Cessna Caravan
Maximum Range
1,070 nm
Maximum Cruise Speed
186 ktas
Maximum Passengers
10 - 14
Full Fuel Payload
3,305 lb
Takeoff Ground Roll
11,60 ft
Engine Model
PT6A-114A
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 the 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 limited warranties, parts availability, and lower direct operating costs.
From Passengers to Cargo to Special Missions
Cessna Caravan
The Reliable Multi-tasker
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.
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)
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)
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
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 17 ft 4 in (5.28 m)
Maximum Occupants 10 – 14
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)
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 159 ktas (294 km/h)
Maximum Range 875 nm (1,620 km)
Takeoff Distance 3,660 ft (1,116 m)
Takeoff Water Run 2,341 ft (714 m)
Maximum Operating Altitude 20,000 ft (6,096 m)
Maximum Climb Rate 939 fpm (286 mpm)
Manufacturer Pratt & Whitney Canada
Model PT6A-114A
Power Rating 675 shp (503 kw)
Propeller Manufacturer McCauley
Description 3 blade metal, constant speed, full feathering