PERFORMANCE CESSNA
SPECIFICATION MODEL 152
ii 1 July 1978
PERFORMANCE - SPECIFICATIONS
Speed *
Maximum at Sea Level.......................................................................................................110 knots
Cruise, 75% Power at 8,000 ft............................................................................................107 knots
CRUISE: Recommended lean mixture with fuel allowance for
engine start, taxi, takeoff, climb and 45 minutes
reserve at 45% power
75% Power at 8,000 ft ...................................................... Range 350 NM
24.5 Gallons usable fuel.............................................. Time 3.4 hours
75% Power at 8,000 ft ...................................................... Range 580 NM
37.5 Gallons usable fuel.............................................. Time 5.5 hours
Maximum Range at 10,000 ft ........................................... Range 415 NM
24.5 Gallons usable fuel.............................................. Time 5.2 hours
Maximum Range at 10,000 ft ........................................... Range 690 NM
37.5 Gallons usable fuel.............................................. Time 8.7 Hours
RATE OF CLIMB AT SEA LEVEL.......................................................................................715 FPM
SERVICE CEILING............................................................................................................14,700 FT
TAKEOFF PERFORMANCE
Ground Roll...................................................................................................................725 ft
Total Distance over 50 ft obstacle..............................................................................1340 ft
LANDING PERFORMANCE
Ground roll....................................................................................................................475 ft
Total Distance over 51 ft obstacle..............................................................................1200 ft
STALL SPEED (CAS)
Flaps up, power off..................................................................................................48 knots
Flaps down, power off .............................................................................................43 knots
MAXIMUM WEIGHT
Ramp ......................................................................................................................1675 lb
Takeoff or landing......................................................................................................1670 lb
STANDARD EMPTY WEIGHT
152 ......................................................................................................................1101 lb
152 II 1..................................................................................................................1133 lbs
MAXIMUM USEFUL LOAD
152 ......................................................................................................................574 lbs
152 II ......................................................................................................................54 lbs2
BAGGAGE ALLOWANCE......................................................................................................120 lbs
WING LOADING (Pounds / s.f.) ..................................................................................................10.5
POWER LOADING (Pounds / HP) ..............................................................................................15.2
FUEL CAPACITY
Standard Tanks ........................................................................................................ 26 GAL
Long Range Tanks ................................................................................................... 39 GAL
OIL CAPACITY ..........................................................................................................................6 qts
ENGINE: Avco Lycoming 110 bhp at 255o rpm................................................................O235-L2C
PROPELLER: Fixed Pitch, diameter .........................................................................................69 in.
* Speed performance is shown for an airplane equipped with optional speed fairings which
increase the speeds by approximately 2 kts. There is a corresponding difference in range
while all other performance figures are unchanged when speed fairings are installed.
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