Piper CHEROKEE 180 E Owner's Handbook Manual
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Piper CHEROKEE 180 E Owner's Handbook Manual

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CHEROKEE 180
E
OWNER'S HANDBOOK

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Summary of Contents for Piper CHEROKEE 180 E

  • Page 1 CHEROKEE 180 OWNER'S HANDBOOK...
  • Page 2 WARNING The rudder pedals are suspended from a torque tube which extends across the fuselage. The pilot should become familiar with the proper positioning of his feet on the rudder pedals so as to avoid interference with the torque tube when moving the rudder pedals or operating the toe brakes.
  • Page 3 CHEROKEE 180 E PA 28 180 This handbook for airplanes with serial nos. 28 5601 through 28-5859. Owner's Handbook Piper Aircraft Corporation, Vero Beach, Florida U.S.A.
  • Page 4 A line opposite the page number will indicate that material was relocated. Additional copies of this manual, Part No. 753 806, may be obtained fromyour Piper Dealer. Published by PUBLICATIONS DEPARTMENT Piper Aircraft Corporation...
  • Page 7 INDEX SECTION I Page Specifications: Performance Weights Power Plant Fuel and Oil Baggage Dimensions Landing Gear SECTION II Design Information: Engine and Propeller Structures Landing Gear Control Systems Fuel System Electrical System Heating and Ventilating System Cabin Features SECTION III Operating Instructions: Preflight Starting Engine...
  • Page 8 INDEX (cont) SECTION III (cont) Page Engine Power Loss Mooring Weight and Balance Operating Tips SECTION IV Emergency Procedures: Introduction Engine Power Loss During Takeoff Engine Power Loss In Flight Power Off Landing Fire Loss of Oil Pressure Loss of Fuel Pressure High Oil Temperature Alternator Failure Engine Roughness...
  • Page 9 INDEX (cont) SECTION VI Page General Maintenance: Landing Gear Service Brake Service Tire Inflation Care of Windshield and Windows Battery Service Fuel and Oil Requirements Fuel System . Care of Air Filter Leveling and Rigging Serial Number Plate 753 806 740118...
  • Page 11 SECTION I SPECIFICATIONS Performance Weights Power Plant Fuel and Oil Baggage Dimensions Landing Gear 691015...
  • Page 13 CHEROKEE " E " SECTION I SECTION I SPECIFICATIONS PERFORMANCE Published figures are for standard airplanes flown at gross weight under standard conditions at sea level, unless otherwise stated. Performance for a specific airplane may vary from published figures depending upon the equipment installed, the condition of engine, airplane and equipment, atmospheric conditions and piloting technique.
  • Page 14 SECTION I CHEROKEE " E " SPECIFICATIONS (cont): WEIGHTS Gross Weight (lbs) 2400 Empty Weight (Standard) (lbs) 1310 USEFUL LOAD (Standard) (lbs) 1090 POWER PLANT Engine (Lycoming) O-360-A4A Rated Horsepower Rated Speed (rpm) 2700 Bore (in.) 5.125 Stroke (in.) 4.375 Displacement (cu in.) 361.0 Compression Ratio...
  • Page 15 CHEROKEE " E " SECTION I SPECIFICATIONS (cont): DIMENSIONS Wing Span (ft) Wing Area (sq ft) Wing Loading (lbs per sq ft) 15.0 Length (ft) 23.5 Height (ft) Power Loading (lbs per hp) 13.3 LANDING GEAR Wheel Base (ft) Wheel Tread (ft) Tire Pressure (psi) Nose Main Tire Size...
  • Page 16 SECTION I CHEROKEE " E " 691015...

  • Page 17: Table Of Contents

    SECTION II DESIGN INFORMATION Engine and Propeller Structures Landing Gear Control Systems Fuel System Electrical System Heating and Ventilating System Cabin Features 691015...
  • Page 19 CHEROKEE " E " SECTION II SECTION II DESIGN INFORMATION ENGINE AND PROPELLER The Cherokee " E " is powered by a Lycoming O-360-A4A four cylinder, direct drive, horizontally opposed engine rated at 180 HP at 2700 RPM. It is furnished with a starter, 60 ampere 12 volt alternator, shielded ignition, vacuum pump drive, fuel pump, and a dry, automotive type carburetor air filter.
  • Page 20 SECTION II CHEROKEE " E " the rear spar and at an auxiliary front spar. The wing airfoil section is a laminar flow type, NACA659- 415 with the maximum thickness about 40% aft of the leading edge. This permits the main spar carry-through structure to be located under the rear seat providing unobstructed cabin floor space ahead of the rear seat.

  • Page 21: Control Systems

    CHEROKEE " E " SECTION II CONTROL SYSTEMS Dual controls are provided as standard equipment with a cable system used between the controls and the surfaces. The horizontal tail is of the Flying Tail type (stabilator), with a trim tab mounted on the trailing edge of the stabilator to reduce the control system forces.
  • Page 22 CHEROKEE " E " SECTION II CARBURETOR VENT FUEL PRESSURE GAUGE FUEL QUANTITY GAUGES VENT ENGINE FUEL PUMP VENT ELECTRIC FUEL PUMP DRAIN PRIMER GASCOLATOR FUEL SELECTOR VALVE LEFT TANK RIGHT TANK DRAIN DRAIN FUEL SYSTEM SCHEMATIC 691015...

  • Page 23: Electrical System

    CHEROKEE " E " SECTION II water before each flight. The fuel strainer, which is also equipped with a quick drain, is located on the front lower left corner of the firewall. This strainer should be drained regularly to check for water or sediment accumulation.
  • Page 24 SECTION II CHEROKEE " E " Standard accessories include a starter, electric fuel pump, stall warning indicator, cigar lighter,fuel gauge and ammeter. The navigation lights, anti-collision light, landing light, instrument lighting and cabin dome light are optional. Circuits will handle an entire complement of communications and navigational equip- ment.
  • Page 25 CHEROKEE " E " SECTION II ELECTRICAL SYSTEM 691015...

  • Page 26: Heating And Ventilating System

    CHEROKEE "E" SECTION II Cherokee Cabin Heat, Defroster, Fresh Air HEATING AND VENTILATING SYSTEM 691212...

  • Page 27: Cabin Features

    Maintenance on the alternator should prove to be a minor factor. Should service be required, contact the local Piper Dealer. HEATING AND VENTILATING SYSTEM Heat for the cabin interior and the defroster system is pro- vided by a heater muff attached to the exhaust system.
  • Page 28 691212...
  • Page 29 CHEROKEE " E " SECTION II NOTES 691015...
  • Page 31 SECTION III OPERATING INSTRUCTIONS Preflight Starting Engine Warm-Up and Ground Check Take-Off Climb Stalls Cruising Approach and Landing Stopping Engine Engine Power Loss Mooring Weight and Balance Operating Tips 691015...

  • Page 33: Operating Instructions

    CHEROKEE " E " SECTION III SECTION III OPERATING INSTRUCTIONS PREFLIGHT 1. Master switch and ignition OFF. 2. a. Check for external damage and operational interfer- ence of control surfaces or hinges. b. Insure that wings and control surfaces are free of snow, ice or frost.

  • Page 34: Starting Engine

    CHEROKEE " E " SECTION III b. Drain fuel tank sumps (two). c. Drain fuel system sump (left side of aircraft). d. Check that fuel system vents are open. e. Check main landing gear shock struts for proper in- flation (approximately 4.50 inches showing). f .
  • Page 35 CHEROKEE " E " SECTION 5. Engage the starter by rotating magneto switch clockwise and pressing in. 6. When the engine fires, advance throttle to desired setting. If the engine does not fire within five to ten seconds, disengage starter and prime with one to three strokes of the priming pump. Repeat the starting procedure.
  • Page 36 SECTION V PERFORMANCE CHARTS Altitude Conversion Chart Takeoff Distance vs Density Altitude Rate of Climb vs Density Altitude Range vs Density Altitude True Airspeed and RPM vs Density Altitude Landing Distance vs Density Altitude Power Setting Table 753 806 740118...

  • Page 37: Climb

    CHEROKEE " E " SECTION III The take-off technique is conventional for the Cherokee. The tab should be set slightly aft of neutral, with the exact setting determined by the loading of the aircraft. Allow the air- plane to accelerate to 50 to 60 MPH, then ease back on the wheel enough to let the airplane fly itself off the ground.

  • Page 38: Cruising

    CHEROKEE " E " SECTION III STALL SPEED TABLE Angle of Bank Flaps 40° Flaps Retracted 0° 57 MPH 67 MPH 20° 59 MPH 69 MPH 40° 65 MPH 77 MPH 81 MPH 95 MPH 60° Power Off - Gross Weight 2400 lbs. CRUISING The cruising speed is determined by many factors including power setting, altitude, temperature, loading and equipment in-...

  • Page 39: Approach And Landing

    CHEROKEE " E " SECTION III temperature (EGT) gauge, a more accurate means of leaning is available to the pilot. For best power mixture, lean the mixture until the peak EGT is reached, then enrich the mixture until the temperature drops a minimum of 25° F. For best economy mixture, lean until the peak EGT is reached and continue to lean until the temperature drops a minimum of 25°...

  • Page 40: Stopping Engine

    SECTION III CHEROKEE " E " It is generally good practice to contact the ground at minimum possible safe speed consistent with existing conditions. Normally, the best technique for short and slow landings is to use full flap and enough power to maintain the desired airspeed and approach flight path.

  • Page 41: Mooring

    CHEROKEE " E " SECTION III If changing to another tank does not restore the engine: 1. Check fuel pressure and turn on electric fuel pump if off. 2. Push mixture control to full "RICH." 3. Check ignition switch. Turn to best operating magneto - left, right, or both.
  • Page 42 SECTION III CHEROKEE " E " ground. 2. The best speed for take-off is about 60 MPH under normal conditions. Trying to pull the airplane off the ground at too low an airspeed decreases the controllability of the airplane in event of engine failure.
  • Page 43 CHEROKEE " E " SECTION III The shape of the wing fuel tanks is such that in certain maneuvers the fuel may move away from the tank outlet. If the outlet is uncovered, the fuel flow may be interrupted and a temporary loss of power may result.
  • Page 45 SECTION IV EMERGENCY PROCEDURES Introduction Engine Power Loss During Takeoff Engine Power Loss In Flight Power Off Landing Fire Loss of Oil Pressure Loss of Fuel Pressure High Oil Temperature Alternator Failure Engine Roughness Spins Open Door 753 806 740118...

  • Page 47: Emergency Procedures

    CHEROKEE"E" SECTION IV SECTION IV EMERGENCY PROCEDURES INTRODUCTION This section contains procedures that are recommended if an emergency condition should occur during ground operation, takeoff, or in flight. These procedures are suggested as the best course of action for coping with the particular condition described, but are not a substitute for sound judgement and common sense.

  • Page 48: Engine Power Loss In Flight

    SECTION IV CHEROKEE " E " If you have gained sufficient altitude to attempt a restart, proceed as follows: MAINTAIN SAFE AIRSPEED FUEL SELECTOR - SWITCH TO ANOTHER TANK CONTAINING FUEL ELECTRIC FUEL PUMP - CHECK ON MIXTURE - CHECK RICH CARBURETOR HEAT - ON NOTE If engine failure was caused by fuel exhaustion,...

  • Page 49: Power Off Landing

    CHEROKEE " E " SECTION IV When power is restored: Carburetor Heat - Off Electric Fuel Pump - Off If the above steps do not restore power, prepare for an emergency landing. If time permits: Ignition Switch - "L" then "R" then back to "BOTH." Throttle and Mixture - Different settings.

  • Page 50: Fire

    SECTION IV CHEROKEE "E" When you have located a suitable field, establish a spiral pattern around this field. Try to be at 1000 feet above the field at the downwind position, to make a normal approach. Excess altitude may be lost by widening your pattern, using flaps or slipping, or a combination of these.

  • Page 51: Loss Of Oil Pressure

    CHEROKEE " E " SECTION IV Engine Fire In Flight: Fuel Selector - Off Throttle - Closed Mixture - Idle cut-off Heater - Off (In all cases of fire) Defroster - Off (In all cases of fire) If terrain permits, land immediately. The possibility of an engine fire in flight is extremely remote.

  • Page 52: Loss Of Fuel Pressure

    SECTION IV CHEROKEE " E " A complete loss of oil pressure indication may signify oil exhaustion or may be the result of a faulty gauge. In either case, proceed toward the nearest airport, and be prepared for a forced landing.

  • Page 53: Alternator Failure

    CHEROKEE " E " SECTION IV ALTERNATOR FAILURE Loss of alternator output is detected through a zero reading on the ammeter. Before executing the following procedure, insure that the reading is zero and not merely low by actuating an electrically powered device, such as the landing light.

  • Page 54: Spins

    SECTION IV CHEROKEE " E " Magneto Switch - "L" then "R," then back to "BOTH." If operation is satisfactory, on either magneto, proceed on that magneto at reduced power, with mixture full rich, to a landing at the first available airport.

  • Page 55: Open Door

    CHEROKEE " E " SECTION IV OPEN DOOR The cabin door on the Cherokee is double latched, so the chance of its springing open in flight at both the top and bottom is remote. However, should you forget the upper latch, or not fully engage the lower latch, the door may spring partially open.
  • Page 57 SECTION V PERFORMANCE CHARTS Altitude Conversion Chart Takeoff Distance vs Density Altitude Rate of Climb vs Density Altitude Range vs Density Altitude True Airspeed and RPM vs Density Altitude Landing Distance vs Density Altitude Power Setting Table 753 806 740118...
  • Page 59 CHEROKEE " E " SECTION V PA-28-180 PIPER CHEROKEE THIS CHART SHOULD BE USED TO DETERMINE DENSITY ALTITUDE FROM EXISTING TEMPERATURE AND PRESSURE ALTITUDE CONDITIONS FOR USE WITH PERFORMANCE CHARTS. 24000 20000 10000 12000 8000 4000 TEMPERATURE °F 753 806...
  • Page 60 CHEROKEE"E" SECTION V PA-28-18O PIPER CHEROKEE MAXIMUM EFFORT 2 5 ° FLAPS PAVED LEVEL DRY RUNWAY 7000 1000 5000 4000 3000 2000 1000 1000 2000 3500 1500 2500 3000 TAKE Of F DISTANCE FT. 753 806 740118...
  • Page 61 CHEROKEE " E " SECTION V PA-28-18O PIPER CHEROKEE 2400 LBS. GROSS WT. 16000 14000 12000 10000 8000 6000 4000 2000 1000 RATE OF CLIMB FT/MIN. 753 806 740118...
  • Page 62 SECTION V CHEROKEE " E " PA-28-180 PIPER CHEROKEE 2400 LBS GR0SS WT 50 GAL. FUEL FULL TANKS LEAN MIXTURE 12000 10000 8000 6000 4000 2000 RANGE (STATUTE MILES) 753 806 740118...
  • Page 63 CHEROKEE " E " SECTION V PA-28-18O PIPER CHEROKEE DENSITY ALTITUDE FT 740118...
  • Page 64 CHEROKEE " E " SECTION V PA-28-180 PIPER CHEROKEE 2400 LBS GROSS WT. 6000 5000 4000 3000 2000 1000 1000 1200 1400 LANDING DISTANCE 753 806 740118...
  • Page 65 CHEROKEE"E" SECTION V 753 806 740118...
  • Page 67 SECTION VI GENERAL MAINTENANCE Landing Gear Service Brake Service Tire Inflation Care of Windshield and Windows Battery Service Fuel and Oil Requirements Fuel System Care of Air Filter Leveling and Rigging Serial Number Plate 753 806 740118...

  • Page 69: General Maintenance

    Service Manual for this airplane. Any complex repairs or modification should be accomplished by a Piper Certified Service Center or equivalent. LANDING GEAR SERVICE The main wheels are Cleveland Aircraft Products, Model #40-86, with Cleveland single disk hydraulic brake assemblies, Model #30-55.
  • Page 70 In jacking the Cherokee for landing gear or other service, a jack kit (available through Piper Dealers or Distributors) should be used. This kit consists of two hydraulic jacks and a tail stand.

  • Page 71: Brake Service

    CHEROKEE "E" SECTION VI Alignment of the nose wheel can be checked by pushing the air- plane back and forth with the rudder centered to determine that the plane follows a perfectly straight line. The turning arc of the nose wheel is 22 degrees in either direction and factory ad- justed at stops on the bottom of the forging.

  • Page 72: Care Of Windshield And Windows

    1. Flush with clean water and dislodge excess dirt, mud, etc. with your hand. 2. Wash with mild soap and water or Piper Plastic Cleaner. Use a soft cloth or sponge. Do not rub. 3. Remove oil, grease or sealing compounds with a soft cloth and kerosene.

  • Page 73: Fuel And Oil Requirements

    CHEROKEE "E" SECTION VI If the battery is not up to charge, recharge starting at a 4 ampere rate and finishing with a 2 ampere rate. Quick charges are not recommended. FUEL AND OIL REQUIREMENTS Aviation Grade 91/96 Octane (minimum) fuel must be used engine.

  • Page 74: Care Of Air Filter

    SECTION VI CHEROKEE "E" CARE OF AIR FILTER The carburetor air filter must be cleaned at least once every fifty hours. Under extremely adverse conditions of operation it may be necessary to clean the filter daily. Extra filters are in- expensive and a spare should be kept on hand and used as a rapid replacement.

  • Page 75: Serial Number Plate

    CHEROKEE"E" SECTION VI 3. Fin should be vertical and in line with center of fuselage. 4. Aileron Travel: 30° up, 15° down, tolerance ±2°. 5. Flap Travel: 10°, 25°, 40° tolerance ±2°. 6. Rudder Travel: 27° right and left, tolerance ±2°. 7.
  • Page 76 SECTION VI CHEROKEE "E" NOTES 753 806 740118...
  • Page 77 CHEROKEE"E" SECTION VI 753 8O6 5 1 / 5 2 740118...

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