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
PT6A-140
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
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
KN-63 DME
Flight Stream 510 for 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 2,000 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