• Maximum Range

    912 nm

  • Maximum Cruise Speed

    185 ktas

  • Maximum Occupants

    10 - 14

  • Useful Load

    3,532 lb

  • Takeoff Distance

    2,160 ft

THE ULTIMATE UTILITY VEHICLE

The Cessna® Grand Caravan® EX aircraft is known for its dependable and efficient performance by regional airlines, charter operators and cargo carriers worldwide. The Grand Caravan EX turboprop was engineered for challenging missions, high payloads and short, rough runways while delivering single-engine economy and simplicity.

The Grand Caravan® EX aircraft has a reputation as a revenue generator. It carries up to 14 occupants with an increased speed and climb capability, plus a takeoff ground roll of only 1,399 ft. Its powerful Pratt & Whitney Canada engine delivers 867 horsepower for dependable payload performance and superior efficiency. Experience true value with low direct operating costs and factory support.

INTERIOR 360°

Explore the large, spacious cabin of the Grand Caravan® EX aircraft.
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*Oasis interior shown

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Exterior Cabin Avionics

Exterior

THE RELIABLE MULTITASKER

The Grand Caravan® EX turboprop was engineered for challenging missions, high payloads and short, rough runways while delivering single-engine economy and simplicity.

Ramp Vision

Cessna Grand Caravan EX

ONE AIRCRAFT. EVERY ENVIRONMENT.

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Interior

Ultimate Cabin Flexibility

  • 10 Commuter
  • 13 Club
  • 13 Commuter
  • 14 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.

  • Oasis

    The Oasis optional third party interior is the optimal blend of precision craftsmanship, quality materials, and luxury appointments.

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
  • Garmin® SafeTaxi
  • GTX 345DR In/Out Capability
  • 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 provid e 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

41 ft 7 in (12.7 m)

Height

15 ft 6 in (4.7 m)

Wingspan

52 ft 1 in (15.9 m)

Dimensions

Length 41 ft 7 in (12.7 m)
Height 15 ft 6 in (4.7 m)
Wingspan 52 ft 1 in (15.9 m)
Wing Area 279 sq ft (25.96 sq m)
Wheelbase 13 ft 4 in (4.05 m)
Tread 11 ft 8 in (3.56 m)

Cabin Interior

Height 54 in (1.4 m)
Width 64 in (1.63 m)
Length 16 ft 9 in (5.1 m)
Maximum Occupants 10 - 14

Baggage Capacity

Weight 1,410 lb (640 kg)
Volume 143 cu ft (4.05 cu m)

Weights

Maximum Ramp Weight 8,842 lb (4,011 kg)
Maximum Takeoff Weight 8,807 lb (3,995 kg)
Maximum Landing Weight 8,500 lb (3,856 kg)
Usable Fuel Weight 2,246 lb (1,019 kg)
Usable Fuel Volume 335 gal (1,269 l)
Basic Empty Weight 5,310 lb (2,409 kg)
Useful Load 3,532 lb (1,602 kg)
Maximum Payload 3,190 lb (1,447 kg)
Full Fuel Payload 1,286 lb (583 kg)

Performance

Maximum Cruise Speed 185 ktas (343 km/h)
Maximum Range 912 nm (1,689 km)
Takeoff Distance 2,160 ft (658 m)
Ground Roll 1,399 ft (426 m)
Landing Distance 1,836 ft (560 m)
Ground Roll 1,004 ft (306 m)
Maximum Operating Altitude 25,000 ft (7,620 m)
Maximum Climb Rate 1,275 fpm (389 mpm)
Maximum Limit Speed 175 kias (324 km/h)
Stall Speed 61 kcas (113 km/h)

Powerplant

Manufacturer Pratt & Whitney Canada
Model PT6A-140
Power Rating 867 shp (867 shp)
Propeller Manufacturer McCauley
Description 4 blade aluminum, constant speed, full feathering

Dimensions

Length 41 ft 7 in (12.7 m)
Height 17 ft 5 in (5.3 m)
Wingspan 52 ft 1 in (15.9 m)
Wing Area 279 sq ft (25.96 sq m)
Wheelbase N/A
Tread 7 ft 2 in (2.18 m)

Cabin Interior

Height 54 in (1.4 m)
Width 64 in (1.63 m)
Length 16 ft 9 in (5.1 m)
Maximum Occupants 10 - 14

Baggage Capacity

Weight 920 lb (417 kg)
Volume 100.1 cu ft (2.83 cu m)

Weights

Maximum Ramp Weight 9,097 lb (4,126 kg)
Maximum Takeoff Weight 9,062 lb (4,110 kg)
Maximum Landing Weight 9,062 lb (4,110 kg)
Usable Fuel Weight 2,246 lb (1,019 kg)
Usable Fuel Volume 335 gal (1,269 l)
Basic Empty Weight 5,975 lb (2,710 kg)
Useful Load 3,122 lb (1,416 kg)
Maximum Payload 3,087 lb (1,400 kg)
Full Fuel Payload 876 lb (397 kg)

Performance

Maximum Cruise Speed 164 ktas (304 km/h)
Maximum Range 813 nm (1,506 km)
Takeoff Distance 3,271 ft (997 m)
Ground Roll 2,000 ft (610 m)
Landing Distance 2,004 ft (611 m)
Ground Roll 873 ft (266 m)
Maximum Operating Altitude 20,000 ft (6,096 m)
Maximum Climb Rate 1,212 fpm (369 mpm)
Maximum Limit Speed 175 kias (324 km/h)
Stall Speed 59 kcas (109 km/h)

Powerplant

Manufacturer Pratt & Whitney Canada
Model PT6A-140
Power Rating 867 shp (867 shp)
Propeller Manufacturer McCauley
Description 4 blade aluminum, constant speed, full feathering