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F406 Caravan II French Utility Aircraft

F406

Twin-Engine Utility Aircraft
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Basic Information
Name
F406 Caravan II French Utility Aircraft
Designation
F406
Alternate Designation
Equipment Type
Twin-Engine Utility Aircraft
Manufacturer
Reims Aviation
Date of Introduction
1983
Description

The Reims-Cessna F406 Caravan II is a turboprop twin engine utility aircraft manufactured and designed by Reims Aviation in cooperation with Cessna.

Air & Air Defense Specifications
Crew 1
Engine Turboprop (373 hp)
Max Speed 424.0 km/h
Range 2135.0 km
Service Ceiling 9145 m
System
Alternate Designation(s) F406 Caravan II
Type Twin-Engine Utility Aircraft
Manufacturer Reims Aviation
Crew 1
Passenger Capacity 12
Number of Engines 2
Number of Hard Points INA
Dimensions
Length 11.89 m
Width (Wing Span) 15.09 m
Wing Area 23.48 m2
Height 4.01 m
Empty Weight 2,283 kg
Gross Weight 4,246 kg
Automotive
Engine Name 2 × Pratt & Whitney Canada PT6A-112
Engine Type Turboprop
Engine Power 373 kW (500 hp) each
Maximum Range 2,135 km
Maximum Speed 424 km/h
Cruising Speed 260 km/h
Service Ceiling 9,145 m
Rate of Climb 9.4 m/s
Protection
Stealth Properties None
Heat Signature Reduction No
Add on Armor No
NBC Protection INA
EW Counter Measures No
Chaffs/Flares No
Details
Country of Origin France
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
F
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
11.89 m
Width
15.09 m
Height
4.01 m
Weight
4246 kg
Operators (6)
France
United Kingdom
South Korea
Australia
Greece
Namibia
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