***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