*****AIRCRAFT “Cessna – C310”*****

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: 11.3 m

Length: 9.7 m

Height: 3.3 m

Power plant: 2 x 240 HP Continental IO-470-M or 2 x 260 HP Continental IO-470-D or

2 x 285 HP Continental IO-520-M piston engines with 3 blade propellers.

T310: 2 x 285 HP Continental TSIO-520-B turbocharged piston engines with 3

blade propeller.

Accommodation: One pilot and 4 (optional 5) passengers.

Notes: Light piston aircraft. In service since 1954. First civil twin engine aircraft designed

by CESSNA. Exists in both civil and military versions. A development of 310F was the turbocharged 320 Skyknight (ICAO designator: C320) with a fourth cabin window.

It was replaced by the similar T310. The 310G introduced tiptanks, 310K replaced the

rear two windows on each side by a single unit. Production ended in 1987 after more

than 5400 civil- and 196 of the military versions had been built . US-mil. type: U-3.

The Turbo-charged version has got a ceiling of FL274.
Alternative names:
65,Rocket,Super 310,Turbo-Rocket, AVIONES COLOMBIA 310, Bearcat, CESSNA 310,

T310 (U-3,L-27), COLEMILL Bearcat,Executive 600, Executive 600, L-27, RILEY 65,Rocket,Super 310,Turbo-Rocket, Rocket, Super 310, T310, Turbo-Rocket, U-3,

CESSNA 310,T310

 

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

000,000 lbs – 2.494 kg

VMO - Maximum Operating Speed 175 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:         507 mt

V2 (IAS):         95 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:                 125 kt

ROC:               1000 ft/min

-(to FL150)

IAS:                 125 kt

ROC:               800 ft/min

-(to FL240)

IAS:                 nd kt

ROC:               nd ft/min

-(mach)

mach:              nd

ROC:               nd ft/min

 

*****Cruise*****

TAS:                175 kt

MACh:             nd

Ceiling:            FL200

Range:             500 NM

 

*****Descent *****

- (to FL240)

mach:              nd

ROD:               nd ft/min

- (to FL100)

IAS:                 150 kt

ROD:               800 ft/min

 

*****Approach*****

IAS:                 130 kt

MCS:               nd kt

ROD:               500 ft/min

 

*****Landing*****

Vht (IAS):        94 kt

APC:                B

Distance:         546 mt