*****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