R22 Beta II Specifications and Dimensions
Robinson R22 Beta II · Specifications
Overview
This document provides detailed specifications and dimensions for the Robinson R22 Beta II helicopter. It is intended for pilots, aviation enthusiasts, and maintenance personnel who require precise information about the aircraft's performance, weight, and powerplant. Key specifications include weight limits, engine details, and performance metrics such as airspeed and climb rates. This reference is crucial for understanding the operational capabilities and limitations of the R22 Beta II.
- Gross Weight: 1,370 lb
- Empty Weight Equipped: 855 lb
- Maximum Airspeed (Vne): 118 mph (102 kts)
- Cruise Airspeed @ 70% Power: 110 mph (96 kts)
- Rate-of-Climb at Sea Level: Over 1,000 fpm
- Maximum Operating Altitude: 14,000 feet
- Average Fuel Consumption: 8 to 10 gph
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Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at www.aviation-broker.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Specifications
- Pages ·
- 1
- File size ·
- 26 KB
- Copy found at ·
- www.aviation-broker.com
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In this document
Weights
The document outlines the weight specifications for the Robinson R22 Beta II. The gross weight is listed as 1,370 lb, with an empty equipped weight (including full oil) of 855 lb. The fuel weight for 19.2 gallons is 115 lb, and there is an optional auxiliary fuel capacity of 10.5 gallons weighing 63 lb. The maximum weight for passengers and baggage with standard fuel is 63 lb.
Powerplant
The R22 Beta II is powered by a Lycoming O-360 four-cylinder, air-cooled engine. This engine is derated to produce 131 horsepower at 2,652 rpm, providing reliable performance for the helicopter.
Performance
Performance metrics for the R22 Beta II include a maximum airspeed (Vne) of 118 mph (102 knots) and a cruise airspeed at 70% power of 110 mph (96 knots). The helicopter has a maximum range of over 200 miles without reserve and over 300 miles with auxiliary fuel. Average fuel consumption ranges from 8 to 10 gallons per hour.
Climb Performance
The rate of climb at sea level is over 1,000 feet per minute, while at 10,000 feet, the rate of climb is over 600 feet per minute. The maximum operating altitude for the R22 Beta II is 14,000 feet, with a hover ceiling in ground effect at gross weight of 9,400 feet.
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Full document text
R22 Beta II Specifications and Dimensions Weights Gross Weight 1,370 lb Empty Weight Equipped (w/full oil) 855 lb Fuel (19.2 gal) 115 lb Optional Auxiliary Fuel (10.5 gal) 63 lb Passengers and Baggage w/stnd fuel 63 lb Powerplant Lycoming O-360 Four-Cylinder, Air-Cooled Derated to 131 horsepower at 2652 rpm Performance Maximum Airspeed (Vne) 118 mph (102 kts) Cruise Airspeed @ 70% Power 110 mph (96 kts) Maximum Range (no reserve) Over 200 miles Maximum Range (w/aux fuel) Over 300 miles Average Fuel Consumption 8 to 10 gph Rate-of-Climb at Sea Level Over 1,000 fpm Rate-of-Climb at 10,000 Feet Over 600 fpm Maximum Operating Altitude 14,000 feet Hover Ceiling IGE @ 1370 GW 9,400 feet