• Maximum Range

    1,070 nm

  • Maximum Cruise Speed

    186 ktas

  • Maximum Occupants

    10 - 14

  • Useful Load

    3,305 lb

  • Takeoff Distance

    2,055 ft

THE ORIGINAL TRAILBLAZER

The Cessna® Caravan® aircraft is known for its rugged utility and flexibility. With its powerful turboprop engine, the Caravan aircraft delivers the rare combination of high performance, low operating costs and ability to adapt to a wide variety of missions.

The powerful, efficient, dependable 675-horsepower PT6A-114A turbine engine gives the Caravan® turboprop its exceptional payload capabilities.

Operators in the world’s most demanding environments immediately adopted the rugged, dependable turboprop and have been rewarded with unparalleled dispatch reliability. On top of more than 30 years of proven capability comes even greater value with the Caravan® turboprop’s lower direct operating costs and factory support.

Exterior

RUGGED LANDING GEAR

Large, rough-field tires and rugged landing gear allow you to operate from grass, gravel and even more rudimentary runways.


Ramp Vision

Cessna Caravan

ONE AIRCRAFT. EVERY ENVIRONMENT.

Click to see how the Caravan® turboprop family can adapt to any environment.

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Interior

Ultimate Cabin Flexibility

  • 10 Commuter
  • 11 Club
  • 11 Commuter

Choose an Interior Package

  • Canyon

    The high contrast black and khaki of Canyon is warm and sophisticated.

  • Savanna

    The classic neutral khaki of Savanna is contemporary and clean.

Advanced Display Technology

Enjoy the spacious cockpit powered by the latest technology — Garmin® G1000® NXi avionics suite. Managing the flight deck has never been easier with an improved graphical interface, more powerful hardware, higher-resolution displays and added functionality for increased situational awareness.

  • GDU 1050A Pilot and Copilot Primary Flight Displays (PFD)
  • GDU 1050A Multifunction Display (MFD)
  • GDL® 60 Datalink
  • GI 275 Electronic Standby Indicator
  • GDC 72 Dual Air Data Computer (ADC)
  • GEA 71B Engine/Airframe Unit
  • GRS 79 Dual Attitude and Heading Reference System (AHRS)
  • GMA 1360D Dual Audio System with bluetooth capability and 3D audio
  • GTX 335R ADS-B Out Transponder
  • Garmin® Relative Terrain/Obstacles
  • Garmin® FliteCharts
  • GTX 345DR In/Out Capability
  • Garmin® SafeTaxi
  • Integrated VFR Sectional Charts
  • IFR High and Low Altitude Charts with Auto/Day/Night Modes
  • KN-63 DME
  • Wireless database uploads and flight plan transfers

Featuring Next-Generation Garmin G1000 NXi Options

  • Enhanced Automatic Flight Control System
    Adds electronic stability and protection (ESP), under speed protection (USP), emergency descent mode (EDM), auto-level function, coupled go-around, automatic autopilot activation and expanded envelope engagement to the standard automatic flight control system.
  • Garmin® GSR 56 Iridium Transceiver
    Provides access to datalink weather services. Worldwide coverage is provided by the Iridium satellite network, which also provides satellite voice communication and text message capabilities. An Iridium service account and accompanying data/weather subscription plans are required.
  • TAWS-A
    Provides visual and aural warning alerts for terrain avoidance. It supports steep approach functionality and warning modes such as excessive descent rate, altitude loss after takeoff and inadvertent descent below glideslope. In addition, the Class A TAWS uses GPS input and a worldwide terrain database to display an enhanced graphical plan view of terrain, color coded in relation to the aircraft’s position. This option requires the KRA 405B Radar Altimeter described below.
  • KRA 405B Radar Altimeter
    Gives an absolute altitude indication from 2,500 to 0 feet AGL. Provides selection of warning altitude and annunciation via both a decision height light (displayed on the pilot and co-pilot’s PFD) and an aural warning.
  • GWX™ 8000
    Advanced Doppler weather radar with volumetric scanning capability which automatically adjusts antenna sweep pattern to accurately profile weather cells and provide threat analysis.
  • Synthetic Vision Technology
    Improved topographical clarity of Synthetic Vision Technology terrain creating more distinct mountains, valleys and other terrain features.
  • Taxi Routing
    The Taxiway Routing feature is designed to reduce runway incursions by providing guidance while taxiing for airports contained in the SafeTaxi Database.
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Specifications

Length

37 ft 7 in (11.5 m)

Height

14 ft 10 in (4.5 m)

Wingspan

52 ft 1 in (15.9 m)

Dimensions

Length 37 ft 7 in (11.5 m)
Height 14 ft 10 in (4.5 m)
Wingspan 52 ft 1 in (15.9 m)
Wing Area 279 sq ft (25.96 sq m)
Wheelbase 11 ft 8 in (3.54 m)
Tread 11 ft 8 in (3.56 m)

Cabin Interior

Height 54 in (1.4 m)
Width 64 in (1.63 m)
Length 12 ft 9 in (3.9 m)
Maximum Occupants 10 - 14

Baggage Capacity

Weight 325 lb (147 kg)
Volume 31.5 cu ft (0.89 cu m)

Weights

Maximum Ramp Weight 8,035 lb (3,645 kg)
Maximum Takeoff Weight 8,000 lb (3,629 kg)
Maximum Landing Weight 7,800 lb (3,538 kg)
Usable Fuel Weight 2,224 lb (1,009 kg)
Usable Fuel Volume 332 gal (1,257 l)
Basic Empty Weight 4,730 lb (2,145 kg)
Useful Load 3,305 lb (1,499 kg)
Maximum Payload 3,070 lb (1,393 kg)
Full Fuel Payload 1,081 lb (490 kg)

Performance

Maximum Cruise Speed 186 ktas (344 km/h)
Maximum Range 1,070 nm (1,982 km)
Takeoff Distance 2,055 ft (626 m)
Ground Roll 1,160 ft (354 m)
Landing Distance 1,625 ft (495 m)
Ground Roll 715 ft (218 m)
Maximum Operating Altitude 25,000 ft (7,620 m)
Maximum Climb Rate 1,234 fpm (376 mpm)
Maximum Limit Speed 175 kias (324 km/h)
Stall Speed 61 kcas (113 km/h)

Powerplant

Manufacturer Pratt & Whitney Canada
Model PT6A-114A
Power Rating 675 shp (503 kW)
Propeller Manufacturer McCauley
Description 3 blade metal, constant speed, full feathering

Dimensions

Length 38 ft 1 in (11.6 m)
Height 17 ft 7 in (5.4 m)
Wingspan 52 ft 1 in (15.9 m)
Wing Area 279 sq ft (25.96 sq m)
Wheelbase 14 ft 7 in (4.44 m)
Tread 10 ft 8 in (3.25 m)

Cabin Interior

Height 54 in (1.4 m)
Width 64 in (1.63 m)
Length 12 ft 9 in (3.9 m)
Maximum Occupants 10 - 14

Baggage Capacity

Weight 925 lb (420 kg)
Volume 100.1 cu ft (2.83 cu m)

Weights

Maximum Ramp Weight 8,785 lb (3,985 kg)
Maximum Takeoff Weight 8,750 lb (3,969 kg)
Maximum Landing Weight 8,750 lb (3,969 kg)
Usable Fuel Weight 2,224 lb (1,009 kg)
Usable Fuel Volume 332 gal (1,257 l)
Basic Empty Weight 5,585 lb (2,533 kg)
Useful Load 3,200 lb (1,451 kg)
Maximum Payload 3,165 lb (1,436 kg)
Full Fuel Payload 976 lb (443 kg)

Performance

Maximum Cruise Speed 159 ktas (294 km/h)
Maximum Range 875 nm (1,620 km)
Takeoff Distance 3,660 ft (1,116 m)
Ground Roll 2,341 ft (714 m)
Landing Distance 1,853 ft (565 m)
Ground Roll 1,206 ft (368 m)
Maximum Operating Altitude 20,000 ft (6,096 m)
Maximum Climb Rate 939 fpm (286 mpm)
Maximum Limit Speed 175 kias (324 km/h)
Stall Speed 60 kcas (111 km/h)

Powerplant

Manufacturer Pratt & Whitney Canada
Model PT6A-114A
Power Rating 675 shp (503 kW)
Propeller Manufacturer McCauley
Description 3 blade metal, constant speed, full feathering