Page 3 - SERIES IMPACT 36 PLUS II; TABLE OF CONTENTS; SERVICE
PART TITLE 1 THE AC GENERATOR 2 ENGINE MECHANICAL 3 GASOLINE FUEL SYSTEM 4 GASEOUS FUEL SYSTEM 5 ENGINE OIL & COOLING SYSTEM 6 ENGINE ELECTRICAL SYSTEM 7 TROUBLESHOOTING 8 SPECIFICATIONS & CHARTS SERIES IMPACT 36 PLUS II TABLE OF CONTENTS SERVICE MANUAL
Page 5 - COMPUTER; Series Impact 36 Plus II
Page 1 PART 1 GENERAL INFORMATION COMPUTER CONTROLLED VARIABLE SPEED RV GENERATORS Series Impact 36 Plus II SECTION TITLE 1.1 GENERATOR FUNDAMENTALS 1.2 GENERATOR MAJOR COMPONENTS 1.3 OPERATIONAL ANALYSIS 1.4 INSULATION RESISTANCE 1.5 COMPONENTS TESTING 1.6 CONTROL PANEL 1.7 SHEET METAL
Page 6 - NOTES
Page 8 - Figure 5. Alternating Current Sine Wave
Section 1.1GENERATOR FUNDAMENTALS ALTERNATING CURRENT A simple generator consists of a coil of wires called aStator and a magnetic field called a Rotor. As theRotor's magnetic field cuts across the Stator coil, av o l t a g e i s i n d u c e d i n t o t h e S t a t o r w i n d i n g s . T h eamount ...
Page 9 - GENERATOR FUNDAMENTALS; Figure 6. Electrical Units; OHMS; REACTANCE IN AC CIRCUITS; Figure 8. Inductive Reactance
Section 1.1 GENERATOR FUNDAMENTALS Figure 6. Electrical Units OHM:The OHM is the unit of RESISTANCE. In every circuitthere is a natural resistance or opposition to the flowof electrons. When an EMF is applied to a completecircuit, the electrons are forced to flow in a singledirection rather than the...
Page 13 - Item; UPPER FAN HOUSING
Section 1.2 MAJOR GENERATOR COMPONENTS INTRODUCTION Major components of the generator proper are shownin Figure 1, below. External sheet metal and otherunrelated components are omitted from the drawingfor clarity. These parts are: Item Description 1 Upper Fan Housing 2 Upper Cooling Fan 3 Permanent ...
Page 15 - MAJOR GENERATOR COMPONENTS
Section 1.2 MAJOR GENERATOR COMPONENTS Figure 5. Schematic- Stator Windings Page 1.2-3
Page 20 - TEST ALL STATOR WINDINGS TO GROUND; TEST FOR SHORTS BETWEEN WINDINGS
Section 1.4INSULATION RESISTANCE TEST ALL STATOR WINDINGS TO GROUND Connect the ends of all Stator leads together. Makesure none of the leads are touching any terminal orany part of the generator.Connect one Tester probe to the junction of all Statorleads; the other Tester probe to a clean frame gro...
Page 23 - NOMINAL RESISTANCE- POWER PHASE WINDINGS
Section 1.5 COMPONENTS TESTING INTRODUCTION Problems that occur In the computer-controlled RVgenerator generally involve the following systems orcomponents: 1. The engine. 2. The Speed Control System. 3. The AC Generator. 4. Battery Charge Circuit. 5. A6060 Circuit Board. 6. Wiring Harness and Front...
Page 25 - BATTERY CHARGE WINDING RESISTANCE
Section 1.5 COMPONENTS TESTING 7. Connect one test lead to Stator lead PS1, the other to Stator lead 77. The VOM should read"infinity". 8. Connect one VOM test lead to Stator lead TIM1, the other test lead to Stator lead 77. "Infinity"should be Indicated. TESTING THE BATTERY CHARGE C...
Page 27 - Figure 1. Exploded View of Control Panel
Section 1.6 CONTROL PANEL CONSTRUCTION The panel is constructed of sheet metal and includesa panel box, a panel back cover and a front controlpanel. The panel box is retained to an engine-genera-tor divider plate by five M5 screws. Removal of thesescrews will permit the panel to be removed from thed...
Page 29 - Impact Plus Generator
Section 1.7 SHEET METAL See "Exploded View of Sheet Metal" on next page. ADIVIDER PLATE (Item 1) separates the AC generatorcomponents from the engine. The engine Itself isenclosed by a BASE HOUSING WRAPPER (Item 4),a FRAME (Item 24), and a BELLY PAN (Item 23).These components are sealed by m...
Page 30 - EXPLODED VIEW OF SHEET METAL (GASOLINE UNITS)
Section 1.7SHEET METAL Page 1.7-2 5 35 7 8 6 33 34 23 44 45 53 30 29 5 25 39 59 59 3 3 20 21 22 54 5 26 4 2 30 4 59 3 57 22 38 3 57 24 3 1 TO CARBURETOR 40 41 53 29 30 31 5 32 37 47 50 37 28 27 39 60 49 37 51 36 30 75 77 72 78 81 5 71 73 79 74 76 70 59 12 13 19 48 5 17 5 18 80 65 42 63 7 64 7 64 62 ...
Page 35 - Series Impact 36 Plus; SECTION
PART 2 ENGINE MECHANICAL COMPUTER CONTROLLED VARIABLE SPEED RV GENERATORS Series Impact 36 Plus SECTION TITLE 2.1 GENERAL INFORMATION 2.2 VALVE TRAIN 2.3 PISTON, RINGS, CONNECTING ROD 2.4 CRANKSHAFT & CAMSHAFT
Page 37 - Figure 1. Intake Stroke
Section 2.1 GENERAL INFORMATION INTRODUCTION The engine used on Impact 36 plus Series recreationalvehicle AC generators is a Generac Series GV-220,vertical shaft, single cylinder, overhead valve type.These engines are not equipped with a mechanicalengine governor. Instead. variable engine speeds are...
Page 38 - RECOMMENDED FUELS; carbon formation in the engine.; RECOMMENDED ENGINE OIL
Section 2.1GENERAL INFORMATION TIMING:Valve timing and ignition timing must be preciselycontrolled if the engine is to operate properly and effi-ciently. Intake and exhaust valves must open andclose in a precise timed sequence if the four strokesare to occur. Ignition must occur at exactly the corre...
Page 39 - THE UNIT IS NOW READY FOR SERVICE.
Section 2.1 GENERAL INFORMATION Engine crankcase oil capacity without oil filter changeis about 29 fluid ounces (850m.Engine crankcase oil capacity (with oil filter change) isabout 1 U.S. quart (946m1).Change engine oil and the oil filter after the first eight(8) hours of operation. Thereafter, chan...
Page 40 - NOTE 1:- Item 36 Includes valve seats and
Section 2.1GENERAL INFORMATION ITEM QTY DESCRIPTION 1 1 Connecting Rod 2 1 Piston Pin 3 1 Piston Ring Set (STD) 4 2 1/4" Pipe Plug 5 1 Breather Cover 6 1 Piston 7 2 Piston Pin Retainer 8 1 Crankshaft & Gear Assembly 10 1 Oil Breather Separator 11 1 Crankcase Assembly 12 1 Sleeve Bearing 13 2...
Page 41 - ITEM QTY DESCRIPTION; Figure 1. Valve Train Components; VALVE COMPONENTS REMOVAL; Figure 2. Removal of Rocker Arm over
Section 2.2 VALVE TRAIN VALVE TRAIN COMPONENTS Valve train components are listed below and shown inFigure 1, below. ITEM QTY DESCRIPTION 1 2 Tappet 2 2 Push Rod 3 2 Rocker Arm 4 2 Pivot Ball Stud 5 2 Rocker Arm Jam Nut 6 1 Push Rod Guide Plate 7 2 Valve Spring 8 2 Valve Spring Retainer 9 2 Valve Spr...
Page 42 - VALVE SERVICE
Section 2.2VALVE TRAIN Figure 4. Cylinder Head Removal DANGER! ALWAYS WEAR SAFETY GLASSESWHEN REMOVING THE VALVE SPRINGS. 5. See Figure 5, next page. Hold the valve with your fingers while compressing the spring with your thumb, then proceed as fol-lows: a. While the spring is compressed, slide the ...
Page 43 - VALVE TRAIN; VALVE SPRING FREE LENGTH; VALVE COMPONENTS INSTALLATION
Section 2.2 VALVE TRAIN NOTE: After the valve guides have been over-sized, be sure to recut the valve seats so they willalign with the guides. Figure 8. Valve Guides VALVE TAPPETS:Valve tappets can be removed during removal of theengine camshaft. Intake and exhaust valve tappetsare identical. Howeve...
Page 44 - TIGHTENING TORQUE; ADJUSTING VALVE CLEARANCE
Section 2.2VALVE TRAIN VALVE COMPONENTS INSTALLATION (CONTINUED) 3. Install the valve spring washers, valve springs and valve spring retainers over the valve guides. a. Hold the valve with your fingers and use your thumbs to compress the spring. b. When the spring is compressed sufficiently, slide t...
Page 45 - VALVE CLEARANCE GV-220 ENGINE; ROCKER ARM COVER INSTALLATION
Section 2.2 VALVE TRAIN VALVE CLEARANCE GV-220 ENGINE INTAKE VALVE: 0.001-0.0022 inch (0.03-0.056mm) EXHAUST VALVE: 0.0018-0.003 inch (0.046-0.07mm) Adjust the valve clearance as follows: 1. Rotate the crankshaft until the piston is at top dead center (TDC) of its compression stroke. Both valves sho...
Page 48 - PISTON RINGS
Section 2.3PISTON, RINGS, CONNECTING ROD Figure 4. Piston Minor Diameter PISTON MINOR DIAMETER GV-220) Design DIAMETER: 2.747-2.748 inch (69.789-69.809mm) Figure 5. Piston Major Diameter PISTON MAJOR DIAMETER GV-220) Design DIAMETER: 2.753-2.754 inch (69.939-69.959mm) NOTE: Always apply engine oil t...
Page 50 - CYLINDER SERVICE; STANDARD CYLINDER BORE DIAMETER
Section 2.3PISTON, RINGS, CONNECTING ROD hammer handle to gently tap the piston down into the cylinder. 4. Check that the connecting rod's large diameter bearing is coat- ed with oil, as well as the crank throw and the connecting rodcap. 5. Guide the large end of the connecting rod onto the cranksha...
Page 52 - CAMSHAFT INSPECTION; Figure 4. Points to Check on Camshaft; CRANKSHAFT INSPECTION; • Inspect timing gear teeth for chipping or cracking. If
Section 2.4CRANKSHAFT AND CAMSHAFT CAMSHAFT INSPECTION Carefully inspect the entire camshaft for wear, nicks,damage. All areas indicated in Figure 4 should bechecked for wear. Figure 4. Points to Check on Camshaft The following should be measured carefully to checkfor wear: MAIN CAMSHAFT BEARING DIA...
Page 53 - COMPRESSION RELEASE LIFT FOR GV-220 ENGINE; INSTALLING THE CRANKSHAFT
Section 2.4 CRANKSHAFT AND CAMSHAFT Figure 6. Bearing Bore in Crankcase Cover COMPRESSION RELEASE MECHANISM A mechanical compression release is provided on thecamshaft. See Figure 7. A PIN extends over the camlobe. This PIN pushes on the tappet, to lift the valveand relieve compression for easier cr...
Page 57 - Figure 1. Sharing a Fuel Supply Tank; EVAPORATION CONTROL SYSTEMS
Section 3.1 INTRODUCTION TO FUEL SYSTEM GENERAL Recreational vehicle generators equipped with agasoline fuel system are usually installed so that theyshare the fuel supply tank with the vehicle engine.When this is done, the generator Installer must nevertee off the vehicle fuel supply line to delive...
Page 58 - Figure 2. Typical Gasoline Fuel System
Section 3.1INTRODUCTION TO FUEL SYSTEM altered. Service technicians working on the RV gener-ator systems must not do anything that might changethe vehicle fuel system design. Figure 2. Typical Gasoline Fuel System Page 3.1-2
Page 61 - FUEL PUMP NOMINAL COIL RESISTANCE
Section 3.3 FUEL FILTER AND FUEL PUMP FUEL FILTER The fuel filter should be removed and replaced every100 hours of operation or once each year, whicheveroccurs first. Figure 1. Fuel Filter (Typical) FUEL PUMP DESCRIPTION:The 12 volts DC electric fuel pump has a zinc platefinish. Flow through the pum...
Page 63 - Figure 2. Carburetor Sectional View
Section 3.4 CARBURETOR GENERAL INFORMATION Proper engine performance depends on the carbure-tion system. The use of clean, fresh gasoline and awell-maintained air cleaner are extremely important toproper operation, as well as engine reliability andpower.Most causes of carburetion problems are relate...
Page 66 - Figure 6. Carburetor Removal
Section 3.4CARBURETOR Page 3.4-4 Figure 6. Carburetor Removal
Page 67 - Figure 1. Choke Solenoid Parts; OPERATION; Figure 2. Choke Adjustment
Section 3.5 AUTOMATIC CHOKE GENERAL The GV-220 vertical shaft engines are equipped withan automatic choke. A choke solenoid is attached tothe carburetor choke shaft by means of a choke con-trol link. Solenoid operation is controlled by the A6060circuit board. The circuit board energizes and de-energ...
Page 70 - TESTING THE STEPPER MOTOR
Section 3.6SPEED CONTROL SYSTEM ELECTRICAL CONNECTIONS BROKEN:If one or more of the electrical connections to thestepper motor are broken or disconnected, either ofthe following might occur: 1. The stepper motor may not turn at all. 2. The stepper motor may turn erratically. If the stepper motor doe...
Page 75 - Figure 2. Gas Carburetion Diagram; LEAKAGE TESTING
Section 4.1 INTRODUCTION TO FUEL SYSTEM GASEOUS CARBURETION Gas at positive pressure is delivered from the fuellockoff solenoid to the inlet of the regulator (about 11-14 inches of water).As the engine piston moves downward on its intakestroke, air is drawn into the area above the pistonthrough the ...
Page 77 - LP Gas Regulator; ADJUSTMENTS; Figure 2. LP Gas Regulator; TESTING THE FUEL LOCKOFF SOLENOID
Section 4.2 SHUTOFF VALVE AND REGULATOR GENERAL See Figure 1. The fuel shutoff valve (lockoff solenoid)and the secondary regulator are retained to a flatmounting bracket which, in turn, mounts to the gener-ator base cover. The fuel lockoff solenoid is retainedto the mounting bracket by means of a u-...
Page 78 - Figure 3. Fuel Lockoff Solenoid
Section 4.2SHUTOFF VALVE AND REGULATOR TEST PROCEDURE: 1. Set a volt-ohm-milliammeter (VOM) to read battery voltage (12 VDC). 2. Connect the VOM test leads across Wire 14 (Red) at the sole- noid and a clean frame ground. 3. Set the fuel primer switch onthe generator panel to its ON position. a. The ...
Page 83 - PUMP TIP CLEARANCE
Section 5.1 ENGINE OIL SYSTEM INTRODUCTION TO OIL SYSTEM The engine oil system serves to (a) reduce frictionbetween parts, (b) cool the engine, and (c) establish aslightly negative pressure in the crankcase to preventoil leakage. Major components that will be discussedin this section include the fol...
Page 84 - Figure 3. Oil Pump Check Points; CRANKSHAFT OIL SEALS; Figure 4. Crankshaft Oil Seals; PRESSURE RELIEF VALVE; Figure 5. Oil Pressure Relief Valve; FORCE REQUIRED TO COMPRESS; BREATHER ASSEMBLY
Section 5.1ENGINE OIL SYSTEM OIL PUMP (CONTINUED) INSPECTION (CONT'D):Inspect the outer drive pins on the camshaft. Look forbreakage, bending, other damage. These are roll pinswhich can be removed and replaced. Figure 3. Oil Pump Check Points CRANKSHAFT OIL SEALS An oil seal is provided in the crank...
Page 85 - ENGINE OIL SYSTEM; Figure 6. Breather Assembly; OIL SUMP; CRANKSHAFT BEARING BORE DIAMETER; OIL FILTER SUPPORT; Figure 7. Oil Filter Support
Section 5.1 ENGINE OIL SYSTEM The breather serves to maintain a partial vacuum inthe engine crankcase, to prevent oil from being forcedpast oil seals, gaskets or rings.See Figure 6. A reed type breather valve permitsexcess pressure to be vented out of the crankcasea n d t o a t m o s p h e r e t h r...
Page 87 - Figure 1 — Air Flow Through Engine-Generator; COOLING AIR INLET OPENINGS; Figure 2 — Air Inlet in Compartment Door; • By providing an opening in the vehicle skirt and space
Section 5.2 ENGINE COOLING SYSTEM It is absolutely essential that an adequate flow of airfor cooling, ventilating and engine combustion be sup-plied to the generator set. Without sufficient air flow,the engine-generator quickly overheats. Such over-heating can cause serious operating difficulties an...
Page 88 - COMPENSATING FOR RESTRICTIONS
Section 5.2ENGINE COOLING SYSTEM Figure 3 — Suspended Mount Inlet Door Figure 4. Ductwork Figure 5 — Air Inlet in Vehicle Skirt COMPENSATING FOR RESTRICTIONS Such materials as screening, louvers, or expandedmetal can restrict the free flow of air. Compensate forthis restriction by making the actual ...
Page 91 - Engine cranking system components
Section 6.1 ENGINE DC CONTROL SYSTEM GENERAL The engine DC control system consists of all thoseelectrical components required for cranking, startingand running the engine. These components includethe following: 1. Engine cranking system components a. A 12 VDC battery. b. A Start-Run-Stop Switch (SW1...
Page 92 - HOW IT WORKS
Section 6.1ENGINE DC CONTROL SYSTEM HOW IT WORKS ENGINE NOT RUNNING: 1. Battery output (12VDC) is available to the contacts of a starter contactor (SC). However, the contacts are open. 2. Battery output is delivered to Terminals J2 - 5 of the A6060 cir- cuit board, via Wire 13, a 15 amp fuse, and Wi...
Page 93 - Figure 2. Receptacle J2; PIN; — Not
Section 6.2 A6060 CIRCUIT BOARD GENERAL The A6060 circuit board controls all phases of engineoperation including cranking, starting, running andshutdown.The circuit board interconnects with other compo-nents of the engine electrical system.The board Is powered by fused 12 VDC battery out-put, availa...
Page 94 - CIRCUIT BOARD CONNECTIONS
Section 6.2A6060 CIRCUIT BOARD CIRCUIT BOARD CONNECTIONS (CONTINUED) RECEPTACLE J4:The A6060 circuit board mounts a 3-pin receptacleJ4. A 3-pin connector plug connects to the A6060.This harness then connects to Bridge Rectifier. DCLink Voltage is supplied to the circuit board for volt-age sensing. R...
Page 95 - CABLE LENGTH
Section 6.3 ENGINE CRANKING SYSTEM INTRODUCTION COMPONENTS:The engine cranking system is shown schematicallyin Figure 1, below. The system consists of the follow-ing components:• A 12 volts Battery.• A Start-Run-Stop Switch (SW1).• A Starter Contactor (SC).• A Starter Motor (SM1). • A6060 Circuit Bo...
Page 96 - STARTER CONTACTOR
Section 6.3ENGINE CRANKING SYSTEM BATTERY (CONTINUED) TESTING A BATTERY:The best method of testing a battery is with an auto-motive type battery hydrometer. Some "MaintenanceFree" batteries cannot be tested with a hydrometer.Most batteries can be tested for both STATE OFCHARGE and CONDITION ...
Page 97 - ENGINE CRANKING SYSTEM; Figure 3. Starter Contactor; STARTER MOTOR; Figure 4. Starter Motor
Section 6.3 ENGINE CRANKING SYSTEM Figure 3. Starter Contactor STARTER MOTOR DESCRIPTION:The Starter Motor is a 12 volts negative ground type.It is capable of operating on heavy duty battery inputat temperatures as low as -30 F. without any signifi-cant change in performance. Its pinion is a 10-toot...
Page 99 - Figure 1. Ignition Cage Assembly; IGNITION SENSOR; Figure 2. Ignition Sensor; IGNITION MODULE
Section 6.4 ENGINE IGNITION SYSTEM INTRODUCTION The engine ignition system consists of the followingmajor components:• Ignition Cage Assembly.• Ignition Sensor Assembly.• Ignition Module (IM).• Ignition Coil (IC).• Spark Plug (SP1). IGNITION CAGE ASSEMBLY An IGNITION CAGE ASSEMBLY is factory install...
Page 100 - Figure 4. Ignition Module; IGNITION COIL; Figure 5. Ignition Coil; SPARK PLUG; Figure 6. Setting Spark Plug Gap; SUMMARY OF OPERATION; Figure 7. Ignition System Diagram; IGNITION TIMING; Ignition timing is fixed and non-adjustable.; TESTING THE SYSTEM
Section 6.4ENGINE IGNITION SYSTEM IGNITION MODULE (CONTINUED) Figure 4. Ignition Module IGNITION COIL Primary ignition voltage (12 VDC) is delivered fromthe Ignition Module to the Ignition Coil. The Coilboosts the voltage and delivers the high voltage tothe engine Spark Plug. Figure 5. Ignition Coil...
Page 101 - ENGINE IGNITION SYSTEM
Section 6.4 ENGINE IGNITION SYSTEM TESTING FOR SPARK:To test the ignition system, a suitable spark testermay be used. Such spark testers are commerciallyavailable. Test the system as follows: Warning! Do NOT use a screwdriver to test forspark. Personal injury or damage to equip-ment may result. 1. D...
Page 103 - Figure 1. Engine Protective Circuit
Section 6.5 SHUTDOWN FEATURES GENERAL The engine mounts an Oil Pressure Switch (LOP) andan Oil Temperature Switch (HTO). These two switch-es, in conjunction with the A6060 circuit board, pro-tect the engine against (a) low oil pressure and (b)high oil temperature.The engine protective circuit Is sho...
Page 104 - ADDITIONAL SHUTDOWN FEATURES
Section 6.5SHUTDOWN FEATURES ADDITIONAL SHUTDOWN FEATURES The A6060 Circuit Board also incorporates the follow-ing protective shutdown features: LOSS OF 12-PIN CABLE SIGNALS TO INVERTER:The generator will shutdown if the 12-pin connector isdisconnected from the inverter when CB1 is turned toON.This ...
Page 105 - Figure 1. Remote Panel Plug-In Receptacle
Section 6.6 OPTIONAL REMOTE PANEL GENERAL An optional remote-mounted Start-Stop panel is avail-able. This panel will permit the generator to be startedand stopped from some convenient remote location inthe recreational vehicle. REMOTE PLUG-IN RECEPTACLEA plug-in receptacle (Figure 2.24) is provided ...
Page 107 - SHOOTING; SECTION TITLE
PART 7 TROUBLE- SHOOTING COMPUTER CONTROLLED VARIABLE SPEED RV GENERATORS Series Impact 36 Plus SECTION TITLE 7.1 GENERATOR & SPEED CONTROL 7.2 ENGINE DC CONTROL SYSTEM/ AC TROUBLESHOOTING
Page 113 - ENGINE DC CONTROL SYSTEM / AC TROUBLESHOOTING
Section 7.2 ENGINE DC CONTROL SYSTEM / AC TROUBLESHOOTING Page 7.2-3 PROBLEM 3 - ENGINE CRANKS BUT WILL NOT START (CONTINUED)
Page 114 - PROBLEM 4 - ENGINE STARTS HARD AND RUNS ROUGH
Section 7.2ENGINE DC CONTROL SYSTEM / AC TROUBLESHOOTING Page 7.2-4 PROBLEM 4 - ENGINE STARTS HARD AND RUNS ROUGH
Page 118 - PROBLEM 10 - NO AC OUTPUT
Section 7.2ENGINE DC CONTROL SYSTEM / AC TROUBLESHOOTING Page 7.2-8 12-WIRE 12 12 PROBLEM 10 - NO AC OUTPUT
Page 120 - a. And if priming function does not work, go to; TEST 2- CHECK POWER TO PRIMER SWITCH; Figure 2. Primer Switch; TEST 3- CHECK POWER TO FUEL PUMP; Connect the VOM test leads across the Wire 14A from the
Section 7.2ENGINE DC CONTROL SYSTEM / AC TROUBLESHOOTING TEST 1- CHECK 7.5 AMP FUSE DISCUSSION:The panel-mounted 7.5 amp fuse is connected inseries with the 12 VDC power supply to the engineDC control system. A blown fuse will prevent enginepriming, cranking and running. TEST PROCEDURE:Push in on fu...
Page 126 - TEST 26- TEST OIL PRESSURE SWITCH
Section 7.2ENGINE DC CONTROL SYSTEM / AC TROUBLESHOOTING ENGINE COMPRESSION PRESSURE NOMINAL PRESSURE: 60 psi MINIMUM ALLOWABLE: 55 psi N O T E : F u l l c o m p r e s s i o n p r e s s u r e c a n n o t b eobtained at cranking speeds, due to the action ofa compression release mechanism. RESULTS:If ...
Page 135 - SPECIFICATIONS & CHARTS
Part 8 SPECIFICATIONS & CHARTS Page 8-3 LOP F1 IC SM TC HTO IS GRD IM SC BCR 12VBATTERY CUSTOMER SUPPLIED VIO DC DC AC GENERATOR CONTROL ENGINE GENERATOR SW2 STATOR M REMOTEPANELCONNECTOR CC CH HM - + GRD CUSTOMER AC CONNECTION BR1 BR2 BR3 BR4 PCB1 CB1A CB1B 10A SW1 CHASSIS INVERTER INVERTERCONT...
Page 136 - CRANKSHAFT END PLAY; MODEL
ALLOWABLEEND PLAY 0.006-0.023 inch (0.14-0.60mm) Part 8SPECIFICATIONS & CHARTS Page 8-4 MODEL GV-220 VALVE SEAT WIDTH:DESIGN WIDTH 0.034-0.044 inch (0.87-1.13mm) VALVE SEAT ANGLE 45 degrees VALVE MARGIN:DESIGN MARGIN 0.034-0.044 inch (0.87-1.13mm) INTAKE VALVE STEMDIAMETER:DESIGN DIAMETER 0.274-...
Page 137 - CRANKCASE ASSEMBLY; CRANKCASE COVER ASSEMBLY
Part 8 SPECIFICATIONS & CHARTS Page 8-5 CRANKCASE ASSEMBLY MODEL GV-220 CYLINDER BORE:DESIGN DIAMETER 2.953-2.954 inch (75.000-75.025mm) VALVE TAPPET BORE:DESIGN DIAMETER 0.295-0.296 inch (7.494-7.520mm) CRANKSHAFT SLEEVEBEARING:DESIGN DIAMETER 1.104-1.106 inch *(WHERE APPLICABLE) (28.044-28.099...
Page 138 - CRANKSHAFT; CONNECTING ROD ASSEMBLY; PISTON
Part 8SPECIFICATIONS & CHARTS Page 8-6 CRANKSHAFT MODEL GV-220 CRANKPIN DIAMETER: DESIGN DIAMETER 1.180-1.181 inch (29.99-30.01mm) CRANKSHAFTMAIN BEARING(FLYWHEEL END):DESIGN DIAMETER 1.102-1.103 inch (28.000-28.012mm) CRANKSHAFTMAIN BEARING(PTO END):DESIGN DIAMETER 1.102-1.103 inch (28.000-28.0...
Page 140 - CAMSHAFT ASSEMBLY; OIL PUMP
Part 8SPECIFICATIONS & CHARTS Page 8-8 CAMSHAFT ASSEMBLY MODEL GV-220 MAIN CAMSHAFT BEARING DIAMETER(FLYWHEEL END): DESIGN DIAMETER 1.022-1.023 inch (25.96-25.98mm) MAIN CAMSHAFT BEARING DIAMETER (PTO END): DESIGN DIAMETER 1.297-1.298 inch (32.96-32.98mm) CAM LIFT:DESIGN LIFT 0.210-0.212 inch (5...
Page 141 - COMPRESSION PRESSURE; TORQUE SPECIFICATIONS
Part 8 SPECIFICATIONS & CHARTS Page 8-9 OIL PUMP (CONTINUED) MODEL GV-220 OIL PRESSURE RELIEFVALVE SPRING: Forcerequired to compress 0.85-0.95 pounds spring to 1.035 inch (0.39-0.43kg) (26.3mm) COMPRESSION PRESSURE MODEL GV-220 WHILE CRANKING(COLD ENGINE) 60 psi min. TORQUE SPECIFICATIONS MODEL ...