Description
Diamond DA20-C1 Aircraft Maintenance Manual DA201-C1 Rev 22 is the full ATA Spec 2200-formatted Aircraft Maintenance Manual (AMM) for the Diamond DA20-C1 single-engine, two-seat composite aeroplane. Published by Diamond Aircraft Industries Inc. of London, Ontario, Canada, this Revision 22 edition carries the document number DA201-C1 and is written in AECMA Simplified English so that every inspection step, torque value and adjustment figure reads unambiguously. It is the manual a maintenance shop reaches for when servicing, inspecting, fault-isolating, removing, installing, testing, adjusting or repairing the DA20-C1 airframe and its systems.
File Details
- Manual type: Aircraft Maintenance Manual (AMM), ATA Spec 2200 chapter numbering
- Manufacturer: Diamond Aircraft Industries Inc., London, Ontario, Canada
- Aircraft model: DA20-C1
- Document number: DA201-C1
- Revision: Rev 22, dated 30 May 2014
- Engine covered: Teledyne Continental IO-240-B
- Language: English (AECMA Simplified English)
- File format: PDF
- Pages: 1372
Chapters Covered
- 01-00-00 Introduction – general, revision service, warnings/cautions/notes, manual configuration, page numbering system, figures, record of revisions, list of effective pages, service bulletins, safety, acronyms, manual change request form
- 02-00-00 Organization and Handling of the Manual – applicability, revisions, temporary revisions, service bulletins, service instructions, abbreviations, conversion factors, torque conversion graphs
- 03-00-00 General Description of the Aircraft – description, equipment data with supplier addresses
- 04-00-00 Airworthiness Limitations – paint zones, aircraft life limited components, component life tracking
- 05-00-00 Time Limits and Maintenance Checks – time limits, scheduled maintenance checks, 6000 hour inspection, maintenance practices, flightline checks, unscheduled maintenance checks
- 06-00-00 Dimensions and Areas – dimensions, adjustment values, control surface gaps, weight and static moments of control surfaces
- 07-00-00 Lifting and Shoring – jacking
- 08-00-00 Leveling and Weighing – weighing, leveling
- 09-00-00 Towing and Taxiing – towing procedure, taxiing procedure
- 10-00-00 Parking, Mooring, Storage and Return to Service
- 11-00-00 Placards and Markings – exterior placards and markings, interior placards and markings
- 12-00-00 Servicing – replenishing (fuel, engine oil, brake, tires), scheduled servicing and lubrication schedule, unscheduled servicing and ice/snow removal
- 20-00-00 Standard Practices – Airframe – bolt and nut types, standard torque values, special torque values, torque measurement
- 21-00-00 Heating and Ventilation – cabin heat system, cold air system, equipment cooling, heat control valve and distribution box
- 23-00-00 Communications – speech communication, audio integrating, static discharging and bonding
- 24-00-00 Electrical Power – DC generation, battery system, external power unit (EPU) system, DC electrical load distribution
- 25-00-00 Equipment/Furnishings – flight compartment, emergency, emergency locator transmitter (ELT)
- 26-00-00 Fire Protection
- 27-00-00 Flight Controls – ailerons and tabs, rudder and tab, elevator, elevator trim, flaps
- 28-00-00 Fuel – fuel storage, fuel distribution, fuel indicating
- 31-00-00 Indicating Systems – instrument and control panels, independent instruments, warning systems, Aspen EFD1000, Garmin G500 integrated display system, Traffic Advisory System (TAS) 600
- 32-00-00 Landing Gear – main landing gear, nose landing gear, wheels and brakes
- 33-00-00 Lights – cockpit lighting, exterior lights
- 34-00-00 Navigation – flight environment data, attitude and direction, landing and taxiing aids, dependent position determining
- 37-00-00 Vacuum – vacuum distribution, vacuum indicating
- 51-00-00 Standard Practices – Structures – structural classification, design and wear limits, repair limitations, inspection techniques, approved materials and suppliers, resin handling, bonding of fiber reinforced plastics, curing, control surface balancing
- 52-00-00 Doors – canopy, access panels
- 53-00-00 Fuselage – fuselage shells, firewall, T-panel, floor, forward and aft control bulkheads, center tunnel, spar bridge, seat back, rollbar, ring bulkheads, vertical stabilizer structure
- 55-00-00 Stabilizers – horizontal stabilizer, elevator, lower fin, rudder and tab
- 56-00-00 Windows – repair of the canopy transparency, replacement of the rear window
- 57-00-00 Wings – wing structure, wing attachment bolts, flaps, ailerons
- 61-00-00 Propeller – propeller assembly, Sensenich W69EK7-63, W69EK7-63G and W69EK-63 installation
- 71-00-00 Power Plant – description and operation, engine specifications, cowling, mounts, air intakes, engine drains
- 72-00-00 Engine – Teledyne Continental IO-240-B description
- 73-00-00 Engine Fuel and Control – induction air filter, fuel pressure sensor and indicator, engine fuel system bleeding procedure
- 74-00-00 Ignition – ignition switch test and removal/installation, ignition switch cables, spark plug leads
- 75-00-00 Air Cooling – baffles and winter kit baffles
- 76-00-00 Engine Controls – throttle, mixture and alternate air bowden cables, throttle/mixture and alternate air range of movement tests
- 77-00-00 Engine Indicating – RPM indicator and flexible drive, CHT and EGT thermocouple probes and indicators, Tanis engine preheat system
- 78-00-00 Exhaust – exhaust system, muffler and heat exchanger
- 79-00-00 Oil Systems – engine oil filter, oil cooler, vernatherm valve, oil temperature and pressure sensors, events switch, indicators, air/oil separator and vent
- 80-00-00 Starting – starting vibrator battery test and removal/installation
- 92-00-00 Wiring Diagrams – system wiring diagrams/schematics and avionics wiring diagrams/schematics
Read together, these chapters give a technician a complete working picture of the DA20-C1. The document opens by fixing the rules of the airframe itself – airworthiness limitations, component life tracking, paint zone restrictions, maintenance intervals and the published dimensions and control surface gaps – before moving into the practical systems chapters. Each of those follows a consistent pattern of description and operation, a troubleshooting table of symptom, probable cause and repair, and maintenance practices that spell out access, removal/installation, adjustment, testing, cleaning, repair and the associated torque or clearance values. Structural content is handled separately under the composite practices chapter, which covers the restricted repair areas, the tap test and light test inspection methods, approved resins, glass and carbon cloth, fillers, bonding paste mixtures and the post-cure schedule used on this airframe.
Serial Number Applicability
Several systems and installations in this manual are tied to aircraft serial number, and the text marks those differences inline rather than burying them. The external power receptacle location, for example, is given separately for C0001 through C0148 and C0150, and for C0149 and C0151 onwards, with different relay removal procedures for each. Battery forward electrical schematics are split between C0001 and later production, and between C0648 and up. Placard figure sets distinguish panels up to S/N 0149 from S/N 0150 and subsequent aircraft. Ignition switch procedures are also split between pre-SB DAC1-74-03 Rev 2 and post-SB DAC1-74-03 Rev 2 configurations. Checking the applicability note before starting a task is a normal part of using this manual.
Avionics, Instrument Panels and Optional Equipment
The AMM deliberately documents more than the baseline aircraft, which is why the communications, indicating and navigation chapters run long. Covered installations include the Bendix/King KX 125 and KX 155 NAV COMM, KLX 135/135A GPS COMM, KLN 35A GPS, KT 76A and KI 208/209 indicators, the Bendix/King KMA 24 audio/marker receiver, Garmin GNS430W, GNS530W, GNC 420W, GTN 650 and GTR 225, Garmin GTX 327, GTX 328 and GTX 330 transponders, the GMA 340 and GMA 340H audio panels, SL40 and IC-A200 transceivers, PM 501 and PM 1000 intercoms, the Aspen EFD1000 electronic flight instrument system, the Garmin G500 integrated display system and the optional TAS 600 traffic advisory system. Standard, reversed and G500 instrument panel layouts are illustrated, as are the placard sets that go with each. The wiring diagram chapter at the back ties these together with system schematics and avionics interconnect drawings.
What You Can Do With This Manual
The maintenance schedule in Chapter 05 drives the day-to-day workload: 25, 50, 100, 200, 1000 and 6000 hour checks plus annual inspection, each broken down into zone-by-zone inspection items with the applicable interval marked, followed by the engine ground test, maintenance report, maintenance check flight report and engine ground test record forms. The unscheduled maintenance chapter then covers the situations nobody plans for – hard landing inspection areas, propeller strike, hydraulic lock and engine fire – and tells you what to examine and in what order. Chapter 20 provides the standard and special torque values, including the propeller, engine mount, landing gear and exhaust figures, so fasteners go back on correctly rather than approximately.
Beyond the schedule, this DA20-C1 AMM supports real repair work. Composite damage assessment and repair is covered with the restricted area diagrams showing where external skin damage up to 250 mm or 50 mm may be repaired and where only the manufacturer or an approved repair facility may work. Bonding paste mix ratios, resin-to-hardener tables, pre-cure and post-cure times are all printed. Control surface weighing and balancing procedures are given for the rudder, elevator, aileron and flap, with the reminder that any repair, paint or reported in-flight control vibration requires re-balancing before flight. Landing gear, wheels and brakes, fuel storage and distribution, electrical generation and distribution, vacuum instruments, canopy latch force adjustment and stall warning maintenance are all documented with the access notes and safety warnings that accompany them.
Why Correct Procedures Matter Here
The DA20-C1 is a composite airframe with carbon fiber spar caps, a spar bridge that carries wing and landing gear loads, and control surfaces whose balance is critical to flutter prevention. Working from manufacturer procedures rather than assumption is what keeps those structures and systems within their limits. This manual states the wear limits, the fit tolerances on wing attachment bolts, the radial and axial play allowances, the bleed and leak test figures, the pitot and static leak acceptance rates and the flap pre-load values, so an inspection produces a defensible result rather than a guess.
Complete PDF Bookmark Tree
Complete Bookmarks
The complete bookmarks in the “Diamond DA20-C1 Aircraft Maintenance Manual DA201-C1 Rev 22 – PDF Download” are as follows:
+DA20-C1 – AIRCRAFT MAINTENANCE MANUALp. 1
+FrontMatterp. 1
Record of Revisionsp. 3
Highlightsp. 5
List of Service Bulletinsp. 7
List of Temporary Revisionsp. 11
List of Effective Pages
Table of Contentsp. 39
+CHAPTER 01-00 INTRODUCTIONp. 49
+INTRODUCTIONp. 53
1. Generalp. 53
2. Revision Servicep. 54
3. Warning, Cautions and Notesp. 54
+4. Manual Configurationp. 54
A. The ATA iSpec2200 Numbering Systemp. 55
B. Groups of Chaptersp. 55
C. Chapter Configurationp. 57
5. Page Numbering Systemp. 57
6. Figuresp. 57
7. Record of Revisionsp. 58
8. Record of Temporary Revisionsp. 58
9. List of Applicable Publicationsp. 58
10. List of Effective Pagesp. 58
11. Service Bulletinsp. 58
12. Safetyp. 58
13. Acronymsp. 58
14. Request for Manual Changep. 58
+CHAPTER 02-00 ORGANIZATION AND HANDLING OF THE MANUALp. 61
+ORGANIZATION AND HANDLING OF THE MANUALp. 65
1. Generalp. 65
2. Applicabilityp. 65
3. Revisionsp. 65
4. Temporary Revisionsp. 65
5. Service Bulletinsp. 66
6. Service Instructionsp. 66
7. Document Notificationsp. 66
8. Abbreviationsp. 67
9. Conversions of Factors and Abbreviationsp. 68
10. Torque Conversion Graphp. 70
+CHAPTER 03-00 GENERAL DESCRIPTION OF THE AIRCRAFTp. 73
+GENERAL DESCRIPTION OF THE AIRCRAFTp. 77
1. Generalp. 77
2. Descriptionp. 77
3. Equipment Datap. 78
+CHAPTER 04-00 AIRWORTHINESS LIMITATIONSp. 81
+Airworthiness Limitations
+1. Generalp. 87
A. Airworthiness Limitationsp. 87
B. Airframep. 87
C. Paintp. 87
D. Engine Life Limited Componentsp. 87
E. Aircraft Life Limited Componentsp. 88
2. Component Life Trackingp. 88
+CHAPTER 05-00 TIME LIMITS AND MAINTENANCE CHECKSp. 91
+Time Limits and Maintenance Checksp. 95
1. Generalp. 95
+2. Chapter Configurationp. 95
A. Chapter 05-10p. 95
B. Chapter 05-20p. 95
C. Chapter 05-30p. 95
D. Chapter 05-50p. 95
3. Words with Special Meaningsp. 96
+05-10 – Time Limitsp. 97
1. Generalp. 97
2. Regulatory Authoritiesp. 97
3. Scheduled Maintenance Time Limitsp. 97
4. Component Time Limitsp. 98
5. Component Time Trackingp. 98
+05-20 – Scheduled Maintenance Checksp. 99
1. Generalp. 99
+2. Maintenance Checklistp. 99
A. Engine Compartmentp. 99
B. Front Fuselagep. 99
C. Cockpitp. 99
D. Center Fuselage, Internalp. 99
E. Rear Fuselagep. 99
F. Tailp. 100
G. Wingsp. 100
H. Generalp. 100
+3. 6000 Hour Inspectionp. 100
A. Types of Inspectionp. 100
B. Defect Limits for Compositesp. 101
+Maintenance Practicesp. 103
1. Generalp. 103
2. Preparationp. 103
3. Engine Ground Testp. 104
+4. Maintenance of Checklist Zonesp. 105
A. Engine Compartmentp. 105
B. Front Fuselagep. 113
C. Cockpitp. 116
D. Center Fuselage, Internalp. 119
E. Rear Fuselagep. 121
F. Tailp. 122
G. Wingsp. 124
H. Generalp. 127
5. 6000 Hour Inspectionp. 129
6. Maintenance Reportp. 135
7. Maintenance Check Flight Reportp. 136
8. Engine Ground Test Recordp. 138
+05-30 – Flightline Checksp. 141
1. Generalp. 141
2. Flightline Checksp. 141
3. Post Flight Checkp. 141
+05-50 – Unscheduled Maintenance Checksp. 143
1. Generalp. 143
+2. Hard Landing Checkp. 143
A. Equipmentp. 143
B. Procedurep. 143
3. Propeller Strikep. 145
+4. Hydraulic Lockp. 145
A. Restricted or clogged induction system drains or cylinder intake port drain(s).p. 146
B. Extended operation of the electric boost pump:p. 146
C. Over priming and attempting engine start with the aircraft parked on an incline that negates the effective operation of the drain system.p. 146
D. A failure to drain oil from cylinders that have been preserved.p. 146
5. Engine Firep. 146
6. Overspeed Flap Extension
+CHAPTER 06-00 DIMENSIONS AND AREASp. 151
+Dimensions and Areasp. 155
+1. Generalp. 155
A. Unit Conversionsp. 155
2. Dimensionsp. 157
3. Adjustment Valuesp. 161
4. Control Surface Gapsp. 161
5. Weight And Static Moments Of Control Surfacesp. 161
+CHAPTER 07-00 LIFTING AND SHORINGp. 163
+Lifting and Shoringp. 167
+07-10- Jackingp. 169
1. Generalp. 169
+2. Lifting the Aircraft on the Jacksp. 169
A. Equipmentp. 169
B. Procedurep. 169
C. Lowering the Aircraftp. 170
D. Rear Fuselage Trestle Pointp. 170
+CHAPTER 08-00 LEVELING AND WEIGHINGp. 173
+Leveling and Weighingp. 177
+08-10 – Weighingp. 179
1. Generalp. 179
+2. Weighingp. 179
A. Equipmentp. 179
B. Weighingp. 180
+08-20 – Levelingp. 185
1. Generalp. 185
+2. Make the Aircraft Level with Jacksp. 185
A. Equipmentp. 185
B. Procedurep. 185
+CHAPTER 09-00 TOWING AND TAXIINGp. 189
+Towing and Taxiingp. 193
+09-10 – Towingp. 195
1. Generalp. 195
2. Tools and Equipmentp. 195
+3. Towing Procedurep. 196
A. Equipmentp. 196
B. Towing by Handp. 196
C. Towing with a Towing Vehiclep. 197
D. Pushing or Pulling the Aircraftp. 198
+09-20 – Taxiingp. 199
1. Generalp. 199
2. Taxiing Procedurep. 199
+CHAPTER 10-00 PARKING, MOORING, STORAGE AND RETURN TO SERVICEp. 201
+Parking, Mooring, Storage and Return to Servicep. 203
+10-10 – Parking/Storagep. 207
1. Generalp. 207
+2. Parkingp. 207
A. Equipmentp. 207
B. Short Term Parking (Less than 5 days)p. 207
C. Long Term Parking (From 15 to 30 days)p. 208
+3. Storagep. 208
A. Materialp. 208
B. Preparationp. 209
C. Weekly Routine Checkp. 209
+10-20 – Mooringp. 211
1. Generalp. 211
+2. Mooringp. 211
A. Equipmentp. 211
B. Mooring Procedurep. 211
+10-30 – Return to Servicep. 213
1. Generalp. 213
2. Return to Service Procedurep. 213
+CHAPTER 11-00 PLACARDS AND MARKINGSp. 215
+Placards and Markingsp. 219
1. Generalp. 219
+2. Replace the Plastic Foil Placardsp. 219
A. Materialp. 219
B. Replace a Placardp. 219
+11-20 – Exterior Placards and Markings
+11-30 – Placards and Markings
+CHAPTER 12-00 SERVICINGp. 241
+Servicingp. 245
+12-010 – Replenishingp. 247
1. Generalp. 247
+2. Fuel Systemp. 247
A. Refuelingp. 247
B. Defuelingp. 248
+3. Engine Oil Systemp. 250
A. Replenish the Engine Oil Systemp. 250
+4. Brake Systemp. 252
A. Fill the Brake System Reservoirsp. 252
+5. Tiresp. 252
A. Examine the Tires and Measure the Pressurep. 252
+12-20 – Scheduled Servicingp. 253
1. Generalp. 253
2. Lubrication Schedulep. 254
+12-30 – Unscheduled Servicingp. 261
1. Generalp. 261
2. Exterior Cleaningp. 261
3. Canopy Cleaningp. 261
4. Interior Cleaningp. 261
5. Engine Cleaningp. 261
6. Ice and Snow Removalp. 262
+CHAPTER 20-00 STANDARD PRACTICES AIRFRAMEp. 263
+Standard Practices – Airframep. 267
1. Generalp. 267
2. Bolt and Nut Types Used in the Aircraftp. 267
+3. Standard Torque Valuesp. 268
A. AN Fine Thread Seriesp. 268
B. AN Coarse Thread Seriesp. 268
C. DIN Specificationsp. 269
4. Special Torque Valuesp. 269
5. Torque Measurementp. 270
6. Torque Conversion Graphsp. 270
+CHAPTER 21-00 AIR CONDITIONINGp. 273
+Heating and Ventilationp. 277
1. Generalp. 277
+2. Description and Operationp. 277
A. Cabin Heat Systemp. 277
B. Cold Air Systemp. 278
C. Equipment Coolingp. 278
+Heating and Ventilation – Troubleshootingp. 281
+Heating and Ventilation – Maintenance Practicesp. 283
1. Generalp. 283
+2. Remove/Install the Heat Control Valvep. 283
A. Remove the Heat Control Valvep. 283
B. Install the Heat Control Valvep. 283
3. Test/Adjust the Heat Control Valvep. 284
+4. Remove/Install the Distribution Boxp. 285
A. Remove the Distribution Box.p. 285
B. Install the Distribution Boxp. 287
5. Test/Adjust the Distribution Box Valvep. 289
+6. Remove/Install the Heat Exchanger Shroudp. 291
A. Remove the Heat Exchanger Shroudp. 291
B. Install the Heat Exchanger Shroudp. 292
7. Inspect the Heat Exchangerp. 292
+8. Remove/Install the Avionics Cooling Fanp. 294
A. Remove the Avionics Cooling Fanp. 294
B. Install the Avionics Cooling Fanp. 294
+CHAPTER 23-00 COMMUNICATIONSp. 297
+Communications
1. General
+2. Description
A. Speech Communication
B. Audio Integrating
C. Static Discharging
+23-10 – Speech Communicationp. 303
1. Generalp. 303
+2. Descriptionp. 304
A. Bendix\King KX 125 NAV COMMp. 304
B. Bendix\King KLX 135\135A GPS COMMp. 305
C. Bendix/King KX 155 NAV COMp. 306
D. Garmin GPS COMMp. 308
E. SL40 VHF COMM Transceiverp. 313
F. ICOM IC-A200 VHF Air Band Transceiverp. 315
G. Garmin GTR 225 Comm
+Speech Communication – Troubleshootingp. 319
+Speech Communication – MAINTENANCE PRACTICESp. 321
1. Generalp. 321
+2. Remove/Install the Bendix/King KX-125 NAV COMMp. 321
A. Remove the Bendix/King KX-125 NAV COMMp. 321
B. Install the Bendix/King KX-125 NAV COMMp. 321
C. Bendix\King KX 125 NAV COMM Adjustment/Testp. 322
+3. Remove/Install the Bendix\King KLX 135/135A GPS COMMp. 323
A. Remove the Bendix\King KLX 135/135A GPS COMMp. 323
B. Install the Bendix\King KLX 135/135A GPS COMMp. 323
C. Adjustment/Test KLX 135/135A GPS COMMp. 324
D. Database Loadingp. 324
+4. Remove/Install the Garmin GNC 420W/GNS 430W/GTN 650p. 325
A. Remove the Garmin GNC 420W/GNS 430W/GTN 650p. 325
B. Install the Garmin GNC 420W/GNS 430W/GTN 650/p. 325
C. Garmin GNC 420W/GNS 430W/GTN 650- Adjustment/Testp. 326
D. Database Loadingp. 326
+5. Remove/Install the Garmin GNS530Wp. 327
A. Remove the Garmin GN530Wp. 327
B. Install the Garmin GN530Wp. 327
C. Garmin GNS530W – Adjustment/Testp. 328
D. Database Loadingp. 328
+6. Remove/Install the Bendix/King KX155 NAV COMMp. 329
A. Remove the Bendix/King KA155 NAV COMMp. 329
B. Install the Bendix/King KA155 NAV COMMp. 329
C. Bendix/King KA155 NAV COMM – Adjustment/Testp. 330
+7. Remove/Install the IC-A200 VHF Air Band Transceiverp. 331
A. Remove the IC-A200 VHF Air Band Transceiverp. 331
B. Install the IC-A200 VHF Air Band Transceiverp. 331
C. Operational Test of IC-A200 VHF Air Band Transceiverp. 332
+8. Remove/Install the SL40/GTR 225VHF COMM Transceiverp. 333
A. Remove the SL40 VHF COMM Transceiverp. 333
B. Install the SL40/GTR 225VHF COMM Transceiverp. 333
C. Operational Test of the SL40/GTR 225VHF COMM Transceiverp. 334
9. Antennasp. 334
10. Connectorsp. 334
+23-50 – Audio Integratingp. 337
1. Generalp. 337
+2. Descriptionp. 337
A. PM 501 Intercomp. 337
B. PM 1000 Intercomp. 338
C. Bendix\King KMA 24 Audio\Marker Receiverp. 339
D. Garmin GMA 340 Audio Panelp. 340
+Audio Integrating – Troubleshootingp. 343
+1. Generalp. 343
A. PM 501/PM 1000p. 343
B. GMA 340p. 344
+Audio Integrating – Maintenance Practicesp. 345
1. Generalp. 345
+2. Remove/Install the PM 501 Intercomp. 345
A. Remove the PM 501 Intercomp. 345
B. Install the PM 501 Intercomp. 345
C. Adjustment/Test – PM 501 Intercomp. 346
+3. Remove/Install the PM 1000 Intercomp. 346
A. Remove the PM 1000 Intercomp. 346
B. Install the PM 1000 Intercomp. 347
C. Adjustment/Test – PM 1000 Intercomp. 347
+4. Remove/Install the Bendix\King KMA 24 Audio/Marker Receiverp. 348
A. Remove the Bendix\King KMA 24 Audio/Marker Receiverp. 348
B. Install the Bendix\King KMA 24 Audio/Marker Receiverp. 348
C. Adjustment/Test KMA 24 Audio/Marker Receiverp. 349
+5. Remove/Install the GMA 340 Audio Panelp. 350
A. Remove the GMA 340 Audio Panellp. 350
B. Install the GMA 340 Audio Panelp. 350
C. Adjustment/Test of the GMA 340 Audio Panelp. 351
6. Connectorsp. 352
+23-60 – static dischargingp. 355
1. Generalp. 355
2. Descriptionp. 355
+Static Discharging – MAINTENANCE PRACTICESp. 357
1. Generalp. 357
+2. Repair/Install the New Copper Tapep. 357
A. Materialp. 357
B. Repair/Installation Procedurep. 358
+3. Replace/Install the New Bonding Tabsp. 358
A. Materialp. 358
B. Procedurep. 358
+CHAPTER 24-00 ELECTRICAL POWERp. 359
+Electrical Powerp. 363
1. Generalp. 363
2. Component Identificationp. 365
3. Component Locationp. 365
+24-30 – DC Generationp. 367
1. Generalp. 367
+2. Description and Operationp. 367
A. Generatorp. 367
B. Generator Controlp. 368
C. Generator Identificationp. 370
+DC Generation – troubleshootingp. 371
+DC Generation – Maintenance Practicesp. 377
1. Generalp. 377
2. Electrical Safetyp. 377
+3. Remove/Install the Over Voltage Sensorp. 377
A. Remove the Over Voltage Sensorp. 377
B. Install the Over Voltage Sensorp. 378
+4. Adjust/Test the Over Voltage Sensorp. 378
A. Equipmentp. 378
B. Test the Over Voltage Sensorp. 378
+5. Remove/Install the Generator/Alternator Mounting Bracketp. 379
A. Remove the Generator/Alternator Mounting Bracketp. 379
B. Install the Generator/Alternator Mounting Bracketp. 380
+6. Remove/Install the Generator/Alternatorp. 383
A. Remove the Generator/Alternatorp. 383
B. Install the Generator/Alternatorp. 383
+7. Adjust/Test the Generator/Alternatorp. 385
A. Equipmentp. 385
B. Test the Generator/Alternatorp. 385
+24-31 – Battery Systemp. 389
1. Generalp. 389
+Battery System – Troubleshootingp. 393
+Battery System – Maintenance Practicesp. 395
1. Generalp. 395
2. Safety Precautionsp. 395
+3. Batteryp. 396
A. Remove the Battery from the Aircraftp. 396
B. Install the Batteryp. 396
C. Fill the Battery with Distilled Waterp. 397
D. Disconnect the Battery for Maintenancep. 397
E. Connect the Battery for Maintenancep. 397
+4. Remove/Install the Battery Relayp. 398
A. Remove the Battery Relayp. 398
B. Install the Battery Relayp. 398
C. Battery Relay Functional Testp. 399
+5. Remove/Install the Battery Relay on the Firewallp. 399
A. Remove the Battery Relayp. 399
B. Install the Battery Relayp. 399
+6. Remove/Install the Ammeter
A. Remove the Ammeter
B. Install the Ammeter
C. Ammeter Functional Test
+7. Remove/Install the Voltmeter
A. Equipment
B. Remove the Voltmeter
C. Install the Voltmeter
D. Voltmeter Functional Test
+24-40 – External Power Unit (EPU) Systemp. 405
1. Generalp. 405
2. Descriptionp. 405
3. Operationp. 405
+EPU System – Maintenance Practicesp. 409
1. Generalp. 409
2. Electrical Safetyp. 409
+3. Remove/Install the EPU Relay to C0001 through C0148 and C0150p. 409
A. Remove the External Power Relayp. 409
B. Install the EPU Relayp. 410
C. EPU Testp. 410
+4. Remove/Install the EPU Relay to C0149 and C0151 onwardsp. 411
A. Remove the External Power Relayp. 411
B. Install the EPU Relayp. 411
C. EPU Testp. 412
+epu system – troubleshootingp. 407
+24-60 – DC Electrical Load Distributionp. 413
1. Generalp. 413
+2. Descriptionp. 413
A. Main Busp. 413
B. Avionic Busp. 413
C. Circuit-breakersp. 415
3. Operationp. 415
+DC electrical load distribution – troubleshootingp. 419
+DC Electrical Load Distribution – Maintenance Practicesp. 421
1. Generalp. 421
2. Electrical Safetyp. 421
+3. Remove/Install the Avionic Master Relayp. 421
A. Remove the Avionic Master Relayp. 421
B. Install the Avionic Master Relayp. 422
C. Avionic Master Relay Functional Testp. 422
+4. Remove/Install a Circuit-breakerp. 422
A. Remove a Circuit-breakerp. 422
B. Install a Circuit-breakerp. 423
C. Circuit-breaker Functional Testp. 423
+CHAPTER 25-00 EQUIPMENT/FURNISHINGp. 425
+Equipment/Furnishingp. 429
+25-10 – Flight Compartmentp. 431
1. Generalp. 431
+2. Descriptionp. 431
A. Pilot’s Seatsp. 431
B. Safety Beltsp. 431
C. Fabric Wall Panelsp. 431
D. Instrument Panel Coverp. 431
E. Center Console Access Panelp. 431
F. Baggage Compartment Floor Panelp. 431
G. Baggage Netp. 431
+Equipment/F urnishing – Maintenance Practicesp. 433
1. Generalp. 433
+2. Remove/Install a Pilot’s Seatp. 433
A. Remove a Pilot’s Seatp. 433
B. Install a Pilot’s Seatp. 433
+3. Remove/Install a Safety Beltp. 435
A. Remove a Safety Beltp. 435
B. Install a Safety Beltp. 435
+4. Remove/Install the Instrument Panel Coverp. 437
A. Remove the Instrument Panel Coverp. 437
B. Install the Instrument Panel Coverp. 437
+5. Remove/Install the Baggage Compartment Floor Panelp. 437
A. Remove the Baggage Compartment Floor Panel.p. 437
A. Install the Baggage Compartment Floor Panel.p. 438
+6. Cleaningp. 438
A. Seatsp. 438
B. Safety Beltsp. 438
+25-60 – Emergencyp. 439
1. Generalp. 439
2. Descriptionp. 439
+ELT – Maintenance Practicesp. 441
1. Generalp. 441
2. ELT Functional Testp. 441
+25-60 – ME 406 Emergency Locator Transmitter (ELT)p. 443
1. Generalp. 443
+2. Descriptionp. 443
A. ELT Equipmentp. 443
B. ELT Batteriesp. 443
+3. Operationp. 444
+ME 406 ELT – Troubleshootingp. 447
+ME 406 ELT – Maintenance Practicesp. 449
1. Generalp. 449
+2. Remove/Install the ELTp. 449
A. Remove the ELTp. 449
B. Install the ELTp. 449
3. ELT Functional Testp. 451
4. Replace the ELT Batteriesp. 452
5. ELT Periodic Inspectionp. 453
+CHAPTER 26-00 FIRE PROTECTIONp. 455
+Fire Protectionp. 459
1. Generalp. 459
2. Descriptionp. 459
+CHAPTER 27-00 FLIGHT CONTROLSp. 461
+Flight Controlsp. 467
1. Generalp. 467
2. Descriptionp. 467
3. Control Rodsp. 467
+Flight Controls – Maintenance Practicesp. 469
1. Generalp. 469
+2. Remove/Install the Control Stickp. 469
A. Remove the Control Stickp. 469
B. Install the Control Stickp. 470
+27-10 – Flight Controls – Ailerons and Tabsp. 473
1. Generalp. 473
2. Descriptionp. 473
3. Operationp. 473
+Aileron Control – Troubleshootingp. 477
+Aileron Control – Maintenance Practicesp. 479
1. Generalp. 479
+2. Aileron Control System Test For Correct Range Of Movementp. 479
A. Equipmentp. 479
B. Aileron Control Test Procedurep. 479
+3. Aileron Control System Adjustmentsp. 481
A. Equipmentp. 481
B. Aileron Adjustment Procedurep. 481
4. Aileron Control Rod Accessp. 485
5. Aileron Bellcrank Accessp. 486
+27-20 – Flight Controls – Rudder and Tabp. 487
1. Generalp. 487
2. Descriptionp. 487
3. Operationp. 488
+Rudder Control – Troubleshootingp. 493
+Rudder Control – Maintenance Practicesp. 495
1. Generalp. 495
+2. Rudder Control System Test for Correct Range Of Movementp. 495
A. Equipmentp. 495
B. Rudder Control Test Procedurep. 495
+3. Rudder Control System Adjustmentsp. 496
A. Equipmentp. 496
B. Rudder Adjustment Procedurep. 496
+4. Remove/Install Rudder Control Cablesp. 498
A. Equipmentp. 498
B. Remove the Cockpit Rudder Control Cables (From the firewall to the yoke)p. 498
C. Install the Cockpit Rudder Control Cables (From the firewall to the yoke)p. 499
D. Remove the Aft Fuselage Rudder Control Cables (From the yoke to the rudder)p. 500
E. Install the Aft Fuselage Rudder Control Cables (From the yoke to the rudder)p. 501
+27-30 – Flight Controls – Elevatorp. 503
1. Generalp. 503
2. Descriptionp. 503
3. Operationp. 503
+Elevator Control – Troubleshootingp. 505
+Elevator Control – Maintenance Practicesp. 507
1. Generalp. 507
+2. Elevator Control System Test for Correct Range of Movementp. 507
A. Equipmentp. 507
B. Elevator Control Test Procedurep. 507
+3. Elevator Control System Adjustmentsp. 508
A. Equipmentp. 508
B. Elevator Adjustment Procedurep. 508
+27-31 – Flight Controls – Elevator Trimp. 511
1. Generalp. 511
2. Descriptionp. 511
3. Operationp. 513
+Elevator Control Trim – Troubleshootingp. 515
+Elevator Trim – Maintenance Practicesp. 517
1. Generalp. 517
+2. Remove/Install the Elevator Trim Actuatorp. 517
A. Remove the Elevator Trim Actuatorp. 517
B. Install the Elevator Trim Actuatorp. 518
C. Adjust the Elevator Trim Position Indicatorp. 519
+27-50 – Flight Controls – Flapsp. 521
1. Generalp. 521
+2. Descriptionp. 521
A. Flap Actuatorp. 521
B. Control Rods and Bellcranksp. 521
C. Flap Electrical Controlp. 521
3. Operation
4. Fail Safe Operationp. 523
+Flaps – Troubleshooting
+Flaps – Maintenance Practicesp. 533
1. Generalp. 533
+2. Remove/Install the Flap Actuatorp. 533
A. Remove the Flap Actuatorp. 533
B. Install the Flap Actuatorp. 534
+3. Adjust/Test the Flap Systemp. 534
A. Equipmentp. 534
B. Procedurep. 535
+CHAPTER 28-00 FUELp. 541
+Fuelp. 545
1. Generalp. 545
2. Descriptionp. 545
3. Operationp. 547
+28-10- – Fuel Storagep. 549
1. Generalp. 549
2. Descriptionp. 549
+Fuel Storage – Troubleshootingp. 551
+Fuel Storage – Maintenance Practicesp. 553
1. Generalp. 553
+2. Remove/Install the Fuel Tankp. 553
A. Remove the Fuel Tankp. 553
B. Install the Fuel Tankp. 554
+3. Remove/Install the Fuel Filler Neckp. 555
A. Remove the Fuel Filler Neckp. 555
B. Install the Fuel Filler Neckp. 556
4. Flush the Fuel System Procedurep. 556
5. Overhaul the Fuel Capp. 558
+28-20 – Fuel Distributionp. 561
1. Generalp. 561
+2. Descriptionp. 561
A. Maintenance shut-off valvep. 561
B. Gascolatorp. 561
C. Electrical Fuel Pumpp. 561
D. Maintenance Drain Tapsp. 561
E. Fuel Shut-Off Valvep. 563
F. Check Valvep. 563
G. Fuel Hosesp. 563
+Fuel Distribution – Troubleshootingp. 565
+Fuel Distribution – Maintenance Practicesp. 567
1. Generalp. 567
+2. Remove/Install the Electric Fuel Pumpp. 567
A. Remove the Electric Fuel Pumpp. 567
B. Install the Electric Fuel Pumpp. 568
C. Clean the Filter Element in the Gascolatorp. 569
+3. Remove/Install the Fuel Shut-Off Valvep. 570
A. Remove the Fuel Shut-Off Valvep. 570
B. Install the Fuel Shut-Off Valvep. 571
4. Functional Test of the Fuel Shut-Off Valvep. 572
+28-40 – Fuel Indicatingp. 575
1. Generalp. 575
2. Description and Operationp. 575
+Fuel Indicating – Troubleshooting
+Fuel Indicating – Maintenance Practicesp. 581
1. Generalp. 581
+2. Remove/Install the Fuel Quantity Sensorp. 581
A. Remove the Fuel Quantity Sensorp. 581
B. Install the Fuel Quantity Sensor
3. Calibrate the VDO Fuel Quantity Indication System.
4. Adjust the VDO Fuel Quantity Gauge
5. Calibrate the Diamond Fuel Probe
+6. Remove/Install the Fuel Quantity Gaugep. 585
A. Remove the Fuel Quantity Gaugep. 585
B. Install the Fuel Quantity Gaugep. 585
+CHAPTER 31-00 INDICATING SYSTEMSp. 589
+Indicating Systemsp. 595
+31-10 – Instrument and Control Panelsp. 597
1. Generalp. 597
+2. Descriptionp. 597
A. Instrument Panelp. 597
B. Control Panelp. 606
+Instrument and Control Panels – Troubleshootingp. 609
+Instrument and Control Panels – Maintenance Practicesp. 611
1. Generalp. 611
+2. Remove/Install the Instrument Panelp. 611
A. Remove the Instrument Panelp. 611
B. Install the Instrument Panelp. 613
+3. Remove/Install the Control Panelp. 615
A. Remove the Control Panel in the Center Consolep. 615
B. Install the Control Panel in the Center Consolep. 616
+31-20 – Independent Instrumentsp. 619
1. Generalp. 619
+2. Description and Operationp. 619
A. Electronic Clockp. 619
B. Engine-Operated Hours Meter (Hobbs Meter)p. 619
+Independent Instruments – Troubleshootingp. 621
+Independent Instruments – Maintenance Practicesp. 623
1. Generalp. 623
+2. Remove/Install the Clockp. 623
A. Remove the Clockp. 623
B. Install the Clockp. 623
+3. Remove/Install the Engine Operated Hourmeterp. 624
A. Remove the Engine Operated Hourmeterp. 624
B. Install the Engine Operated Hourmeterp. 624
+31-50 – Warning Systemsp. 625
1. Generalp. 625
2. Description and Operationp. 625
+Warning Systems – Troubleshootingp. 627
+Warning Systems – Maintenance Practicesp. 629
1. Generalp. 629
+2. Remove/Install a Warning Lamp Bulbp. 629
A. Replace a Warning Lamp Bulbp. 629
+3. Remove/Install an Annunciator Unitp. 630
A. Remove an Annunciator Unitp. 630
B. Install an Annunciator Unitp. 630
+31-60 – Aspen EFD1000p. 631
1. Generalp. 631
+2. Descriptionp. 631
A. Primary Flight Displayp. 631
B. Remote Sensor Module (RSM)p. 632
C. Configuration Modulep. 632
D. Analog Converter Unit (ACU)p. 633
+3. Operationp. 634
A. Control Knobsp. 635
B. Navigation Source Selectionp. 635
C. Range Controlp. 635
D. Reversion Controlp. 635
E. Menu Controlp. 636
F. Attitude Indicatorp. 636
G. Airspeed Indicatorp. 636
H. Altimeterp. 636
I. Data Bar (TAS, GS, OAT, Winds, Barometric pressure Set)p. 636
J. Horizontal Situation Indicatorp. 638
K. Hot Key Operationp. 639
+Aspen EFD1000 – Troubleshootingp. 641
+1. Generalp. 641
A. The table that follows will assist in the troubleshooting of the Aspen EFD1000 system. It does not give information about the equipment or associated systems. For faults on an item of equipment or an associated system refer to that ATA Chapter in …p. 641
B. If the fault is shown in column 1, the possible cause is listed in column 2, the recommended repair is shown in column 3. .p. 641
+Aspen EFD1000 System – Maintenance Practicesp. 645
1. Generalp. 645
+2. Remove/Install the Primary Flight Display (PFD)p. 645
A. Remove the PFDp. 645
B. Install the PFDp. 647
+3. Remove/Install the Remote Sensor Module (RSM)p. 648
A. Remove the RSMp. 648
B. Install the RSMp. 649
+4. Remove/Install the Configuration Module (CM)p. 650
A. Remove the CMp. 650
B. Install the CMp. 651
+5. Remove/Install the Analog Converter Unit (ACU)p. 651
A. Remove the ACUp. 651
B. Install the ACUp. 652
+31-61 – Garmin G-500 Integrated Display Systemp. 655
1. Generalp. 655
+2. Description and Operationp. 655
A. GDU 620 Displayp. 655
B. GRS 77 Attitude and Heading Reference System (AHRS)p. 657
C. GDC 74A Air Data Computer (ADC)p. 657
D. GMU 44 Magnetometerp. 658
E. Databasesp. 658
+Garmin G500 – Troubleshootingp. 663
1. Generalp. 663
2. Garmin G500 Alertsp. 665
+Garmin G500 – Maintenance Practicesp. 669
1. Generalp. 669
+2. Remove/Install the GDU 620 Displayp. 669
A. Remove the GDU 620 Displayp. 669
B. Install the GDU 620 Displayp. 670
+3. Remove/Install the GDC 74A Air Data Computer (ADC)p. 671
A. Remove the GDC 74A Air Data Computer (ADC)p. 671
B. Install the GDC 74A Air Data Computer (ADC)p. 671
+4. Remove/Install the GRS77 Attitude, Heading and Reference Unit (AHRS)p. 672
A. Remove the GRS77 Attitude, Heading and Reference Unit (AHRS)p. 672
B. Install the GRS77 Attitude, Heading and Reference Unit (AHRS)p. 672
+5. Remove/Install the GMU 44 Magnetometerp. 673
A. Remove the GMU 44 Magnetometerp. 673
B. Install the GMU 44 Magnetometerp. 674
+6. Remove/Install the Temperature Probe (GTP 59)p. 674
C. Remove the Temperature Probe (GTP 59)p. 674
D. Install the Temperature Probe (GTP 59)p. 675
+31-62 – Traffic Advisory System (TAS) 600 – Troubleshootingp. 679
1. Generalp. 679
+Traffic Advisory System (TAS) 600p. 681
1. Generalp. 681
2. Descriptionp. 681
+3. Operationp. 682
A. Processorp. 682
B. Transponder Couplerp. 682
C. Antennasp. 682
4. Integration with Garmin G500p. 683
+Traffic Advisory System (TAS) 600 – Maintenance Practicesp. 685
1. Generalp. 685
+2. Remove/Install the TAS 600 Processor Unitp. 685
A. Remove the TAS 600 Processor Unitp. 685
B. Install the TAS 600 Processor Unitp. 686
+3. Remove/Install the TAS Transponder Couplerp. 687
A. Remove the TAS Transponder Couplerp. 687
B. Install TAS Transponder Couplerp. 687
+4. Remove/Install the TAS Antennap. 688
A. Remove the TAS Antennap. 688
B. Install TAS Antennap. 688
+CHAPTER 32-00 LANDING GEARp. 691
+Landing Gearp. 695
1. Generalp. 695
2. Description and Operationp. 695
+32-10 – Main Landing Gearp. 697
1. Generalp. 697
2. Description and Operationp. 697
+Main Landing Gear – Troubleshootingp. 699
+Main Landing Gear – Maintenance Practicesp. 701
1. Generalp. 701
+2. Remove/Install the Main Landing Gearp. 701
A. Equipmentp. 701
B. Remove the Main Landing Gear Strutp. 701
C. Install the Main Landing Gear Strutp. 702
+3. Remove/Install the Hardware at the Inner and Outer Mounts of the Main Landing-Gear Strutp. 704
A. Equipmentp. 704
B. Remove the Hardware from the Inner/Outer Mount of the Main Landing-Gear Strutp. 704
C. Install the Hardware from the Inner/Outer Mount of the Main Landing-Gear Strutp. 705
+4. Test/Adjust the Main Landing Gearp. 706
A. Equipmentp. 706
B. Procedurep. 706
+32-20 – Nose Landing Gearp. 713
1. Generalp. 713
2. Description and Operationp. 713
+Nose Landing Gear – Troubleshootingp. 715
+Nose Landing Gear – Maintenance Practicesp. 717
1. Generalp. 717
+2. Remove/Install the Nose Landing Gear (NLG)p. 717
A. Equipmentp. 717
B. Remove the Nose Landing Gear Strutp. 717
C. Install the Nose Landing Gear Strutp. 718
+3. Remove/Install the NLG Fork Assemblyp. 720
A. Equipmentp. 720
B. Remove the NLG Forkp. 720
C. Install the NLG Fork Assemblyp. 720
+4. Remove/Install the Shock Absorber Assemblyp. 721
A. Equipmentp. 721
B. Remove the Shock Absorber Assemblyp. 721
C. Install the Shock Absorber Assemblyp. 722
5. Replace the Shock Absorber Assembly Elementsp. 722
+6. Adjust the Nose Landing Steering Frictionp. 724
A. Equipmentp. 724
B. Procedurep. 724
7. Nose Wheel Balancingp. 724
+32-40 – Wheels and Brakesp. 731
1. Generalp. 731
+2. Description and Operationp. 731
A. Main Wheelp. 731
B. Nose Wheelp. 731
C. Brake Systemp. 731
+Wheels and Brakes – Troubleshootingp. 737
+Wheels and Brakes – Maintenance Practicesp. 739
1. Generalp. 739
+2. Remove/Install the Main Wheelp. 739
A. Equipmentp. 739
B. Remove the Main Wheelp. 739
C. Install the Main Wheelp. 740
+3. Remove/Install the Nose Wheelp. 741
A. Equipmentp. 741
B. Remove the Nose Wheelp. 741
C. Install the Nose Wheelp. 742
+4. Remove/Install a Brake Master Cylinderp. 743
A. Remove a Brake Master Cylinderp. 743
B. Install a Brake Master Cylinderp. 744
+5. Remove/Install a Brake Caliperp. 744
A. Remove a Brake Caliperp. 744
B. Install a Brake Caliperp. 745
+6. Remove/Install the Parking Brake Valvep. 745
A. Remove the Parking Brake Valvep. 745
B. Install the Parking Brake Valvep. 746
+7. Bleed the Brake Systemp. 746
A. Equipmentp. 746
B. Bleeding Procedurep. 747
8. Condition of the Brake Liningsp. 748
+9. Wheels and Brakes Cleaning Proceduresp. 748
A. Inspectionp. 748
B. Cleaningp. 749
+CHAPTER 33-00 LIGHTSp. 753
+Lightsp. 757
1. Generalp. 757
2. Descriptionp. 757
+33-20 – Cockpit Lightingp. 759
1. Generalp. 759
+2. Descriptionp. 759
A. General Instrument Panel Lightingp. 759
B. Map Lightp. 759
C. Instrument Panel Rheostatp. 759
D. DIM/BRIGHT Switchp. 760
+Cockpit Lighting – Troubleshootingp. 761
+Cockpit Lighting – Maintenance Practicesp. 763
1. Generalp. 763
+2. Remove/Install the General Instrument Light/Map Light Modulep. 763
A. Remove the General Instrument Light/Map Light Modulep. 763
B. Install the General Instrument Light/Map Light Modulep. 763
+33-40 – Exterior Lightsp. 765
1. Generalp. 765
+2. Descriptionp. 765
A. Position Lightsp. 765
B. Anti-Collision Lights (ACL)p. 765
C. Landing Lightp. 765
D. Taxi Lightp. 765
E. Recognition lights (optional)p. 765
+Exterior Lights – Troubleshootingp. 767
+Exterior Lights – Maintenance Practicesp. 769
1. Generalp. 769
+2. Remove/Install the Taxi Lightp. 769
A. Remove the Taxi Lightp. 769
B. Install the Taxi Lightp. 770
+3. Remove/Install the Landing Lightp. 770
A. Remove the Landing Lightp. 770
B. Install the Landing Lightp. 771
4. Adjust the Position of the Taxi/Landing Light Beamp. 772
5. Replace a Bulb in the Wing Tipp. 773
+6. Remove/Install The Light Unit In The Wing Tipp. 773
A. Remove the Light Unit in the Wing Tipp. 773
B. Install the Light Unit in the Wing Tipp. 774
+7. Remove/Install the Power Unit for the Anti-Collision Lightsp. 775
A. Remove the Power Unit for the Anti-Collision Lightsp. 775
B. Install the Power Unit for the Anti-Collision Lightsp. 775
+CHAPTER 34-00 NAVIGATIONp. 781
+Navigationp. 787
1. Generalp. 787
+2. Descriptionp. 787
A. Flight Environment Datap. 787
B. Attitude and Directionp. 788
C. Landing and Taxiing Aidsp. 788
D. Dependent Position Determiningp. 788
+34-10 – Flight Environment Datap. 789
1. Generalp. 789
+2. Descriptionp. 789
A. Pitot-Static Systemp. 789
B. Blind Altitude Encoderp. 789
C. OAT Indicating Systemp. 789
+Flight Environment Data – Troubleshootingp. 793
+1. Generalp. 793
A. Pitot-Static and OAT Systemsp. 793
B. Blind Encoder (Mode C Fault Analysis)p. 794
+Flight Environment Data – Maintenance Practicesp. 801
1. Generalp. 801
+2. Remove/Install a Pitot-Static Instrumentp. 801
A. Remove a Pitot-Static Instrumentp. 801
B. Install a Pitot-Static Instrumentp. 801
+3. Remove/Install Pitot-Static Probe (probe without optional Pitot Heat)p. 802
A. Remove the Pitot-Static Probep. 802
B. Install the Pitot-Static Probep. 802
+4. Remove/Install and Functional Check of the Pitot-Static Probe (Probe with optional Pitot Heat System).p. 803
A. Remove the Pitot-Static Probep. 803
B. Install the Pitot-Static Probep. 803
C. Pitot Static Heat Systemp. 804
D. Pitot Static Heat System Functional Checkp. 804
+5. Remove/Install the Blind Altitude Encoderp. 805
A. Equipmentp. 805
B. Remove the Blind Altitude Encoderp. 805
C. Install the Blind Altitude Encoderp. 806
D. Adjust/Test the Blind Altitude Encoderp. 806
+6. Remove/Install the OAT Indicatorp. 807
A. Remove the OAT Indicatorp. 807
B. Install the OAT Indicatorp. 808
+7. Pitot and Static Leak Testsp. 808
A. Test Precautionsp. 808
B. Equipmentp. 809
C. Low Range Static Leak Testp. 809
D. Pitot Testp. 810
+34-20 – Attitude and Directionp. 811
1. Generalp. 811
+2. Description and Operationp. 811
A. Attitude Indicatorp. 811
B. Turn Coordinatorp. 811
C. Stall Warningp. 812
D. Magnetic Compassp. 812
E. Directional Gyro (DG)p. 812
F. Artificial Horizon Indicatorp. 812
+Attitude and Direction – Troubleshootingp. 817
+Attitude and Direction – Maintenance Practicesp. 819
1. Generalp. 819
+2. Remove/Install the Magnetic Compassp. 819
A. Remove the Magnetic Compassp. 819
B. Install the Magnetic Compassp. 819
+3. Test/Adjust the Magnetic Compassp. 820
A. Equipmentp. 820
B. Compass Swingp. 820
+4. Remove/Install the Stall Warning Horn Assemblyp. 821
A. Remove the Stall Warning Horn Assemblyp. 821
B. Install the Stall Warning Horn Assemblyp. 822
5. Procedure to Remove Water from the Stall Warning Systemp. 822
+6. Remove/Install the Backup Artificial Horizon Indicatorp. 823
C. Remove the Artificial Horizon Indicatorp. 823
D. Install the Artificial Horizon Indicatorp. 823
+34-30 – Landing and Taxiing Aidsp. 825
1. Generalp. 825
2. Description and Operationp. 825
+Landing and Taxiing Aids – Troubleshootingp. 827
+Landing and Taxiing Aids – Maintenance Practicesp. 829
1. Generalp. 829
+2. Remove/Install the Bendix\King KMA 24 Audio/Marker Receiverp. 829
A. Remove the Bendix/King KMA 24 Receiverp. 829
B. Install the Bendix/King KMA 24 Receiverp. 829
C. Adjustment/Test Bendix/King KMA 24 Receiverp. 830
3. Connectorsp. 830
+34-50 – Dependent Position Determiningp. 833
1. Generalp. 833
+2. Description and Operationp. 834
A. Bendix/King KX 125 NAV COMMp. 834
B. Bendix/King KI 208 VOR, LOC Indicatorp. 836
C. Bendix/King KX 155 NAV COMp. 837
D. Bendix/King KI 209 VOR, LOC G/S Indicatorp. 838
E. Bendix/King KLN 35A GPSp. 839
F. Bendix/King KLX 135/135A GPS COMMp. 840
G. Bendix/King KT 76A Transponderp. 841
H. Garmin GTX 327 Transponderp. 843
I. Garmin GTX 328/330/330D Transponderp. 845
J. Garmin GNC 420Wp. 847
K. Garmin GNS 430Wp. 850
L. Garmin GNS 530Wp. 852
M. GNS430W/GNS530W VOR, LOC, G/S INDICATORp. 853
N. GTN 650p. 854
+Dependent Position Determining – Troubleshootingp. 857
+1. Generalp. 857
A. Transponderp. 857
B. NAV – Bendix\King KX 125 VOR, LOC, KI 208p. 858
+Dependent Position Determining – Maintenance Practicesp. 859
1. Generalp. 859
+2. Remove/Install the Bendix\King KX 125 NAV COMMp. 859
A. Remove the Bendix/King KX 125 NAV COMMp. 859
B. Install the Bendix/King KX 125 NAV COMMp. 859
C. Adjustment/Test Bendix/King KX 125 NAV COMMp. 860
+3. Remove/Install the Bendix\King KX 155 NAV COMMp. 861
A. Remove the Bendix/King KX 155 NAV COMMp. 861
B. Install the Bendix/King KX 155 NAV COMMp. 861
C. Adjustment/Test Bendix/King KX 155 NAV COMMp. 862
+4. Remove/Install the Bendix\King KLN 35A GPS Receiverp. 863
A. Remove the Bendix\King KLN 35A GPS Receiverp. 863
B. Install the Bendix/King KLN 35A GPS Receiverp. 863
C. Adjustment/Test Bendix/King KLN 35A GPS Receiverp. 864
D. Data Base Loadingp. 864
+5. Remove/Install the Bendix\King KLX 135/135A GPS COMMp. 865
A. Remove the Bendix\King KLX 135/135A GPS COMMp. 865
B. Install the Bendix\King KLX 135/135A GPS COMMp. 865
C. Adjustment/Test Bendix/King KLX 135/135A GPS COMMp. 866
D. Data Base Loadingp. 866
+6. Remove/Install the Bendix\King KI 208/209 Indicatorp. 867
A. Remove the Bendix\King KI 208 /209Indicatorp. 867
B. Install the Bendix\King KI 208 /209Indicatorp. 867
C. Adjustment/Test – Bendix\King KI 208 /209Indicatorp. 868
+7. Remove/Install the Bendix\King KT 76A Transponderp. 868
A. Remove the Bendix\King KT 76A Transponderp. 868
B. Install the Bendix\King KT 76A Transponderp. 869
C. Adjustment/Test – Bendix\King KT 76A Transponderp. 869
+8. Remove/Install the GTX 327 Transponderp. 870
A. Remove the GTX 327 Transponderp. 870
B. Install the GTX 327 Transponderp. 870
C. Operational Test of GTX 327 Transponderp. 871
+9. Remove/Install the GTX 328 Transponderp. 871
A. Remove the GTX 328 Transponderp. 871
B. Install the GTX 328 Transponderp. 872
C. Operational Test of GTX 328 Transponderp. 872
+10. Remove/Install the GTX 330 Transponderp. 873
A. Remove the GTX 330 Transponderp. 873
B. Install the GTX 330 Transponderp. 873
C. Operational Test of GTX 330 Transponderp. 874
+11. Remove/Install the Garmin GNC 420W/GNS 430W/GTN 650p. 874
A. Remove the Garmin GNC420W/GNS 430W/GTN 650p. 874
B. Install the Garmin GNC 420W/GNS 430W/GTN 650p. 875
C. Adjustment/Test – Garmin GNC 420W/GNS 430W/GTN 650p. 875
D. Data Base Loadingp. 875
+12. Remove/Install the Garmin GNS530Wp. 876
A. Remove the Garmin GNS530Wp. 876
B. Install the Garmin GNS530Wp. 876
C. Adjustment/Test – Garmin GNS530Wp. 877
D. Data Base Loadingp. 877
+13. Remove/Install the GNS 430W/GNS 530W VOR, LOC, G/S Indicatorp. 877
A. Remove the GNS 430W/GNS 530W VOR, LOC, G/S Indicatorp. 877
B. Install the GNS 430W/GNS 530W VOR, LOC, G/S Indicatorp. 878
14. Antennap. 878
15. Connectorsp. 878
+CHAPTER 37-00 VACUUMp. 885
+Vacuump. 889
1. Generalp. 889
+2. Descriptionp. 889
A. Vacuum Pumpp. 889
B. Vacuum regulatorp. 889
C. Vacuum Inlet Filterp. 889
D. Vacuum Gaugep. 889
E. Connectionsp. 889
3. Operationp. 891
+37-10 – Vacuum Distributionp. 893
1. Generalp. 893
+Tacuum Distribution – Troubleshootingp. 895
+Vacuum Distribution – Maintenance Practicesp. 897
1. Generalp. 897
+2. Remove/Install the Vacuum Pumpp. 897
A. Remove the Vacuum Pumpp. 897
B. Install the Vacuum Pumpp. 897
+3. Remove/Install the Vacuum Regulatorp. 898
A. Remove the Vacuum Regulatorp. 898
B. Install the Vacuum Regulatorp. 898
4. Replace the Vacuum Inlet Filterp. 899
5. Adjust the Vacuum Regulatorp. 900
+37-10 – Vacuum Indicatingp. 903
1. Generalp. 903
+Vacuum Indicating – Troubleshootingp. 905
+Vacuum Indicating – Maintenance Practicesp. 907
1. Generalp. 907
+2. Remove/Install the Vacuum Gaugep. 907
A. Remove the Vacuum Gaugep. 907
B. Install the Vacuum Gaugep. 907
+CHAPTER 51-00 STANDARD PRACTICES STRUCTURESp. 909
+Standard Practices – Structuresp. 913
1. Generalp. 913
+2. Structural Classificationp. 913
A. Limited Area 1p. 913
B. Limited Area 2p. 913
C. Prohibited Repair Areap. 913
+3. Design, Dimensions, Clearances and Wear Limitsp. 915
A. Design Dimensionsp. 915
B. Clearances and Wear Limitsp. 915
4. The Description and Location of Partsp. 915
5. Repair Limitationsp. 915
+6. Inspection Techniquesp. 917
A. Examine Visuallyp. 917
B. Light Testp. 917
C. Coin Tap Testp. 917
+7. Approved Materials and Suppliersp. 919
A. Resin and Hardnerp. 919
B. Glass Fiber Clothp. 919
C. Carbon Fiber Clothp. 919
+8. Resin Handlingp. 921
A. Introductionp. 921
B. Materialsp. 921
C. Procedurep. 922
9. Resin to Hardner Mixturep. 922
+10. Bonding of Fiber Reinforced Plasticsp. 923
A. Introductionp. 923
B. Materialsp. 923
C. Procedurep. 923
+11. Curingp. 924
A. Introductionp. 924
B. Materialp. 924
C. Procedurep. 924
+51-30 – Control Srface Balancingp. 927
1. Generalp. 927
2. Control Surface Balancep. 927
+CHAPTER 52-00 DOORSp. 931
+Doorsp. 935
+52-10 – Canopyp. 937
1. Generalp. 937
+2. Descriptionp. 937
A. Canopy Structurep. 937
B. Canopy Hingesp. 937
C. Canopy Lockingp. 937
D. Alignment Pinsp. 938
+3. Operationp. 938
A. Canopy Closedp. 938
B. Canopy Openp. 938
+Canopy – Troubleshootingp. 941
+Canopy – Maintenance Practicesp. 943
1. Generalp. 943
+2. Remove/Install the Canopyp. 943
A. Remove the Canopyp. 943
B. Install the Canopyp. 943
+3. The Canopy Latch Force Testp. 944
A. Equipmentp. 944
B. The Canopy Latch Force Test – Canopies With Internal Handles Onlyp. 944
C. The Canopy Latch Force Test – Canopies With External Handlesp. 945
4. Adjust the Canopy Latch Forcep. 946
5. Adjust the Canopy Warning Light Micro-Switchp. 946
+6. Remove/Install the Sliding Side Windowp. 947
A. Remove the Sliding Side Windowp. 947
B. Install the Sliding Side Windowp. 948
+52-40 – Access Panelsp. 953
+CHAPTER 53-00 FUSELAGEp. 955
+Fuselagep. 959
+53-10 – Fuselage Structurep. 961
1. Generalp. 961
+2. Descriptionp. 961
A. Fuselage Shellsp. 961
B. Firewallp. 961
C. T-Panelp. 963
D. Floorp. 963
E. Forward Control Bulkheadp. 963
F. Center tunnelp. 963
G. Spar bridgep. 963
H. Seat Backp. 963
I. Rollbarp. 965
J. Aft Control Bulkheadp. 965
K. B-bulkheadp. 965
L. Half bulkheadp. 965
M. Ring-Bulkhead #1p. 965
N. Ring-Bulkhead #2p. 965
O. Ring-Bulkhead #3p. 965
P. Ring-Bulkhead #4p. 965
Q. Vertical Stabilizer Lower Ribp. 965
R. Vertical Stabilizer Upper Ribp. 967
S. Vertical Stabilizer Sparp. 967
+Fuselage – Maintenance Practicesp. 969
1. Generalp. 969
2. High Temperature Paint Repair of a Cowlingp. 969
+CHAPTER 55-00 STABILIZERSp. 973
+Stabilizersp. 977
+55-10 – Horizontal Stabilizerp. 979
1. Generalp. 979
2. Descriptionp. 979
+Horizontal Stabilizer – Maintenance Practicesp. 981
1. Generalp. 981
+2. Remove/Install the Horizontal Stabilizerp. 981
A. Remove the Horizontal Stabilizerp. 981
B. Install the Horizontal Stabilizerp. 982
+55-20 – Elevatorp. 985
1. Generalp. 985
2. Descriptionp. 985
+Elevator – Maintenance Practicesp. 987
1. Generalp. 987
+2. Remove/Install the Elevatorp. 987
A. Remove the Elevatorp. 987
B. Install the Elevatorp. 987
+55-30 – Lower Finp. 989
1. Generalp. 989
2. Descriptionp. 989
+Lower Fin – Maintenance Practicesp. 991
1. Generalp. 991
+2. Remove/Install the Lower Finp. 991
A. Remove the Lower Finp. 991
B. Install the Lower Finp. 991
+55-40 – Rudder and Tabp. 993
1. Generalp. 993
2. Descriptionp. 993
+Rudder and Tab – Maintenance Practicesp. 995
1. Generalp. 995
+2. Remove/Install the Rudderp. 995
A. Remove the Rudderp. 995
B. Install the Rudderp. 995
+3. Remove/Install the Top Pivot Bushingp. 996
A. Remove the Top Pivot Bushingp. 996
B. Install the Top Pivot Bushingp. 996
+CHAPTER 56-00 WINDOWSp. 999
+Windowsp. 1003
1. Generalp. 1003
2. Descriptionp. 1003
3. Removal and Installationp. 1003
+56-10 – Repair of the Canopy Transparencyp. 1005
1. Damage Limitsp. 1005
2. Tools and Equipmentp. 1005
3. Materialsp. 1005
4. Fillersp. 1005
5. Temporary Repair to the Canopy Transparencyp. 1005
6. Permanent Repair to the Canopy Transparencyp. 1006
+56-11 – Replacement of the Rear Windowp. 1011
1. Damage Limitsp. 1011
2. Tools and Equipmentp. 1011
3. Materialsp. 1011
4. Replacement of the Rear Windowp. 1012
+CHAPTER 57-00 WINGSp. 1015
+Wingsp. 1019
+57-10 – Wing Structurep. 1021
1. Generalp. 1021
+2. Descriptionp. 1021
A. Wing Shellsp. 1021
B. Sparp. 1021
C. Root Ribp. 1022
D. Aft Inner Webp. 1022
E. Aft Outer Webp. 1022
F. Flap Control Support Ribp. 1022
G. Flap Control Ribp. 1022
H. Center Ribp. 1022
I. Aileron Control Ribp. 1022
J. Aileron Mass Balance Ribp. 1022
K. Tie-Down Insertp. 1023
+Wing Structure – Maintenance Practicesp. 1027
1. Generalp. 1027
+2. Remove/Install the Wingsp. 1027
A. Equipmentp. 1027
B. Remove the Wingsp. 1027
C. Install the Wingsp. 1031
3. Install a Wing Spar Bushing to a New Replacement Wingp. 1033
+4. Bolt Playp. 1034
A. Radial Playp. 1034
B. Axial Playp. 1034
+57-50 – Flapsp. 1037
1. Generalp. 1037
+2. Descriptionp. 1037
A. Top Shellp. 1037
B. Bottom Shellp. 1037
C. End Ribsp. 1037
D. Flap Hornp. 1037
E. Flap Hingesp. 1037
+Flaps – Maintenance Practicesp. 1039
1. Generalp. 1039
+2. Remove/Install the Flapp. 1039
A. Remove the Flapp. 1039
B. Install the Flapp. 1040
+57-60 – Aileronsp. 1043
1. Generalp. 1043
+2. Descriptionp. 1043
A. Top Shellp. 1043
B. Bottom Shellp. 1043
C. End Ribsp. 1043
D. Aileron Hornp. 1043
E. Aileron Hingesp. 1043
+Ailerons – Maintenance Practicesp. 1045
1. Generalp. 1045
+2. Remove/Install the Aileronp. 1045
A. Remove the Aileronp. 1045
B. Install the Aileronp. 1045
+CHAPTER 61-00 PROPELLERp. 1047
+Propellerp. 1051
+61-10 – Propeller Assemblyp. 1053
1. Generalp. 1053
+2. Descriptionp. 1053
A. Deletedp. 1053
B. Sensenich W69EK7-63, W69EK7-63G and W69EK-63 Propellerp. 1053
+propeller assembly – troubleshootingp. 1055
+propeller Assembly – MAINTENANCE PRACTICESp. 1057
1. Generalp. 1057
2. Deletedp. 1057
+3. Remove/Install the Sensenich Propellerp. 1057
A. Remove the Sensenich W69EK-63, W69EK7-63 or W69EK7-63G Propellerp. 1057
B. Install the Sensenich W69EK-63, W69EK7-63 or W69EK7-63G Propellerp. 1058
+CHAPTER 71-00 POWER PLANTp. 1063
+Power Plantp. 1067
1. Generalp. 1067
+2. Description and Operationp. 1069
A. Cowlingp. 1069
B. Engine Mounting Framep. 1069
C. Electrical Harnessp. 1069
D. Air Intakesp. 1069
E. Heat-Shieldp. 1069
F. Engine Drain Pipesp. 1069
3. Engine Specificationsp. 1070
+Power Plant – Troubleshootingp. 1073
+Power Plant – Maintenance Practicesp. 1075
1. Generalp. 1075
+2. Remove/Install the Enginep. 1075
A. Equipmentp. 1075
B. Remove the Enginep. 1077
C. Install the Enginep. 1087
+71-10 – Cowlingp. 1097
1. Generalp. 1097
2. Descriptionp. 1097
+Cowling – Troubleshootingp. 1099
+Cowling – Maintenance Practicesp. 1101
1. Generalp. 1101
+2. Remove/Install the Cowlingsp. 1101
A. Remove the Cowlingsp. 1101
B. Install the Cowlingsp. 1101
3. High Temperature Paint Repair of a Cowlingp. 1102
+71-20 – Mountsp. 1107
1. Generalp. 1107
2. Descriptionp. 1107
+Mounts – Maintenance Practicesp. 1109
1. Generalp. 1109
+2. Remove/Install the Engine Mounting Framep. 1109
A. Remove the Engine Mounting Framep. 1109
B. Install the Engine Mounting Framep. 1110
+71-60 – Air Intakesp. 1113
1. Generalp. 1113
2. Descriptionp. 1113
+Air Intakes – Maintenance Practicesp. 1115
1. Generalp. 1115
+2. Remove/Install the Air Intakep. 1115
A. Remove the Air Intakep. 1115
B. Install the Air Intakep. 1116
+71-70 – Engine Drainsp. 1117
1. Generalp. 1117
+2. Descriptionp. 1117
A. Fuel Distribution Manifold Drainp. 1117
B. Cylinder Drainp. 1117
C. Fuel Pump Drainp. 1117
+Engine Drains – Troubleshootingp. 1121
+Engine Drains – Maintenance Practicesp. 1123
1. Generalp. 1123
+2. Remove/Install the Fuel Distribution Manifold Drainp. 1123
A. Remove the Fuel Distribution Manifold Drainp. 1123
B. Install the Fuel Distribution Manifold Drainp. 1123
+3. Remove/Install The Cylinder Drainp. 1124
A. Remove the Cylinder Drainp. 1124
B. Install the Cylinder Drainp. 1124
+4. Remove/Install the Fuel Pump Drainp. 1125
A. Remove the Fuel Pump Drainp. 1125
B. Install the Fuel Pump Drainp. 1125
+CHAPTER 72-00 ENGINEp. 1127
+Enginep. 1131
1. Generalp. 1131
2. Descriptionp. 1131
+CHAPTER 73-00 ENGINE FUEL AND CONTROLp. 1133
+Engine Fuel and Controlp. 1137
1. Generalp. 1137
+2. Descriptionp. 1137
A. Engine Fuel Controlp. 1137
B. Indicationp. 1138
C. Fuel Hoses in the Engine Compartmentp. 1138
+Engine Fuel and Control – Troubleshootingp. 1143
+Engine Fuel and Control – Maintenance Practicesp. 1145
1. Generalp. 1145
+2. Remove/Install the Induction Air Filterp. 1145
A. Remove the Induction Air Filterp. 1145
B. Install the Induction Air Filterp. 1145
+3. Remove/Install the Fuel Pressure Sensorp. 1146
A. Remove the Fuel Pressure Sensorp. 1146
B. Install the Fuel Pressure Sensorp. 1147
+4. Remove/Install the Fuel Pressure Indicatorp. 1148
A. Remove the Fuel Pressure Indicatorp. 1148
B. Install the Fuel Pressure Indicatorp. 1148
5. Fuel Pressure Indicator Functional Testp. 1149
6. Engine Fuel System Bleeding Procedurep. 1149
+CHAPTER 74-00 IGNITIONp. 1153
+Ignitionp. 1157
1. Generalp. 1157
+2. Description and Operationp. 1157
A. Ignition Switchp. 1159
B. Ignition Switch Cablesp. 1159
C. Magnetosp. 1159
D. High Tension Cables (Ignition Harness)p. 1159
E. Spark Plugsp. 1159
+Ignition – Troubleshootingp. 1161
+Ignition – Maintenance Practicesp. 1163
1. Generalp. 1163
2. Ignition Switch Testp. 1163
+3. Remove/Install the Ignition Switch (Pre-SB DAC1-74-03 Rev 2)p. 1164
A. Remove the Ignition Switchp. 1164
B. Install the Ignition Switchp. 1165
+4. Remove/Install the Ignition Switch (Optional) (Post-SB DAC1-74-03 Rev 2)p. 1166
A. Remove the Ignition Switchp. 1166
B. Install the Ignition Switchp. 1166
+5. Remove/Install the Ignition Switch Cablesp. 1167
A. Remove the Ignition Switch Cablesp. 1168
B. Install the Ignition Switch Cablesp. 1168
+6. Remove/Install the Spark Plug Leadsp. 1169
A. Remove the Spark Plug Leadsp. 1170
B. Install the Spark Plug Leadsp. 1171
+CHAPTER 75-00 AIRp. 1175
+Air Coolingp. 1179
1. Generalp. 1179
+2. Descriptionp. 1179
A. Apron Bafflep. 1179
B. LH and RH Bafflesp. 1179
C. LH Aft and RH Aft Bafflesp. 1179
D. Aft Bafflep. 1179
E. Winter Kit Bafflesp. 1179
+AIr cooling – Maintenance Practicesp. 1181
1. Generalp. 1181
+2. Remove/Install the Bafflesp. 1181
A. Remove the Bafflesp. 1181
B. Install the Bafflesp. 1185
+CHAPTER 76-00 ENGINE CONTROLSp. 1193
+Engine Controlsp. 1197
1. Generalp. 1197
+2. Description and Operationp. 1197
A. Throttlep. 1197
B. Mixture Controlp. 1199
C. Alternate Airp. 1199
D. Friction Adjusterp. 1200
+Engine Controls – Troubleshootingp. 1201
+Engine Controls – Maintenance Practicesp. 1203
1. Generalp. 1203
+2. Remove/Install The Throttle Bowden Cablep. 1203
A. Remove the Throttle Bowden Cablep. 1203
B. Install the Throttle Bowden Cablep. 1207
+3. Remove/Install the Mixture Control Bowden Cablep. 1209
A. Remove the Mixture Control Bowden Cablep. 1209
B. Install the Mixture Control Bowden Cablep. 1212
+4. Remove/Install the Alternate Air Control Bowden Cablep. 1216
A. Remove the Alternate Air Control Bowden Cablep. 1216
B. Install the Alternate Air Control Bowden Cablep. 1218
+5. Throttle/Mixture Control Range Of Movement Testp. 1223
A. Throttle Control Range Of Movement Testp. 1223
B. Mixture Control Range of Movement Testp. 1225
6. Alternate Air Control Range of Movement Testp. 1228
+CHAPTER 77-00 ENGINE INDICATINGp. 1231
+Engine Indicatingp. 1235
1. Generalp. 1235
+2. Descriptionp. 1235
A. RPM Indicatorp. 1235
B. Cylinder Head Temperature (CHT)p. 1235
C. Exhaust Gas Temperature (EGT)p. 1235
D. Tanis Engine Preheat System (Optional)p. 1236
+Engine Indicating – Troubleshootingp. 1239
+Engine Indicating – Maintenance Practicesp. 1241
1. Generalp. 1241
+2. Remove/Install the RPM Indicatorp. 1241
A. Remove the RPM Indicatorp. 1241
B. Install the RPM Indicatorp. 1242
+3. Remove/Install the RPM Indicator Flexible Drivep. 1242
A. Remove the RPM Indicator Flexible Drivep. 1242
B. Install the RPM Indicator Flexible Drivep. 1243
+4. Remove/Install the Cylinder Head Temperature (CHT) Thermocouple Probep. 1244
A. Remove the CHT Thermocouple Probep. 1244
B. Install the CHT Thermocouple Probep. 1244
+5. Remove/Install the Exhaust Gas Temperature (EGT) Thermocouple Probe
A. Remove the EGT Thermocouple Probe
B. Install the EGT Thermocouple Probe
+6. Remove/Install The Exhaust Gas Temperature (EGT) Indicator
A. Remove the EGT Indicator
B. Install the EGT Indicator
+7. Remove/Install the Cylinder Head Temperature Indicator
A. Remove the CHT Indicator
B. Install the CHT Indicator
+8. Remove/Install the Tanis Engine Preheat System (Optional)p. 1249
A. Remove the Tanis Engine Preheat Systemp. 1249
B. Install the Tanis Engine Preheat Systemp. 1249
+CHAPTER 78-00 EXHAUSTp. 1251
+Exhaustp. 1255
1. Generalp. 1255
2. Descriptionp. 1255
+Exhaust – Troubleshootingp. 1257
+Exhaust – Maintenance Practicesp. 1259
1. Generalp. 1259
+2. Remove/Install the Exhaustp. 1259
A. Remove the Exhaustp. 1259
B. Install the Exhaustp. 1260
+CHAPTER 79-00 OILp. 1263
+Oil Systemsp. 1267
1. Generalp. 1267
2. Description and Operationp. 1267
+Oil Systems – Troubleshootingp. 1273
+Oil Systems – Maintenance Practicesp. 1275
1. Generalp. 1275
+2. Remove/Install the Engine Oil Filterp. 1276
A. Remove the Engine Oil Filterp. 1276
B. Install the Engine Oil Filterp. 1276
+3. Remove/Install the Oil Coolerp. 1277
A. Remove the Oil Coolerp. 1277
B. Install the Oil Coolerp. 1278
+4. Remove/Install the Vernatherm Valvep. 1279
A. Remove the Vernatherm Valvep. 1279
B. Install the Vernatherm Valvep. 1279
+5. Remove/Install the Oil Temperature Sensorp. 1280
A. Remove the Oil Temperature Sensorp. 1280
B. Install the Oil Temperature Sensorp. 1280
+6. Remove/Install the Oil Pressure Sensorp. 1281
A. Remove the Oil Pressure Sensorp. 1281
B. Install the Oil Pressure Sensorp. 1281
+7. Remove/Install the Events Switchp. 1282
A. Remove the Events Switchp. 1282
B. Install the Events Switchp. 1282
+8. Remove/Install the Oil Pressure Indicator
A. Remove the Oil Pressure Indicator
B. Install the Oil Pressure Indicator
+9. Remove/Install the Oil Temperature Indicator
A. Remove the Oil Temperature Indicator
B. Install the Oil Temperature Indicator
+10. Remove/Install the Air/Oil Separatorp. 1285
A. Remove the Air/Oil Separatorp. 1285
B. Install the Air/Oil Separatorp. 1285
+11. Remove/Install the Air/Oil Separator Ventp. 1286
A. Remove the Air/Oil Separator Ventp. 1286
B. Install the Air/Oil Separator Ventp. 1286
+CHAPTER 80-00 STARTINGp. 1287
+Startingp. 1291
1. Generalp. 1291
2. Description and Operationp. 1291
+Starting – Troubleshootingp. 1293
+Engine Starting – Maintenance Practicesp. 1295
1. Generalp. 1295
2. Starting Vibrator Battery Testp. 1295
+3. Remove/Install The Starting Vibrator Batteryp. 1295
A. Remove the Starting Vibrator Batteryp. 1295
B. Install the Starting Vibrator Batteryp. 1296
+CHAPTER 92-00 WIRING DIAGRAMSp. 1297
Table of Contentsp. 1297
+Wiring Diagramsp. 1303
+List of Wiring Diagrams/Schematicsp. 1303
Delivery is instant. The Diamond DA20-C1 Aircraft Maintenance Manual DA201-C1 Rev 22 arrives as a PDF download immediately after checkout, with no shipping and no waiting for a printed copy. Open it on a laptop, tablet or phone in the hangar, search or scroll to the chapter you need, and print the pages you want to take to the aircraft. Whether you are running a 100 hour check, chasing a generator that will not come on line, replacing a canopy latch, installing an avionics upgrade or assessing composite damage, this DA20-C1 AMM keeps the procedure and the numbers in front of you.
Reviews
There are no reviews yet.