*****AIRCRAFT “Cessna - C150 Citation”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

*****Aircraft Features*****

Wing position: High wing (wing struts)

Engine position: Nose mounted

Tail configuration: Regular tail, mid set

Landing gear: Tricycle fixed

Wing Span: 10.2 m

Length: 6.6 m

Height: 2.1 m

Power plant: 1 x 100 HP Continental O-200-A piston engine with two blade propeller.

Accommodation: One pilot and trainee side by side.

Notes: Primary and aerobatic trainer. In service since 1958. CESSNAs return development

to the two seat trainer market. Replaced by CESSNA 152 (ICAO-Designator: C152) from 1977.

Note: Has 1 side window
Alternative names:
A-150,A-A150,Aerobat, A150,Commuter,Aerobat, A-A150,Aerobat, Aerobat (150),

AVIONES COLOMBIA 150, CESSNA 150,A150,Commuter,Aerobat, Commuter (CESSNA)
F150,FA150,FRA150,Aerobat, FA150,FRA150,Aerobat, FMA A-150,A-A150,Aerobat
FRA150,Aerobat, REIMS F150,FA150,FRA150,Aerobat, CESSNA 150,A150,Commuter

 

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

000,000 lbs - 680 kg

VMO - Maximum Operating Speed 100 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:         250 mt

V2 (IAS):         55 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:                 85 kt

ROC:               400 ft/min

-(to FL150)

IAS:                 nd kt

ROC:               nd ft/min

-(to FL240)

IAS:                 nd kt

ROC:               nd ft/min

-(mach)

mach:              nd

ROC:               nd ft/min

 

*****Cruise*****

TAS:                100 kt

MACh:             nd

Ceiling:            FL140

Range:            250 NM

 

****Descent *****

- (to FL240)

mach:              nd

ROD:               nd ft/min

- (to FL100)

IAS:                 90 kt

ROD:               500 ft/min

 

*****Approach*****

IAS:                 80 kt

MCS:               nd kt

ROD:               500 ft/min

 

*****Landing*****

Vht (IAS):        55 kt

APC:                A

Distance:         200 mt