Cessna 152 - Performance Specifications for O-235-N2 C Engine

O-235-N2C
ENGINE
MODEL
152
PILOT'S
OPERATING
HANDBOOK
SUPPLEMENT
PERFORMANCE-SPECIFICATIONS
•SPEED:
Maximum
at
Sea
Level.
. . . . . . . . . . . . .
Cruise,
75%
Power
at
8500
Ft
. • . . . . . . . . .
CRUISE:
Recommended
lean
mixture
with
fuel
allowance
for
engine
start,
taxi,
takeoff,
climb
and
45
minutes
reserve
at
45%
power.
75%
Power
at
8500
Ft
. .
24.5
Gallons
Usable
Fuel
75%
Power
at
8500
Ft
. .
37.5
Gallons
Usable
Fuel
Maximum
Range
at
10,000
Ft
.
24.5
Gallons
Usable
Fuel
Maximum
Range
at
10,000
Ft
.
37.5
Gallons
Usable
Fuel
RATE
OF
CLIMB
AT
SEA
LEVEL
SERVICE
CEILING
TAKEOFF
PERFORMANCE:
Ground
Roll
. . . .
Total
Distanoe
Over
50-Ft
Obstacle
LANDING
PERFORMANCE:
Ground
Roll
. . . . . . . .
Total
Distance
Over
50-Ft
Obstacle
STALL
SPEED
(CAS):
Flaps
Up,
Power
Off.
.
Flaps
Down,
Power
Off
MAXIMUM
WEIGHT:
~P-
.....
.
Takeoff
or
Landing
. .
STANDARD
EMPTY
WEIGHT:
152.
. . . . . . .
152
II.
. . . . . .
MAXIMUM
USEFUL
LOAD:
152.
. . . . . .
152
II
. . . . . . .
BAGGAGE
ALLOWANCE
.
WING
LOADING:
Pounds/Sq
Ft
.
POWER
LOADING:
Pounds/HP
FUEL
CAPACITY:
Total
Standard
Tanks
.
Long
Range
Tanks
.
OIL
CAPACITY
. . . .
ENGINE:
Avco
Lycoming
108
BHP
at
2550
RPM
PROPELLER:
Fixed
Pitch,
Diameter
Range
Time
Range
Time
Range
Time
Range
Time
109
KNOTS
106KNOTS
335NM
3.3
HRS
560NM
5.4
HRS
375NM.
4.2HRS
630NM
6.9HRS
715FPM
14,700FT
725
FT
1340
FT
475FT
1200
FT
48KNOTS
43KNOTS
1675
LBS
1670
LBS
1101
LBS
1133
LBS
574
LBS
542
LBS
120
LBS
10.5
15.5
26
GAL.
39
GAL.
6QTS
O-235-N2C
69
IN.
*Speed
performance
is
shown
for
an
airplane
equipped
with
optional
speed
fairings,
which
increase
the
speeds
by
approximately
2
knots.
There
is
a
corresponding
difference
in
range,
while
all
other
performance
figures
are
unchanged
when
speed
fairings
are
in-
stalled.
2
1
July
1978
Revision
1 -
31
March
1983