*****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