*****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