*****AIRCRAFT
“Cessna – C425 Corsair”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: (Front)
Wing leading mounted
Tail configuration: Regular
tail (Dihedral)
Landing gear: Tricycle retractable
Wing Span: 13.5 m
Length: 10.9 m
Height: 3.9 m
Power plant: 2 x 450 SHP PW
PT6A-112 turboprops with 3 blade propellers.
Accommodation: One or two pilots and 4 passengers in corporate -, up
to 6 in high density configuration.
Notes: Executive transport aircraft. In service since 1980. Turbo-prop
powered version of CESSNA 421 Golden Eagle. Cessna renamed the Corsair to
Conquest 1 and the Conquest to Conquest 2 in 1983. Production ceased in 1986.
Alternative names:
CESSNA 425 Corsair,Conquest 1, Conquest 1, Corsair (CESSNA), CESSNA 425 Corsair.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs – 3.900 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
1 000
2 000
5 000
10 000
15 000
25 000
30 000
40 000
*****Take-off*****
WTC: L
Distance: 750
mt
V2 (IAS): 105
kts
*****Climbing*****
-(to 5000 ft)
IAS: 135
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
Ceiling: FL310
Range: 1250
NM
*****Descent
*****
- (to FL240)
mach: nd
ROD: nd ft/min
- (to FL100)
IAS: 240
kt
ROD: 1500
ft/min
*****Approach*****
IAS: 240
kt
MCS: nd kt
ROD: 1500
ft/min
*****Landing*****
Vht
(IAS): 110 kt
APC: B
Distance: 650
mt