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CESSNA 150/152 SPECIFICATIONS

CESSNA 152 SPECIFICATIONS

CESSNA 152 SPECIFICATIONS

GENERAL CHARACTERISTICS

 
Crew:
one pilot
 
 
Capacity:
one passenger
 
 
Length:
24 feet, 1 inches 
 
 
Wingspan:
33 feet, 4 inches
 
 
Height:
8 feet, 6 inches
 
 
Empty weight:
1,081 pounds 
 
 
Max. takeoff weight:
1,670 pounds
 
 
Powerplant:
(1) Lycoming O-235-L2C flat-4 engine, 110 hp driving a 69-inch, two-blade, fixed-pitch McCauley propeller or a 72-inch, two-blade, fixed-pitch Sensenich propeller

PERFORMANCE

 
Maximum speed:
126 mph (110 knots)
 
 
Cruise Speed:
123 mph (107 knots)
 
 
Stall speed:
49 mph (43 knots) unpowered, flaps down
 
 
Takeoff roll:
725 feet
 
 
Range:
414 nm (477 miles)
 
 
Extended range:
690 nm (795 miles) with long-range tanks
 
 
Service ceiling:
14,700 feet
 
 
Rate of climb:
715 fpm
 

CESSNA 150M SPECIFICATIONS

CESSNA 150M SPECIFICATIONS

GENERAL CHARACTERISTICS

 
Crew:
 one
 
 
Capacity:
one passenger (plus two children, limited to 132 pounds with optional rear child seat) 
 
Length:
24 feet, 9 inches 
 
 
Wingspan:
33 feet, 4 inches
 
 
Height:
8 feet, 6 inches
 
 
Empty weight:
1,111 pounds 
 
 
Useful load:
490 pounds
 
 
Max. takeoff weight:
1,600 pounds
 
 
Powerplant:
(1) Continental O-200-A flat-4 engine, 100 hp at 2,750 rpm 

PERFORMANCE

 
Never exceed speed:
141 knots (162 mph) 
 
 
Cruise Speed:
107 knots (123 mph) 
 
 
Stall speed:
42 knots (48 mph)
 
 
Range:
366 nm (421 miles) 
 
 
Service ceiling:
14,000 feet 
 
 
Rate of climb:
670 fpm 
 
 
Fuel consumption:
6 gallons (US) of Avgas