R-22 System Discription Flashcards

1
Q

Main rotor

A

Articulation - free to teeter and cone, rigid inplane

Diameter- 25ft 2inch

Blade cord - 7.2 inches

Blade twist - -8 degrees

Tip speed @ 100% - 672 feet per minute

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2
Q

Tail rotor

A

Articulation- free to teeter, rigid inplane

Diameter- 3 feet 6 inches

Blade cord - 4 inches (constant)

Blade twist - 0 degrees

Pre-cone angle - 1 degree 11 minutes

Tip speed @ 100% - 599 feet per minute

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3
Q

Engine limitations

A

Engine max speed - 2652 RPM (104%)

Cylinder head max temp - 500F (260C)

Oil max temp - 245F (118C)

Oil pressure

  • min during idle 25 psi
  • min during flight 55 psi
  • max during flight 95 psi
  • max during start & warm 115 psi
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4
Q

Weight limits

A

Max gross weight - 1370 lbs

Min gross weight - 920 lbs

Max per seat + baggage compartment 240 lbs

Max in baggage compartment- 50 lbs

Solo weight with doors - 135 lbs

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5
Q

Flight and maneuver limitations

A

Aerobatic flight maneuvers

Low G cyclic pushovers

Flight prohibited with gov off - except for gov malfunction or emergency flight training.

Flight in known icing conditions

Max operating density altitude - 14000 ft

G- governor
O- outside air temp gauge
A- alternator
L- low rpm horn and light

Left seat belt must be buckled

Operations with doors on or off approved

Fuel - 100LL

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6
Q

Fuel capacity

A

with bladders - main 18.3g aux 9.7g

Usable- main 16.9g aux 9.4g

Combined- 28g usable 26.3g

without bladders - main 19.8g aux 10.9g

Usable- main 19.2g aux 10.5g

Combined- 30.7 usable 29.7g

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7
Q

Airspeed indicator

A

Green arc - 50 to 102 KIAS

Red line - 102 KIAS

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8
Q

Rotor tach

A

Upper red line - 100%

Yellow arc - 104 - 110% special operating range

Yellow arc lower - 90 - 101% precautionary range

60 - 70 % harmonic resonance

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9
Q

Oil temp

A

Green arc - 75 to 245 degrees Fahrenheit

Red line - 245

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10
Q

Cylinder head temp

A

Green arc - 200 to 500 degrees Fahrenheit

Red line - 500

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11
Q

Carb air temp

A

Yellow arc -15 to 5 degrees Celsius

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12
Q

Turbulence

A

Reduce airspeed to 60 knots or .7vne but no less then 57 knots.

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