Robinson 44 Definitions and Abbreviations (5/17/2024) Flashcards

1
Q

Vh

A

Stabilized level-flight speed at maximum continuous power.

The maximum speed that the helicopter can fly to ensure structural integrity and stability.

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2
Q

KIAS

A

Knots Indicated Airspeed is speed shown on the airspeed indicator.

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3
Q

KCAS

A

Knots Calibrated Airspeed is speed shown on the airspeed indicator corrected for instrument and position error.

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4
Q

KTAS

A

Knots True Airspeed is airspeed relative to undistributed air. It is KCAS corrected for pressure altitude and temperature.

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5
Q

BHP (Name and definition)

A

Brake Horsepower, Actual power output of the engine.

“brake”denotes the type of dynamometer that is used to access engine output at the crankshaft.

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6
Q

MAP (Name and definition)

A

Manifold Absolute Pressure, is the absolute pressure in the engine intake manifold

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7
Q

MCP (name)

A

Maximum Continuous Power

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8
Q

TOP (name)

A

Takeoff Power (or 5-minute power)

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9
Q

Critical Altitude

A

Maximum altitude at which full throttle produces maximum allowable power

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10
Q

TOGW

A

Takeoff Gross Weight

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11
Q

Reference Datum (location on the R44)

A

100 inches forward of the main rotor shaft

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12
Q

Arm

A

Horizontal distance from a reference datum to the CG of an item

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13
Q

Moment

A

Weight of an item multiplied by its arm

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14
Q

Useful load

A

Difference between maximum gross weight and basic empty weight

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15
Q

OAT

A

Outside Air Temperature

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16
Q

CAT

A

Carburetor Air Temperature

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17
Q

CHT

A

Cylinder Head Temperature

18
Q

GPH

A

Gallons Per Hour

19
Q

AGL

A

Above Ground Level

20
Q

IGE

A

In Ground Effect

21
Q

OGE

A

Out of Ground Effect

22
Q

ALT

A

Alternator

23
Q

Station

A

A fore-and-aft location along the helicopter fuselage usually given in terms of distance in inches from the reference datum.

24
Q

Center of Gravity (CG)

A

The point at which a helicopter would balance if suspended. Its distance from the reference datum is found by dividing the total moment by the total weight of the helicopter.

25
Q

CG Arm

A

The arm from the reference datum obtained by adding the helicopter’s individual moments and dividing the sum by the total weight.

26
Q

CG Limits

A

The extreme center gravity locations within which the helicopter must be operated at a given weight.

27
Q

Usable Fuel

A

Fuel available for flight planning.

28
Q

Unusable Fuel

A

Fuel remaining after a runout test has been completed in accordance with government regulations.

29
Q

Standard Empty Weight

A

Weight of a standard helicopter including unusable fuel and full operating fluids (i.e. hydraulic, engine oil, etc.).

30
Q

Basic Empty Weight

A

Standard empty weight plus weight of installed optional equipment.

31
Q

Payload

A

Weight of occupants, cargo, and baggage.

Anything that is paying to be on the aircraft.

32
Q

Useful Load

A

Difference between maximum takeoff weight and basic empty weight.

33
Q

Vy

A

Speed for best rate of climb

The airspeed at which the helicopter will get to a specific altitude in the shortest amount of time.

34
Q

Vne

A

Speed never exceed

35
Q

MSL Altitude

A

Altitude above mean sea level, indicated by the altimeter (corrected for instrument error)

36
Q

Pressure Altitude

A

Altitude indicated by the altimeter (corrected for instrument error) when the barometric subscale is set to 29.92

37
Q

Density Altitude

A

Pressure altitude, corrected for non-standard temperature

38
Q

ISA

A

International Standard Atmosphere exists when pressure is 29.92 and temperature is 15 C

39
Q

What is centrifugal force?

A

Pulls the blades outward

40
Q

What is centripetal force?

A

Pulls you inward (the moon is orbit because of this)