Grand Caravan EX

Maximum Range

912 nm

Maximum Cruise Speed

185 ktas

Maximum Passengers

10 - 14

Full Fuel Payload

3,532 lb

Takeoff Ground Roll

13,99 ft

Engine Model


Single-Engine Economy Delivered With Simplicity.

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 climbs 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, limited warranties, and a wide breadth of parts available on demand.

Passengers, Cargo and Special Mission’s Solution

Grand Caravan EX

The Reliable Multitasker

The Grand Caravan EX was engineered for challenging missions, high payloads, and short, rough runways while delivering a single-engine economy to be loved by the charter operators and cargo carriers.

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.

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)

GDU 1050A Pilot and Copilot Primary Flight Displays (PFD)

GDU 1050A Multifunction Display (MFD)

GDC 72 Dual Air Data Computer (ADC)

GEA 71 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

Integrated VFR Sectional Charts

IFR High and Low Altitude Charts with Auto/Day/Night Modes


Flight Stream 510 for wireless database uploads and flight plan transfers


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.


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 2,000 to 0 feet AGL. Provides a 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.

Height 54 in (1.37 m)

Width 64 in (1.63 m)

Length 21 ft 4 in (6.50 m)

Maximum Occupants 10 – 14

Weight 1,410 lb (640 kg)

Volume 143 cu ft (4.05 CU m)

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)

Maximum Cruise Speed 185 ktas (343 km/h)

Maximum Range 912 nm (1,689 km)

Takeoff Distance 2,160 ft (658 m)

Takeoff Ground Roll 1,399 ft (426 m)

Landing Distance 1,836 ft (560 m)

Landing Ground Roll 1,004 ft (306 m)

Maximum Operating Altitude 25,000 ft (7,620 m)

Maximum Climb Rate 1,275 fpm (389 mpm)

Manufacturer Pratt & Whitney Canada

Model PT6A-140

Power Rating 867 shp (647 kW)

Propeller Manufacturer McCauley

Description 4 blade aluminum, constant speed, full feathering