*****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