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Continental IO-470 Series Aircraft Engine Overhaul Manual X30588A - C, D, E, F, G, H, J, K, L, M, N, P, R, S, U, V & VO Models

Continental IO-470 Series Aircraft Engine Overhaul Manual X30588A – C, D, E, F, G, H, J, K, L, M, N, P, R, S, U, V & VO Models

Name: Continental IO-470 Series Aircraft Engine Overhaul Manual X30588A - C, D, E, F, G, H, J, K, L, M, N, P, R, S, U, V &amp; VO Models
SKU: TCM-IO470-X30588A-HD
Availability: InStock

Original price was: $39.95.Current price is: $24.95.

Complete Teledyne Continental Motors overhaul manual for the IO-470 series aircraft engine, covering all seventeen dash-number variants from disassembly and inspection through final assembly and overhaul test run. Form X30588A.

SKU: TCM-IO470-X30588A-HD Category: Aircraft Engine Manuals Tags: Continental IO-470 overhaul manual, IO-470 aircraft engine rebuild manual, IO-470 series engine service manual, Teledyne Continental X30588A PDF Vendor: Parts Catalog Hub

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Description

Continental IO-470 Series Overhaul Manual – Form X30588A

This is the full Teledyne Continental Motors Overhaul Manual for the IO-470 series aircraft engine, published under form number X30588A and prepared in the GAMA (General Aviation Manufacturers Association) format. It is the document a certified airframe and powerplant mechanic works from when an IO-470 comes off the airframe for major overhaul, and it carries the same chapter and subsystem numbering used across the Continental engine line so that cross-referencing the IO-470 Series Parts Catalog X30589A is direct.

The manual covers the naturally aspirated, fuel injected, air cooled six cylinder horizontally opposed IO-470 in all of its dash-number configurations. Every procedure is written against the actual engine – not a generic reciprocating engine text – with the model-specific differences in fuel injection plumbing, induction layout, oil sump, oil cooler and generator or alternator drive called out model by model.

File Details

Manual type: Overhaul Manual (Maintenance and Overhaul Manual)
Brand / manufacturer: Teledyne Continental Motors, Aircraft Products Division
Engine family: IO-470 series, six cylinder horizontally opposed, fuel injected, air cooled
Document number: Form X30588A
Companion publication: IO-470 Series Parts Catalog X30589A
Language: English
Page count: 370 pages
File format: PDF
Technical content: Accepted by the FAA
Revision dates appearing in the document: October 1991 and August 1992

Chapters Covered

1 – Introduction: scope, related publications, service bulletins and service reports, 100% replacement parts, definitions and abbreviations, engine model code, basic design features, special tools, products and application chart of sealants and lubricants
4 – Airworthiness Limitations: mandatory replacement times, mandatory inspection intervals, other related procedures, distribution of changes
5 – Time Limits / Maintenance Checks: general, time limits and inspection program, scheduled maintenance, preflight inspection, 50 hour inspection, 100 hour inspection, unscheduled maintenance
70 – Standard Practices: lockwire procedure, crankcase threading procedure, application of adhesives, installation of gaskets, cylinder leakage check including master orifice assembly tool, static seal and dynamic seal, differential pressure tester, performing the check
72 – Engine Reciprocating: general description of crankcase, crankshaft, connecting rods, camshaft, pistons, lifters, cylinders, gear train, lubrication system, valve mechanism, induction system, exhaust system and ignition system; disassembly; cleaning, repair and replacement; inspection; specific inspections; assembly of subassemblies; final assembly; testing after overhaul; engine preservation
73 – Engine Fuel System: set-up procedure for naturally aspirated and turbocharged engines, fuel pressure regulators, special set-up procedures, fuel system pressure and flow valve charts, fuel system troubleshooting chart
74 – Ignition: TCM ignition system general, magneto installation, harness assembly installation, ignition troubleshooting, Slick ignition system general, magneto installation, harness assembly installation, ignition troubleshooting
75 – Air: induction system components, air throttle assembly, induction manifold, cylinder intake ports
76 – Engine Controls: general, cruise control by performance curve, cruise control by E.G.T., performance charts
77 – Engine Indicating: general, operating limits, engine troubleshooting chart
78 – Exhaust: general
79 – Oil: general, approved products, oil system troubleshooting chart
80 – Starting: prestarting, starting, ground warm-up, pre-takeoff check, flooded engine, cold weather operation, hot weather operation, ground operation at high altitude airports
81 – Turbines

Beyond the chapter list, the working substance of this IO-470 overhaul manual sits in the assembly and inspection sections. The disassembly chapter steps through the ignition system, each of the nine different fuel injection system layouts by engine model, the induction system by model, oil sump, oil cooler, alternator, starter and starter drive adapter, oil pump, cylinders and pistons, crankcase, camshaft and crankshaft. The cleaning and repair chapter then covers cylinders, pistons, valves, rocker shafts, pushrods, camshaft and crankshaft, crankcase, gears, sheet metal and intake manifold, castings, stud replacement, helical coil insert installation, spark plug hole helical coil inserts, fin repairs, valve guides, valve rockers, hydraulic valve lifters, connecting rods, piston pin bushing replacement, crankshaft assembly, idler gear, magneto and accessory drive adapter assembly, tachometer drive housing, starter drive adapter, oil pump assembly and ignition cables. Inspection is split into visual, magnetic particle, ultrasonic, fluorescent particle and dimensional inspection, and is backed by a multi-page table of limits that carries the service limits and new parts limits for gear backlash, cylinder and head assemblies, rocker arms and shafts, pistons, rings and pins, connecting rods, crankshaft, camshaft, crankcase, accessory drive idler assembly, oil pressure pump assembly, oil pressure relief valve assembly, tachometer drive assembly, magneto and accessory drive assembly, starter drive and fuel pump assembly.

The final assembly chapter rebuilds the engine in sequence: crankcase, cylinders and pistons, oil pump, fuel pump, starter drive adapter, alternator or generator, magneto and accessory drive adapters, oil cooler, valve mechanism, oil sump, induction system, fuel injection system, magneto drive gears, placing the crankshaft in timing position, magnetos, ignition harness, fuel lines and hoses and exhaust system. Testing after overhaul sets out the test stand, test club, cooling air scoop, induction air intake, exhaust stacks, controls, electrical wiring, instruments, breather, fuel system and governor pad cover requirements, followed by the standard acceptance test run, oil consumption determination and test flight guidance. The engine preservation chapter closes with flyable storage, temporary storage and indefinite storage procedures.

What This Manual Lets You Do

With this document on the bench, an A&P can tear an IO-470 down to a bare crankcase and build it back up to published fits and limits. That means pulling cylinders and pistons, measuring bore diameter and choke, checking ring gaps and side clearances at the specified 6.34 inch depth, inspecting valve guides and seats, reaming and replacing guides, installing valve seat inserts by the heat-shrink method, checking connecting rod twist and convergence, polishing and inspecting crankshaft journals, checking counterweight bushing diameter across three points, and confirming gear backlash at each mesh point in the train. It also means timing both magnetos to the engine with the correct full advance firing angle for the specific dash number, since the ignition timing table in this manual varies from 20 degrees to 26 degrees BTC depending on model.

The model-specific detail is what makes an overhaul manual worth having. The IO-470-J and K use a straight valve cylinder and a 7:1 compression ratio, run on a lower minimum fuel grade than the rest of the family, and have their own cylinder assembly dimensions, their own reamer series and their own induction layout. The IO-470-C and H share one induction configuration. The D, E, G, L, P, R, U, V and VO share another. The F, J, K, M and S each have their own. The IO-470-P carries a crankshaft extension and housing that no other model uses. The fuel injection chapter alone breaks out separate disassembly sequences for C and H, D and U, E, G, P and R, F, K and N, L, M, S, and V and VO. Getting any of this wrong means parts that do not fit or an engine that does not run right.

Torque values are given in a single consolidated table – crankcase flange, cylinder base stud nuts, through bolts, connecting rod nuts, crankshaft gear screws, camshaft gear bolts, oil pump cover, rocker shaft hold-down bolts, intake flange screws, fuel injection line nuts, spark plug torque and pipe plug torque – with the caution that connecting rod nuts must be torqued to the low limit first and only increased gradually if the cotter pin will not enter.

Why Correct Procedures and Specifications Matter Here

An aircraft engine is not a place to work from memory. The cylinder leakage check section explains the difference between the static seal – valve to seat, spark plug to port, cylinder head to barrel – where no leakage at all is permissible, and the dynamic seal at the piston rings, where leakage varies with cylinder displacement, choke, ring end gap and piston design. It also explains how to calibrate the differential pressure tester against the master orifice tool at 80 psi before trusting any reading, because an uncalibrated gauge produces a false picture of cylinder health. That kind of procedural detail is exactly what separates a serviceable overhaul from one that fails in the field.

Complete PDF Bookmark Tree

Complete Bookmarks

The complete bookmarks in the “Continental IO-470 Series Aircraft Engine Overhaul Manual X30588A – C, D, E, F, G, H, J, K, L, M, N, P, R, S, U, V & VO Models” are as follows:

X30588 – OVERHAUL MANUAL – MODELS IO-470-C, D, E, F, G, H, J, K, L, M, N, P, R, S, U, V, VOp. 1

SUPERSEDURE NOTICEp. 2

EFFECTIVE CHANGES FOR THIS MANUALp. 2

LIST OF EFFECTIVE PAGESp. 2

WARNINGp. 3

NOTICEp. 4

INTRODUCTIONp. 5

LIST OF ILLUSTRATIONSp. 6

1-10-04 – THREE QUARTER RIGHT FRONT VIEW OF THE IO-470 SANDCAST SERIES ENGINEp. 22

1-10-04 – INSTALLATION DRAWING IO-470 SERIES ENGINEp. 23

1-20-01 (1) – STRAP WRENCHp. 28

1-20-01 (2) – OIL FILTER CAN CUTTERp. 28

1-20-01 (3) – CYLINDER BASE NUT WRENCHESp. 29

1-20-01 (4) – CYLINDER BASE NUT WRENCHES FOR BONANZA AIRCRAFTp. 29

1-20-01 (5) – CYLINDER BASE NUT, WRENCHp. 29

1-20-01 (5A) – SPARK PLUG WRENCHp. 29

1-20-01 (6) – CYLINDER BASE NUT WRENCHES FOR 0470 AND 520p. 30

1-20-01 (7) – CYLINDER BASE NUT WRENCHES FOR GTSIO 520 F & Kp. 30

1-20-01 (8) – CYLINDER BASE NUT WRENCH FOR CONTINENTAL 550 ENGINEp. 30

1-20-01 (9) – GENERATOR BASE NUT WRENCHESp. 30

1-20-01 (10) – PISTON PIN REMOVERS 8121 SERIESp. 31

1-20-01 (11) – CYLINDER HONEp. 31

1-20-01 (12) – CRANKSHAFT BLADE AND DAMPER BUSING REMOVERS/REPLACERSp. 31

1-20-01 (13) – HOLDING FIXTURE ADAPTERSp. 32

1-20-01 (14) – UNIVERSAL CYLINDER HOLDING FIXTUREp. 32

1-20-01 (15) – VALVE GUIDE CLEANER 122p. 33

1-20-01 (16) – SEAL SEAT CUTTERp. 33

1-20-01 (17) – SPRING CHECKERp. 33

1-20-01 (18) – VALVE GUIDE REMOVERSp. 33

1-20-01 (19) – VALVE GUIDE REPLACERSp. 34

1-20-01 (20) – ROCKER ARM BUSHING REMOVER/INSTALLER SETp. 34

1-20-01 (21) – PISTON RING COMPRESSORSp. 34

1-20-01 (22) – PISTON RING COMPRESSORSp. 34

1-20-01 (23) – FLOATING HOLDERp. 35

1-20-01 (24) – VALVE SPRING COMPRESSORp. 35

1-20-01 (25) – PUSH ROD SPRING COMPRESSORp. 35

1-20-01 (26) – FLARING TOOL FOR PUSH ROD HOUSINGp. 35

1-20-01 (27) – VALVE GUIDE REMOVERp. 35

1-20-01 (28) – VALVE SEAT INSERT REMOVER AND REPLACERp. 36

1-20-01 (29) – VALVE SEAT INSERT REMOVER AND REPLACERp. 36

1-20-01 (30) – INSTALLER VALVE SEAT INSERTSp. 36

1-20-01 (31) – VALVE GUIDE TO VALVE SEAT ALIGNMENT SYSTEMp. 37

1-20-01 (32) – VALVE GUIDE TO VALVE SEAT ALIGNMENT SYSTEMp. 37

1-20-01 (33) – COMMON PARTS KITp. 37

1-20-01 (34) – VALVE STEM HOLE REAMERSp. 38

1-20-01 (35) – BORING BARSp. 38

1-20-01 (36) – BORING BARSp. 38

1-20-01 (37) – EXPANDING GUIDE BODIESp. 38

1-20-01 (38) – VALVE SEAT INSERT CUTTERSp. 39

1-20-01 (39) – ROSAN STUD REMOVERp. 39

1-20-01 (40) – CONNECTING ROD REAMING AND ALIGNMENT CHECKING FIXTUREp. 40

1-20-01 (41) – ADAPTER KITSp. 40

1-20-01 (42) – REAMERS, CONNECTING ROD BUSHINGp. 40

1-20-01 (43) – UNIVERSAL CONNECTING ROD BUSHING REMOVER AND INSTALLER SETp. 41

1-20-01 (44) – COMMON DRIVE HANDLE AND PILOTSp. 41

1-20-01 (45) – NEEDLE BEARING INSTALLERSp. 42

1-20-01 (46) – HYDRAULIC CRANKSHAFT DAMPENER BUSHING REMOVER/REPLACER SETp. 42

1-20-01 (47) – COUNTER WEIGHT BUSHING REMOVER/INSTALLERp. 42

1-20-01 (48) – ALL POSITION ENGINE STANDp. 43

1-20-01 (49) – TORK BAND TENSION ADJUSTERp. 43

1-20-01 (50) – GENERATOR DRIVE HOLDERSp. 43

1-20-01 (51) – CYLINDER HEATING STANDp. 44

1-20-01 (52) – BLIND NEEDLE BEARING PULLERp. 44

1-20-01 (53) – STARTER CLUTCH SHAFT BEARING PULLERSp. 44

1-20-01 (54) – DIFFERENTIAL PRESSURE GAUGEp. 45

1-20-01 (55) – DIFFERENTIAL PRESSURE CYLINDER CHECKERp. 45

1-20-01 (56) – BELT TENSION GAUGEp. 45

1-20-01 (57) – HYDRAULIC VALVE LIFTER TESTERp. 45

1-20-01 (58) – IN AIRCRAFT ALTERNATOR GENERATOR TESTERp. 46

1-20-01 (59) – ENGINE TIMING DISCp. 46

1-20-01 (60) – PULLEY HOLDERp. 46

1-20-01 (61) – PULLEY ALIGNMENT GAGE BARp. 46

1-20-01 (62) – CRANKCASE DRILL FIXTURE FOR STARTER CLUTCH ADAPTERp. 47

1-20-01 (63) – VACUUM PUMPp. 47

1-20-01 (64) – GENERATOR PULLEY PULLERp. 47

1-20-01 (65) – BEARING AND BUSHING DRILL FIXTUREp. 47

1-20-01 (66) – SPARK PLUG INSERT REPLACERp. 48

1-20-01 (67) – THRU-BOLT BORE STEP CUTTERSp. 48

1-20-01 (68) – SPARK PLUG INSERT TAPp. 48

1-20-01 (69) – SPARK PLUG INSERT REMOVERp. 48

1-20-01 (70) – SLIDE HAMMERp. 48

1-20-01 (71) – SPARK PLUG TAPp. 48

1-20-01 (72) – ROSAN LOCK RING INSTALLERp. 49

1-20-01 (73) – STUD DRIVERSp. 49

1-20-01 (74) – SCAVENGE PUMP DRILL FIXTUREp. 49

1-20-01 (75) – CRANKCASE SPLITTER SETp. 49

1-20-01 (76) – PROPELLER SHAFT OIL SEAL INSTALLERp. 50

1-20-01 (77) – OIL PRESSURE RELIEF SPOT FACERSp. 50

1-20-01 (78) – RUNOUT BLOCK SETp. 50

1-20-01 (79) – POLISHING TOOLS FOR CRANKSHAFT BEARINGSp. 50

1-20-01 (80) – INJECTOR NOZZLE REMOVER AND INSTALLERp. 51

1-20-01 (81) – CRANKCASE THRU-BOLT REMOVERSp. 51

1-20-01 (82) – HEX DRIVE FOR HEX TUBE NUTSp. 51

1-20-01 (83) – ROTABROACH CUTTERSp. 51

1-20-01 (84) – PULLERSp. 52

1-20-01 (85) – PULLERSp. 52

1-20-01 (86) – PULLERSp. 52

1-20-01 (87) – PULLERSp. 52

1-20-01 (88) – OUTSIDE MICROMETERSp. 53

1-20-01 (89) – DIAL BORE GAGESp. 53

1-20-01 (90) – BLADE MICROMETERSp. 54

1-20-01 (91) – SCREW THREAD MICROMETERp. 54

1-20-01 (92) – DEPTH MICROMETERSp. 54

1-20-01 (93) – REAMERS, ROCKER SHAFT SUPPORT BOSSp. 55

1-20-01 (94) – REAMERS, VALVE GUIDE BOSSp. 55

1-20-01 (95) – VALVE GUIDE STEM HOLE REAMERSp. 56

1-20-01 (96) – ADAPTER, SQUARE SHANK REAMERSp. 56

1-20-01 (97) – PLUG GAUGES VALVE STEM HOLEp. 56

1-20-01 (98) – DIAL THICKNESS GAGEp. 57

1-20-01 (99) – PRECISION VERNIER CALIPERSp. 57

1-20-01 (100) – INSIDE MEASURING INSTRUMENTSp. 57

1-20-01 (101) – OUTSIDE MICROMETERSp. 57

1-20-01 (102) – ALTERNATOR ANALYZERp. 58

1-20-01 (103) – ALTERNATOR/REGULATOR/BATTERY TESTERp. 58

1-20-01 (104) – MULTIPLE VOLTAGE & CIRCUIT TESTERp. 58

1-20-01 (105) – DIFFERENTIAL CYLINDER PRESSURE TESTERp. 59

1-20-01 (106) – AIRCRAFT TIMING INDICATORp. 59

1-20-01 (107) – AIRCRAFT MAGNETO TIMING LIGHTp. 59

1-20-01 (108) – COLD CYLINDER TESTERp. 60

1-20-01 (109) – HI-VOLTAGE CABLE TESTERp. 60

1-20-01 (110) – MASTER ORIFICE TOOLp. 60

1-20-01 (111) – ALCOR PORTABLE DIGITAL EGT UNITp. 61

1-20-01 (112) – ALCOR PORTABLE DIGITAL CHT UNITp. 61

70-10-00 – LOCKWIRE PROCEDUREp. 93

70-20-00 – PERMATEX AND THREADING PROCEDUREp. 94

70-50-01 – MASTER ORIFICE ASSEMBLY TOOLp. 96

70-50-02 – CYLINDER STATIC SEAL & DYNAMIC SEALp. 96

70-50-03 – DIFFERENTIAL PRESSURE TESTERp. 98

70-50-04 – DYNAMIC SEAL CHECKp. 100

72-00-03 – CRANKSHAFT NUMBERINGp. 112

72-00-09 – GEAR TRAIN DIAGRAMp. 115

72-00-10 – LUBRICATION SYSTEMp. 117

72-00-11 – HYDRAULIC LIFTERp. 118

72-10-05 – EXPLODED VIEW OF IGNITION SYSTEMp. 125

72-10-06A – FUEL INJECTION SYSTEM IO-470-C, H & Jp. 127

72-10-06B – FUEL INJECTION SYSTEM IO-470-D & Up. 129

72-10-06C – FUEL INJECTION SYSTEM IO-470,E,G, P & Rp. 131

72-10-06D – FUEL INJECTION SYSTEM IO-470-Fp. 133

72-10-06E – FUEL INJECTION SYSTEM IO-470-K& Np. 135

72-10-06F – FUEL INJECTION SYSTEM IO-470-Lp. 137

72-10-06G – FUEL INJECTION SYSTEM IO-470-Mp. 139

72-10-06H – FUEL INJECTION SYSTEM IO-470-Sp. 141

72-10-06I – FUEL INJECTION SYSTEM IO-470-V & VOp. 143

72-10-07A – INDUCTION SYSTEM IO-470-C & Hp. 144

72-10-07B – INDUCTION SYSTEM IO-470-D,E,G,L,P,R,U, V & VOp. 145

72-10-07C – INDUCTION SYSTEM IO-470-Fp. 146

72-10-07D – INDUCTION SYSTEM IO-470-Jp. 147

72-10-07E – INDUCTION SYSTEM IO-470-K & Np. 148

72-10-07F – INDUCTION SYSTEM IO-470-Mp. 149

72-10-07G – INDUCTION SYSTEM IO-470-Sp. 150

72-10-08 – MAGNETO & ACCESSORY DRIVESp. 151

72-10-09A – OIL SUMP IO-470,C,H,J, & Np. 152

72-10-09B – OIL SUMP IO-470,D,E,F,G,L,M,P,R,S, U & Vp. 153

72-10-10A – OIL COOLER IO-470-Fp. 154

72-10-10B – OIL COOLER IO-470,C,E,G,H,J,K,N, R & Sp. 155

72-10-10C – OIL COOLER IO-470,D,L,M,N, U & Vp. 156

72-10-11A – GENERATOR IO-470,C,D,E,F,G,H,J,K,L,N,P, R & Sp. 157

72-10-11B – GENERATOR IO-470-Mp. 158

72-10-11C – GENERATOR IO-470-U & Vp. 159

72-10-11 – ALTERNATOR, ALL MODELSp. 160

72-10-12 – STARTER AND STARTER DRIVE ADAPTERp. 163

72-10-13A – OIL PUMP ASSEMBLYp. 165

72-10-13B – OIL PUMP COVER AND TACHOMETER DRIVEp. 166

72-10-14A – CYLINDER AND PISTON ASSEMBLY (ALL EXCEPT IO-470-J & K)p. 169

72-10-14B – CYLINDER AND PISTON ASSEMBLY IO-470-J & Kp. 170

72-10-15A – CRANKCASE ASSEMBLYp. 173

72-10-15B – LEFT C/C & SHAFTS SUPPORTED FOR DISMANTLING OR FINAL ASSEMBLYp. 174

72-10-15C – C/C & CIS EXTENSION (IO-470-P)p. 175

72-10-16 – CAMSHAFT ASSEMBLYp. 176

72-10-17 – CRANKSHAFT GROUPp. 177

72-20-12A – CRANKCASE STUD SETTING HEIGHTSp. 185

72-20-12B – STANDARD & OVERSIZED STUD IDENTIFICATIONp. 185

72-20-13A – HELICOIL & SPECIAL TOOL DATAp. 187

72-20-13B – INSTALLING TYPICAL HELICAL INSERTp. 188

72-20-14A – INSTALLING SPARK PLUG HOLE HELICAL INSERTp. 188

72-20-14B – EXPANDING SPARK PLUG HOLE HELICAL INSERTp. 188

72-20-14C – REMOVING SPARK PLUG HOLE HELICAL INSERTp. 188

72-20-15A – CYLINDER ASSEMBLY DIMENSIONS (INCLINED VALVE)p. 189

72-20-15B – CYLINDER ASSEMBLY DIMENSIONS (STRAIGHT VALVE)p. 190

72-20-17 – VALVE, ROCKER BUSHING DIMENSIONSp. 188

72-20-18 – HYDRAULIC LIFTERp. 192

72-20-20 – CONNECTING ROD AND BUSHING DIMENSIONSp. 193

72-20-27 – IGNITION WIRING DIAGRAMp. 196

72-30-04 – CRANKSHAFT ULTRASONIC INSPECTION PROCEDUREp. 204

72-40-03 – COUNTERWEIGHT BUSHING DIAMETER CHECKp. 228

72-40-07A – INSPECTION RING SIDE CLEARANCEp. 229

72-40-07B – MEASURING RING GAP IN CYLINDERp. 229

72-40-08 – PISTON TO CYLINDER DOME CLEARANCEp. 230

72-40-13A – SPARK PLUGSp. 232

72-40-13B – REVERSE SPARK PLUG PROCEDUREp. 232

72-50-04 – VALVE SPRING INSTALLATIONp. 247

72-50-10A – FUEL MANIFOLD VALVE FITTING ORIENTATIONp. 252

72-50-10B – FUEL CONTROL VALVE FITTING ORIENTATIONp. 253

72-50-10C – FUEL PUMP FITTING LOCATIONS FOR ALL (EXCEPT IO-470-V, VO)p. 254

72-50-10E – FUEL PUMP FITTING LOCATIONS FOR IO-470-V & VOp. 255

72-60-02 – IDLER GEAR, SUPPORT PIN AND TIMING MARKSp. 260

72-60-02 – TORQUING SEQUENCEp. 261

72-60-02 – LEFT SIDE OF COMPLETE CRANKCASE ON STANDp. 262

72-60-03 – INSTALLING NO. 5 CYLINDERp. 263

72-60-03 – TIGHTENING CYLINDER BASE NUTp. 263

72-60-03 – CYLINDER FLANGE TORQUE SEQUENCE FOR SINGLE CYLINDER INSTALLATIONp. 264

72-60-04 – OIL PUMP, FUEL PUMP AND STARTER ADAPTER INSTALLEDp. 264

72-60-10 – INSTALLING PUSHROD HOUSINGp. 268

72-60-11 – BOTTOM VIEW WITH VALVE MECHANISM AND OIL SUMP SUCTION TUBEp. 268

72-60-14 – POSITION OF MAGNETO COUPLINGSp. 272

72-60-17 – IGNITION WIRING DIAGRAMp. 275

72-70-05 – EXHAUST FLANGE DIMENSIONSp. 280

73-00-00 – FUEL SYSTEM SCHEMATICp. 297

74-00-04 – COATING INSULATING SLEEVEp. 305

74-00-04 – INSTALLATION OF ELBOW CLAMPp. 305

LIST OF CHARTSp. 10

1-10-04 – ENGINE DIMENSIONSp. 10

1-20-01 – SPECIAL TOOLS PROCUREMENT SOURCESp. 26

1-20-01 – IDENTIFICATION CODE FOR TOOLSp. 27

1-20-01 – SPECIAL TOOL INDEXp. 63

1-30-00 – APPLICATION CHART SEALANTS/LUBRICANTSp. 77

70-50-05 – CYLINDER LEAKAGE CHECKp. 101

72-20-12A – CRANKCASE STUD SETTING HEIGHTSp. 185

72-20-12B – STANDARD AND OVERSIZE STUD LDENTIFICATIONp. 185

72-30-03 – MAGNETIC PARTICLE INSPECTIONp. 201

72-30-08 – TABLE OF LIMITS CHART (1)p. 207

72-30-08 – TABLE OF LIMITS CHART (2)p. 208

72-30-08 – TABLE OF LIMITS CHART (3)p. 212

72-30-08 – TABLE OF LIMITS CHART (4)p. 215

72-30-08 – TABLE OF LIMITS CHART (5)p. 218

72-30-09 – CRITICAL NEW PART DIMENSIONSp. 221

72-40-15 – INSPECTION CHARTp. 233

72-50-01 – GENERAL USE – TIGHTENING TORQUESp. 243

72-50-01 – TABLE OF TIGHTENING TORQUESp. 244

72-50-01 – PIPE PLUGSp. 244

72-50-10A – FUEL MANIFOLD VALVE FITTING LOCATIONSp. 252

72-50-10B – FUEL CONTROL VALVE FITTING LOCATIONSp. 253

72-50-10C – FUEL PUMP FITTING LOCATIONS FOR ALL IO-470 (EXCEPT IO-470-V & VO)p. 254

72-50-10D – FUEL PUMP FITTING LOCATIONS FOR (IO-470-V & VO)p. 255

72-60-02 – CRANKCASE ASSEMBLY PROCEDUREp. 10

72-60-15 – MAGNETO-TO-ENGINE TIMINGp. 10

72-70-14 – STANDARD ACCEPTANCE TESTp. 282

72-70-14 – OIL CONSUMPTION DETERMINATIONp. 283

72-70-14 – TEST OPERATING LIMITSp. 284

73-10-06 – FUEL INJECTION SYSTEM TROUBLESHOOTING CHARTp. 300

74-00-04 – COUPLING NUT TORQUE VALUES (TCM)p. 306

74-20-00 – IGNITION TROUBLESHOOTING (TCM)p. 307

74-30-04 – COUPLING NUT TORQUE VALUES (SLICK)p. 310

74-50-00 – IGNITION TROUBLESHOOTING (SLICK)p. 311

76-30-00 – PERFORMANCE CHARTSp. 320

77-10-00 – OPERATING LIMITSp. 344

77-20-00 – ENGINE TROUBLE SHOOTINGp. 346

79-10-00 – APPROVED OIL PRODUCTSp. 357

79-20-00 – LUBRICATION SYSTEM TROUBLESHOOTINGp. 358

CHAPTER 1 – INTRODUCTIONp. 11

1-00-00 – SCOPEp. 13

1-00-01 – RELATED PUBLICATIONSp. 13

1-00-02 – SERVICE BULLETINSp. 14

1-00-03 – SERVICE REPORTS AND INQUIRIESp. 14

1-00-04 – 100% REPLACEMENT PARTSp. 14

1-10-00 – DEFINITIONS & ABBREVIATIONSp. 15

1-10-01 – ABBREVIATION/SYMBOLSp. 15

1-10-02 – DEFINITIONSp. 17

1-10-03 – DESCRIPTION OF ENGINE MODEL CODEp. 21

1-10-04 – BASIC DESIGN FEATURESp. 21

1-20-00 – TOOLSp. 25

1-20-01 – SPECIAL TOOLSp. 25

1-30-00 – PRODUCTSp. 76

1-30-01 – PRODUCT LISTp. 11

CHAPTER 4 – AIRWORTHINESS LIMITATIONSp. 81

CHAPTER 5 – TIME LIMITS/MAINTENANCE CHECKSp. 85

5-00-00 – GENERALp. 87

5-10-00 – TIME LIMITS/INSPECTION PROGRAMp. 87

5-20-00 – SCHEDULED MAINTENANCEp. 87

5-20-01 – PREFLIGHT INSPECTIONp. 87

5-20-02 – 50 HOUR INSPECTIONp. 87

5-20-03 – 100 HOUR INSPECTIONp. 88

5-30-00 – UNSCHEDULED MAINTENANCEp. 90

CHAPTER 70 – STANDARD PRACTICESp. 91

70-00-00 – GENERALp. 92

70-10-00 – LOCKWIRE PROCEDUREp. 93

70-20-00 – CRANKCASE THREADING PROCEDUREp. 94

70-30-00 – APPLICATION OF ADHESIVESp. 95

70-40-00 – INSTALLATION OF GASKETSp. 95

70-50-00 – CYLINDER LEAKAGE CHECKp. 95

70-50-01 – LEAKAGE CHECKSp. 97

70-50-02 – EQUIPMENTp. 97

70-50-03 – PERFORMING THE CHECKp. 98

CHAPTER 72 – ENGINE RECIPROCATINGp. 103

72-00-00 – GENERALp. 106

72-00-01 – INTRODUCTIONp. 111

72-00-02 – CRANKCASEp. 111

72-00-03 – CRANKSHAFTp. 111

72-00-04 – CONNECTING RODSp. 112

72-00-05 – CAMSHAFTp. 113

72-00-06 – PISTONSp. 113

72-00-07 – LIFTERSp. 113

72-00-08 – CYLINDERSp. 113

72-00-09 – GEAR TRAINp. 113

72-00-10 – LUBRICATION SYSTEMp. 116

72-00-11 – VALVE MECHANISMp. 118

72-00-12 – INDUCTION SYSTEMp. 118

72-00-13 – EXHAUST SYSTEMp. 119

72-00-14 – IGNITION SYSTEMp. 119

72-10-00 – DISASSEMBLYp. 121

72-10-01 – GENERALp. 123

72-10-02 – EXTENT OF DISASSEMBLYp. 124

72-10-03 – PARTS TO BE DISCARDEDp. 124

72-10-04 – PRELIMINARY CLEANINGp. 124

72-10-05 – IGNITION SYSTEMp. 124

72-10-06 – FUEL INJECTION SYSTEMp. 126

72-10-07 – MAGNETO AND ACCESSORY DRIVESp. 151

72-10-08 – INDUCTION SYSTEMp. 144

72-10-09 – OIL SUMPp. 152

72-10-10 – OIL COOLERp. 154

72-10-11 – ALTERNATOR ASSEMBLYp. 160

72-10-12 – STARTER AND STARTER DRIVE ADAPTERp. 162

72-10-13 – OIL PUMP ASSEMBLYp. 164

72-10-14 – CYLINDERS AND PISTONSp. 167

72-10-15 – CRANKCASEp. 172

72-10-16 – CAMSHAFT ASSEMBLYp. 176

72-10-17 – CRANKSHAFT GROUPp. 176

72-10-18 – EXHAUST SYSTEMp. 178

72-10-19 – OPTIONAL ACCESSORIESp. 103

72-20-00 – CLEANING, REPAIR AND REPLACEMENTp. 179

72-20-01 – GENERALp. 181

72-20-02 – CYLINDERSp. 181

72-20-03 – PISTONSp. 181

72-20-04 – VALVESp. 182

72-20-05 – ROCKER SHAFTSp. 182

72-20-06 – PUSHRODS, VALVE ROCKERS AND OTHER SMALL STEEL PARTSp. 182

72-20-07 – CAMSHAFT AND CRANKSHAFTp. 182

72-20-08 – CRANKCASEp. 182

72-20-09 – GEARSp. 182

72-20-10 – SHEET METAL PARTS AND INTAKE MANIFOLDp. 182

72-20-11 – CASTINGSp. 182

72-20-12 – STUD REPLACEMENTp. 183

72-20-13 – HELICAL COIL INSERT INSTALLATIONp. 186

72-20-14 – SPARK PLUG HOLE HELICAL COIL INSERTSp. 191

72-20-15 – FIN REPAIRSp. 191

72-20-16 – VALVE GUIDESp. 191

72-20-17 – VALVE ROCKERSp. 192

72-20-18 – HYDRAULIC VALVE LIFTERSp. 192

72-20-19 – CONNECTING RODSp. 193

72-20-20 – PISTON PIN BUSHING REPLACEMENTp. 193

72-20-21 – CRANKSHAFT ASSEMBLYp. 193

72-20-22 – IDLER GEARp. 194

72-20-23 – MAGNETO AND ACCESSORY DRIVE ADAPTER ASSEMBLYp. 194

72-20-24 – TACHOMETER DRIVE HOUSINGp. 194

72-20-25 – STARTER DRIVE ADAPTERp. 195

72-20-26 – OIL PUMP ASSEMBLYp. 195

72-20-27 – IGNITION CABLESp. 195

72-30-00 – INSPECTIONp. 197

72-30-01 – GENERALp. 199

72-30-02 – VISUAL INSPECTIONp. 200

72-30-03 – MAGNETIC PARTICLE INSPECTIONp. 200

72-30-04 – ULTRASONIC INSPECTIONp. 202

72-30-05 – FLOURESCENT PARTICLE INSPECTIONp. 205

72-30-06 – DIMENSIONAL INSPECTIONp. 205

72-30-07 – DIMENSIONAL LIMITSp. 205

72-30-08 – TABLE OF LIMITSp. 207

72-30-09 – ORIGINAL DIMENSIONp. 221

72-30-10 – PROTECTIVE COATINGp. 224

72-30-11 – APPLICATION OF ANODIZINGp. 224

72-30-12 – REPAIR OF ANODIZED SURFACESp. 224

72-30-13 – ENAMEL COATINGSp. 224

72-40-00 – SPECIFIC INSPECTIONSp. 225

72-40-01 – CRANKCASEp. 227

72-40-02 – CRANKSHAFTp. 227

72-40-03 – CRANKSHAFT AND COUNTERWEIGHT PINS AND BUSHINGSp. 227

72-40-04 – CAMSHAFTp. 228

72-40-05 – CONNECTING RODSp. 228

72-40-06 – GEARSp. 228

72-40-07 – PISTONS AND RINGSp. 228

72-40-08 – CYLINDERSp. 230

72-40-09 – HYDRAULIC VALVE LIFTERSp. 231

72-40-10 – INTAKE TUBESp. 231

72-40-11 – LUBRICATION SYSTEMp. 231

72-40-12 – FUEL INJECTION SYSTEMp. 231

72-40-13 – IGNITION SYSTEMp. 231

72-40-14 – EXHAUST SYSTEMp. 232

72-40-15 – INSPECTION CHARTp. 233

72-50-00 – ASSEMBLY OF SUBASSEMBLIESp. 241

72-50-01 – GENERALp. 243

72-50-02 – OIL PUMP ASSEMBLYp. 245

72-50-03 – STARTER AND DRIVE ASSEMBLYp. 245

72-50-04 – CYLINDER ASSEMBLYp. 246

72-50-05 – PISTON AND RING ASSEMBLIESp. 247

72-50-06 – PUSHROD HOUSINGp. 247

72-50-07 – CRANKSHAFT AND CONNECTING RODSp. 247

72-50-08 – CAMSHAFTp. 248

72-50-09 – CRANKCASEp. 248

72-50-10 – FUEL INJECTION CONTROL AND AIR THROTTLE BODY ASSEMBLYp. 249

72-60-00 – FINAL ASSEMBLYp. 257

72-60-01 – GENERALp. 259

72-60-02 – CRANKCASEp. 259

72-60-03 – CYLINDERS AND PISTONSp. 263

72-60-04 – OIL PUMPp. 264

72-60-05 – FUEL PUMPp. 265

72-60-06 – STARTER DRIVE ADAPTERp. 265

72-60-07 – ALTERNATOR ASSEMBLYp. 265

72-60-08 – MAGNETO AND ACCESSORY DRIVE ADAPTERSp. 265

72-60-09 – OIL COOLERp. 265

72-60-10 – VALVE MECHANISMp. 266

72-60-11 – OIL SUMPp. 266

72-60-12 – INDUCTION SYSTEMp. 269

72-60-13 – FUEL INJECTION SYSTEMp. 270

72-60-14 – MAGNETO DRIVE GEARSp. 272

72-60-15 – PLACING CRANKSHAFT IN TIMING POSITIONp. 273

72-60-16 – MAGNETOSp. 274

72-60-17 – IGNITION HARNESSp. 274

72-60-18 – FUEL LINESp. 276

72-60-19 – EXHAUST SYSTEMp. 276

72-70-00 – TESTING AFTER OVERHAULp. 277

72-70-01 – TEST STANDp. 279

72-70-02 – TEST CLUBp. 279

72-70-03 – COOLING AIR SCOOPp. 279

72-70-04 – INDUCTION AIR INTAKEp. 279

72-70-05 – EXHAUST STACKSp. 279

72-70-06 – CONTROLSp. 279

72-70-07 – ELECTRICAL WIRINGp. 280

72-70-08 – INSTRUMENTSp. 280

72-70-09 – BREATHERp. 280

72-70-10 – FUEL SYSTEMp. 281

72-70-11 – GOVERNOR PAD COVERp. 281

72-70-12 – ENGINE TESTp. 281

72-70-13 – STARTING PROCEDUREp. 281

72-70-14 – OVERHAUL TEST RUNp. 282

72-80-00 – ENGINE PRESERVATIONp. 287

72-80-01 – GENERALp. 289

72-80-02 – FLYABLE STORAGEp. 289

72-80-03 – TEMPORARY STORAGEp. 290

72-80-04 – INDEFINITE STORAGEp. 291

CHAPTER 73 – ENGINE FUEL SYSTEMp. 295

73-00-00 – ENGINE FUEL SYSTEMp. 297

73-10-00 – SET-UP PROCEDUREp. 298

73-10-01 – NATURALLY ASPIRATED ENGINESp. 298

73-10-02 – TURBOCHARGED ENGINESp. 295

73-10-03 – FUEL PRESSURE REGULATORSp. 295

73-10-04 – SPECIAL SET-UP PROCEDURESp. 295

73-10-05 – FUEL SYSTEM PRESSURE AND FLOW VALVE CHARTSp. 295

73-10-06 – FUEL SYSTEM TROUBLESHOOTING CHARTp. 300

CHAPTER 74 – IGNITIONp. 303

(TCM IGNITION SYSTEM)p. 304

74-00-00 – GENERALp. 304

74-00-01 – MAGNETO INSTALLATIONp. 304

74-00-02 – HARNESS ASSEMBLY INSTALLATIONp. 305

74-10-00 – IGNITION TROUBLESHOOTINGp. 307

(SLICK IGNITION SYSTEM)p. 308

74-30-00 – GENERALp. 308

74-30-01 – MAGNETO INSTALLATIONp. 308

74-30-02 – HARNESS ASSEMBLY INSTALLATIONp. 309

74-50-00 – IGNITION TROUBLESHOOTINGp. 311

CHAPTER 75 – AIRp. 313

75-00-00 – GENERALp. 315

CHAPTER 76 – ENGINE CONTROLSp. 317

76-00-00 – GENERALp. 319

76-10-00 – CRUISE CONTROL BY PERFORMANCE CURVEp. 319

76-20-00 – CRUISE CONTROL BY E.G.T.p. 319

76-30-00 – PERFORMANCE CHARTSp. 320

CHAPTER 77 – ENGINE INDICATINGp. 341

77-00-00 – GENERALp. 343

77-10-00 – OPERATING LIMITSp. 344

77-20-00 – ENGINE TROUBLESHOOTING CHARTp. 346

CHAPTER 78 – EXHAUSTp. 353

78-00-00 – GENERALp. 354

CHAPTER 79 – OILp. 355

79-00-00 – GENERALp. 357

79-10-00 – APPROVED PRODUCTSp. 357

79-20-00 – OIL SYSTEM TROUBLESHOOTING CHARTp. 358

CHAPTER 80 – STARTINGp. 359

80-00-00 – GENERALp. 361

80-00-01 – PRESTARTINGp. 361

80-00-02 – STARTINGp. 361

80-00-03 – GROUND WARM-UPp. 362

80-00-04 – PRE-TAKEOFF CHECKp. 362

80-00-05 – FLOODED ENGINEp. 364

80-00-06 – COLD WEATHER OPERATIONp. 364

80-00-07 – PREHEATINGp. 365

80-00-08 – HOT WEATHER OPERATIONp. 366

80-00-09 – GROUND OPERATION AT HIGH ALTITUDE AIRPORTSp. 367

CHAPTER 81 – TURBINESp. 369

81-00-00 – GENERAL (NOT APPLICABLE)p. 370

The same applies to the 100% replacement parts list, the mandatory replacement and inspection intervals in the airworthiness limitations chapter, and the oil change and filter intervals in the time limits chapter. All of it is in here.

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Continental IO-470 Series Aircraft Engine Overhaul Manual X30588A – C, D, E, F, G, H, J, K, L, M, N, P, R, S, U, V & VO Models

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Continental IO-470 Series Overhaul Manual – Form X30588A

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