F406 Caravan II French Utility Aircraft
F406
Twin-Engine Utility Aircraft
Other



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
Something went wrong. Please reload the page.
Reload