Piper CHEROKEE CRUISER PA-28-140 Information Manual Download Page 196

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AFMS, Garmin G5 AML STC

190-01112-13 Rev. 5

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Abbreviations and Terminology

The following glossary is applicable within the airplane flight manual supplement

ADI

Attitude Direction Indicator

AFMS

Airplane Flight Manual Supplement

ATT

Attitude

CDI

Course Deviation Indicator

Directional Gyro

Dead Reckoning

FAA

Federal Aviation Administration

GPS

Global Positioning System

GPSS

GPS Roll Steering

HDG

Heading

HSI

Horizontal Situation Indicator

ILS

Instrument Landing System

LOC

Localizer (no glideslope available)

LOI

Loss of Integrity

VFR

Visual Flight Rules

VHF

Very High Frequency

VOR

VHF Omni-directional Range

Summary of Contents for CHEROKEE CRUISER PA-28-140

Page 1: ......

Page 2: ......

Page 3: ...mplete without an APPROPRIATE FAA APPROVED AIRPLANE FLIGHT MANUAL and an APPROPRIATE WEIGHT AND BALANCE REPORT BY REFERENCE ONLY THIS ELECTRONIC VERSION OF THE POM AFM IS NOT APPROVED TO REPLACE ANY O...

Page 4: ...lane is safe for flight The pilot is also responsible for remaining within the operating limitations outlined by the Airplane Flight Manual instrument markings and placards This Pilot s Operating Manu...

Page 5: ...section 3 Page numbers followed by a small letter shall be inserted in direct sequence with the same common numbered page II Identification of Revised Material Revised text and illustrations shall be...

Page 6: ...lite Liner June 13 1974 PR740613 2 1 Added reference to Flite Liner to The Airplane relocate info to page 2 2 2 2 Added info from page 2 1 2 8 Added annunciator panel info and foot note relocated info...

Page 7: ...761 555 1 2 Revised footnote Nov 1 1974 PR7411Ol AF M Added Rev 3 to Report VB 557 W B Added Rev 4 to Report VB 546 7 4 Added new item 9 and revised existing item nos under Takeoff 8 2 Added item 11...

Page 8: ...m page 10 8 relocated Draining Fuel Valves and Lines to page 10 10 10 10 Added info from page 10 9 and relocated Facts You Should Know to page 10 11 10 11 Added info from page 10 10 and relocated info...

Page 9: ...sed fuel info AF M Added Rev 7 to Report VB 557 W B Added Rev 13 to Report VB 546 7 1 Revised Preflight 7 4 Added ending serial number effectivity 8 1 9 i Added Warning 10 8 Revised Fuel Requirements...

Page 10: ...RIPTION AIRPLANE AND SYSTEMS AIRPLANE FLIGHT MANUAL F A A APPROVED EMERGENCY PROCEDURES F A A APPROVED EMERGENCY PROCEDURES WEIGHT AND BALANCE LOADING INSTRUCTIONS OPERATING INSTRUCTIONS OPERATING TIP...

Page 11: ...GENERAL SPECIFICATIONS Performance I I Weights 1 2 Power Plant 1 2 Fuel 1 2 Oil 1 2 Baggage 1 2 Dimensions 1 3 Landing Gear 1 3 l i...

Page 12: ...g ft Cruise Speed at best power mixture optimum altitude TAS mph 65 power 10 250 ft 55 power 11 900 ft Range at best power mixture optimum altitude mi 75 power 7 800 ft 65 power 10 250 ft 55 power 11...

Page 13: ...ler Sensenich FUEL OIL AVGAS ONLY Fuel Capacity U S gal Standard Fuel Capacity U S gal Reserve Fuel Aviation Grade Minimum Octane Specified Octane Alternate Fuels Oil Capacity quarts BAGGAGE Maximum B...

Page 14: ...Height ft Power Loading Ibs per hp LANDING GEAR Wheel Base ft Wheel Tread ft Tire Pressure Ibs Tire Size Nose Main Nose 4 ply rating Main 4 ply rating GENERAL SPECIFICATIONS REVISED JULY 13 1984 CHER...

Page 15: ...CHEROKEE CRUISER 0 63 75 1 10 23 5 4 1 4 STATIC GROUND LINE GENERAL SPECIFICATIONS ISSUED JULY 6 1973...

Page 16: ...ng Gear 2 2 Flight Controls 2 5 Fuel System 2 5 Electrical Systen1 2 8 Vacuum System 2 11 Instrument Panel 2 11 Pitot Static System 2 14 Heating and Ventilating System 2 14 Cabin Features 2 16 Baggage...

Page 17: ...side of the fuselage by insertion of the butt ends of the respective main spars into a spar box carry through which is an integral part of the fuselage structure providing in effect a continuous main...

Page 18: ...et altitude LANDING GEAR The three landing gears use Cleveland 6 00 x 6 wheels the main wheels are being provided with brake drums and Cleveland single disc hydraulic brake assemblies The nose wheel a...

Page 19: ...1 I I i AIRPLANE AND SYSTEMS ISSUED JULY 6 1973 Main Wheel Assembly CHEROKEE CRUISER 2 3...

Page 20: ...CHEROKEE CRUISER 2 4 Throttle Quadrant and Console AIRPLANE AND SYSTEMS ISSUED JULY 6 1973...

Page 21: ...to return to the up position A past center lock incorporated in the actuating linkage holds the flap when it is in the up position so that it may be used as a step on the right side The flap will not...

Page 22: ...left corner of the fire wall This strainer should be drained during preflight to check for water or sediment and proper fuel a special bottle is furnished for this operation To drain the lines from t...

Page 23: ...AHTnl GAUGES FUEL TANK SELECTOR VALVE MAIN TANK AIRPLANE AND SYSTEMS ISSUED JULY 6 1973 FUEL PRESSURE GAUGE CARBURETOR Fuel System Schematic CHEROKEE CRUISER MAIN TANK ENGINE FUEL PUMP ELECTRIC FUEL P...

Page 24: ...or and low oil pressure indicator lights When the optional gyro system is installed the annunciator panel also includes a low vacuum indicator light The annunciator panel lights are provided only as a...

Page 25: ...EIt EXTERNAL POWE RECEPTACLE SOLENOID I I L _______ L __ J MASTE ICX EPIOID CHEROKEE CRUISER IlMTDt I I jL u MA IOURCI I OWIII RILM UCllGlllNG 1 MAITU SWITCH Alternator and Starter Schematic Ser nos 7...

Page 26: ...T I EXTERNAL I I POWER SOLENOID I l I EXTERNAL POWER I STARTER SOLENOID STARTER RECEPTACLE y _ I____ _________ J I I I I 1 _ _ _ _ _ _ _ _ _ J AMht TER ER J SOURCE POWER RELAY ENERGIZING CIRCUIT 1 MAS...

Page 27: ...AIRPLANE AND SYSTEMS REVISED JULY 18 1975 Circuit Breaker Panel CHEROKEE CRUISER a 8 o uJ z J t Z Q o II UJUJ c to ID I J _II t UUJ Z uO 2 10...

Page 28: ...e In the event of any gauge variation from the norm the pilot should have a mechanic check the system to prevent possible damage to the system components or eventual failure of the system A vacuum reg...

Page 29: ...Olb 0 _0 l lo nlb lz40 olb _0 _ 14 15 11 11 j O O I I I I C J 27 28 29 3D 31 32 33 34 35 36 31 40 31 16 NAV SELECTOR SWITCH 17 SUCTION GAUGE 18 CIGAR LIGHTER 19 MIKE JACK 20 PHONE JACK 21 AUTOPILOT 22...

Page 30: ...CHEROKEE CRUISER 2 12a THIS PAGE INTENTIONALLY LEFT BLANK AIRPLANE AND SYSTEMS ISSUED JUNE 13 1974...

Page 31: ...AIRPLANE AND SYSTEMS ISSUED JULY 6 1973 Pitot Static System CHEROKEE CRUISER 2 13...

Page 32: ...heat should be shut off and the system inspected for leaks The airflow may be regulated between the front and rear seats by the use of the levers located on top of the heat ducts next to the control c...

Page 33: ...f a w x x z en w a a u u 0 NM cnO AIRPLANE AND SYSTEMS ISSUED JULY 6 1973 Heating and Ventilating System CHEROKEE CRUISER I 2 15...

Page 34: ...gage compartment is located behind the seats in the two place model and is accessible from the cabin Maximum baggage capacity is 200 pounds NOTE It is the pilot s responsibility to be sure when the ba...

Page 35: ...l The temperature control regulates the temperature of the cabin Turn the control clockwise for increased cooling counterclockwise for decreased cooling Located inboard of the temperature control is t...

Page 36: ...ely 114 inch the clutch will engage and the scoop will extend again supplying cool dry air PIPER EXTERNAL POWER An optional starting installation known as Piper External Power PEP is accessible throug...

Page 37: ...RCRAFT CORPORATION SUBSEQUENT REVISIONS SUPPLIED BY PIPER AIRCRAFT CORPORATION MUST BE PROPERLY INSERTED MODEL PA 28 140 AIRCRAFT SERIAL NO REGISTRATION NO AIRPLANE FLIGHT MANUAL REPORT NUMBER VB 557...

Page 38: ...AIRPLANE FLIGHT MANUAL Log of Revisions 3 iii Limitations 3 1 Procedures 3 7 Performance 3 9 Supplements 3 11...

Page 39: ...3 2 G Baggage Capacity 3 2 H C G Range 3 2 1 Maneuvers 3 3 J Placards 3 3 K Air Conditioned Airplanes 3 6 SECTION II Procedures 3 7 SECTION III Performance 3 9 SECTION IV Supplements 3 11 A Electric P...

Page 40: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 557 PAGE 3 ii MODEL PA 28 140 FAA APPROVED MAY 14 1973...

Page 41: ...emaining Items 3 5 Added Spins Prohibited to Item 2 under Maneuvers Placard for Utility Category with Air Condo or Vent Blower 3 11 Deleted existing Items A B and E revised remaining Items 3 13 Delete...

Page 42: ...A 28 140 Description and Revision FAA Approved Date Added Applicable Serial Numbers LJ NOTE AIRCRAFT DELIVERED WITH MANUALS PRIOR TO THIS REVISION Ward Evans DO NOT REQUIRE THIS REVISION Sept 30 1977...

Page 43: ...f 1950 lbs Not under 2275 not over 2425 for max allowable weight of 2150 lbs No additional tolerance permitted D POWER INSTRUMENTS OIL TEMPERATURE Green Arc Normal Operating Range Red Line Maximum OIL...

Page 44: ...3 8 Utility Category 4 4 No inverted maneuvers approved 171 MPH 148 KTS 140 MPH to 171 MPH 121 KTS to 148 KTS 64 MPH to 140 MPH 56 KTS to 121 KTS 55 MPH to 115 MPH 48 KTS to 100 KTS 1950 LBS 2150 LBS...

Page 45: ...les J PLACARDS In full view of the pilot 1 Models Without Air Conditioning or Ventilation Blower Entry Speed Stall 129 MPH 129 MPH 129 MPH Entry Speed 129 MPH 129 MPH 129 MPH THIS AIRPLANE MUST BE OPE...

Page 46: ...d landing check lists will be installed TAKEOFF CHECK LIST Fuel on proper tank Electric fuel pump on Engine gauges checked Flaps set Carb heat off Mixture set Seat backs erect LANDING CHECK LIST Fuel...

Page 47: ...CEEDS SO F On the instrument panel in full view of the pilot when the AutoFlite is installed FOR HEADING CHANGES PRESS DISENGAGE SWITCH ON CONTROL WHEEL CHANGE HEADING RELEASE DISENGAGE SWITCH In full...

Page 48: ...TE TURN KNOB FOR TURN COMMANDS PUSH TURN KNOB IN TO ENGAGE TRACKER PUSH TRIM KNOB IN FOR HI SENSITIVITY LIMITATIONS AUTOFLITE OFF FOR TAKEOFF AND LANDING On the instrument panel in full view of the pi...

Page 49: ...he electric fuel pump must be on for both takeoff and landing 3 Except as noted above all operating procedures for this airplane are normal 4 Air Conditioned Models only Warning The air conditioner mu...

Page 50: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 557 PAGE 3 8 MODEL PA 28 140 FAA APPROVED MAY 14 1973...

Page 51: ...off versus angle of bank Calibrated Airspeed Angle of Bank Flaps Up Flaps Down Air Conditioner Models only 0 64 55 When the full throttle position is not used or in the event of a malfunction which ca...

Page 52: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 557 PAGE 3 10 MODEL PA 28 140 FAA APPROVED MAY 14 1973...

Page 53: ...L ONLY IF THE EQUIPMENT WHICH IS THE SUBJECT OF THE SUPPLEMENT IS INSTALLED A Electric Pitch Trim Installation B AutoFlite II Installation C Air Conditioner Installation D Piper AutoControl III and or...

Page 54: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 557 PAGE 3 12 MODEL PA 28 140 FAA APPROVED MAY 14 1973...

Page 55: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK FAA APPROVED MAY 14 1973 REVISED NOVEMBER 1 1974 REPORT VB 557 PAGE 3 13 MODEL PA 28 140...

Page 56: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFf BLANK REPORT VB 557 PAGE 3 14 MODEL PA 28 140 FAA APPROVED MAY 14 1973 REVISED NOVEMBER 1 1974...

Page 57: ...on disengage electric pitch trim by pushing pitch trim switch on instrument panel to OFF position 2 In an emergency electric pitch trim may be overpowered using manual pitch trim 3 In cruise configura...

Page 58: ...tion PRESS disconnect switch on pilot s control wheel 2 Rocker switch on instrument panel OFF 3 Unit may be overpowered manually 4 In cruise configuration malfunction 3 seconds delay results in 60 ban...

Page 59: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK FAA APPROVED MAY 14 1973 REVISED NOVEMBER 1 1974 REPORT VB 557 PAGE 3 17 MODEL PA 28 140...

Page 60: ...r control switch to OFF the AIR COND DOOR OPEN warning light will go out thereby indicating the air conditioner condenser door is in the up position 4 If the AIR COND DOOR OPEN light does not respond...

Page 61: ...ft and right slowly Observe that control wheel rotates in direction of needle movement d Disengage by placing the AlP ON OFF switch to the OFF position b IN FLIGHT 1 Trim airplane ball centered 2 Chec...

Page 62: ...sired HDG match course 2 Rotate OBS to the new course Aircraft will automatically turn to the intercept heading for the new course c To change stations I If same course is desired merely tune receiver...

Page 63: ...45 to ILS inbound course dial inbound course on Course Selector D G and position coupler mode selector to LOC NORM mode d At the missed approach point M A P or when missed approach is elected positio...

Page 64: ...trol wheel 3 An Autopilot runaway with a 3 second delay in the initiation of recovery while operating in a climb cruise or descending flight could result in a 60 bank and 100 foot altitude loss 4 An A...

Page 65: ...F A A APPROVED EMERGENCY PROCEDURES NONE APPLICABLE TO THIS AIRPLANE...

Page 66: ...e Power Loss During Takeoff 4 1 Engine Power Loss In Flight 4 2 Power Off Landing 4 2 Spins 4 3 Open Door 4 3 Fire 4 4 Loss of Oil Pressure 4 5 Loss of Fuel Pressure 4 5 High Oil Temperature 4 5 Alter...

Page 67: ...ide information on procedures which are not the same for all aircraft It is suggested that the pilot review standard emergency procedures periodically to remain proficient in them ENGINE POWER LOSS DU...

Page 68: ...striction 3 Try other fuel tanks Water in the fuel could take some time to be used up and allowing the engine to windmill may restore power If power loss is due to water fuel pressure indications will...

Page 69: ...VEL FLIGHT ATTITUDE OPEN DOOR The cabin door on the Cherokee is double latched so the chances of its springing open in flight at both the top and bottom are remote However should you forget the upper...

Page 70: ...s extremely remote The procedure given above is general and pilot judgment should be the deciding factor for action in such an emergency 3 Engine Fire During Start Engine fires during start are usuall...

Page 71: ...make an off airport landing while power is still available particularly if other indications of actual oil pressure loss such as sudden increases in temperatures or oil smoke are apparent and an airp...

Page 72: ...Turn carburetor heat on See Note RPM will decrease slightly and roughness will increase Wait for a decrease in engine roughness or an increase in RPM indicating ice removal If no change in approximate...

Page 73: ...ED IS VALID FOR USE WITH THE AIRPLANE IDENTIFIED BELOW WHEN APPROVED BY PIPER AIRCRAFT CORPORATION SUBSEQUENT REVISIONS SUPPLIED BY PIPER AIRCRAFT CORPORATION MUST BE PROPERLY INSERTED MODEL PA 28 140...

Page 74: ...and Propeller Accessories 5 15 B Engine and Engine Accessories 5 16 C Landing Gear and Brakes 5 17 D Electrical Equipment 5 18 E Instruments 5 19 F Miscellaneous 5 20 G Engine and Engine Accessories...

Page 75: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 546 PAGE 5 ii MODEL PA 28 140 ISSUED MAY 14 1973...

Page 76: ...ng and Main Wheel Fairing Weights Arms and Moments Changed Jump Seat to 4 Install Revised Ash Trays Weight and Moment Removed Baggage Tie Down Straps Revised Right and Left Vert Adj Front Seat Weights...

Page 77: ...Assist Strap Revised Utility Category Aft e G Limit Nov 1 1974 Revised Airborne Vacuum Pump Moment o tqf Revised King Dual KNI 520 Weight Revised equations Jan 21 1975 Added two Overhead Vent Systems...

Page 78: ...Weight and Balance info July 13 1984 5 3 Revised Weight and Balance Data info t J 5 7 5 15 Revised Equipment List 5 16 Added Niagara N D M 20002A to existing oil cooler description added ending serial...

Page 79: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB S46 PAGE S vi MODEL PA 28 140 ISSUED SEPTEMBER 30 1977...

Page 80: ...m as intended Before the airplane is licensed it is weighed and a licensed empty weight and e G location is computed licensed empty weight consists of the standard empty weight of the airplane plus th...

Page 81: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 546 PAGE 5 2 MODEL PA 28 140 ISSUED MAY 14 1973...

Page 82: ...l all undrainable fuel is used and engine stops CAUTION Whenever the fuel system is completely drained and fuel is re plenished it will be necessary to run the engine for a minimum of 3 minutes at 100...

Page 83: ...ol Reading Tare Weight Nose Wheel N Right Main Wheel R Left Main Wheel L Airplane Empty Weight as Weighed T 4 EMPTY WEIGHT CENTER OF GRAVITY a The following geometry applies to the PA 28 140 airplane...

Page 84: ...and parallel to the airplane centerline to each side of the nose wheel axle Then average the measurements d The empty weight center of gravity as weighed including optional equipment and undrainable o...

Page 85: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 546 PAGE 5 6 MODEL PA 28 140 ISSUED MAY 14 1973...

Page 86: ...nsed Empty Weight Empty weight is defined as dry empty weight including paint and hydraulic fluid plus 1 8 lbs undrainable engine oil AIRPLANE USEFUL LOAD Gross Weight Licensed Empty Weight Useful Loa...

Page 87: ...Divide the total moment by the total weight to determine the e G location 5 By using the figures of Item 1 and Item 4 locate a point on the e G range and weight graph If the point falls within the e G...

Page 88: ...r of gravity e G of this sample loading problem is at inches aft of the datum line Locate this point on the e G range and weight graph Since this point faIls within the weight C G envelope this loadin...

Page 89: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 546 PAGE 5 10 MODEL PA 28 140 ISSUED MAY 14 1973...

Page 90: ...ble Baggage Capacity Area D 200 lbs B Maximum Allowable Baggage Capacity Area 100 lbs Aircraft are eligible for lOO lb maximum baggage in this area when modified in accordance with Piper drawing 66671...

Page 91: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 546 PAGE 5 12 MODEL PA 28 140 ISSUED MAY 14 1973...

Page 92: ...LU c 200 0 J 150 100 V 50 V r 0 r 5 10 ISSUED MAY 14 1973 CHEROKEE CRUISER LOADING GRAPH r cf t r S e li o t e t er 1 eO V V V V VL L v V V e V e j 15 20 25 30 35 40 45 50 MOMENT 1000 POUNDS INCHES RE...

Page 93: ...OKEE CRUISER C G RANGE AND WEIGHTS 2200 Normel Category 2000 L V I 1800 Utility Category J V 1600 1400 1200 84 86 REPORT VB 546 PAGE 5 14 MODEL PA 28 140 88 90 92 INCHES AFT DATUM 94 ISSUED MAY 14 197...

Page 94: ...when the airplane was licensed by the manufacturer Item Item A Propeller and Propeller Accessories Propeller Sensenich 74DM6 0 SS Spinner and Attachment Plates Installation PAC Dwg 995 I6 ISSUED MAY 1...

Page 95: ...r Purolator AFP 2 Starter Lycoming 76210 Prestolite MZ4204 Oil Filter Lycoming 75528 AC OF5578770 Oil Filter Lycoming LW 13743 Champion CH 48110 Included in Engine Weight Serial nos 28 7525001 through...

Page 96: ...4 Ply Rating Tires 6 00 6 with Regular Tubes One Nose Wheel 6 00 6 a Cleveland Aircraft Products Wheel Assembly No 38501 Less Brake Drum b One Nose Wheel 4 Ply Rating Tire 6 00 6 with Regular Tubes IS...

Page 97: ...B Battery 12V 25 A H Rebat Model S 25 Overvoltage Relay Wico Electric No X16799 Annunciator Lights I Serial nos 28 7525001 through 28 7625275 REPORT VB 546 PAGE 5 18 MODEL PA 28 140 Weight Lbs 2 9 21...

Page 98: ...62177 2 3 or 8 7 Engine Cluster Piper Dwg 95241 17 8 Altimeter Piper PS50008 2 or 3 1 0 Ammeter Piper Dwg 66696 3 ISSUED MAY 14 1973 CHEROKEE CRUISER Arm Aft Cert Datum Moment Basis 64 9 58 TSO C7c 6...

Page 99: ...Piper Dwg 66804 66805 Flight Manual Logs Tow Bar Piper Dwg 99458 Toe Brakes Dual Piper Dwg 63476 3 63473 8 REPORT VB 546 PAGE 5 20 MODEL PA 28 140 Weight Lbs 1 5 1 5 1 2 2 6 1 3 11 0 Arm Aft Cert Dat...

Page 100: ...ion CH 48 110 2 8 40 5 113 TC 2AI3 Vacuum Regulator Airborne Mfg Co 133A4 6 57 0 34 TC 2AI3 Vacuum Filter Airborne Mfg Co 1J7 1 3 57 0 17 TC 2AI3 Vacuum Pump Airborne Mfg Co Model 211 cc and Drive PAC...

Page 101: ...Speaker Co Oakton Ind 8 104 0 83 TC 2A13 Auxiliary Power Receptacle Piper Dwg 65529 3 0 133 0 399 TC 2A13 External Power Cable Piper Dwg 62355 7 4 6 117 0 538 TC 2A13 Piper Pitch Trim Piper Dwg 67496...

Page 102: ...29 PR or PG Cable Wing Lights A417 J 388 A417 J 326 Overhead Red Panel Lights 2 Grimes 15 0083 7 Instrument Panel Lights ISSUED MAY 14 1973 REVISED JUNE 13 1974 Weight Lbs 4 4 3 0 3 2 0 2 3 CHEROKEE C...

Page 103: ...Temperature Gauge Piper Dwg 99479 0 or 2 2 77 6 16 TC2A13 Clock 4 67 4 27 TC 2A13 Tru Speed Indicator Piper Dwg 62143 or 62143 12 same as Standard Equipment Weight Turn and Slip Indicator Piper PS5003...

Page 104: ...s 28 7425001 through 28 7425454 Serial nos 28 752500 I through 28 7625275 ISSUED MAY 14 1973 REVISED JULY 13 1984 Weight Lbs 2 5 1 2 7 2 3 3 2 9 2 5 7 2 4 2 5 1 0 5 2 7 2 9 1 0 CHEROKEE CRUISER Arm Af...

Page 105: ...XI75 VHF Comm Nav Transceiver Single Transceiver Dual King KI201 VORILOC Ind King Dual KI20 I VORILOC Ind King Kl214 VOR LOC GS Ind Serial nos 28 7425001 through 28 7425454 REPORT VB 546 PAGE 5 26 MOD...

Page 106: ...Cable Audio Amplifier Sense Antenna and Cable Serial nos 28 742500 I through 28 7425454 ISSUED MAY 14 1973 REVISED JUNE 13 1974 Weight Lbs 5 9 3 4 3 5 1 0 0 4 1 0 0 5 0 5 1 2 3 3 3 5 8 1 7 1 3 2 3 4...

Page 107: ...rophone Piper Dwg 68856 10 Microphone Dynamic Piper Dwg 68856 12 Headset Piper Dwg 68856 10 Weight includes Antenna and Cable REPORT VB 546 PAGE 5 28 MODEL PA 28 140 Weight Lbs 2 4 1 8 4 5 3 0 6 8 2 0...

Page 108: ...KN65A DME I Serial nos 28 7525001 through 28 7625275 ISSUED JUNE 13 1974 REVISED JULY 13 1984 Weight Lbs 2 5 3 9 1 5 1 3 0 8 0 4 3 9 1 5 1 3 3 0 3 2 3 6 7 8 7 6 0 2 0 3 1 0 3 7 1 0 5 6 12 5 13 0 CHER...

Page 109: ...63 6 159 TC 2AI3 Narco Nav 112 VHF Receiver 3 3 63 6 210 TC 2AI3 Narco Nav 14 VHF Receiver 2 5 62 4 156 TC 2AI3 Narco Nav 114 VHF Receiver 2 5 62 4 156 TC 2Al3 Narco UGR 3 Glide Slope Receiver 2 4 141...

Page 110: ...Dynamic Piper Dwg 68856 11 I Serial nos 28 7525001 through 28 7625275 ISSUED JUNE 13 1974 REVISED JULY 13 1984 Weight Lbs 5 0 3 5 1 6 0 6 0 4 1 6 0 6 3 0 2 0 5 2 0 3 0 4 0 6 CHEROKEE CRUISER Arm Aft...

Page 111: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 546 PAGE 5 28d MODEL PA 28 140 ISSUED JUNE 13 1974...

Page 112: ...Seats 2 16 2 117 0 1895 TC 2AI3 Seat Back 99948 0 2 Seat Bottom 99949 0 2 Ash Trays 2 2A20580 _ Grand Rapids Metalcraft 4 110 2 44 TC 2AI3 Jump Seat Belts and Cables PS50039 4 3 96908 0 3 1 1 123 0 1...

Page 113: ...stem Piper Dwg 79183 3 6 5 6 159 8 893 TC 2A13 Cabin Overhead Vent System With Ground Ventilating Blower Piper Dwg 79183 4 6 13 1 171 4 2246 TC 2A13 Super Cabin Sound Proofing Piper Dwg 78030 0 16 3 8...

Page 114: ...s TOTAL OPTIONAL EQUIPMENT EXTERIOR FINISH Base Color Trim Color___ Accent Color ISSUED MAY 14 1973 REVISED MAY 16 1975 CHEROKEE CRUISER Weight Arm Aft Lbs Datum Moment Cert Basis TC 2AD Registration...

Page 115: ...CHEROKEE CRUISER THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 546 PAGE 5 32 MODEL PA 28 140 ISSUED MAY 14 1973...

Page 116: ...LOADING INSTRUCTIONS THIS SECTION IS NOT APPLICABLE TO THIS AIRPLANE 6 i...

Page 117: ...round Check Takeoff Climb Stalls Cruising Turbulent Air Operation Maneuvers Approach and Landing Stopping Engine Airspeed Data Mooring Weight and Balance Air Conditioning Air Conditioner Operational C...

Page 118: ...re that wings and control surfaces are free of snow ice or frost 3 a Visually check fuel supply secure caps b Drain all fuel system sumps and lines and check for water sediment and proper fuel See Fue...

Page 119: ...g brake ON 2 Set the carburetor heat control in the full COLD OFF position 3 Select the desired tank with fuel selector valve STARTING ENGINE WHEN COLD 1 Open throttle approximately 114 inch 2 Turn th...

Page 120: ...xternal 12 volt battery and BLACK lead to NEGATIVE terminal 3 Insert plug of jumper cable into socket located on aircraft fuselage 4 Turn aircraft MASTER SWITCH to ON and proceed with NORMAL engine st...

Page 121: ...set 7 Seat backs erect 8 Safety Belts harness fastened 9 Empty seats seat belts snugly fastened 10 Trim tab set 11 Controls free 12 Door latched 13 Air conditioner off NOTE Mixture full rich except a...

Page 122: ...ally between 5 and 10 miles per hour above stall speed Gross weight stalling speed with power off and full flaps is 55 miles per hour at 2150 pounds With flaps up this speed is increased 9 miles per h...

Page 123: ...s are prohibited when air conditioning is installed Intentional spins are prohibited in the normal category airplane Lazy eights and chandelles may be performed in the normal category provided a 60 an...

Page 124: ...with partial or no flaps STOPPING ENGINE At the pilot s discretion the flaps should be raised and the electric fuel pump turned off After parking the air conditioner and radios should be turned off a...

Page 125: ...und or in flight 1 Start the engine ground operation 2 Turn the air conditioning Master Switch to ON 3 Turn TEMP control to desired temperature Clockwise rotation increases cooling 4 Select desired FA...

Page 126: ...NOTE To insure maximum climb performance the air conditioner must be turned off manually before takeoff to disengage the compressor and retract the condenser door Also the air conditioner must be tur...

Page 127: ...th three slotted head nylon screws for ease of removal these screws may be readily removed with a variety of common items such as a dime a key a knife blade etc If there are no tools available in an e...

Page 128: ...positions and is placarded ON RESET and ARM NORMAL POSITION The switch is normally left in the down or ARM position To turn the transmitter off move the switch to the ON RESET position for one second...

Page 129: ...OPERATING TIPS Operating Tips 8 8 i...

Page 130: ...0 output from the alternator The relay may be reset by switching the ALT switch to OFF for approximately 1 second and then returning the ALT switch to ON If after recycling the ALT switch the conditi...

Page 131: ...spacial disorientation Do not operate strobe lights when taxiing in the vicinity of other aircraft 10 The rudder pedals are suspended from a torque tube which extends across the fuselage The pilot sho...

Page 132: ...rformance Range Standard Fuel Capacity 9 6 Cruise Performance Range Maximum Fuel Capacity 9 7 Glide Performance 9 8 Stall Speed vs Aircraft Gross Weight 9 9 Stall Speed vs Angle of Bank 9 10 Landing P...

Page 133: ...z Q 8000 4000 V f4 1 V V THIS CHART SHOULD BE USED TO DETERMINE DENSITY ALTITUDE FROM EXISTING TEMPERATURE AND PRESSURE ALTITUDE CONDITIONS FOR USE WITH PERFORMANCE CHARTS V STD I TEMP V I V 1 V I V V...

Page 134: ...EXTRAPOLATION OF CHART ABOVE 7000 FT IS ItVAUO t I 1 il I GROSS WEIGHT V I 1950 LBS I I 2150 LBS I JII V iii V 1 II I ill I r I I I I I AIRSPEED THROUGH 50 FEET 1950 LBS 72 MPH CAS I 2150 LBS 76 MPH...

Page 135: ...lE CHEROKEE CRUISER MIXTURE LEAN PER LYCOMING INSTRUCTIONS 14000 1 12000 10000 t 1000 c a i S 10DO c I en 4000 c a 2000 89 MPH CAS f f 211 400 600 100 RATE OF CUIB FEET PER IllITE NOTE SEE SECTION 7 F...

Page 136: ...ro ro OO f OOM ro GROSS WEIGHT 2150 LBS WHEEL FAIRINGS INSTALLED MIXTURE LEAN PER LYCOMING INSTRUCTIONS BEST POWER V I II V I j I i V L 1 f fJ I o q I r A 2100 2200 2300 2400 2500 ENGINE R P M NOTE SE...

Page 137: ...INGS INSTALLED BEST POWER MIXTURE LEAN PER LYCOMING INSTRUCTIONS r FUll THROTILE K I I NOTE ADD 3 MPH WHEN WHEEL FAIRINGS ARE INSTALLED II I 1 II I I I EI C Q W L 1 ff I J 1 j I I V L II J I 100 110 1...

Page 138: ...ING INSTRUCTIONS I I I ZERO WIND NO RESERVE 45 MIN RESERVE AT 55 POWER 9 6 12000 10000 8000 i c SOOO t z 4000 2000 o I r i 300 gl I I I QI PERCENT co I co RATED I c o POWER I Q I 75 k 65 55 z i I II I...

Page 139: ...FUEL BEST ECONOMY MIXTURE LEAN PER LYCOMING INSTRUCTIONS ZERO WIND I I I NO RESERVE t 45 MIN RESERVE AT 55 POWER J I l a I CGI I 1 e II 1 I 1 II i J te I i I t I z I II I I Q I I II III I I I I I I 1...

Page 140: ...f OO OO Mti ro GROSS WEIGHT 2150 LBS PROP WINDMILLING FLAPS 00 ZERO WIND STANDARD DAY CONDITIONS 85 MPH CAS V jV V V V I V V 2000 jV S l V o 9 8 5 10 15 20 25 GLIDE DISTANCE STATUTE MILES NOTE SEE SEC...

Page 141: ...HEROKEE I I I I I v L L prnrn Wrs ru V ru wrn g lf POWER OFF 4 V v O 1400 V 1600 1800 2000 2200 AIRCRAR GROSS WEIGHT POUNDS NOTE SEE SECTION 7 FOR EFFECTS OF AIR CONDITIONING INSTALLATION ON PERFORMAN...

Page 142: ...10 PA 28 140 CHEROKEE I r J J r 11 L L P p W OO Il f OO OO 16 GROSS WEIGHT 2150 LIS POWER OFF V fU S i V f S 20 30 40 50 ANGLE OF BANK DEGREES V 60 NOTE SEE SECTION 7 FOR EFFECTS OF AIR CONDITIONING I...

Page 143: ...OO OO AA ro GROSS WEIGHT 2150 lBS PAVED LEVEL DRY RUNWAY POWER OFF 40 FLAPS ZERO WIND MAXIMUM BRAKING APPROACH AIRSPEED 71 MPH CAS s I to Q CII 0 I 40 101 WlDItC DlSTlJICE FEET NOTE SEE SECTION 7 FOR...

Page 144: ...ant Induction Air Filter 10 5 Removal of Induction Air Filter 10 5 Cleaning Induction Air Filter 10 5 Installation of Induction Air Filter 10 5 Brake Service 10 7 Landing Gear Service 10 7 Propeller S...

Page 145: ...ound personnel should be instructed and approved by a qualified person authorized by the owner Engine starting and shut down procedures as well as taxi techniques should be covered When it is ascertai...

Page 146: ...nder varying weather conditions The following procedure should be used for proper mooring of the airplane a Head the airplane into the wind if possible b Lock the aileron and stabilator controls by lo...

Page 147: ...Do not operate the engine until excess solvent has evaporated or otherwise been removed d Remove the protective covers from the magnetos e Lubricate controls bearing surfaces etc in accordance with t...

Page 148: ...shing A heavier coating of wax on the leading surfaces will reduce the abrasion problems in these areas CLEANING WINDSHIELD AND WINDOWS A certain amount of care is needed to keep the plexiglas windows...

Page 149: ...ensive and a spare should be kept on hand and used as a rapid replacement REMOVAL OF INDUCTION AIR FILTER The air filter is located below the spinner assembly If a landing light is installed it will b...

Page 150: ...NO RUOOER PEDAL 3 LEFT BRAKE ANO RUODER PEDAL 4 RIGHT BRAKE CYLINDER 5 LEFT BRAKE CYLINDER Ii BRAKE HANDLE 7 HANDLE RELEASE BUTTON 8 LINE INLET 9 CLEVIS PIN 10 MASTER CYLINDER ASSEMBLY 11 BOLT ASSEMBL...

Page 151: ...uid it will be visible up to the bottom of the filler plug hole and will then require only proper inflation Should fluid be below the bottom of the filler plug hole oil should be added Replace the plu...

Page 152: ...s of operation The interval between oil and oil filter changes should not exceed a total of four 4 months Under unfavorable dusty conditions the oil and oil filter should be changed more frequently Sh...

Page 153: ...5 of the operating time of the higher leaded fuels can result in increased engine deposits both in the combustion chamber and in the engine oil It may require increased spark plug maintenance and more...

Page 154: ...CHEROKEE CRUISER 10 8b THIS PAGE INTENTIONALLY LEFT BLANK HANDLING AND SERVICING ISSUED MARCH 16 1990...

Page 155: ...45 purple 4 6 none none none 1151145 purple 4 6 Grade 100LL fuel in some over seas countries is colored green and designated as 100L Commercial fuel grade 100 and grade 100 130 having TEL content of u...

Page 156: ...of the drain valve and turn counterclockwise to hold the drain open The remaining fuel in the system may be drained through the filter bowl Any individual tank may be drained by closing the selector...

Page 157: ...are sent to Piper Service Centers and if necessary to the latest FAA registered owners in the U S Owners should give careful attention to Service Letter information Service Spares Letters offer improv...

Page 158: ...mation about what has or has not been accomplished PREVENTIVE MAINTENANCE The holder of a Pilot Certificate issued under FAR Part 61 may perform certain preventive maintenance described in FAR Part 43...

Page 159: ...tins issued by Piper Aircraft Corporation instructions issued by the engine propeller or accessory manufacturers or Airworthiness Directives issued by the FAA A Programmed Inspection approved by the F...

Page 160: ...PLATES FROM INSTRUMENT PANEL LUBRICATE 0 RING AND REASSEMBLE LUBRICAllON POINTS WIPE ALL LUBRICAllON POINTS CLEAN OF OLD GREASE OIL DIRT ETC BEFORE LUBRICAllNG INTERVALS BETWEEN OIL CHANGES CAN BE IN...

Page 161: ...HANDLING AND SERVICING ISSUED JULY 6 1973 CHEROKEE CRUISER 0 Ie I J 10 15...

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Page 180: ...28 140 HK 1791G S N 28 7625144 ELABORADO POR OSCAR WILMAN MOSQUERA Inspector de avi nica AIT CDF119 2229 JUAN SEBASTIAN SANTAMARIA Asistente de Ingenier a REVISADO POR CARLOS ALBERTO NU EZ TAPIERO In...

Page 181: ...EROKEE PA 28 140 Registration number HK 1791G Serial number 28 7625144 This document serves as an PILOT OPERATING HANDBOOK SUPLEMENT when Garmin GTX335 System is installed in Accordance with Technical...

Page 182: ...INSTALACI N DE UN TRANSPONDER MODELO GTX335 W GPS ADS B EN LA AERONAVE HK 1791G OPERADA POR AEROCLUB DE COLOMBIA Calle 24D N 40 53 Quinta Paredes Bogot Colombia Tel fonos 57 1 5702743 Fax 57 1 357550...

Page 183: ...interrogations at 1030 MHz and transmitting a coded response of pulses to ground based radar on a frequency of 1090 MHz This unit is equipped with IDENT capability and will reply to ATCRBS Mode A Mode...

Page 184: ...GPS ADS B with the following interfaces features Equipment Installed Transponder 1 Interfaced GPS SBAS Position Source s GPS 1 Interfaced Pressure Altitude Source Pressure Altitude Source 1 1 5 Defin...

Page 185: ...2 2 6 ADS B Out when all required functions are operational When the system is not operational ADS B Out transmit failure messages will be present on the remote control display interface or the GTX 33...

Page 186: ...ID POSITION SECTION 4 NORMAL PROCEDURES The procedures described below are specific only to the panel mounted GTX 335 W GPS ADS B transponders Cockpit Reference Guides and Pilot Guides for interfaced...

Page 187: ...em to meet the requirements specified in RAC Part 4 2 2 6 ADS B Out This system must be operational in certain airspaces after January 1 2020 as specified by RAC Part 4 2 2 6 ADS B Out SECTION 5 PERFO...

Page 188: ......

Page 189: ...Piper PA 28 140 28 7625144 HK 1791 G...

Page 190: ...download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed and to print one copy of this manual or of any revision here...

Page 191: ...ROVED 1 ALL Original Issue 7 22 2016 Robert Murray ODA STC Unit Administrator 2 ALL Added information regarding G5 DG HSI 4 28 2017 Robert Murray ODA STC Unit Administrator 3 ALL Added interface to 3r...

Page 192: ...AFMS Garmin G5 AML STC 190 01112 13 Rev 5 Page ii This page intentionally left blank...

Page 193: ...ude Aligning Keep Wings Level 3 2 Loss of Electrical Power to the G5 Display 3 2 Loss of Electrical Power to the GAD 29B If Installed 3 3 Section 4 Normal Procedures 4 1 G5 Power Button and Knob 4 1 B...

Page 194: ...AFMS Garmin G5 AML STC 190 01112 13 Rev 5 Page iv This page intentionally left blank...

Page 195: ...lace of the rate of turn indicator the primary function of the G5 is to provide turn rate and slip ball information to the pilot When installed in place of the directional gyro the primary function of...

Page 196: ...light Manual Supplement ATT Attitude CDI Course Deviation Indicator DG Directional Gyro DR Dead Reckoning FAA Federal Aviation Administration GPS Global Positioning System GPSS GPS Roll Steering HDG H...

Page 197: ...imary indications for these parameters If the G5 Electronic Flight Instrument is installed in place of the rate of turn indicator the original type design approved instrument for attitude remains in t...

Page 198: ...AFMS Garmin G5 AML STC 190 01112 13 Rev 5 Page 2 2 This page intentionally left blank...

Page 199: ...a Garmin authorized repair facility Attitude Failure Attitude failure is indicated by removal of the sky ground presentation a red X and a yellow ATTITUDE FAIL on the display Rate of turn and slip in...

Page 200: ...essage will clear when the attitude solution is within the systems internal accuracy tolerances It is recommended to maintain wings level to reduce the time for the system to align Attitude Aligning K...

Page 201: ...be unavailable to the autopilot and the autopilot may deviate from the intended path or may disconnect GPS flight plan course information may be displayed on the HSI and VFR will be displayed in amber...

Page 202: ...AFMS Garmin G5 AML STC 190 01112 13 Rev 5 Page 3 4 This page intentionally left blank...

Page 203: ...setting on the secondary altitude display For the HSI rotate to adjust the heading or track bug Turn to select the desired value when editing numeric data or selecting from a list Backlight Intensity...

Page 204: ...ine the best intercept angles when operating in NAV mode Heading Bug Coupling Capability to the Autopilot If Configured When operating the autopilot in HDG mode the difference between the HDG bug loca...

Page 205: ...TC Page 4 3 navigator If the GPSS data is invalid for example if there is no active GPS leg or the selected HSI source on the G5 HSI is not GPS the annunciated GPSS text will be yellow and a zero turn...

Page 206: ...AFMS Garmin G5 AML STC 190 01112 13 Rev 5 Page 4 4 This page intentionally left blank...

Page 207: ...190 01112 13 Rev 5 AFMS Garmin G5 AML STC Page 5 1 SECTION 5 PERFORMANCE No change...

Page 208: ...AFMS Garmin G5 AML STC 190 01112 13 Rev 5 Page 5 2 This page intentionally left blank...

Page 209: ...190 01112 13 Rev 5 AFMS Garmin G5 AML STC Page 6 1 SECTION 6 WEIGHT AND BALANCE See current weight and balance data...

Page 210: ...AFMS Garmin G5 AML STC 190 01112 13 Rev 5 Page 6 2 This page intentionally left blank...

Page 211: ...to charge the internal battery The DG circuit breaker supplies power to the G5 instrument for normal power operation when configured as a DG and to charge the internal battery if installed The HSI ci...

Page 212: ...s in conjunction with Network Address Conflict message Factory calibration data invalid Unit calibration data not valid unit needs service Magnetic field model database out of date Internal magnetic f...

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