***AIRCRAFT
“Cessna – T303”***
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: (Front)
Wing leading mounted
Tail configuration: Cruciform tail
Landing gear: Tricycle retractable
Wing Span: 11.9 m
Length: 9.3 m
Height: 4.1 m
Power plant: 2 x 250 HP
Continental TSIO 520 - AE turbocharged piston engines with 3
blade
propellers.
Accommodation: One pilot and 5 passengers.
Notes: Corporate and utility aircraft. In service since 1981.
Turbocharged model of
CESSNA 303 to
replace the CESSNA 310. Production ceased in 1985 after 297 aircraft
were built.
Alternative names:
CESSNA T303 Crusader,
Crusader, T303
Crusader
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs – 2.340 kg
VMO - Maximum Operating Speed 180 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: 533
mt
V2 (IAS): 85
kts
*****Climbing*****
-(to 5000 ft)
IAS: 115
kt
ROC: 1000
ft/min
-(to FL150)
IAS: 130
kt
ROC: 800
ft/min
-(to FL240)
IAS: 130
kt
ROC: 500
ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
TAS: 180
kt
MACh: nd
Ceiling: FL250
Range: 800 NM
*****Descent
*****
- (to FL240)
mach: nd
ROD: nd ft/min
- (to FL100)
IAS: 160
kt
ROD: 800
ft/min
*****Approach*****
IAS: 125
kt
MCS: nd kt
ROD: 500
ft/min
*****Landing*****
Vht
(IAS): 90 kt
APC: A
Distance: 445
mt