Section 1 - General Flashcards
Main Rotor - Articulation
Free to teeter and cone, rigid inplane
Main Rotor - Diameter
33 ft
Main Rotor - Tip Speed at 102% RPM
705 feet per second
Number of Blades
Two
Main Rotor - Blade Chord
10.0 inches inboard,
10.6 inches outboard
Main Rotor - Blade Twist
-6 degrees
Tail Rotor - Articulation
Free to teeter, rigid inplane
Tail Rotor - # of Blades
Two
Tail Rotor - Diameter
58 inches
Tail Rotor - Blade Chord
5.1 inches (constant)
Tail Rotor - Blade Twist
Zero
Tail Rotor - Precone Angle
1 Degree
Tail Rotor - Tip Speed at 102% RPM
614 feet per second
Drive System - Engine to Upper Sheave
Four double Vee-belts with 0.778:1 speed reducing ratio
Drive System - Upper Sheave to Drive Line
Spray-type overrunning clutch
Drive System - Drive Line to Main Rotor
Spiral-bevel gears with 11:57 speed reducing ration
Drive System - Drive Line to Tail Rotor
Spiral-bevel gears with 31:27 speed increasing ratio
Powerplant - Model
Lycoming 0-540-F1B5
Powerplant - Type
Six cylinder, horizontally opposed, direct drive, air cooled, carbureted, normal aspirated
Powerplant - Displacement
541.6 cubic inches
Powerplant - Normal Rating
260 BHP @ 2800 RPM
Powerplant - Maximum continuous rating in R44
205 BHP at 2718 RPM (102% on tachometer)
Powerplant - 5 Minute take off rating in R44
225 BHP at 2718 RPM
Powerplant - Cooling System
Direct drive squirrel-cage blower
Performance Definitions - KIAS
Knots Indicated Airspeed is speed shown on the airspeed indicator
Performance Definitions - KCAS
Knots Calibrated Airspeed is speed shown on the airspeed indicator corrected for instrument and postion error
Performance Definitions - KTAS
Knots True Airspeed is airspeed relative to undisturbed air. It is KCAS corrected for pressure altitude and temperature
Performance Definitions - VNE
Never-Exceed Airspeed
Performance Definitions - Vy
Speed for best rate of climb
Performance Definitions - Vh
Stabilized level-flight speed at maximum continous power
Performance Definitions - MSL Altitude
Altitude above mean sea level, indicated by the altimeter )corrected for instrument error) when the barometric sub-scale is set to the atmospheric pressure existing at sea level
Performance Definitions - Pressure Altitude
Altitude indicated by the altimeter (corrected for instrument error) when the barometric sub-scale is set to 29.92 inches of mercury (1013.2 mb)
Performance Definitions - Density Altitude
Altitude in ISA conditions at which the air would have the same density (it is pressure altitude corrected for OAT)
Performance Definitions - ISA
International Standard Atmosphere exists when pressure is 29.92 inches of mercury at sea level, temperature is 15 degrees C at sea level, and temperature decreases 1.98 degrees C per 1000 feet of altitude
Performance Definitions - BHP
Brake Horsepower is actual power output of the engine
Performance Definitions - MAP
Manifold Absolute Pressure is the absolute pressure in the engine intake manifold
Performance Definitions - RPM
Revolutions Per Minute or speed of engine or rotor. (Shown by tachometer as percentage of 2665 engine RPM and 400 main rotor RPM)
Performance Definitions - RPM
Revolutions Per Minute or speed of engine or rotor. (Shown by tachometer as percentage of 2665 engine RPM and 400 main rotor RPM)
Performance Definitions - MCP
Maximum Continuous Power
Performance Definitions - TOP
Takeoff Power (limited to 5 minutes in the R44)
Performance Definitions - Critical Altitude
Altitude at which full throttle produces maximum allowable power (MCP or TOP).
Performance Definitions - TOGW
Take off Gross Weight
Performance Definitions - OAT
Outside Air Temperature
Performance Definitions - CAT
Carburetor Air Temperature
Performance Definitions - CHT
Cylinder Head Temperature
Performance Definitions - GPH
Gallons Per Hour
Performance Definitions - AGL
Above Ground Level
Performance Definitions - IGE
In Ground Effect
Performance Definitions - OGE
Out of Ground Effect
Performance Definitions - ALT
Alternator
Weight and Balance Definitions - Reference Datum
A vertical plane from which horizontal distances are measured for balance purposes. The Longitudinal reference datum is 100 inches forward of the main rotor shaft centerline for the R44.
Weight and Balance Definitions - Station
Fore-and-aft location along the helicopter fuselage given in terms of distance in inches from the longitudinal reference datum.
Weight and Balance Definitions - Arm
Horizontal distance from a reference datum to the center of gravity (CG) of an item.
Weight and Balance Definitions - Moment
The weight of an item multiplied by its arm
Weight and Balance Definitions - Center of Gravity (CG)
Location on the fuselage (usually expressed in inches from the reference datum) at which the helicopter would balance. CG is calculated by dividing the total helicopter moment by total helicopter weight.
Weight and Balance Definitions - CG Limits
Extreme CG location within which the helicopter must be operated at a given weight
Weight and Balance Definitions - Usable Fuel
Fuel available for flight planning
Weight and Balance Definitions - Unusable Fuel
Fuel remaining in the tank that cannot reliably proceed uninterrupted fuel flow in the critical flight attitude.
Weight and Balance Definitions - Standard Empty Weight
Weight of a standard helicopter including unusable fuel, full operating fluids, and full engine oil.
Weight and Balance Definitions - Basic Empty Weight
Standard empty wight plus weight of installed optional equipment
Weight and Balance Definitions - Payload
Weight of occupants, cargo, and baggage
Weight and Balance Definitions - Useful Load
Difference between maximum gross weight and basic empty weight.