*****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