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There is a corresponding difference in range, while all other performance figures are unchanged when speed fairings are installed. Welcome to the ranks of Cessna owners! Your Cessna has been designed and constructed to give you the most in performance, economy, and comfort. It is our desire that you will find flying it, either for business or pleasure, a pleasant and profitable experience. This Pilot's Operating Handbook has been prepared as a guide to help you get the most pleasure and utility from your airplane.

It contains information about your Cessna's equipment, operating procedures, and performance; and suggestions for its servicing and care.

We urge you to read it from cover to cover, and to refer to it frequently. Our interest in your flying pleasure has not ceased with your purchase of a Cessna. Specific benefits and provisions of warranty, plus other important benefits for you, are contained in your Customer Care Program book, supplied with your airplane.

Warranty service is available to you at authorized Cessna Dealers throughout the world upon presentation of your Customer Care Card which establishes your eligibility und. We urge all Cessna owners to use the Cessna Dealer Organization to the fullest. A current Cessna Dealer Directory accompanies your new airplane.

The Directory is revised frequently, and a current copy can be obtained from your Cessna Dealer. Make yqur Directory one of your cross-country flight planning aids; a warm welcome awaits you at every Cessna Dealer. This handbook will be kept current by Service letters published by Cessna Aircraft Company. If you are not receiving subscription service, you will want to keep in touch with your Cessna Dealer for information concerning the change status of the handbook.

Subsequent changes will be made in the form of stickers. These should be examined and attached to the appropriate page in the handbook immediately after receipt; the handbook should not be used for operational purposes until it has been updated to a current status. Cabin And Entry Dimensions.

Baggage Space Dimensions. Maximum height shown with nose gear depressed, all tires and nose strut properly inflated, and flashing beacon installed. Wheel base length is 58". Propeller ground clearance is 12", Wing area is. It also contains supplemental data supplied by Cessna Aircraft Company. Section 1 provides basic data and information of general interest. It also contains definitions or explanations of symbols. Engine Manufacturer: Avco Lycoming.

Engine Model Number: L2C. Engine Type: Normally-aspirated. Number of Blades: 2. Propeller Diameter. Maximum: 69 inches.

Minimum: Propeller Type: Fixed pitch. Total Capacity Each Tank: 13 gallons. Total Usable: Total Capacity Each Tank: Due to cross-feeding between fuel tanks, the tanks should be re-topped after each refueling to assure maximum capacity. Continue to use until a total of 50 hours has accumulated or oil consumption has stabilized. NOTE The airplane was delivered from the factory with a corrosion preventive aircraft engine oil. This oil should be drained after the first 25 hours of operation.

Oil Capacity: Sump: 6 Quarts. Total: 7 Quarts if oil filter installed. See note below. Baggage Area 2 - Station 76 to 40 lbs. NOTE The maximum combined weight capacity for baggage areas 1 and 2 is lbs.

Maximum Useful Load, lbs. Knots calibrated airspeed is equal to KTAS in standard atmosphere at sea level. Knots True Airspeed is the airspeed expressed in knots relative to undisturbed air which is KCAS corrected for altitude and temperature.

Manuevering Speed is the maximum speed at which you may use abrupt control travel. Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position. Maximum Structural Cruising Speed is the speed that should not be exceeded except in smooth air, then only with caution.

Never Exceed Speed is the speed limit that may not be exceeded at any time. Stalling Speed or the minimum steady night speed at which the airplane is controllable.

Stalling Speed or the minimum steady flight speed at which the airplane is controllable in the landing configuration at the most forward center of gravity. Best Angle-of-Climb Speed is the speed which results in the greatest gain of altitude in a given horizontal distance.

Best Rate-of-Climb Speed is the speed which results in the greatest gain in altitude in a given time. Pressure Altitude is the altitude read from an altimeter when the altimeter's barometric scale has been set to Revolutions Per Minute is engine speed.

Static RPM is engine speed attained during a full-throttle engine runup when the airplane is on the ground and stationary. The value shown is not considered to be limiting. Usable Fuel is the fuel available for flight planning. Unusable Fuel is the quantity of fuel that can not be safely used in flight.

Gallons Per Hour is the amount of fuel in gallons consumed per hour. Station is a location along the airplane fuselage given in terms of the distance from the reference datum. Arm is the horizontal distance from the reference datum to the center of gravity C. Moment is the product of the weight of an item multiplied Moment divided by the constant is used in this handbook to simplify balance calculations by reducing the number of digits.

Center of Gravity is the point at which an airplane, or equipment, would balance if suspended. Its distance from the reference datum is found by dividing the total moment by the total weight of the airplane. Center of Gravity Arm is the arm obtained by adding the airplane's individual moments and dividing the sum by the total weight. Center of Gravity Limits are the extreme center of gravity locations within which the airplane must be operated at a given weight. Standard Empty Weight is the weight of a standard airplane, including unusable fuel, full operating fluids and full engine oil.

Basic Empty Weight is the standard empty weight pl us the weight of optional equipment. Useful Load is the difference between takeoff weight and the basic empty weight. Gross Loaded Weight is the loaded weight of the airplane.

Maximum Takeoff Weight is the maximum proved for the start of the takeoff run. Maximum Landing Weight is the maximum proved for the landing touchdown. Tare is the weight of chocks, blocks, stands, etc. Tare is deducted from the scale reading to obtain the actual net airplane weight. Center Of Gravity Limits. Maneuver Limits The limitations included in this section have been approved by the Federal Aviation Administration. When applicable, limitations associated with optional systems or equipment are included in Section 9.

Do not exceed this speed except in smooth air, and then only with caution. Do not make full or abrupt control movements above this speed. Do not exceed this speed with flaps down. Do not exceed this speed with windows open. Lower limit is maximum -weight VSo in landing configuration. Upper limit is maximum speed permissible with flaps extended. Normal Operating Range. Lower limit is maximum weight Vs at most forward C.

Upper limit is maximum structural cruising speed. Operations must be conducted with caution and only in smooth air. Maximum speed for all operations.

Oil Pressure, Minimum: 25 pst, Maximum: psi. Propeller Diameter, Maximum: 69 inches. Maximum Landing Weight: lbs. Aft:


Cessna 152 POH

By using our site, you acknowledge that you have read and understand our Cookie Policy , Privacy Policy , and our Terms of Service. Aviation Stack Exchange is a question and answer site for aircraft pilots, mechanics, and enthusiasts. It only takes a minute to sign up. I'm training in a C and the POH in the backseat has seen its days and I can barely use it, much less keep it from being getting worse than it is. This is a C Trainer aircraft. A lot of questions that I am doing in my flight planning and solo quizzes can be answered through the POH but because the plane is shared I don't want to take it out of the cockpit because it would anger other pilots who also need it.


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