1979 CESSNA 152 POH PDF

Page Count: Standard Tem perature Chart added January 2, 3. Performance - S pecifications. Maximum at Sea Level ……………………………………. Range NM. Time 3.

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Quick Links. Download this manual. Table of Contents. Aircrafts Cessna Handbook Two-seat, fixed tricycle gear, general aviation airplane 34 pages. Page 2: July This is a duplicate manual issued to replace one originally provided for the airplane identified on the cover page on All revisions, if any, have been incorporated as of Subsequent revisions supplied by Cessna Aircraft Company must be properly inserted Cessna Aircraft Co.

Page 3: Model Our interest in your flying pleasure has not ceased with your purchase of a Cessna. Page 9: Introduction This handbook contains 9 sections, and includes the material required to be furnished to the pilot by CAR Part 3. 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, abbreviations, and terminology commonly used.

Its distance from the reference datum is found dividing the total moment by the total weight of the airplane C. A19 as Cessna Model No Lower limit is maximum weight V-so in landing configuration. In the acquisition of various certificates such as commercial pilot and flight instructor, certain maneuvers are required.

The markings and placards installed in this airplane contain operating limitations which must be complied with when operating this airplane in the Utility Category.

Near fuel shutoff valve standard tanks. FUEL — Near fuel tank filler cap standard tanks. On oil filler cap. On control lock. Emergencies caused by airplane or engine malfunctions are extremely rare if proper preflight inspections and maintenance are practiced. Enroute weather emergencies can be minimized or eliminated by careful flight planning and good judgment when unexpected weather is encountered.

Airspeed -- 60 KIAS. Carburetor Heat -- ON. Fuel Shutoff Valve -- ON. Mixture -- RICH. Master Switch -- OFF. Airspeed -- 85 KIAS If fire is not extinguished, increase glide speed to find an airspeed which will provide an incombustible mixture. NOTE Perform a sideslip to keep the flames away from the fuel tank and cabin, and land as soon as possible, with flaps retracted. Those extra items on the checklist will provide added safety after a failure of this type.

Apply full rich mixture. Use full carburetor heat. Adjust the elevator trim for a stabilized descent at 70 KIAS. NOTE If disorientation precludes a visual determination of the direction of rotation, the symbolic airplane in the turn coordinator may be referred to for this information.

Select different power settings and enrich the mixture to determine if continued operation on BOTH magnetos is practicable. The alternator control unit includes an over-voltage sensor that normally will automatically shut down the alternator if the charge voltage reaches approximately Normal procedures associated with optional systems can be found in Section 9. In cold weather, remove even small accumulations of frost, ice or snow from wing, tail and control surfaces.

Also, make sure that control surfaces contain no internal accumulations of ice or debris. CABIN 1. Ignition Switch —OFF 4. Master Switch — ON NOSE 1. Engine Oil —4 qts minimum —5 qts maximum for flights less than 3 hours—6 qts maximum 2. Before first flight of day, and after each refueling, pull out fuel strainer knob for 4 seconds 4. Carburetor Heat -- ON apply full heat before closing throttle. Ignition Switch -- OFF. In warm weather, one stroke of the primer should be sufficient.

In temperatures near freezing, up to 3 strokes of the primer may be necessary. When the knob is pulled out to the heat position, air entering the engine is not filtered. Any sign of rough engine operation or sluggish engine acceleration is good cause for discontinuing the takeoff. If this occurs, you are justified in making a thorough full-throttle static runup before another takeoff is attempted. The engine RPM and corresponding fuel consumption for various altitudes can be determined by using your Cessna Power Computer or the data in Section 5.

Page Stalls No spins should be attempted without first having received dual instruction in both spin entries and spin recoveries from a qualified instructor who is familiar with the spin characteristics of the Cessna At least feet of altitude loss should be allowed for a 1-turn spin and recovery, while a 6-turn spin and recovery may require somewhat more than twice that amount.

Slightly higher approach speeds should be used under turbulent air conditions. Mixture RICH. The data in the charts has been computed from actual flight tests with the airplane and engine in good condition and using average piloting techniques. A typical cruising altitude and the expected wind enroute have been given for this sample problem. However, the power setting selection for cruise must be determined based on several considerations.

The corresponding distance during the climb is 9 nautical miles. These values are for a standard temperature as shown on the climb chart' and are sufficiently accurate for most flight planning purposes. However, a further correction for the effect of temperature may be made as noted on the climb chart.

Airspeed Calibration 1 July Mixture leaned above 3, ft for maximum RPM 3. This chart allows for the fuel used for engine start, taxi, takeoff, and climb, and distance during climb as shown in figure 2.

This chart allows for the fuel used for engine start, taxi, takeoff, and climb, and distance during climb as shown in figure 4. Short field technique as specified in Section 4 2. Sample forms are provided for reference.

Procedures for calculating the weight and moment for various operations are also provided. Use the data pertaining Refer to the Loading Arrangements Diagram for forward and aft limits of occupant C.

A separate equipment list of items installed in your specific airplane is provided in your aircraft file. The following list and the specific list for your airplane have a similar order of listing. Some equipment described herein is optional and may not be installed in the airplane. AIRFRAME The airplane is an all-metal, two-place, high-wing, single-engine airplane equipped with tricycle landing gear and designed for general utility purposes.

When a rudder pedal is depressed, a spring-loaded steering bungee which is connected to the nose gear and to the rudder bars will turn the nose wheel through an arc of approximately 8. If a tow bar is not available, or pushing is required, use the wing struts as push points.

The pilot's and passenger's seats are available in two designs: four way and six-way adjustable. The pilot's and passenger's seats are also equipped with separate shoulder harnesses. The windows are equipped with a spring-loaded retaining arm which will help rotate the window outward, and hold it there. If required, the windows may be opened at any speed up to KIAS. All other cabin windows are of the fixed type and cannot be opened.

The oil pressure gage, located on the left switch and control panel, is operated by oil pressure. If, during the first 25 hours, oil must be added, use only aviation grade straight mineral oil conforming to specification No. The R and L positions are for checking purposes and emergency use only. When the switch is rotated to the spring-loaded START position, with the master switch in the ON position , the starter contactor is energized and the starter will crank the engine.

The cooling air is directed around the cylinders and other areas of the engine by baffling, and is then exhausted through an opening at the bottom aft edge of the cowling. With the valve in the ON position, fuel flows through a strainer to the carburetor. From the carburetor, mixed fuel and air flows to the cylinders through intake manifold tubes.

Each brake is connected, by a hydraulic line to a master cylinder attached to each of the pilot's rudder pedals. Bank attitude is presented by a pointer at the top of the indicator relative to the bank scale which has index marks at , , 30', , and either side of the center mark. The following paragraphs discuss these items. NOTE Cessna radios are equipped with sidetone capability monitoring of the operator's own voice transmission. Sidetone will be heard on either the airplane speaker or a headset as selected with the AUTO selector switch.

Sidetone may be eliminated by placing the AUTO selector switch in the OFF position, and utilizing the individual radio selector switches. The control is used to adjust the level of sidetone volume heard on the airplane speaker only. Page Introduction Department.

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