Specifications for the Robinson R22 Beta II
Robinson R22 Beta II · Specifications
Overview
This document provides detailed specifications for the Robinson R22 Beta II helicopter, a well-regarded model in the aviation community known for its reliability and performance. It highlights the aircraft's engine specifications, weight limits, fuel capacities, and performance metrics. The document is intended for pilots, aviation enthusiasts, and potential owners, offering insights into the helicopter's operational capabilities and maintenance requirements. Key features include the engine type, maximum gross weight, and various performance parameters such as airspeed and range.
- Engine: Lycoming O-360, 131 hp takeoff, 124 hp continuous
- Max Gross Weight: 1370 lb (622 kg)
- Cruise Speed: Up to 95 kts (176 km/h)
- Max Range: Approx. 250 nm (460 km)
- Hover Ceiling IGE: 9400 ft at max gross weight
- Hover Ceiling OGE: 5000 ft at max gross weight, 8000 ft at 1300 lb
Document
Source
Originally published by robinsonstrapistorprod.blob.core.windows.net. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Specifications
- Year
- 2025
- Pages
- 6
- File size
- 7.0 MB
- Publisher
- robinsonstrapistorprod.blob.core.windows.net
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 250
- Engine (hp)
- 131
- Engine model
- Lycoming O-360
- Max speed (kt)
- 102
- Cruise speed (kt)
- 95
- Empty weight (lb)
- 880
- Fuel capacity (gal)
- 16.9
- Service ceiling (ft)
- 14,000
- Max takeoff weight (lb)
- 1,370
V-speeds
- VNE
- 102
Weight & balance
- Useful load (lb)
- 389
- Basic empty weight (lb)
- 880
- Max takeoff weight (lb)
- 1,370
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In this document
Engine Specifications
The Robinson R22 Beta II is powered by a Lycoming O-360 engine, which is a four-cylinder, carbureted engine. It is derated to provide 131 horsepower at takeoff and 124 horsepower for continuous operation.
Weight and Capacity
The maximum gross weight of the R22 Beta II is 1370 pounds (622 kg). The approximate empty weight, including oil and standard avionics, is 880 pounds (399 kg). It has a standard fuel capacity of 16.9 gallons (101 lb / 46 kg) and an auxiliary fuel capacity of 9.4 gallons (56 lb / 25 kg). The combined weight of the pilot, passengers, and baggage with standard fuel is limited to 389 pounds (176 kg).
Performance Metrics
The R22 Beta II has a maximum airspeed (Vne) of 102 knots (189 km/h) at maximum gross weight. The cruise speed at maximum gross weight can reach up to 95 knots (176 km/h). The helicopter has a maximum range of approximately 250 nautical miles (460 km) without reserve.
Hover Ceiling
At maximum gross weight, the hover ceiling in ground effect (IGE) is 9400 feet. The hover ceiling out of ground effect (OGE) at maximum gross weight is 5000 feet, while at a weight of 1300 pounds, the hover ceiling OGE is 8000 feet.
Electrical System
The Robinson R22 Beta II is equipped with a 14-volt electrical system, which is standard for this model.
Full document text
DEPENDABILITY & VALUE · Proven workhorse, delivering class-leading performance for 45 years. · Powered by Lycoming’s renowned O-360 engine, derated for unmatched reliability and reserve power. · Crafted with a lightweight yet sturdy airframe and an aerodynamically refined fuselage, the R22 aircraft maximizes airspeed and fuel efficiency. · Two-bladed main rotor system maximizes efficiency and minimizes hangar space requirements. SAFETY FEATURES · 4K cockpit camera and robust fuel system prioritize occupant well-being. · Crashworthy fuel system enhances overall safety. · Carburetor heat assist increases safety and reduces pilot workload. · Optional: Bird-strike-resistant windshields showcase Robinson’s commitment to continuous safety improvements. OWNERSHIP & MAINTENANCE · Enjoy more time flying and less time managing logistics. · Life-limited components with 2200-hour or 12-year service lives reduce maintenance costs. · 50-hour oil changes; engine and airframe have TBOs of 2200 hours or 12 years, whichever comes first. · A straightforward maintenance schedule simplifies flying and ownership. UNMATCHED WARRANTY & SUPPORT · Two-year or 1000-hour limited aircraft warranty for peace of mind. · Robinson’s extensive support network guarantees that you’re prepared to fly with confidence. DISTINCTIVE DESIGN · Standard instruments and optional glass avionics from Garmin provide clear information and increase situational awareness. · Strategically arranged instruments provide the pilot with instantly accessible information on aircraft performance. · Ergonomic controls ensure precise handling in all conditions. CUSTOMIZABLE · Leather seats in tan, gray, or charcoal. · Cabin heater and defogger. · Engine priming system. · Xenon HID landing lights. · Bose A30 headsets for superior audio clarity and noise cancellation. Helicopter R22 Beta II Engine Lycoming O-360, four cylinder, carbureted Horsepower derated to 131 hp takeoff & 124 hp continuous Maximum Gross Weight 1370 lb (622 kg) Approximate Empty Weight (Including Oil & Std Avionics) 880 lb (399 kg) Standard Fuel Capacity / Weight 16.9 gal capacity / 101 lb (46 kg) Auxiliary Fuel Capacity / Weight 9.4 gal capacity / 56 lb (25 kg) Pilot, Passengers, and Baggage (with Standard Fuel) 389 lb (176 kg) Maximum Airspeed (Vne) at Maximum Gross Weight 102 kts (189 km/h) Cruise Speed at Maximum Gross Weight up to 95 kts (176 km/h) Maximum Range (No Reserve) approx 250 nm (460 km) Hover Ceiling IGE at Maximum Gross Weight 9400 ft at 1370 lb Hover Ceiling OGE at Maximum Gross Weight 5000 ft at 1370 lb Hover Ceiling OGE at 1300 lb 8000 ft at 1300 lb Maximum Operating Altitude 14,000 ft Electrical System 14 volt Experience the R22 Beta II. Contact your local Robinson Helicopter dealer today. 2901 Airport Drive Torrance, CA 90505 USA www.robinsonheli.com 310-539-0508 © Robinson Helicopter Company. Robinson and R22 are registered trademarks of Robinson Helicopter Company. All other trademarks or registered trademarks are property of their respective companies. (Mar. 2025) CLIMB HIGHER
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