Systems Flashcards
FACU Abbreviation and Use
-Fuel Air Controller Unit
-mixture controlling amount of air in the fuel
How Fuel System is Organized (flow)
-Fuel tank to auxiliary
-Auxiliary to main fuel pump
-Main fuel pump to FACU (fuel air controller unit)
-FACU then to cylinder
Three Valves from Under Nose Pull From:
-fuel selector valve
-fuel reservoir
-fuel strainer
Fuel used by Cessna 172
100LL (low lead)
blue
Two Types of Engines
-Carbureted: overall runs harder, can get carb icing.
-Fuel Injected: overall better, except runs harder in summer and more likely to get deposits
Clean vs Dirty Configurations
Clean configuration: no flaps, no gear
Dirty configuration: flaps down, gear down
3 Main Flight Controls
-Aileron: roll, longitudinal rotation, lateral stability
-Elevator: pitch, lateral rotation, longitudinal stability
-Rudder: yaw, vertical rotation, directional stability
Process of How a 4 Stroke Engine Works
-All parts are never happening at the same time, hence its 4 strokes
4 Strokes:
- Intake stroke: fuel and air centers the cylinder
- Compression: this fuel air mixture is now compressed
- Power: spark plugs ignite the fuel air mixture which cause the piston to create a downward motion.
- Exhaust: The exhaust is released through the pushrod and exits the engine.
Type of Propeller on Cessna 172
-Alternative?
-McCauley Two Blade Fixed Pitch Propeller
Alternative:
-constant speed prop, pitch can be adjusted
Purpose of Oil
Cleans
Cools
Lubricates
Type of Engine on Cessna 172-S
Lycoming-IO-360-L2A
-I= fuel injected
-O= horizontally opposed (cylinders are on side of engine, pushing side-by-side, improves visibility over cowling and aerodynamics)
-360= cubic inches of displacement
-4 cylinders, naturally aspirated
-air cooled
-wet sump oil system
-180 hp @2700 rpm
-direct driven= cylinders are directly attached to pushrod that drives the propeller directly
3 Types of Power Options on Planes
Highest Ceiling
1. Turbo
2. Turboprop
3. Reciprocating- our Cessna
Lowest Ceiling
Principle of How Brakes Work
Pascal’s Principle
-hydraulic advantage
-solenoid under pedal for brakes provides more pressure at the disk end of the brakes
-brake/hydraulic fluid is red
Ignition System Process
- starter motor slowly moves the flywheel and magnetos attached
- One of Two magneto runs during startup, wound like a windup toy, that then winds and runs the spark plugs from the one magneto.
- After it starts, both magnetos run
Number of Magnetos and Spark Plugs
-2 magnetos: one that run 4 spark plugs, one for each head.
-The other magneto also has connections to the same heads, with 4 more spark plugs.
-8 total spark plugs.
Shock Absorption on Cessna 172
-main wheels have tubular spring steel main landing gear struts
-Nose wheel have air/oil nose gear shock strut (oleo strut)
-Air is actually Nitrogen which is more consistent at higher altitudes or a lower
Carburetor Heat Use
-more airflow, less velocity at the Venturi, pressure decreases, can get carb icing
-70 degrees or lower can and probably will get icing
-If running full power for a long period of time, the valve flap at the Venturi stays open and get colder temps
To Solve:
-Turn on carb heater, will have two drops in RPM then an increase. After increase, carb is clear.
Essential Aircraft Equipment List
A TOMATO FLAMES:
Cannot fly without these ALL in operation:
-Airspeed Indicator
-Tach
-Oil pressure
-Manifold pressure (only for controllable pitch propeller)
-Altimeter (not required during day)
-Temp gauge
-Oil temp
-Fuel Level
-Landing gear indicator
-AntiCollision Lights
-Magnetic compass
-ELT
-Seat belts
Which regulation states essential aircraft equipment requirements?
91.205
VFR Required Equipment for Night
A TOMATO FLAMES AND
FLAPS:
-Fuses
-(some aircraft have circuit breaks instead. We have these because they can be put back in and reset)
-If it is an essential circuit, we can reset once. If it is nonessential and it pops, leave it. The reason is because it could cause a fire.
-Landing lights
-Anti-collision lights
-Position indicator
-Source of Power
Vacuum System Runs Which Gauge?
Attitude Heading
Gyroscope (Attitude Heading Gauge) Works on Which 2 Principles?
- Rigidity in Space
-When spinning, the plane wants to stay in the same plane of field - Precession
-first action is to nose up: secondary precession is tendency to the right
-first action is we descend: secondary precession is tendency to the left
Which gauge runs off of using a gyroscope?
Attitude Heading
Horizontal Situational Indicator (HSI)
-describe makeup and use
Heading indicator
-heading select knob to bug
G5 and G1000 have this for us
Accelerometer
-describe makeup and use
-use springs and tiny gyros to use force and mass to determine acceleration
Turn Coordinator
-describe and use
-plane in the middle
-shows high right or left wing
-has ball or brick to coordinate turns with rudder
-electrically powered or tied to GDUs
Pitot Static System
-indicates?
-Works with which other system? How to fix if this alternate system freezes? Indicators?
-If blocked, how will we know? How to fix?
-Indicates airspeed
-static port: if becomes clogged open alternate static port, will know is blocked if altitude freezes, with static port open, the airspeed will read 15 knots higher than actual. Will read 65 and going 50.
-one port: will read somewhere between 0 and actual.
Two ports: will act as altimeter, rising and falling as we rise and descend
-fix: turn on pitot heater
How to read airspeed indicator:
-green arc
-white arc
-yellow arc
-red arc
-green: normal operating range
-white: safe flap deployment
-yellow: Vno
-red: Vne
What is Indicated Airspeed (IAS)?
-the reading directly from instruments, no temp, no density accounted for
-the main one we use to ensure the airplane knows what he’s doing. Helps us not stall.
What is Calibrated Airspeed (CAS)?
IAS corrected for installation error and instrument error
What is True Airspeed (TAS)?
CAS corrected for altitude and nonstandard temperature