*****AIRCRAFT
“Cessna – F406 Caravan2”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: (Front)
Wing leading mounted
Tail configuration: Cruciform
tail
Landing gear: Tricycle
retractable
Wing Span: 15.1 m
Length: 11.9 m
Height: 4.0 m
Power plant: 2 x 500 SHP
P&W PT6A-112 turboprops with 3 blade propellers.
Accommodation: One or two pilots and 8 passengers in main cabin.
Notes: Executive transport aircraft. In service since 1984. Hybrid
development of CESSNA 404 Titan (unpressurized fuselage) and CESSNA 441
Conquest 2 (wings). Caravan 2 is the only CESSNA turbo-prop twin aircraft
currently in production by REIMS, France.
Alternative names:
CESSNA F406 Caravan
2, F406 Caravan 2, REIMS F406 Caravan 2.
*****Total
Flight Simulator aircraft weight with full fuel*****
0000 lbs - 4.200 kg
VMO - Maximum Operating Speed 240 KIAS
MMO - Maximum Operating Speed Mach nd Mach
Turbulent Air Penetration Speed 000 KIAS/.00 Mach
VLO - Maximum Gear Operating Speed 000 KIAS
VLE - Maximum Landing Gear Extension Speed 000 KIAS/.00 Mach
*****Maximum
Flap Placard Speeds*****
Flaps degrees KIAS
0 000
1 0 0
2 0 0
3 full 0
gear down 0
(stalling 0)
*****Take-off*****
WTC: L
Distance: 700
mt
V2 (IAS): 100
kts
*****Climbing*****
-(to 5000 ft)
IAS: 130
kt
ROC: 2000
ft/min
-(to FL150)
IAS: 200
kt
ROC: 1500
ft/min
-(to FL240)
IAS: 200
kt
ROC: 1000
ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
TAS: 240
kt
MACh: nd data
Ceiling: FL300
Range: 1000 NM
*****Descent
*****
- (to FL240)
mach: nd
ROD: nd ft/min
- (to FL100)
IAS: 240
kt
ROD: 1200
ft/min
*****Approach*****
IAS: 180
kt
MCS: nd kt
ROD: 500
ft/min
*****Landing*****
Vht
(IAS): 95 kt
APC: B
Distance: 650
mt