CESSNA T206H SPECIFICATIONS Powerplant Lycoming TIO-540 ...
CESSNA 310Q · Performance Data
Overview
This document provides detailed specifications and performance data for the Cessna T206H aircraft. It is intended for pilots, aviation enthusiasts, and anyone interested in understanding the capabilities and limitations of this aircraft model. The specifications include information on the powerplant, dimensions, weights, fuel capacity, and performance metrics such as takeoff and landing distances, climb rates, and cruise speeds. The document serves as a comprehensive reference for operational planning and performance assessment.
- Powerplant: Lycoming TIO-540-AJ1A, 310 hp @ 2,500 rpm
- Maximum gross weight: 3,600 lb
- Takeoff distance over 50-ft obstacle: 1,740 ft
- Rate of climb at sea level: 1,050 fpm
- Maximum level speed at 17,000 ft: 178 kt
- Cruise speed at 20,000 ft @ 75% power: 164 kt/3.5 hr (114 pph)
- V X (best angle of climb): 69 KIAS
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
- 53 KB
- Publisher
- airmart.com
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp)
- 310
- Height (ft)
- 9
- Length (ft)
- 28
- Propeller
- McCauley 3-blade, constant-speed
- Wingspan (ft)
- 36
- Engine model
- Lycoming TIO-540-AJ1A
- Max speed (kt)
- 178
- Cruise speed (kt)
- 164
- Empty weight (lb)
- 2,274
- Fuel capacity (gal)
- 92
- Rate of climb (fpm)
- 1,050
- Service ceiling (ft)
- 27,000
- Max takeoff weight (lb)
- 3,600
Performance
- Fuel burn (gph)
- 19
- Landing over 50ft
- 1,395
- Max crosswind (kt)
- 20
- Takeoff over 50ft
- 1,740
- Landing distance (ft)
- 735
- Takeoff distance (ft)
- 910
V-speeds
- VA
- 125
- VR
- 55
- VX
- 69
- VY
- 89
- VFE
- 140
- VNE
- 182
- VNO
- 149
- VS1
- 50
- VSO
- 39
Weight & balance
- Useful load (lb)
- 1,343
- Max ramp weight (lb)
- 3,617
- Baggage allowance (lb)
- 180
- Basic empty weight (lb)
- 2,274
- Max landing weight (lb)
- 3,600
- Max takeoff weight (lb)
- 3,600
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In this document
Specifications
The Cessna T206H is powered by a Lycoming TIO-540-AJ1A engine, producing 310 hp at 2,500 rpm. It has a maximum ramp weight of 3,617 lb and a maximum gross weight of 3,600 lb. The aircraft features a wingspan of 36 ft and a wing area of 174 sq ft, with a wing loading of 20.7 lb/sq ft. The cabin dimensions are 12 ft 1 in in length, 3 ft 8 in in width, and 4 ft 2 in in height.
Performance
The T206H has a takeoff distance of 910 ft for ground roll and 1,740 ft over a 50-ft obstacle. It can climb at a rate of 1,050 feet per minute at sea level. The maximum level speed at 17,000 ft is 178 knots, with cruise speeds varying based on power settings and altitude. For example, at 75% power at 20,000 ft, the cruise speed is 164 knots with a fuel consumption of 114 pounds per hour.
Limiting and Recommended Airspeeds
The document lists critical airspeeds for the T206H, including V X (best angle of climb) at 69 KIAS, V Y (best rate of climb) at 89 KIAS, and V A (design maneuvering) at 125 KIAS. The maximum structural cruising speed (V NO) is 149 KIAS, and the never exceed speed (V NE) is 182 KIAS.
Safety notes
- All performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted.
Full document text
CESSNA T206H SPECIFICATIONS Powerplant Lycoming TIO-540-AJ1A, 310 hp @ 2,500 rpm Recommended TBO 2,000 hr Propeller McCauley 3-blade, constant-speed, 79- in dia. Length 28 ft 3 in Height 9 ft 3 in Wingspan 36 ft Wing area 174 sq ft Wing loading 20.7 lb/sq ft Power loading 11.6 lb/hp Seats 6 Cabin length 12 ft 1 in Cabin width 3 ft 8 in Cabin height 4 ft 2 in Empty weight 2,274 lb Empty weight, as tested 2,355 lb Maximum ramp weight 3,617 lb Maximum gross weight 3,600 lb Useful load 1,343 lb Useful load, as tested 1,262 lb Payload w/full fuel 815 lb Payload w/full fuel, as tested 734 lb Maximum takeoff weight 3,600 lb Maximum landing weight 3,600 lb Fuel capacity, std 92 gal (88 gal usable) 552 lb (528 lb usable) Oil capacity 11 qt Baggage capacity 180 lb PERFORMANCE Takeoff distance, ground roll 910 ft Takeoff distance over 50-ft obstacle 1,740 ft Max demonstrated crosswind component 20 kt Rate of climb, sea level 1,050 fpm Maximum level speed, 17,000 ft 178 kt Cruise speed/endurance w/45-min rsv, std fuel (fuel consumption) @ 75% power, best economy 20,000 ft 164 kt/3.5 hr (114 pph/19 gph) @ 65% power, best economy 24,000 ft 153 kt/4.1 hr (97 pph/16.2 gph) @ 55% power, best economy 24,000 ft 137 kt/4.9 hr (85 pph/14.1 gph) Service ceiling 27,000 ft Landing distance over 50-ft obstacle 1,395 ft Landing distance, ground roll 735 ft LIMITING AND RECOMMENDED AIRSPEEDS V X (best angle of climb) 69 KIAS V Y (best rate of climb) 89 KIAS V A (design maneuvering) 125 KIAS V FE (max flap extended) 140 KIAS V NO (max structural cruising) 149 KIAS V NE (never exceed) 182 KIAS V R (rotation) 55 KIAS V S1 (stall, clean) 50 KIAS V SO (stall, in landing configuration) 39 KIAS For more information, contact Cessna Single Engine Piston Aircraft, One Cessna Boulevard, Independence, Kansas 67301; telephone 800/423-7762 or 316/517- 6056; or visit the Web site. 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.
What's in the CESSNA 310Q TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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