Robinson 22 POH Section 1: General (10/27/22) Flashcards

1
Q

R22 Dimensions (5 items)

A
  • Width 76 inches (Approx. 6 feet)
  • Length 345 inches (Approx. 30 feet)
  • Height 107 inches (Approx. 9 feet)
  • Blade diameter 25 ft, 2 inches
  • Rotor blade diameter 42 inches (Approx. 3.5 feet)
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2
Q

Describe the rotor

A

Semi-rigid, “free to teeter and cone, rigid in-plane”

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3
Q

Describe the tail rotor

A

Free to teeter, rigid in-plane

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4
Q

Describe the engine Beta (8 items)

A

O-320-B2C, Lycoming, 4 cylinder, horizontally opposed, direct drive, air cooled, carbureted, normally aspirated

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5
Q

Describe the cooling system (2 items)

A

Direct drive, squirrel-cage blower

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6
Q

Engine normal rating (BHP and RPM)

A

145 BHP and 2700 RPM

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7
Q

5 min takeoff (BHP and RPM)

A

131 BHP and 2652 RPM

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8
Q

Max. continuous (BHP and RPM)

A

124 BHP and 2652 RPM

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9
Q

Datum location

A

100 inches forward of main rotor

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10
Q

Brake Horsepower

A

Actual power output of the engine

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11
Q

MCP

A

Maximum Continuous Power

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12
Q

TOP

A

Takeoff Power

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13
Q

Critical Altitude

A

Altitude at which full throttle produces maximum allowable power (MCP or TOP)

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14
Q

Standard Empty Weight

A

Weight of standard helicopter including unusable fuel, full operating fluids, and full engine oil

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15
Q

Basic Empty Weight

A

Standard empty weight plus weight of installed optional equipment

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16
Q

Assuring that the helicopter is in airworthy condition is the _______________________

A

Responsibility of the owner

17
Q

Determining that the helicopter is safe for flight is the ____________________________

A

Responsibility of the pilot in command

18
Q

What does rigid in-plane mean?

A

It means that the blades are free to move up and down, but they are “rigid” in the plane of rotation meaning that they can’t lead and lag.

19
Q

What does teetering mean?

A

It means that the blades “teeter” like a see-saw would. If one goes up, the other goes down, in normal operation.

20
Q

What is the primary reason for derating a helicopter engine? (2 reasons)

A

Primary reason: To increase the altitude capability of the helicopter. If a 160 hp (O-320-B2C) is derated to 145 BHP, it will produce 145BHP all the way to the critical altitude.

Secondary reason: higher reliability and longer engine life.