C152
Vy
67 KIAS
Vx
55 KIAS
Vso (most rear CofG)
31 KIAS 41 KCAS
Vso (Most forward CofG)
35 KIAS 42 KCAS
Formula for Vref
1.3 VSO KCAS (max. gross wt.) x Sqr root (Landing weight/ Max. Gross weight)
Max Glide
60 KIAS
Short field T/O Flap setting and speed
10 deg and 54 KIAS
Max mag drop
125RPM and 50RPM max difference
Advance on spark
20 deg
Horsepower
118 BHP
Engine model
Lycoming O-235 L2C
Compression ratio
8.5:1
Oil sump capacity
6 quarts
Min oil quantity
2 quarts
Max oil consumtion per hour
0.27 quarts
Usable fuel
24.5 USG
Usable fuel (long range)
37.5
Max T/O weight
1670 LBS
Max weight in rear
120 LBS Max (120 in baggage area 1, 40 in area 2)
VNE
149 KIAS
VNO
111
VA (max weight)
104 KIAS
VFE
85 KIAS
Oil pressure min and max
25-100PSI
G limits flaps up
4.4 and -1.76