usable)
43
What is the maximum fuel imballance?
9 gal
44
When the Right tank is full, how will you know when you have reached the maximum fuel imbalance?
At about 11 gal indicated in the Left tank
45
How long will the main battery last if your alternator fails?
1. 30 mins at most
BUT
2. There is NO guarantee because the battery may be old
*After the Main Battery is drained, the engine will be powered by the ECU backup batteries.
46
How long will the Backup ECU batteries last?
About 30 mins
47
How long will the Emergency Battery last
About 1.5hrs
48
What happens if you leave the Fuel Transfer Pump on indefinitely?
It will eventually stop once the Left tank becomes full at 19.5 gal.
49
What happens to the Fuel Return when the Fuel Selector is in the Emergency Position?
1. It will continue to transfer fuel to the Left tank through the return line
2. The Left tank will eventually fill and start to overflow through the fuel dump
50
Since our max indicated fuel per tank is 14gal, what must we do to determine the actual amount of fuel in each tank?
You must use the fuel quantity measuring device and the AFM to find the exact fuel available.
51
What is especially unique about the Austro E4-A engine?
Its a Turbo-Diesel
52
What color is Jet fuel?
Clear to straw colored
53
What position must the rear door be in when flying?
Unlocked
54
Above what RPM is considered Propeller Overspeed?
Above 2300 RPM
55
What happens if you move the throttle to full too quickly?
You risk Propeller Overspeed
56
What is the max and min oil Quantity ?
7L = Max
5L = Min
57
What kind of Oil can we use?
1. 5W-30
2. 5W-40
3. OW-40
58
Will your engine run/start if its accidentally fueled with AvGas?
NO
59
What powers our standby Attitude Gyro?
It is electrically powered
60
Describe our Propeller
1. NAME: MTV-6
2. 3 blade
4. Constant Speed
5. Hydraulically operated
6. Wooden (composite) with plastic coating and metal edge
7. Coated with PU tape near the hub
*They are made this way because they provide the lowest weight, while minimizing vibration
61
What controls the pitch of the propeller?
1. The ECUs via the prop governor
How?
2. Via an electro-mechanical actuator
62
What type of engine lubricating system does our engine have?
Wet Sump
63
What is a Wet Sump oil system vs a Dry Sump oil system for oil?
Wet Sump system = Oil sits in a drain pan
Dry Sump System = Oil sits in a reservoir
64
What purposes does oil serve for an engine?
1. Lubrication
2. Cooling
3. Prevents corrosion
4. Cleans out contaminants
5. Seals parts of the engine
65
What are some secondary flight controls?
1. Trim
2. Flaps
3. Spoilers & Slats
66
Why do we sump fuel?
To look for...
1. Water
2. Dirt
3. Improper fuel
67
If the Alternator fails, will our Engine fail as well?
Yes
- After the Main Battery and ECU backup batteries are depleted
68
What are the 4 main components of an electrical system?
1. Sources (alternator, battery)
2. Distribution (buses)
3. Consumers (electronics)
4. Storage (batteries)
69
How many batteries does our aircraft have?
5 in total:
1. Main battery (24v 13.6A)
2. ECU A Backup battery (12V 7.2A )
3. ECU B Backup battery (12V 7.2A)
4. Emergency battery (30v)
5. ELT battery (6v)
70
# s
What is the Voltage/Amps of all 5 batteries on our aircraft?
1. Main Battery - 24V, 13.6A
2. ECU A Backup battery - 12V, 7.2A
3. ECU B Backup battery - 12V, 7.2A
4. Emergency Battery - 30V (Three 10v batteries)
5. ELT Battery - 6V
71
How many Volts and Amps is our Alternator?
28v
70A
72
If the Left (main) fuel tank becomes unusable and you have to switch the Selector to Emergency, what happens to your fuel flow?
Fuel flow will increase dramatically to about 60 gal per hour (with fuel pumps switched on), or 45 gal per hour (fuel pumps off).
So if you had 15 gal in the R tank, you will only have 15 mins of fuel remaining.
| Pumps On: Up to 71gph according to the Diamond Systems slideshow
73
How many Volts and Amps is our Main Battery?
24v
13.6A
74
If your Alternator fails, what will power your aircraft next, and how long will that last?
1. The Main battery (24v 13.6A) MIGHT last 30 mins
2. ECU backup batteries will last 30 mins
75
If your Alternator fails and your Main Battery is emptied, how will the engine be powered and for how long?
The ECU Backup Batteries will power ECU B, keeping your engine running for another 30 mins
76
What is the DA 40NG Gearbox reduction ratio?
1:1.69
| Prop: 1 rotation
Engine: Rotates 1.69 times
77
What exactly does the Gearbox do and why?
1. It ensures that the Prop is at a lower RPM than the engine
2. This is because automotive engines run at higher RPMs than a Propeller can be efficient at, thereby necessitating the need for an RPM reducer for the propeller.
78
Where does our prop governor get its oil from?
It uses Gearbox oil
79
What will happen if your ECU B Backup battery fails?
ECU A Backup Battery and ECU A will also fail because they are wired in series (together) with ECU Backup Battery B
80
What will turning on the Essential Bus do?
1. Eliminate all unnecessary electrical equipment to increase battery life
2. Everything NOT on the Essential Bus circuit breaker will be INOP.
81
What does a BUS do?
It distributes power to the electrical components
82
What are the 4 divisions of an Electrical System?
1. Power Generation
2. Storage
3. Distribution
4. Consumers
83
How many BUS's do we have and what are they?
We have 7:
1. Hot Battery BUS
2. Battery BUS 1
3. Battery BUS 2
4. ECU BUS
5. Main BUS
6. Essential BUS
7. Avionic BUS
84
What does the Hot Battery Bus do?
Distributes power to the...
1. Accessory plug
2. ELT
85
How is our electrical equipment protected from circuit overload?
Via the Circuit Brakers
86
What does the Ammeter do?
It displays..
1. The current/Amps being supplied to electrical equipment by the Alternator
2. The electrical load being placed on the alternator for either Consumers or to recharge the battery
87
What does the Voltmeter do?
It Indicates the Voltage of the Alternator under normal conditions, otherwise it shows the voltage of the battery.
1. When the engine is not running it will read just over 24v, which is the voltage of the battery. (25.1v)
2. When the engine is running it should read 28v (voltage of our alternator)
88
Why is the Alternator voltage (28v) higher than the Main Battery voltage (24v)?
Because the Alternator is intended to keep the Main Battery Charged
89
How does the DA 40NG Cabin Heat work?
Air around the Cabin Heat Exchanger heats up from hot coolant and is routed into the cabin
90
What kind of deicing and anti-icing equipment does the DA 40NG have?
1. Pitot Heat (anti icing)
2. Cabin Heat window defrost (deicing)
2. Alternate Air
91
Describe how our Cooling system works
DRAW IT OUT!
(at least in your head)
92
When does the Thermostat open on our aircraft and what happens?
1. When the engine Temp reaches 80c
2. Coolant now gets routed through the Radiator
93
What Causes Carburetor icing?
Humid air expands rapidly (due to the venturi effect) near the throttle valve, causing a drop in temperature, this leads to the water vapor condensing and if its cold enough it will turn to ice around the throttle valve.
94
What is the first indication of Carburetor icing?
Fixed Pitch Prop = A loss of RPM
Constant Speed Prop = Loss of Manifold pressure
95
In an aircraft that is Carburated (not fuel injected) How can you confirm if Carburetor Ice is present?
1. Turn on Carb Heat
2. RPM/Man Pres will drop further due to the air being warmed
3. If your RPM/Man Pres INCREASES then you have carburetor ice!
96
What are favorable conditions for Carburetor Icing?
Mostly likely to occur..
1. Below 21c
2. Relative humidity above 80%
BUT carb ice can occur in much warmer and dryer conditions than these
97
What is Anti-Icing and Deicing equipment?
Anti-Ice = Prevents ice from forming
- Pitot Heat
- Carb Heat
- Windshield defrost
Deicing = Removes existing ice
- Inflatable wing boots
98
What is Detonation
Uncontrolled ignition of the Fuel/Air mixture
99
What causes Detonation?
Anything that can cause the Cylinders to overheat!
1. Using a lower fuel grade than recommended
2. Operating at high Manifold Pressure and Low RPM settings
3. Operating at high power settings with too Lean of a mixture
4. Extended taxis
5. Steep climbs where air cooling is reduced and power settings are high
*get at least 3 of these right
100
If you suspect Detonation is occurring in your engine, what should you do?
1. Climb slower and Enrich your mixture
2. Avoid steep, high power climbs
101
What is Preignition?
When the Fuel/Air mixture is ignited too EARLY
102
Why is Preignition bad?
Because it causes ignition to happen while the piston head is at or near the top of its cycle, which will create too much pressure in the cylinder.
103
What causes Preignition?
Can be caused by..
1. Carbon deposits creating a hot spot
2. Cracks in the spark plug
104
What should you do if you suspect you are experiencing Preignition?
1. Reduce power
2. Reduce climb for betting air cooling
3. Enrich the mixture to cool down the cylinder
105
What does it mean if your Ammeter reads zero?
1. Inflight - Your Alternator has died. Congrats and don't panic but your engine will die once the batteries run dry (DA40 NG)
2. Ground - This is normal and just means that the aircraft is using the battery instead of the alternator
106
What type of Ammeter do we have?
| DA40 NG
A Left-Zero Ammeter
107
What instruments use the Pitot Static System?
1. Airspeed Indicator
2. Altimeter
3. Vertical Speed Indicator (VSI)
4. ADC
108
What could be suspected if your Oil Pressure is low, but your Oil Temperature is normal?
1. Insufficient or loss of Oil
2. Clogged Oil system
109
How does an Airspeed Indicator work?
1. Dynamic Pressure (ram air) is fed to the Diaphram in the Airspeed Indicator from the Pitot Tube and Static Pressure is fed to the Airspeed Indicator chamber through the Static Port. The Diaphram inflates and deflates as Dynamic Pressure increases or decreases.
2. The Diaphram is connected to the Airspeed Indicator needle through a series of gears and linkages.
110
What are the elements of a Pitot Tube?
1. The Tube itself
2. The drain hole
3. The heating element
111
What are the 3 kinds of pressure that the Pitot-Static System rely on?
1. Dynamic Pressure (ram air) from the pitot tube
2. Static Pressure (weight of the atmosphere) from the static port or drain hole in the pitot tube
3. Total Pressure - total of Dynamic and static pressure as read by the Pitot-Tube
112
What type of Pressure decreases with altitude?
Static Pressure (weight of the atmosphere)
- The higher you go the less atmosphere there is on top of you
113
What will happen to our instrument readings if the Static Port becomes blocked?
Airpspeed indictor will act as a reverse Altimeter
* Airspeed will read higher in a climb, and lower in a descent
Altimeter will freeze at the blockage altitude
VSI will temporarily read a climb
114
Why does the Airspeed Indicator need to be connected to both the Pitot Tube and the Static Port?
1. To get Airspeed readings we need Dynamic Pressure (ram air)
BUT
2. The Pitot Tube reads both Dynamic and Static Pressure (total pressure)
3. So the Static pressure is fed to the Airspeed Indicator chamber surrounding the Pitot Tube fed to the Diaphram, thereby subtracting Static Pressure from Total pressure to isolate Dynamic Pressure (ram air)
115
How does an Altimeter work?
1. An Aneroid Wafer that is sealed at 29.92Hg pressure expands and contracts based on the Static Pressure readings that surround the Wafer. The static air is provided to the Altimeter Chamber via the Static Port.
2. When the Static Pressure (atmospheric pressure) is low, the Aneroid Wafer will will expand causing the gears and linkages to move the needle
116
How do you know if the Pitot Heat is working?
| DA40 NG
Amps will increase when we turn Pitot Heat on
117
How does the VSI work?
1. An Aneroid Wafer is connected to the full-flow-instant Static Pressure line that will instantly respond to changes in pressure
2. There is a Calibrated Pressure Leak line connected to the VSI chamber where Static Pressure changes more slowly than inside the Aneroid Wafer
118
What will happen if the main Pitot Tube port is clogged?
EFFECT:
1. Only the Airspeed Indicator will be effected
CAUSE:
2. Now the Altimeter is only recieving static pressure to the Diaphram.
3. Pressure in the Diaphram and the Chamber are now both reading Static Pressure equally & cancel eachother out
RESULT:
4. Airspeed Indicator now reads ZERO
119
What will happen if both the Pitot Tube and its Drain hole become clogged?
EFFECT:
1. Airspeed Indicator will read like an altimeter
CAUSE:
2. Total Pressure is now trapped in the Diaphram & remains unchanged
3. Only Static Atmospheric Pressure in the chamber is allowed to change
RESULT
4. Airspeed indicator will be FROZEN at the failure speed IF altitude is unchanged
5. Airspeed indicator will now act like an Altimeter
6 Climbing will show an increase in speed, Descending will show a decrease in speed. (this is the opposite of what we would normally expect).
120
What will happen if only the Static Port becomes clogged?
EFFECT:
1. Altimeter will freeze where the failure occurred
2. VSI will now always show zero
3. It will be hard to detect an Airspeed change..
CAUSE:
1. Altimeter freezes because the Static Pressure is clogged in the chamber and the Aneroid Wafer is constantly set to 29.92 Hg
2. VSI will now always show zero because the Static Pressure remains unchanged in the wafer
3. The Airspeed Indicator will appear to be working but will actually be inaccurate. This will be hard to detect at first.
RESULT:
1. Altimeter is frozen and will not change
2. VSI will read zero
3. Airspeed Indicator will only read accurately only at the failure altitude. Otherwise it will behave as a Reverse Altimeter. Above the failure altitude it will read LOWER than actual, below, it will read HIGHER than actual. The farther away you get from the failure altitude the more inaccurate the Airspeed
121
Which instruments rely on only the Static System?
1. Altimeter
2. VSI
## Footnote
Airspeed indicator also relies on the Static Ports, but not soley
122
Which instruments rely on the Pitot Tube?
Only the Airspeed Indicator
123
If your altimeter setting is 30.14 and your destination altimeter setting is 29.84 and you FAIL to change your altimeter setting, what will happen to your Altimeter?
1. It will read HIGHER than you actually are. In other words you will really be at a lower altitude than you think you are.
2. "From high to low (pressure), look out below!"
124
If you fly from a Hot area to a Cold area without changing your altimeter setting, what will happen to your Altimeter?
1. It will read Higher than you actually are.
2. "From Hot to Cold, look out below!"
125
What is Pressure Altitude and how can you determine it?
1. Is the height above the Standard Datum Plane. Its the Altitude corrected for Non-Standard Pressure.
We can find it by...
1. 29.92-current altimeter setting X 1000 and adding the positive or negative value to our Field Elevation
2. Set the Altimeter to ISA, 29.92 and read what altitude shows, this will be Pressure Altitude.
126
What is Density Altitude and how can we find it?
1. Density Altitude is Pressure Altitude corrected for non-standard Temperature.
- It effects the aircrafts performance in all areas
- As Density Altitude increases, performance decreases
2. We find it by using our flight computers to correct Pressure Altitude for Non-Standard temperatures
127
What is Absolute Altitude?
Hight above the ground (AGL)
128
What is True Altitude?
True altitude is the height above Seal Level (MSL)
129
How does the Altimeter work?
By sensing a pressure change between an Aneroid Wafer set constantly to 29.92Hg, and the chamber which is set to changing Static Pressure (atmospheric)
130
How does an Airspeed Indicator work
By sensing Dynamic Pressure (ram air) from the Pitot Tube.
This is done by..
1. Total pressure from Pitot Tube is sent to the Aneroid Wafer and Static Pressure is subtracted form Total Pressure by adding it to the surrounding chamber.
2. The result is that we are left with a Dynamic Pressure reading (ram air).
131
What errors may exist with an Airspeed Indicator?
1. Position Error - Static Port readings may be disrupted by slipstream around the aircraft depending on airspeed, altitude, or configuration
2. Density Error - Changes in Altitude and Temperature are not corrected for by the Static Port
3. Compressibility Error - Air gets packed into the Static Port when at higher airspeeds, resulting in higher than normal Airspeed readings
132
What are the different types of speed?
1. Indicated Airspeed - The speed read directly from the Airspeed Indicated
2. Calibrated Airspeed (CAS) - Indicated Airspeed corrected for Installation and Instrument error.
3. True Airspeed - CAS corrected for Non-Standard temperature and pressure Altitude (the speed the aircraft actually moves through the air)
- True airspeed increases as altitude increases. This is due to the fact that the air is less dense and therefore more air particles are needed to flow through the Pitot Tube to maintain a particular IAS.
4. Groundspeed - The speed that the aircraft physically moves over the ground.
** It is TAS adjusted for wind.
133
How does the VSI work?
1. The Vertical Speed Indicator works by receiving Static Pressure data from the Static Port into an Diaphram and a Calibrated leak in the chamber
2. The instant Static Pressure in the Diaphram changes against the slowly changing Calibrated pressure Leak in the chamber
134
What are the limitations of the VSI?
1. A 6 to 9 second lag is required to equalize or stabilize the pressure recorded by the Static Port after movement begins
2. Turbulent air can cause erroneous VSI readings due to the sudden changes in airflow over the Static Port
135
What instruments contain Gyroscopes?
1. Attitude Gyro
2. Horizontal Situation Indicator (HSI)
3. Turn Coordinator
136
What are the 2 fundamental properties of a Gyroscope?
1. Rigidity in Space - The tendency for a spinning object to remain on the plane in which it is spinning (vertical spinning wheel)
2. Gyroscopic Precession - A force applied to a rotating plane is felt 90 degrees in the plane of rotation
137
How is the rotation for a Gyroscope powered?
They can be powered by..
1. Vacuum pressure
2. Electronic
138
How does the G1000 get its instrument readings?
Through both the...
1. AHRS (Attitude & Heading Reference System)
2. ADC (Air Data Computer)
139
Which G1000 instruments use AHRS and would be effected in a complete AHRS failure?
1. Attitude indicator
2. Heading information (HSI)
140
What G1000 instruments use the ADC and would be effected in a complete ADC failure?
1. Airspeed
2. Altimeter
3. VSI
4. TAS
5. OAT
141
What are the limitations of a traditional Attitude Indicator?
If the pitch and bank limits are exceeded it may cause the instrument to start tumbling
142
How does the AHRS system work?
It works by using a IMU (Inertial Measurement Unit) that contains Silicon..
1. Gyroscopes
2. Accelerometers
3. Magnetometers
143
How does the ADC work?
It uses a *Transducer *to convert Pitot-Static data into digital information signal that is used on the G1000
It also provides:
* TAS
* GS
* OAT
144
How does the Magnetic Compass work?
A magnetized and cardinally labeled device floats inside of a case filled with Kerosene
145
What errors does a Magnetic Compass have?
1. Oscillation error
2. Deviation error
3. Variation error
(Do Mona acronym)
DIP ERRORs
4. Acceleration/Deceleration error (ANDS)
5. Northerly Turning error (UNOS)
146
What is Magnetic Compass Oscillation error?
Erratic movement of the aircraft caused by turbulence or drastic control inputs cause the compass to oscillate.
147
What is Magnetic Compass Deviation error
The electronics inside the aircraft cause the compass to be slightly inaccurate.
148
What are the 2 Magnetic Compass Dip errors?
Acceleration/Deceleration error - On EASTERLY or WESTERLY headings, while Accelerating, the compass shows a turn to the north, while Decelerating it shows a turn to the south
A - Accelerate
N - North (needle will turn)
D - Decelerate
S - South (needle will turn)
Northerly Turning error - When turning from south to north, the compass leads the turn. When turning from North to South, the compass lags the turn.
U - Undershoot
N - North (when turning N)
O - Overshoot
S - South (when turning S)
149
How can you ensure that your G1000 databases are up to date?
Check the dates of the maps and charts on the MFD's start up screen
150
What are your standby instruments?
1. Altimeter
2. Attitude Gyro (electric)
3. Airspeed Indicator
151
What happens if your PFD or MFD fails?
1. PFD failure - You can press the red Display Backupbutton to show a combined PFD/MFD on the right screen
2. MFD Failure - The engine parameters will now be displayed in a hybrid screen on your PFD.
152
What is the FMS?
Flight Management System
- Allows us to program routes, approaches, departures.
- Calculates fuel consumption and time remaining
- Provides data to the Flight Director and Autopilot
153
What are the two types of ADS-B equipment?
ADS-B OUT - Transmits your GPS position, altitude and velocity to ATC ground stations as well as other aircraft. Required where ever a transponder is required.
ADS-B IN -Receives ADS-B OUT signals from other aircraft to inform a Traffic Display. Provides FIS-B and TIS-B
154
What is TIS-B?
Traffic Information Services Broadcast
1. Enables the inflight receipt of traffic that does not have ADS-B but is Transponder equipped AND within ATC radar coverage
2. Bridges the gap between ADS-B and Transponder/Radar aircraft
155
What are the limitations of TIS-B?
1. In addition to ADS-B traffic, TIS-B allows us to see Transponder ONLY aircraft, but ONLY IF they are within ATC radar range
2. TIS-B shadows may appear of your own aircraft
3. TIS-B traffic data may be up to 15 seconds delayed depending on radar quality
156
Will the parking break work if the Breaks fail?
No
157
What effect will turning the Electric Master off have on the aircraft?
It will basically cause a total electrical failure
158
How could using the Autopilot negatively impact risk?
1. Cause complacency via overreliance
2. Degrade our stick and rudder skills
3. Unexpectedly having to reprogram an FMS while in flight may distract us from flying the plane
159
Where is the Air Inlet for the Engine Induction system?
Front righthand side of the engine cowling
160
Where is the Air Inlet for the Radiator Cooling system?
Lower front of the engine cowling
161
Where is the Air Inlet for the Intercooler?
On the upper front side of the engine cowling, on the righthand side
162
Where is the Air Inlet for GearBox cooling?
On the upper front side of the engine cowling, on the right hand side, closest to the propeller.
163
Describe how our Turbocharger works.
DRAW IT OUT!
(or at least do so in your head)
## Footnote
In the DA40 NG, when the waste gate is OPEN, the air flows throught the exhaust, when the waste gate is CLOSED, air flows through the turbine
164
What is a Turbocharger for?
It allows us to be less effected by degradations in aircraft performance due to changes in altitude or high Density Altitude.
165
Explain the BASIC concept of what a turbocharger does
It works by compressing the air tightly, simulating low altitude conditions
166
What is an Intercooler and why do we have one?
The intercooler is part of the Turbo system
1. It allows us to have even more engine power and performance by cooling the air, since cold air is more dense than warm air.
*it essentially compresses the air even further.
167
Where is the Air Inlet for the Cabin Air Heater?
On the upper front left portion of the engine cowling, farthest from the propeller.
168
What Antennas are located on the top of the aircraft, tail included?
1. GPS (canopy)
2. COMM 1 (middle)
3. VHF & NAV (tail)
169
What Antennas or located on the bottom of the aircraft?
1. Transponder (bottom front)
2. Marker Beacon (part of the ILS system) (middle)
3. COMM 2 (rear)
170
What are the two types of ECU failures?
1. Latched - Remains until cleared by MX
2. Non-Latched - Disappears when cleared through an SOP/FOM by the pilot
171
Where is the ELT antenna located?
It is internal to the aircraft, behind the baggage compartment (near COMM 1)
172
What is the Autopilot Minimum Engagement Height for the G1000?
800ft AGL
173
What is the Autopilot Minimum use Height?
200ft AGL
174
What is an electrical Load?
It is basically the consumption or 'power draw' of an electrical component such as your Position Lights or battery charging.
175
How would you know if there is an issue with your main battery?
Voltmeter will read about 2v lower than normal (28v while engine running)
176
Why are Diesel engines more efficient?
1. Higher Compression ratio
2. Jet fuel (Diesel) fuel is more energy dense than gasoline, due to having longer chains of hydro carbons.
3. Ignition happens more quickly and evenly due to compression ignition (instantaneous) vs spark ignition (longer burn).
177
What systems rely on the ECU to function?
1. Prop governor
2. Fuel System
* ECU pumps
* Fuel/Air mixture
* Common Rail Fuel pressure
3. Turbocharger - Wastegate
4. Glow Plugs
178
What will Detonation lead to?
1. Excessive Temperatures
2. Excessive Pressure
3. Engine failure
4. Engine roughness
5. Loss of power
179
What is a major disadvantage of a traditional gyroscopic HSI?
It suffers from Gyroscopic Drift, resulting in the need to correct it with the Magnetic Compass
180
What type of Ailerons does the DA 40NG have?
A combination of Differential and Frise Type Ailerons
1. Differential because the aileron on the outside of the turn deflects down LESS than the aileron on the inside of the turn deflects UP. This is to counteract Adverse Yaw
2. Frise because we have a drag producing structure (scoop) that descends into the airflow on the up moving aileron
181
What are Differential Ailerons?
The Aileron on the inside of the turn (up aileron) moves up MORE than the aileron on the outside of the turn moves DOWN.
This is done to counteract Adverse Yaw
- Adverse Yaw is caused by the down aileron on the outside of the turn producing more lift AND drag which causes the nose to rise.
182
What are Frise type Ailerons?
A portion of the UP aileron on the inside of the turn dips below the wing creating more drag to counteract Adverse Yaw
183
How fast does the High Pressure engine driven fuel pump fuel through the system?
AFM
At about 45 gallons per hour
184
When the DA40 NG has an Alternator failure (or the engine is not running on the ground) what is giving power to the ECUs?
The Main Battery
185
What does switching the Electronic Master to OFF, ON, and START do? (DA40 NG)
1. OFF - Disconnects battery power to distribution systems (buses)
2. ON - Connects battery power to the distribution systems (buses)
START - For starting the engine (engages the Starter?)
186
Which ECU Backup Battery would be worse to lose?
ECU Backup Battery B
Because Both Battery A & B are wired in series. (one after the other)
And power runs through B first.
187
What materials is our propeller made out of?
Name: MTV-6
Wood composite with fiber reinforced plastic coating and metal leading edge protection, it is coated with PU tape near the hub
188
Why do we have to wait 1 min if we run the engine above 10% Load while on the ground after landing? (DA40 NG)
To allow for the Turbo Charger to slowly cool
Running the engine at high power settings without sufficient airflow may overheat the Turbo
189
What does turning the Fuel Pump switch to ON do?
It turns BOTH ECU A & B fuel pumps on.
Otherwise just one ECU pump will always be on.
190
What does the Emergency Battery power?
1. Standby Attitude Indicator
2. Flood light
*it will last for 1.5hrs.
191
What does Battery Bus 1 do, and what controls it?
Provides power to Battery Bus 2 and to the Starter
Controlled by the Electronic Master Switch
192
What does Battery Bus 2 do?
Gets its power from Battery Bus 1 and provides it to the ECU Bus and to the Main Bus
**Power to the Main Bus is controlled by the Electronic Master and the Essential Bus Switch
192
What does the HOT Battery Bus do?
It provides power to the Accessory Plug and the ELT
193
What does the ECU Bus do?
Gets its power from Battery Bus 2 and provides it to the EECUs and the ECU Fuel pumps, as well as charging the ECU backup batteries
**It is connected to the Alternator so that it can charge the backup batteries
** Engine Master must be on to activate power to ECU A & B.
194
What does the Main Bus do?
Gets its power from Battery Bus 2 and provides it to all consumers on the Main Bus CB panel, it also provides power to the Avionic Bus and its consumers.
195
What does the Essential Bus do?
Gets its power from the Main Bus and provides power to its 'essential' consumers (normal ops)
**In the event of an Alternator failure, the Essential Bus is turned on and NOW connected to Battery Bus 2 for power
**Avionics master must be set to on for the Essential Bus to connect to it.
196
What does turning on the Essential Bus do?
It disconnects the Main Bus and its equipment from the electrical system, therefore no power will be provided to the Main Bus.
This allows for us to keep priority equipment running & decreases the overall electrical load on the battery
197
What type of fuselage and empenage construction does the DA40 NG employ?
Semi-Monocoque
Meaning that the skin of the aircraft is supported internally by oval bulkheads which are further supported by connecting stringers and longerons.
198
How are the Ailerons moved?
(AFM)
Control Rods connected to the stick
199
How is the Rudder moved?
Through cables connected to the stick
200
How are the flaps operated?
Electronically through interconnected push rods
201
How is the elevator moved?
Control Rods connected to the stick
202
What is the HP of the Austro E4-A engine?
165 HP
203
What emergency equipment is available onboard the DA40 NG?
1. First Aid kit in the cargo compartment
2. Fire Extinguisher behind the co-pilots seat
3. Crash Axe underneath the co-pilots seat
4. Emergency exit on the ceiling of the rear door.
204
What kind of Flaps does the DA 40 NG have?
Hybrid between Split flaps and Plane flaps
They are split flaps near the fuselage where the flaps blend into the wing, and plane flaps elsewhere
205
What type of Ailerons do we have?
We have Differential and Frise type Ailerons
Differential because the Ailerons do no extend upwards the same number of degrees that they extend downwards (this is to counteract adverse yaw)
Frise type because the Ailerons have an air scoop under them
206
What is one very important thing to remember in regards to the operation of Pitot Heat and icing conditions?
Pitot Heat is Anti-Icing, therefore, it is not an effective or guaranteed way to remove already accumulated ice.
**It is recommended to turn on Pitot Heat anytime the OAT is 5c or below (AOPA)
207
Describe the layout of the G1000 system in the DA40 NG
Draw it out
(at least in your head)
208
What is the Glide Ratio of the DA 40 NG?
Glide ratio is 9.4
For every 1,000FT of altitude lost, 1.54 NM distance can be gained
209
What is the Maximum allowable Oil Consumption rate per hour?
AFM
0.1 Liters per hour
210
What is the maximum amount of time the starter can be engaged (Key ignition on START position) and what is the required cooldown time??
AFM
Starter can be engaged for a maximum of 10 seconds, after which a 60 second cooldown is required.
**This is to ensure no damage is done to the starter
211
What type of Autopilot does our aircraft have?
GFC 700
212
You are flying an aircraft in cold conditions and notice your oil temperature is lower than normal, what could be the possible cause?
The wrong oil viscosity is being used for cold temps
213
Why is it important that we turn off the Air Conditioner (Aux PWR) durring take off and landing?
Engine will not have full power available because it is being used to power the Air Conditioner
214
As fuel is consumed enroute, what action should be taken as the aircraft becomes lighter?
Decrease power to maintain a constant airspeed for maximum efficiency
* As weight decreases, optimum airspeed and power setting may also decrease
| PHAK Pg 11-10 & 11-11
215
When the Turbocharger fails, will the Waste Gate be open or closed?
The Waste Gate will fail in the Closed position, which allows for all the exhaust gas to flow through the turbine, which will power the compressor
216
What are stall strips for & how do they work?
Purpose
* To make a stall more controllable by ensuring the wing stalls away from the Ailerons first
Function
* Stall strips work by changing the Stagnation point on that part of the wing (point at which the air separates above and below the wing)
* The stall strip causes the airflow behind it to separate from the wing before the rest of the wing normally stalls.
## Footnote
DA40 does not have stall strips
217
What are the 8 ways to disengage the GFC 700 Automatic Flight Control System?
1. AP Disconnect button
2. AP button
3. Avionics Master
4. Electric Master
5. Essential Bus
6. CWS button
7. Manual Electric Trim (left side)
8. TOGA button
9. CB - Pull the AP CB.
218
How does the Alternator convert its current from AC to DC?
Via a Rectifier which contains several Diodes
* The Diodes only allow current to flow in one direction (DC) & block the current flowing in the opposite direction
## Footnote
How an Alternator Works: https://youtu.be/jdSKlg80DjU?si=KOUx9pa1VN0iZ7Bq
219
How does the electrical system keep its power output the same, even when the Alternator is running faster at higher engine RPMs?
The Alternator is equipped with a Voltage Regulator which will limit the output of the Alternator when it is running faster.
## Footnote
How an Alternator Works: https://youtu.be/jdSKlg80DjU?si=KOUx9pa1VN0iZ7Bq
220
In regards to the Pitot-Static instruments, which ones have a Diaphram vs an Anneroid Wafer?
1. Airspeed, and VSI both have a Diaphram
2. Altimter has a sealed Anneroid Wafer
221
In regards to the Pitot Static System, what is the difference between a Diaphram & an Anneroid Wafer?
1. Anneroid Wafer in the Altimter is ***sealed*** to a pressure of 29.92
2. The Diaphrams in the Airspeed Ind & VSI expand & deflate as pressure flows in & out
222
What is different about the DA40 NG's **Intake** stroke vs a conventional engine?
| Austro E4A = DA40 NG engine
Conventional
* Intake stroke includes both air & fuel
DA40 NG Engine
* ONLY air gets added on the Intake stroke
* **Fuel** is added at the TOP of the compression stroke
223
Why does the DA40 NG use a Common Rail fuel delivery system?
1. To provide a very specific & accurate amount of fuel to each cylinder
2. ECU cant compute fuel delivery quantities for each cylinder individually, so the Common Rail ensures equal Fuel PSI to each cylinder
225
226
What are the 6 most important chapters of the AFM?
| Theres an ancronym.
**LEAP WS** (WS memory aid: windshear)
(Cha 2.) L - Limitations
(Cha 3.) E - Emergencies
(Cha 4.) A - Abnormal Ops
(Cha 5.) P - Performance
(Cha 6.) W - Weight & Balance
(Cha 7.) S - Systems
227
Where does the G1000 get its data for determining coordinated flight from?
From the ***Accelerometers*** inside the AHRS
228
What do the purple *Trend Vectors* on the G1000 tell you?
They tell you where the aircraft will be in the next ***6 Seconds***, based on computed trend information.
229
Explain how the G1000 CDI works in regards to determining what VOR Radial you are on
Large arrow of needle = Course selected
Small arrow = Two/From flag
1. The large needle will always point towards a course you select to head TO the station
2. When the Large arrow and the Flag are pointing in the same direction, flying to intercept the needle will take you to the station
* In this case, the tail of the needle will indicate what Radial you are on
3. When the Flag is pointing in towards the tail of
4. When the Flag is pointed opposite the large needle (FROM) then you will fly away from the station by flying that course
* In this case the Large needle point to what Radial you are on
