*****AIRCRAFT “Cessna - C152 Aerobat”*****

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: 7.3 m

Height: 2.6 m

Power plant: 1 x 180 HP Lycoming O-235-N26 piston engine with 2 blade propeller.

Accommodation: One pilot and one passenger side by side.

Notes: Primary and aerobatic capable trainer. In service since 1977. World´s most successful light trainer. CESSNA 152 replaced the CESSNA 150 Commuter (ICAO-Designator: C150). More than 31.280 CESSNA 150 and 152 in many versions were built over 27 years. Production ended by CESSNA in 1985 but continued by REIMS in France as F-152. Note: Has 1 side window
Alternative names:
A152,Aerobat, Aerobat (152), AVIONES COLOMBIA 152, CESSNA 152, A152, Aerobat, F152,FA152,Aerobat, FA152,Aerobat, REIMS F152,FA152,Aerobat

 

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

000,000 lbs - 760 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:   220 mt

V2 (IAS):   60 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:        85 kt

ROC:        500 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:    FL147

Range:      315 NM

 

*****Descent *****

- (to FL240)

mach:       nd

ROD:        nd ft/min

- (to FL100)

IAS:        100 kt

ROD:        500 ft/min

 

*****Approach*****

IAS:        80 kt

MCS:        nd kt

ROD:        500 ft/min

 

*****Landing*****

Vht (IAS):  55 kt

APC:        A

Distance:   170 mt