*****AIRCRAFT
“Cessna – C340”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing with
wing tip tanks
Engine position: (Front)
Wing leading mounted
Tail configuration: Regular
tail, mid set
Landing gear: Tricycle retractable
Wing Span: 11.6 m
Length: 10.5 m
Height: 3.8 m
Power plant: 2 x 285 HP
Continental TSIO -520-K or 2 x 310 HP Continental TSIO -520-NB piston engines
with 3 blade propellers.
Accommodation: One pilot and 5 passengers.
Notes: Business aircraft. In service since 1971. Similar production to
BEECHs Duke, slotting in between CESSNA 310 and CESSNA 414/421 with 414s wings
and 310s undercarriage and tail unit. Introduction of a pressuration
system. Production ended in 1984. CESSNA 335 (ICAO designator: C335)
unpressurized, light weight and lower cost development. Built from 1979 to 1980.
Alternative names:
AVIONES COLOMBIA 340,
CESSNA 340, RILEY
Super 340,Rocket 340, Rocket 340
Super 340
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs – 2.710 kg
VMO - Maximum Operating Speed 210 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: 650
mt
V2 (IAS): 95
kts
*****Climbing*****
-(to 5000 ft)
IAS: 125
kt
ROC: 1000
ft/min
-(to FL150)
IAS: 140
kt
ROC: 700
ft/min
-(to FL240)
IAS: 140
kt
ROC: 500
ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
TAS: 210
kt
MACh: nd
Ceiling: FL265
Range: 1200
NM
*****Descent
*****
- (to FL240)
mach: nd
ROD: nd ft/min
- (to FL100)
IAS: 170
kt
ROD: 800
ft/min
*****Approach*****
IAS: 150
kt
MCS: nd kt
ROD: 500
ft/min
*****Landing*****
Vht
(IAS): 93 kt
APC: B
Distance: 500
mt