Main Rotor:
Tail Rotor:
R22 Beta Engine:
- 4cylinder, horizontally oppossed, direct drive, air cooled, carburetted, normally aspirated.
R22 o-320 ratings:
Rotor RPM:
97%-104%
90%-110%
Operating limits:
Oil Pressure limits:
Weight Limits:
GLADIMSMAL
G-Gov off ops prohibited unless training or emergency
L-Low g pushovers prohibited
A-Aerobatic flight prohibited
D-Doors off permitted
I-Flight in known icing conditions prohibited
M-Maximum 14,000 density altitude
S-Solo right seat only
M-Minimum one crew
A-Govenor, oat, alternator, low rotor rpm warning system
L-Left seatbelt buckled at all times
Approved fuels:
Required Equipment:
FAA:
-CAMALSFOOT
Compass Altimeter Manifold Pressure Gauge Airspeed Indicator Landing gear position indicator Seatbelts Fuel gauges Oil temp gauge Oil pressure gauge tachometers
-PALSS
Position Lights Anti-collusion Lights Landing Light(if for hire) Spare fuses Source of power
Required Equipment:
Robinson:
-GOAL Governor OAT Alternator Low rotor rpm warning system
-NAIL+O
Navigation Lights Anticollusion Lights Instrument Lights Landing Light Orientation(Celestial or ground illumination)
Fuel Capacity Without Bladders(Useable):
Airspeed Indicator:
- 102 kias
Rotor Tachs:
Engine Tachs:
Oil Temp:
- 245
Cylinderhead Temp:
- 500
Carb Air Temp:
-Yellow arc
Manifold Pressure:
- 25.2
When encountering moderate , severe, or extreme turbulence
Catastrophic rotor stall occurs at?
when rotor rpm drops below 80% plus 1% per 1000 ft of altitude.
Engine o-320 displacement?
319.8 cubic inches