Cessna 152 1979 Pilot Operating Handbook
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Cessna 152 1979 Pilot Operating Handbook

Cessna 152 1979 Pilot Operating Handbook

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  • Page 2 THIS MANUAL WAS PROVIDED FOR THE AIRPLANE IDENTIFIED ON THE TITLE PAGE ON ____ _ SUBSEQUENT REVISIONS SUPPLIED BY CESSNA AIRCRAFT COMPANY MUST BE PROPERLY IN­ SERTED. CESSNA AIRCRAFT COMPANY. PAWNEE DIVISION °'' J- ':, --'V:l_ tubs�quent revisions supplied by C�silil Aittralt tomp any rnust be properly inserted.
  • Page 3 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. World-wide, the Cessna Dealer Organization backed by the Cessna Customer Services Department stands ready to serve you.
  • Page 4 PERFORMANCE­ CESSNA SPECIFICATIONS MODEL 152 PERFORMANCE - SPECIFICATIONS •SP EE D: /,J/4 � Maximum at Sea Level ....10 KNOTS Cruise, 75% Power at 8000 Ft .

  • Page 6: Table Of Contents

    CESSNA rABLE OF CONTENTS MODEL 152 TABLE OF CONTENTS SECTION GENERAL ......1 LIMITATIONS ......2 EMERGENCY PROCEDURES .... 3 NORMAL PROCEDURES ....4 PERFORMANCE ....... 5 WEIGHT & BALANCE/ E Q UIPMENT LIST ....6 AIRPLANE & SYSTEMS DESCRIPTIONS ....

  • Page 8: General

    CESSNA SECTION 1 GENERAL MODEL 152 NOTES: ,----10'-0"----+l Wing span shown with conical camber wing tips and strobe lights installed. If standard wing tlps without suobe lights are installed, wing span is 32' - 8 1/2", Max;mum height shown wlth nose gear depressed, all tires and nos,, strut prop­...
  • Page 10 THIS DATA APPLICABLE ONLY TO AIRPLANES WITH LYCOMING 0-235-L2C ENGINE. FOR AIRPLANES WITH ENGINE MODIFIED TO 0·235-N2C, REFER TO DATA IN SECTION 9 SUPPLEMENT. CESSNA SECTION 1 MODEL 152 GE NERAL Long Range Tanks: Total Capacity: 39 gallons. Total Capacity Each Tank: 19.5 gallons.
  • Page 11 CESSNA SECTION 1 MODEL 152 GENERAL MAXIMUM CERTIFICATED WEIGHTS Ramp: 1675 lbs. Takeoff: 1670 lbs. Landing: 1670 lbs. Weight in Baggage Compartment: Baggage Area 1 (or passenger on child's seat)- Station 50 to 76: 120 lbs. See note below. Baggage Area 2 - Station 76 to 94: 40 lbs. See note below.
  • Page 12 SECTION 1 CESSNA GENERAL MODEL 152 KIAS Knots Indicated Airspeed is the speed shown on the airspeed indicator and expressed in knots. , __; KTAS Knots True Airspeed is the airspeed expressed in knots relative to undisturbed air which is KCAS corrected for altitude and temperature.
  • Page 13 SEC'rION 1 CESSNA GENERAL MODEL 152 ENGINE POWER TERMINOLOGY Brake Horsepower is the power developed by the engine. Revolutions Per Minute is engine speed. Static Static RPM is engine speed attained during a full-throttle engine runup when the airplane is on the ground and stationary.
  • Page 14 CESSNA SECTION 1 MODEL 152 GENERAL by its arm. (Moment divided by the constant 1000 is used in this handbook to simplify balance calculations by reduc­ ing the number of digits.) Center of Center of Gravity is the point at which an airplane, or Gravity equipment, would balance if suspended.
  • Page 15 CESSNA SECTION 2 MODEL 15 2 LIMITATIONS SECTION 2 LIMITATIONS THIS DATA APPLICABLE ONLY TO AIRPLANES WITH LYCOMING O-235-LZC ENGINE. FOR AIRPLANES WITH ENGINE MODIFIED TO 0-235-N2C, REFER TO DATA IN SECTION 9 SUPPLEMENT. TABLE OF CONTENTS Page Introduction ..

  • Page 18: Limitations

    CESSNA SECTION 2 MODEL 152 LIMITATIONS AIRSPEED INDICATOR MARKINGS Airspeed indicator markings and their color code significance are \� shown in figure 2-2. KIAS VALUE MARKING SIGNIFICANCE OR RANGE 35 - 85 Full Flap Operating Range. Lower White Arc limit is maximum ·weight V 5 0 in landing configuration.
  • Page 19 CESSNA SECTION2 MODEL 152 LIMITATIONS POWER PLANT INSTRUMENT MARKINGS Power plant itistrument markings and their color code significance are shown in figure 2-3. RED LINE GREEN ARC RED LINE INSTRUMENT MINIMUM NORMAL MAXIMUM LIMIT OPERATING LIMIT Tachometer: Sea Level 1900 - 2350 RPM...
  • Page 20 SECTION 2 CESSNA LIMITATIONS MODEL 152 Aft: 36.5 inches aft of datum at all weights. Reference _Datum: Front face of firewall. \ .. __/ MANEUVER LIMITS This airplane is certificated in the utility category and is designed for limited aerobatic flight. In the acquisition of various certificates such as commercial pilot 8.nd flight instructor, certain maneuvers are required.
  • Page 21 CESSNA SECTION2 MODEL 152 LIMITATIONS · · G ence to types of flight operations on the operating limitations placard reflects equipment installed at the time of Airworthiness Certificate issuance. Flight into known icing conditions is prohibited. FUEL LIMITATIONS 2 Standard Tanks: 13 U.S. gallons each.
  • Page 22 CESSNA SECTION2 LIMITATIONS MODEL 152 PLACARDS The following information must be displayed in the form of composite or individual placards. In full view of the pilot: (The "DAY-NIGHT-VFR-IFR" entry, shown on the example below, will vary as the airplane is equipped).
  • Page 23 CESSNA SECTION2 MODEL 15 2 LIMITATIONS 3. Near fuel shutoff valve (standard tanks): FUEL - 24.5 GALS - ON-OFF Near fuel shutoff valve (long range tanks): FUEL - 37.5 GALS - ON-OFF 4. Near fuel tank filler cap (standard tanks): FUEL 100LL/100 MIN.
  • Page 24 CESSNA SECTION2 MODEL 152 LIMITATIONS A, calibration card is provided to indicate the accuracy of the magnetic compass in 30 ° increments. - � 7. On oil filler cap: 6QTS 8. On control lock: CONTROL LOCK - REMOVE BEFORE STARTING ENGINE...

  • Page 26: Emergency Procedures

    CESSNA SECTION3 MODEL 152 EMERGENCY PROCEDURES TABLE OF CONTENTS (Continued) Page \, ___ /i 3-11 Emergency Operation In Clouds (Vacuum System Failure) ° 3-11 Executing A 180 Turn In Clouds 3-11 Emergency Descent Through Clouds Recovery From A Spiral Dive ..
  • Page 27 CESSNA SECTION 3 MODEL 152 EMERGENCY PROCEDURES , � INTRODUCTION Section 3 provides checklist and amplified procedures for coping with emergencies that may occur. Emergencies caused by airplane or engine malfunctions are extremely rare if proper preflight inspections and maintenance are practiced. Enroute weather emergencies can be minim­...
  • Page 28 CESSNA SECTIONS MODEL 152 EMERGENCY PROCEDURES Fuel Shutoff Valve -- OFF. Ignition Switch -- OFF. Wing Flaps -- AS REQUIRED. Master Switch -- OFF. ENGINE FAILURE DURING FLIGHT Airspeed -- 60 KIAS. Carburetor Heat -- ON. Primer -- IN and LOCKED.
  • Page 29 CESSNA SECTION3 MODEL 152 EMERGENCY PROCEDURES DITCHING 1. Radio -- TRANSMIT MAYDAY on 121.5 MHz, giving location and intentions and SQUAWK 7700 if transponder is installed. Heavy Ob j ects ( in baggage area ) -- SECURE OR JETTISON. Approach -- High Winds, Heavy Seas -- INTO THE WIND.
  • Page 30 SECTION3 CESSNA EMERGENCY PROCEDURES MODEL 152 Fuel Shutoff Valve •· OFF. Master Switch .. OFF. Cabin Heat and Air .. OFF (except wing root vents). Airspeed ·• 85 KIAS (If fire is not extinguished, increase glide speed to find an airspeed which will provide an incombustible mixture).
  • Page 31 SECTION3 CESSNA EMERGENCY PROCEDURES MODEL 152 WING FIRE Navigation Light Switch -- OFF. Strobe Light Switch (if installed) -- OFF. 3. Pitot Heat Switch (if installed) -- OFF. NOTE Perform a side slip to keep the flames away from the fuel tank and cabin, and land as soon as possible, with flaps retracted.
  • Page 32 SECTION 3 CESSNA EMERGENCY PROCEDURES MODEL 152 LANDING WITH A FLAT MAIN TIRE Wing Flaps -- AS DESIRED. 2. Approach -- NORMAL. 3. Touchdown -- GOOD TIRE FIRST, hold airplane off flat tire as long as possible with aileron control.
  • Page 33 SEOTION3 CESSNA EMERGENCY PROCEDURES MODEL 152 AMPLIFIED PROCEDURES ENGINE FAILURE If an engine failure occurs during the takeoff run, the most important thing to do is stop the airplane oil the remaining runway. Those extra items on the checklist will provide added safety after a failure of this}ype.

  • Page 35: Emergency Operation In Clouds (Vacuum System Failure)

    CESSNA SECTIONS MODEL 152 EMERGENCY PROCEDURES EMERGENCY OPERATION IN CLOUDS (Vacuum System Failure) In the event of a vacuum system failure during flight, the directional indicator and attitude indicator will be disabled, and the pilot will have to rely on the turn coordinator if he inadvertently flies into clouds. The...

  • Page 36: Recovery From A Spiral Dive

    SECTION3 CESSNA EMERGENCY PROCEDURES MODEL 152 Use full carburetor heat. 3. Reduce power to set up a 500 to 800 ft/min rate of descent. · � Adjust the elevator trim for a stabilized descent at 70 KIAS. 5. Keep hands off control wheel.

  • Page 38: Magneto Malfunction

    SECTIONS CESSNA EMERGENCY PROCEDURES MODEL 152 the ignition switch unless extreme roughness dictates the use of a single ignition position. MAGNETO MALFUNCTION A sudden engine roughness or misfiring is usually evidence of magneto problems. Switching from BOTH to either Lor R ignition switch...

  • Page 39: Insufficient Rate Of Charge

    CESSNA SECTIONS MODEL 152 EMERGENCY PROCEDURES (such '"' extended taxiing) the battery condition will be low enough to accept above normal charging during the initial part of a flight. However, after thirty minutes of cruising flight, the ammeter should be indicating less than two needle widths of charging current.

  • Page 41: Normal Procedures

    SECTION 4 CESSNA NORMAL PROCEDURES MODEL SECTION 4 NORMAL PROCEDURES TABLE OF CONTENTS Page Introduction .., , ', , • 4 -3 Speeds For Normal Operation CHECKLIST PROCEDURES 4- 5 Preflight Inspection ..
  • Page 42 SECTION4 CESSNA NORMAL PROCEDURES MODEL 152 TABLE OF CONTENTS (Continued) Page Before Takeoff . . 4-1 3 Warm-Up 4-13 4-13 Magneto Check Alternator Check 4-13 Takeoff ..4-14 4-1 4 Power Check . 4-14 ·J Wing Flap Settings 4-1 5...

  • Page 43: Introduction

    SECTION4 CESSNA NORMAL PROCEDURES MODEL 152 INTRODUCTION /� Section 4 provides checklist and amplified procedures for the conduct of no" r mal operation. Normal procedures associated with optional systems can be found in Section 9. SPEEDS FOR NORMAL OPERATION Unless otherwise noted, the following speeds are based on a maximum weight of 1670 pounds and may be used for any lesser weight.
  • Page 44 SECTION 4 CESSNA NORMAL PROCEDURES MODEL 152 NOTE Visually check airplane for general condition during walk-around inspection. 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.

  • Page 45: Checklist Procedures

    SECTION 4 CESSNA MODEL 152 NORMAL PROCEDURES CHECKLIST PROCEDURES PREFLIGHT INSPECTION Pilot's Operating Handbook -- AVAILABLE IN THE AIRPLANE. Control Wheel Lock -- REMOVE. Ignition Switch -- OFF. Master Switch -- ON. WARNING When turning on the master switch, using an external : '\ /�...

  • Page 46: Nose

    CESSNA SECTION4 MODEL 152 NORMAL PROCEDURES @NOSE Engine Oil Level -- CHECK, do not operate with less than four quarts. Fill to six quarts for extended flight. Before first flight of the day and after each refueiing, pull out strainer drain knob for about four seconds to clear fuel strainer of possible water and sediment.

  • Page 47: Starting Engine (Temperatures Above Freezing)

    CESSNA SECTION4 NORMAL PROCEDURES MODEL 152 2. Seats, Belts, Shoulder Harnesses -- ADJUST and LOCK. Fuel Shutoff Valve -- ON. 4. Radios, Electrical Equipment -- OFF. Brakes -- TEST and SET. Circuit Breakers -- CHECK IN. STARTING ENGINE (Temperatures Above Freezing) 1, Mixture -- RICH.

  • Page 48: Takeoff

    SECTION4 CESSNA NORMAL PROCEDURES MODEL 152 TAKEOFF NORMAL TAKEOFF Wing Flaps -- 0 ° - 10 ° Carburetor Heat -- COLD. Throttle -- FULL OPEN. Elevator Control -- LIFT NOSE WHEEL at 50 KIAS. Climb Speed -- 65-75 KIAS. SHORT FIELD TAKEOFF Wing Flaps -- 10 °...

  • Page 49: Before Landing

    SECTION4 CESSNA NORMAL PROCEDURES MODEL 152 BEFORE LANDING !� 1. Seats, Belts, Harnesses -- ADJUST and LOCK. 2. Mixture -- RICH. 3. Carburetor Heat -- ON (apply full heat before closing throttle). LANDING NORMAL LANDING Airspeed -- 60-70 KIAS (flaps UP).

  • Page 50: Securing Airplane

    SECTION4 CESSNA NORMAL PROCEDURES MODEL 152 SECURING AIRPLANE 1. Parking Brake -- SET. Radios, Electrical Equipment -- OFF. 3. Mixture -- IDLE CUT-OFF (pull full out). 4. Ignition Switch -- OFF. 5. Master Switch -- OFF. Control Lock -- INSTALL.

  • Page 51: Amplified Procedures

    CESSNA SECTION4 MODEL 152 NORMAL PROCEDURES AMPLIFIED PROCEDURES STARTING ENGINE (Temperatures Above Freezing) During engine starting, open the throttle approximately 1/ 2 inch. In warm weather, one stroke of the primer should be sufficient. In tempera­ tures near freezing, up to 3 strokes of the primer may be necessary. As the engine starts, slowly adjust the throttle as required for 1000 RPM or less.
  • Page 52 CESSNA SEOTION4 MODEL 152 NORMAL PROCEDURES NOTE CODE Strong quartering tail winds require caution. WIND DIRECTION • Avoid sudden bursts of the throttle and sharp braking when the airplane is in this attitude. Use the steerable nose wheel and rudder to maintain direction.
  • Page 53 CESSNA SECTION4 MODEL 152 NORMAL PROCEDURES The carburetor heat control knob should be pushed full in during all ground operations unless heat is absolutely necessary. When the knob is pulled out to the heat position, air entering the engine is not filtered.
  • Page 54 SECTION4 CESSNA NORMAL PROCEDURES MODEL 152 within a needle width of its initial position the alternator and alternator control unit are operating properly. ,_,,/ TAKEOFF POWER CHECK It is important to check full-throttle engine operation early in the takeoff run. Any sign of rough engine operation or sluggish engine acceleration is good cause for discontinuing the takeoff.
  • Page 55 (1 CRUISE Normal cruising is performed between55% and 75% power. 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. NOTE /� Cruising should be done at65% to 75% power until a total of 50 hours has accumulated or oil consumption has stabil­...
  • Page 56 THIS DATA APPLICABLE ONLY TO AIRPLANES WITH LYCOMING 0-235-L2C ENGINE. FOR AIRPLANES WITH ENGINE MODIFIED TO 0-235-N2C, REFER TO DATA IN SECTION 9 SUPPLEMENT. SECTION4 CESSNA NORMAL PROCEDURES MODEL 152 75% POWER 65% POWER 55% POWER ALTITUDE KTAS NMPG KTAS...
  • Page 57 Cessna 152. The cabin should be clean and all loose equipment (including the microphone) should be stowed. For a solo flight in which spins will be conducted, the copilot's seat belt and shoulder harness should be secured.
  • Page 58 4 CESSNA 'IORMAL PROCEDURES MODEL 152 ,hould be taken to ensure that the pilot can easily reach the flight controls md produce maximum control travels. It is recommended that, where feasible, entries be accomplished at b.igh enough altitude that recoveries are completed 4000 feet or more above ground level.
  • Page 59 CESSNA SECTION4 MOD. E L 152 NORMAL PROCEDURES VERIFY THAT AILERONS ARE NEUTRAL AND THROTTLE IS IN IDLE POSITION. APPLY AND HOLD FULL RUDDER OPPOSITE TO THE DIREC· TION OF ROTATION. JUST AFTER THE RUDDER REACHES THE STOP, MOVE THE CONTROL WHEEL BRISKLY FORWARD FAR ENOUGH TO BREAK THE STALL.
  • Page 60 SECTION4 CESSNA NORMAL PROCEDURES MODEL 152 54 KIAS with 30' flaps using enough power to control the glide path. After all approach obstacles are cleared, progressively reduce power and maintain 54 KIAS by lowering the nose of the airplane. Touchdown should be made with power-off and on the main wheels first.
  • Page 61 SECTION4 CESSNA NORMAL PROCEDURES MODEL 152 Parking Brake -- SET. Propeller -- PULL through by hand several revolutions. NOTE Caution should be used to ensure the brakes are set or a qualified person is at the controls. Mixture -- RICH.
  • Page 62 SECTION4 CESSNA MODEL 152 NORMAL PROCEDURES ° to the 0 to 21 °C range, where icing is critical under certain atmospheric conditions. NOISE ABATEMENT Increased emphasis on improving the quality of our environment requires renewed effort on the part of all pilots to minimize the effect of airplane noise on the public.
  • Page 63 SECTION 5 CESSNA PERFORMANCE MODEL 152 SECTION 5 PERFORMANCE TABLE OF CONTENTS Page Introduction ..Use of Performance Charts Sample Problem Takeoff Cruise . . , Fuel Required Landing . . . Demonstrated Operating Temperature...
  • Page 65 SECTION 5 CESSNA PERFORMANCE MODEL 152 , � INTRODUCTION Performance data charts on the following pages are presented so that you may know what to expect from the airplane under various conditions, and also, to facilitate the planning of flights in detail and with reasonable accuracy.
  • Page 66 SECTION 5 CESSNA PERFORMANCE MODEL 152 CRUISE CONDITIONS 320 Nautical Miles Total distance ,.__,,/ Pressure altitude 5500 Feet ° c (16 ° C above standard) Temperature Expected wind enroute 10 Knot Headwind LANDING CONDITIONS Field pressure altitude 2000 Feet Temperature °...
  • Page 68 CESSNA SECTION 5 MODEL 152 PERFORMANCE fuel. 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.
  • Page 69 CESSNA SECTION 5 MODEL 152 PERFORMANCE The total estimated fuel required is as follows: Engine start, taxi, and takeoff Climb Cruise 18.2 Total fuel required 20.2 Gallons This will leave a fuel reserve of: 24.5 -20.2 4.3 Gallons Once the flight is underway, ground speed checks will provide a more accurate basis for estimating the time enroute and the corresponding fuel required to complete the trip with ample reserve.
  • Page 70 CESSNA SECTION 5 MODEL 152 PERFORMANCE AIRSPEED CALIBRATION CONDITIONS: Power required for level flight or maximum rated RPM dive. FLAPS UP KIAS KCAS FLAPS 10 ° KIAS - - - KCAS \� FLAPS 30 ° KIAS - - - - - - KCAS Figure 5-1.
  • Page 71 CESSNA SECTION 5 MODEL 152 PERFORMANCE TEMPERATURE CONVERSION CHART � -2 0 - 4 0 - 40 DEGREES - CELSIUS Figure 5-2. Temperature Conversion Chart 1 July 1978...
  • Page 72 SECTION 5 CESSNA PERFORMANCE MODEL 152 STALL SPEEDS CONDITIONS: Power Off NOTES: Altitude loss during a stall recovery may be as much as 160 feet. KIAS values are approximate and are based on airspeed calibration data with power off. MOST REARWARD CENTER OF GRAVITY...
  • Page 73 ,..TAKEOFF DISTANCE :S:@ � ti UJ SHORT FIELD CONOITIONS: "' --., s :i, ° Flaps 10 Full Throttle Prior to Brake Release Paved, Level, Dry Runway Zero Wind NOTES: Short field technique as specified in Section 4. Prior to takeoff from fields above 3000 feet elevation, the mixture should be leaned to give maximum RPM in a full throttle, --------- static runup.
  • Page 74 SECTION 5 CESSNA PERFORMANCE MODEL 152 RATE OF CLIMB jMAXIMUMI CONDITIONS: Flaps Up Full Throttle NOTE: Mixture leaned above 3000 feet for maximum RPM. PRESS CLIMB RATE OF CLIMB - FPM WEIGHT SPEED ° KIAS ° 1670 70 0 S.L.
  • Page 75 CESSNA SECTION 5 MODEL 152 PERFORMANCE TIME, FUEL, AND DISTANCE TO CLIMB !MAXIMUM RATE OF CLIMB! CONDITIONS: Flaps Up Full Throttle Standard Temperature NOTES: Add 0.8 of a gallon of fuel for engine start, taxi and takeoff allowance. Mixture leaned above 3000 feet for maximum RPM.
  • Page 76 THIS DATA APPLICABLE ONLY TO AIRPLANES WITH LYCOMING 0·235-L2C ENGINE. FOR AIRPLANES WITH ENGINE MODIFIED TO 0-235-N2C, REFER TO DATA IN SECTION 9 SUPPLEMENT. SECTIONS CESSNA PERFORMANCE MODEL 152 CRUISE PERFORMANCE CONDITIONS: 1670 Pounds Recommended Lean Mixture (See Section 4, Cruise)
  • Page 77 THIS DATA APPLICABLE ONLY TO AIRPLANES WITH LYCOMING 0·235·L2C ENGINE. FOR AIRPLANES WITH ENGINE MODIFIED TO 0·235·N2C, REFER TO DATA IN SECTION 9 SUPPLEMENT. CESSNA SECTION 5 MODEL 152 PERFORMANCE RANGE PROFILE 45 MINUTES RESERVE 24.5 GALLONS USABLE FUEL CONDITIONS: 1670 Pounds �...
  • Page 79 THIS DATA APPLI C ABLE ONLY TO AIRPLANES WI T H LYCOMING 0-235-L2C ENGINE. FOR AIRPLANES WITH ENGINE MODIFIED TO 0-235-N2C, REFER TO DATA IN SECTION 9 SUPPLEMENT. SECTION 5 CESSNA PERFORMANCE MODEL 152 ENDURANCE PROFILE 45 MINUTES RESERVE 24.5 GALLONS USABLE FUEL...
  • Page 80 THIS DATA APPLICABLE ONLY TO AIRPLANES WITH LYCOMING 0-235-L2C ENGINE. FOR AIRPLANES WITH ENGINE MODIFIED TO 0-235-N2C, REFER TO DATA IN SECTION 9 SUPPLEMENT. SECTIONS CESSNA PERFORMANCE MODEL 152 ENDURANCE PROFILE 45 MINUTES RESERVE 37.5 GALLONS USABLE FUEL CONOITIONS: 1670 Pounds...
  • Page 81 ..LANDING DISTANCE �Q oi,;i t,00 l,;l 00 SHORT FIELD t<Z ..CONDITIONS: Flaps 30 ° Power Off Maximum Braking Paved, Level, Ory Runway Zero Wind NOTES: Short field technique as specified in Section 4. Decrease distances 10% for each 9 knots headwind. For operation with tailwinds up to 10 knots, increase distances by 10% for each 2 knots.

  • Page 83: Weight & Balance E Q Uipment List

    CESSNA SECTION6 WEIGHT & BALANCE/ MODEL 152 EQUIPMENT LIST SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST TABLE OF CONTENTS Page Introduction . . . , ..6-3 Airplane Weighing Procedures . 6-3 Weight And Balance .
  • Page 84 \ ..l...

  • Page 85: Equipment List

    Sample forms are provided for refe;rence. Procedures for calculating the weight and moment for various operations are also provided. A comprehensive list of all Cessna equip­ ment available for this airplane is included at the back of this section.

  • Page 86: Equipment List

    SECTIONS CESSNA WEIGHT & BALANCE/ MODEL 152 EQUIPMENT LIST Datum {Firewall, Front Face) Sta. Level on Leveling Screws ( Left Side of Tailcone) L&R Scale Position Tare Net Weight Scale Reading Symbol Left Wheel Right Wheel Nose Wheel Sum of Net Weights (As Weighed) ------- I IN.

  • Page 87: Descriptions

    ..;.: 0 SAMPLE WEIGHT AND BALANCE RECORD 01,;) (Continuous History of Changes in Structure or Equipment Affecting Weight and Balance} ..t< I,;) {ll ! PAGE NUMBER I SERIAL NUMBER AIRPLANE MODEL ..:,, WEIGHT CHANGE RUNNING BASIC ITEM NO. EMPTY WEIGHT ADDED(+) DESCRIPTION...

  • Page 88: Section6

    MODEL 152 EQUIPMENT LIST WEIGHT AND BALANCE The following information will enable you to operate your Cessna within the prescribed weight and center of gravity limitations. To figure weight and balance, use the Sample Problem, Loading Graph, and Center of Gravity Moment Envelope as follows:...

  • Page 89: Equipment List

    SECTIONS CESSNA WEIGHT & BALANCE/ MODEL 152 EQUIPMENT LIST LOADING ARRANGEMENTS STATION STATION * Pilot or passenger center of (C,G. ARM) (C.G. ARM) Q� gravity on adjustable seats positioned for average occu- pant, Numbers in parentheses ..L. ..L. indicate forward and aft limits of occupant center of gravity range.
  • Page 90 3ECTION 6 CESSNA WEIGHT & BALANCE/ MODEL 152 EQUIPMENT LIST • CABIN HEIGHT MEASUREMENTS FIREWALL \ __ j ,-­ ---� i------ 56 "--------38'�---+-I 56.0 FACE OF INSTRUMENT PANEL REAR WALL OF C ABIN DOOR OPENING DIMENSIONS WIDTH= WIDTH I WIDTH...
  • Page 91 � YOUR AIRPLANE SAMPLE AIRPLANE 01,CJ SAMPLE 0 (/) «' l,CJ (/) Moment Moment � t< LOADING PROBLEM (lb. -ins. Weight (lb. - ins. Weight �:,, (lbs.) /1000) /1000) Basic Empty Weight (Use the data pertaining to your airplane as it is presently equipped. Includes unusable 3t,ij<...
  • Page 92 LOAD MOMENT/1000 (KILOGRAM-MILLIMETERS) t<J :;; C/l D t<J t<J � c:: ..0 >-l .. :+1 u I 1 · - �l I I • _J...LJ_ J _._ 1 I r-1 I 1 . ; ++Hm _ '1:1 :i: ..•...
  • Page 93 ;;,,. ;� �) ,... "' '-< o 1a1 t:,Ul '< ,... "' Isl {/l t<Z LOADED AIRPLANE MOMENT/1000 (KILOGRAM-MILLIMETERS) "' ,... i> "' 11'1 /I\ 1 _ 1700 775 Ul 750 � CENTER OF GRAVITY '"' 1600 MOMENT ENVELOPE 725 0 a 1 5 00 675 �...
  • Page 94 l'.'J :;J {/J ..D l'.'J l'.'l c:: � � 0 >-3 >cl :i: � AIRPLANE C.G. LOCATION-MILLIMETERS AFT OF DATUM (STA. 0.0) :;:: >-3 0 l'.'J 87 5 � "' �Ill t 800 �� =-775 ::. �z 1700 � :,. <l'.
  • Page 96 :.! ro t'.I EQUIPMENT LIST DESCRIPTION D t'.I t'.I c:: ..ITEM NO REF ORAWING WT LBS ARM INS ..Q.., 'Cl :i: ..is: .., POWERPLANT & ACCESSORIES z .- "' t'J � AO 1-R .., tJj E�GINE, LYCOMI% 0-235-LZC (INCLUDES 0450071 243.5 -19 .2...
  • Page 98 "' EQUIPMENT LIST DESCRIPTION "' WT LBS .0 1,1 1,1 REF DRAWING ARM INS ITEM NO '1:1::r:­ A: , T!METER, SENSITIVE (20 FT MARKINGS) C661025--0102 D07-D- l 17.6 ts1�Z ( FEET ANO MILLIBARS) A!.TIMETER, SENSITIVE 150 FT. MARKINGS! C661J 71-HJ 2 17.6 DO 7-0-2 >-3 1:11...
  • Page 99 "' EQUIPMENT LIST DESCRIPTION 01,;1 <.. ITEM NO REF DRAWING WT LBS ARM INS l,;I C/) "' SHOULDER HARNESS ASSY, PILOT S-2275-232 39.0 El5-S t< � El9-0 0 401Jl2-l SHOULDER HARNESS INERTIA INSTL., PILOT & 11.1 � CO-P !LOT (NET CHANGE I �...
  • Page 100 96. 5 LCLP ANTEN11A INSTALLATION 3 900104-1 24 .2 LAULE INSTALLATION 3950104-14 12.3 , � !SC. INSTALLATICN COMPONENTS 14.4 CESSNA 400 GLIDESLUPE WITH !LS INDICATOR 4.1 * oJ7-A 3910157 -10 78. B* £XLhA�GCD fOR LOC lNDICATO� RECElvcK (x-4438) 42l00-0000 2. l 105.3...
  • Page 101 REF DRAWING WT LBS ARM INS t::I t,,J ..12.9 MCUNT, WikING & MISC HARDWARE � � H22-A-2 CESSNA 300 i�AV/COM, 720 CHANNEL 1ST UNIT 3910183 � 13.6* 32.0* � REC EI VER-TKANSCE IV EK (RT-385A) 46660-110 0 5. 5 13.6...
  • Page 102 9910220-1 18.0 H22-A-l CESSNA 300 NAV/COM RT-385A 3910183 13.4 32.2 J04-A 152 II NAV-PAC EQUIPMENT 12. 1• 16.5• Hl6-A -l CESSNA 300 TRANSPONDER RT-359A 3910127 18.6 H25-A-l R T-385A 2ND UNIT 3910183 9. l 15.7 ..� t<J t<J ..z t<...

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