Beechcraft G36 Bonanza
Beechcraft G36 Bonanza · Performance Data
Overview
This document provides detailed performance data and specifications for the Beechcraft G36 Bonanza, a six-seat, single-engine aircraft. It includes information on the aircraft's powerplant, dimensions, weight limits, fuel capacity, and performance metrics such as takeoff and landing distances, climb rates, and cruise speeds. The data is essential for pilots and aviation enthusiasts who need to understand the aircraft's capabilities and limitations. All specifications are based on standard conditions, which are crucial for accurate flight planning and operational safety.
- Powerplant: Teledyne Continental IO-550-B, 300-hp
- Maximum gross takeoff weight: 3,650 lb
- Takeoff distance over 50-ft obstacle (flaps approach): 1,913 ft
- Cruise speed at high-speed: 174 kt, range: 714 nm
- Demonstrated crosswind component: 17 kt
Document
Source
Originally published by airmart.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Performance Data
- Pages
- 2
- File size
- 82 KB
- Publisher
- airmart.com
Common. Rarer than 24% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Beechcraft G36 Bonanza.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the BEECH G36 Bonanza to your watchlist and track it in one place.
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In this document
Specifications
The Beechcraft G36 Bonanza is powered by a Teledyne Continental IO-550-B engine, delivering 300 horsepower. It has a recommended time between overhaul (TBO) of 1,700 hours. The aircraft measures 27 feet 6 inches in length, 8 feet 7 inches in height, and has a wingspan of 33 feet 6 inches with a wing area of 181 square feet. The wing loading is 20.2 lb/sq ft, and the power loading is 12.2 lb/hp. It seats six and has a standard empty weight of 2,530 pounds, a maximum ramp weight of 3,663 pounds, and a maximum gross takeoff weight of 3,650 pounds.
Performance
The performance metrics of the G36 Bonanza include a takeoff distance of 1,000 feet for ground roll with approach flaps and 1,913 feet over a 50-foot obstacle. With flaps up, the ground roll distance is 1,250 feet, and the distance over a 50-foot obstacle is 2,130 feet. The demonstrated crosswind component is 17 knots, and the rate of climb at sea level is 1,230 feet per minute. The cruise speed at high speed is 174 knots with a range of 714 nautical miles at a fuel consumption of 15.7 gallons per hour.
Limiting and Recommended Airspeeds
The document lists various airspeeds critical for operation: V X (best angle of climb) is 84 KIAS, V Y (best rate of climb) is 100 KIAS, and V A (design maneuvering) is 141 KIAS. The maximum flap extended speed (V FE) for full flaps is 124 KIAS, and for approach flaps, it is 154 KIAS. The maximum gear extended speed (V LE) is also 154 KIAS, with the same speed for gear operating (V LO). The maximum structural cruising speed (V NO) is 167 KIAS, and the never exceed speed (V NE) is 205 KIAS.
Safety notes
- All specifications are based on manufacturer's calculations.
- Performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted.
Full document text
Beechcraft G36 Bonanza Specifications Powerplant Teledyne Continental IO-550-B, 300-hp Recommended TBO 1,700 hr Propeller Hartzell 3-blade, 80-in diameter, constant- speed Length 27 ft 6 in Height 8 ft 7 in Wingspan 33 ft 6 in Wing area 181 sq ft Wing loading 20.2 lb/sq ft Power loading 12.2 lb/hp Seats 6 Standard empty weight 2,530 lb Maximum ramp weight 3,663 lb Maximum gross takeoff weight 3,650 lb Maximum useful load 1,133 lb Maximum payload w/full fuel 689 lb Fuel capacity 80 gal (74 gal usable) Baggage capacity (with six seats) 270 lb, 47 cu ft Performance Takeoff distance, ground roll, flaps approach 1,000 ft Takeoff distance over 50-ft obstacle, flaps approach 1,913 ft Takeoff distance, ground roll, flaps up 1,250 ft Takeoff distance over 50-ft obstacle, flaps up 2,130 ft max Demonstrated crosswind component 17 kt Rate of climb, sea level 1,230 fpm Cruise speed/range w/45-min rsv (fuel consumption) @ High-speed, 8,000 ft, 20-deg rich of peak EGT @ Normal speed, 10,000 ft, 20-deg rich of peak EGT 174 kt/714 nm (15.7 gph) 163 kt/758 nm (13.3 gph) Service ceiling 18,500 ft Landing distance over 50-ft obstacle 1,500 ft Landing distance, ground roll 950 ft Limiting and Recommended Airspeeds V X (best angle of climb) 84 KIAS V Y (best rate of climb) 100 KIAS V A (design maneuvering) 141 KIAS V FE (max flap extended), full flaps 124 KIAS V FE (max flap extended), approach flaps 154 KIAS V LE (max gear extended) 154 KIAS V LO (max gear operating) Extend Retract 154 KIAS 154 KIAS V NO (max structural cruising) 167 KIAS V NE (never exceed) 205 KIAS V R (rotation), flaps up 73 KIAS V R (rotation), flaps approach 67 KIAS V S1 (stall, clean) 68 KIAS V SO (stall, in landing configuration) 61 KIAS For more information, contact Raytheon Aircraft Company, 10511 East Central, Wichita, Kansas 67206; telephone 316/676- 5034; fax 316/676-4819; http://beechcraft.txtav.com/en/bonanza-g36 All specifications are based on manufacturer's calculations. All performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted. Source: www.aopa.org