Cessna Corvalis TT

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Cessna Corvalis TT (Twin Turbocharged) is a single-engine, fixed-gear, low-wing general aviation aircraft built from composite materials by Cessna Aircraft. The 400 is powered by a turbocharged Continental TSIO-550-C engine producing 310 horsepower (230 kW) at 2600 rpm. The 400 features a Garmin G1000 glass cockpit that was later incorporated into the 300 to create the Cessna 350.

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The Cessna Corvalis TT leaves the runway at 1,400 vertical feet per minute. Climb to 25,000 feet. Cruise at 235 confident knots. Nothing releases a pilot’s passion for flight like the Cessna Corvalis TT, the world’s fastest fixed- gear aircraft. Yet it’s more than mere blistering speed that makes the Cessna Corvalis TT such a pleasure to fly. There’s the sophisticated, stylish cabin, glass cockpit and side-stick control. Not to mention, the head-turning gorgeous looks.

The Cessna Corvalis TT Model 400 is a pre-molded, composite built, semi-monocoque, four seat, single engine, low wing, tricycle design airplane.The Corvalis TT Model 400 is certified to the requirements of U.S. Federal Aviation Regulation Part 23 through amendment 23-46, including day, night, VFR and IFR.

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Schedule To Demo The Cessna Corvalis TT Today!

Cessna Corvalis TT Approximate Dimensions
Overall Height . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 ft 0 in (2.74m)
Overall Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25 ft 4 in (7.74m)
Wing
Span (overall) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35 ft 10 in (10.92 m)
Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 141.2 sq ft (13.1sq m)
Cabin
Height (max) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49 in (124.5 cm)
Width (max) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49 in (124.5 cm)
Length (firewall to aft limit of baggage compartment) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 140 in (354.6 cm)

Cabin Door
Minimum Entry Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .33 in (83.8 cm)
Minimum Entry Height . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . 33 in (83.8 cm)
Maximum Entry Clearance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 46 in (116.8 cm)

Baggage Compartment
Maximum Baggage Compartment Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .39 in (97.8 cm)
Maximum Baggage Compartment Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .52 in (132 cm) (Including Shelf)
Maximum Baggage Compartment Height . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .35 in (87.6 cm)
Maximum Baggage Entry Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .28 in (71.1 cm) (Diagonal Measurement)

Cessna Corvalis TT Design Weights and Capacities
Maximum Ramp Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3,600 lbs (1,633 kg)
Maximum Takeoff Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3,600 lbs (1,633 kg)
Maximum Landing Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3,420 lbs (1,551 kg)
Standard Empty Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2,575 lbs (1,168 kg)
Maximum Useful Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1,025 lbs (465 kg)
Baggage Allowance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .120 lbs (54.4kg)

Fuel Capacity
Total Capacity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .106 gal (401 L)
Total Useable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .102 gal (386 L)
Total Capacity each Tank . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .53 gal (201 L)

Oil Capacity
Sump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 qts (7.6 L)
Total Capacity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .10 qts (9.5 L)

Cessna Corvalis TT Performance
All estimated performance data are based on airplane weights at 3,600 pounds; standard atmospheric conditions; level, hard surface, dry runways; and no wind. They are calculated values derived from flight tests under carefully documented conditions and will vary with individual airplanes, pilots, and numerous other factors affecting flight performance.

Certified Ceiling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .25,000 ft
Takeoff Distance Ground Roll (S.L.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1,300 ft
Takeoff Distance To Clear 50 ft Obstacle (S.L.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . .1,900 ft
Max Climb Rate (S.L., ISA, MTOW) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . .1,400 fpm
Max Cruise Speed (85% at 25,000 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .235 kts / 270 mph
Economy Cruise Speed (55% at 25,000 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .208 kts / 239 mph
Range at Max Cruise Speed (85% at 25,000 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .825 nm
Range at Economy Cruise Speed (55% at 25,000 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1,250 nm
Landing Distance Ground Roll (S.L., at Max Landing Weight 3,420 lbs) . . . . . . . . . . . . . . . . . . . . . . . . .1,250 ft
Landing Distance To Clear 50 ft Obstacle (S.L., at Max Landing Weight 3,420 lbs) . . . . . . . . . . . . . . . .2,600 ft

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Cessna Corvalis TT Video Overview

Cessna Corvalis TT Has A GARMIN G1000 Avionics Package

GMA-1347 Digital Audio Panel w/Marker Beacon/Intercom
GCU-476 Keypad Controller
GTX-33 Transponder-Mode S w-TIS
GIA-63W NAV/COM/GPS/WAAS w/GS #1
GIA-63W NAV/COM/GPS/WAAS w/GS #2
GDU-1040 Primary Flight Display (PFD)
GDU-1044 Multi-Function Display (MFD)
GEA-71 Engine/Airframe Computer
GRS-77 AHRS
GDC-74A Air Data Computer w/OAT Probe
GMU-44 Magnetometer
GDL-69A Flight Information System (FIS) w/XM

Radio

Terrain Awareness System (TAWS-B)
Electronic Checklist
GFC-700 Autopilot
Go-Around Switch
Electric Trim
A/P Disconnect
Control Stick Steering Button
Garmin SafeTaxi & FliteCharts (FliteCharts do not provide Geosynchronous Positioning)
Traffic Advisory System (TCAD 9900BX / TAS 620)
Backup Airspeed, Altimeter and Attitude (Electric)

Indicator

Control Stick Push-To-Talk Switch-Pilot/Copilot
Mic & Phone Jacks-Pilot/Copilot/Passengers (Bose and Standard)
Marker Beacon Antenna
Transponder Antenna
WAAS (1)
GPS / XM Antenna (1)
COMM Antenna (2)
NAV Antenna
Artex ELT-ME406 Emergency Locator Transmitter
Pitot System – Heated
Static System
Alternate Static Source

Synthetic Vision Technologies (SVT)
Synthetic Vision utilizes GPS-based graphic technology providing virtual depiction of terrain and water features, complete with obstacles and, in the case of aircraft equipped with Traffic Alert and Collision Avoidance (TCAS) systems, airborne traffic, in 3-D perspective that allows pilots enhanced visual cues and improved situational awareness regardless of meteorological or lighting conditions.

Schedule To Demo The Cessna Corvalis TT Today!

Cessna Corvalis TT Exterior

Fiberglass and Honeycomb Structure
LH and RH Gull Wing Style Doors w/Lock and Key
Remote Keyless Entry with Automatic Light System
Pneumatic Door Seal System
LH Cargo Door, w/Lock and Key
Fixed Landing Gear w/castering Nose Wheel
Lighted Entrance Step
Entry Assist and Exit Handles
Main Gear Fairings
Nose Gear and Strut Fairings
Tie Down Rings, LH/RH Wing & Tail
Tube Type Tires
Static Wicks (9)
Emergency Exterior Door Release
Rear Tinted Passenger Windows
Winterization Kit – includes oil cooler door and ground adjustable flap over oil cooler to assist in obtaining optimal temperatures