*****AIRCRAFT “Cessna – C414 Chancellor”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

*****Aircraft Features*****

Wing position: Low wing

Engine position: (Front) Wing leading mounted

Tail configuration: Regular tail, mid set

Landing gear: Tricycle retractable

Wing Span: 12.5 m

Length: 10.3 m

Height: 3.6 m

Power plant: 2 x 310 HP Continental TSIO-520-NB turbocharged piston engines with 3 blade propellers.

Accommodation: One pilot and typical 6 passengers in main cabin.

Notes: Utility twin aircraft. In service since 1969. Less powerful, light and low cost model of CESSNA 421 Golden Eagle. Features wing of CESSNA 402 and fuselage of CESSNA 421. Improved version CESSNA 414A Chancellor (appeared in 1978) with bonded wet wing, without tip tanks. Remained in production until 1985.
Alternative names:
AVIONES COLOMBIA 414, CESSNA 414,Chancellor, Chancellor, RILEY Rocket Power 414, Rocket Power 414.

 

*****Total Flight Simulator aircraft weight with full fuel*****  

000,000 lbs – 3.060 kg

VMO - Maximum Operating Speed 230 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:         520 mt

V2 (IAS):         100 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:                 130 kt

ROC:               1200 ft/min

-(to FL150)

IAS:                 150 kt

ROC:               1000 ft/min

-(to FL240)

IAS:                 150 kt

ROC:               800 ft/min

-(mach)

mach:              nd

ROC:               nd ft/min

 

*****Cruise*****

TAS:                230 kt

MACh:             nd

Ceiling:                        FL310

Range:            1100 NM

 

*****Descent *****

- (to FL240)

mach:              nd

ROD:               nd ft/min

- (to FL100)

IAS:                 200 kt

ROD:               1000 ft/min

 

*****Approach*****

IAS:                 180 kt

MCS:               nd kt

ROD:               1000 ft/min

 

*****Landing*****

Vht (IAS):        110 kt

APC:                B

Distance:         720 mt