Mod 1 - ACFT Flashcards
Benefits of AC Knowledge and ATS Operations
Enables safe and efficient service
Quality of service
AC Design Categories
Heavier than Air - Fixed and Rotary wing
Lighter than Air
Principle of Propulsion Catergories
Power driven AC
Non power driven AC
Operation Catergories
Landplane
Seaplane
Amphibian
Type Descriptors
L - Landplane S - Seaplane A - Amphibian H - Helicopter G - Gyrocopter T - Tiltwing
Number of Engines or C - Coupled
P - Piston
T - Turboprop
J - Jet
ICAO Type Designators
Maximum 4 characters
Individual to each AC
Unique to type and series
Used on FPs and ATS messages etc.
Group Designators
BALL GLID SHIP GYRO ULAC UHEL ZZZZ
What are the WTC?
L - MTOM 7000kg or less
M - MTOM >7000kg < 136,000kg
H - MTOM > 136,000kg
J - A380 (“Super”).
What features can be used for AC Recognition?
Engines Wing Position Tail Section Size of AC Shape of Fuselage Shape of Nose and Tailfin.
ICAO Approach Catergories
A - Less than 91 kts B - 91 kts + but less than 121 kts C - 121 kts + but less than 141 kts D - 141 kts + but less than 166 kts E - 166 kts + but less than 211 kts.
1.3 x stall speed at threshold in landing configuration at maximum certified landing mass.
AC Components - FW
Fuselage Empennage Power plant Wings Landing Gear
AC Components - RW
Fuselage Tailsection Power plant Rotor Undercarriage
How is the Weight of AC determined?
Combined mass of AC
The greater the mass, the greater the weight force.
What is Thrust?
Generated by the forward movement of the AC through the air
Thrust force provided by the AC engines.
Methods of Thrust
Props - Piston or turbo prop Aerofoil shaped and rotated by engine Subjected to the relative air flow Creates lift and horizontal direction Large air mass pushed back low speed
Jet - Small air mass compressed and ignited
Hot exhaust thrust backwards high speed.
Balance of Forces in Straight and Level Flight
Greater weight = Greater lift required
Greater lift = Greater drag
Greater drag = Greater thrust required.
What is Lift?
The force necessary to overcome the weight of heavier than air AC.
Changing shape of wing changes the properties of air which generate the required lift force.
Explain Static Pressure
Motionless
Acts equally in all directions
Decreases with increasing altitude
Varies day to day.
Explain Dynamic Pressure
Moving in relation to an object
Acts in direction of movement
Proportional to density
The square of air speed.
What is the relationship between Air Density, temperature, humidity and altitude?
Inversely proportional to temperature
Density decreases, humidity increases
Density decrease, altitude increases.
Lift Formula
L = 1/2 p V2 S CL p = density V = speed of relative air flow S = surface area CL = Aerodynamic lift coefficient.
Bernoulli’s Theorem
Cross section area x Speed = Constant
Static pressure + Dynamic pressure = Constant.
“Energy and mass can neither be created or destroyed it can only be changed from one form to another”
Describe an Aerofoil
Leading edge Training edge Chord line Upper camber Lower camber
AOA and how it affects Speed
Angle between chord line and remote relative air flow
Low angle = Level flight - high speed
Average angle = Level flight - moderate speed
High angle = Level flight - Low speed.