*****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