Diamond DA42 L360 Aircraft Maintenance Manual Supplement – D42L-AMM-001 Rev 5 (2012) PDF
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Complete maintenance supplement for the Diamond DA42 L360 aircraft converted to Lycoming IO-360/LIO-360 engines. Covers systems modified by STC SA09-54 including power plant, fuel, ignition, electrical, and flight controls. Essential for licensed mechanics and maintenance facilities.
Description
Diamond DA42 L360 Aircraft Maintenance Manual Supplement – D42L-AMM-001 Rev 5 (2012)
File Details
- Manual Type: Aircraft Maintenance Manual (Supplement)
- Document Number: D42L-AMM-001
- Revision: 5
- Publication Date: October 2012
- Language: English
- Page Count: 648 Pages
- Format: PDF
- Applicability: Diamond DA42 L360 aircraft modified under TCCA STC No. SA09-54 (FAA STC No. SA02725NY) with Lycoming IO-360-M1A (LH) and LIO-360-M1A (RH) engines.
The Diamond DA42 L360 Aircraft Maintenance Manual Supplement – D42L-AMM-001 Rev 5 (2012) is the definitive maintenance guide for the Lycoming-powered DA42 L360. This supplement provides all necessary instructions for the systems and components altered by the Supplemental Type Certificate (STC) No. SA09-54. It must be used in conjunction with the original DA42 TDI AMM (Document Number 7.02.01) for complete aircraft coverage.
Chapters Covered
This supplement focuses exclusively on the modifications introduced by the Lycoming STC. The following chapters contain data specific to the DA42 L360:
- Chapter 03-00: General Description of the Aircraft (STC-specific changes)
- Chapter 04-00: Airworthiness Limitations (Mandatory inspections for new components)
- Chapter 05-00: Time Limits and Maintenance Checks (25, 50, 100, 200, 1000, 2000-hour checks)
- Chapter 06-00: Dimensions and Areas (Adjustment report data)
- Chapter 11-00: Placards and Markings (Interior and exterior placards)
- Chapter 12-00: Servicing (Fuel, oil, and lubrication schedules)
- Chapter 20-00: Standard Practices (Torque values for AN, DIN, and LN fasteners)
- Chapter 24-00: Electrical Power (DC Generation, alternator, voltage regulator, battery)
- Chapter 25-00: Equipment and Furnishings (Ballast installation)
- Chapter 27-00: Flight Controls (Rudder, elevator, flaps, variable elevator stop system)
- Chapter 28-00: Fuel (Distribution, gascolator, booster pump, cross-feed)
- Chapter 30-00: Ice Protection System (Propeller de-icing)
- Chapter 31-00: Indicating Systems (G1000 integrated cockpit, GEA 71)
- Chapter 32-00: Landing Gear (Position and warning micro-switch rigging)
- Chapter 51-00: Standard Practices – Structures (Electrical bonding system)
- Chapter 55-00: Stabilizers (Rudder trim seal)
- Chapter 61-00: Propeller (MT three-blade propeller, governor, accumulator)
- Chapter 71-00: Power Plant (Engine removal/installation, cowling, mounts, air intakes, drains)
- Chapter 72-00: Engine (Lycoming IO-360 M1A / LIO-360 M1A description)
- Chapter 73-00: Engine Fuel and Control (Fuel injector, flow divider, nozzles)
- Chapter 74-00: Ignition (Dual magnetos, SlickSTART booster, ignition switch)
- Chapter 75-00: Air (Cooling baffle assembly)
- Chapter 76-00: Engine Controls (Throttle and mixture Bowden cables)
- Chapter 77-00: Engine Indicating (Sensors for EGT, CHT, oil pressure, fuel pressure, etc.)
- Chapter 78-00: Exhaust (Power Flow Systems exhaust, heat exchanger)
- Chapter 79-00: Oil (Oil cooler, NACA duct)
- Chapter 80-00: Starting (Starter relay, Sky-Tech starter)
- Chapter 92-00: Wiring Diagrams (Full schematics for the modified electrical system)
Complete Bookmarks
The complete bookmarks in the “Diamond DA42 L360 Aircraft Maintenance Manual Supplement – D42L-AMM-001 Rev 5 (2012) PDF” are as follows:
+DA42 L360 – AIRCRAFT MAINTENANCE MANUALp. 1
+FRONT MATTERp. 23
+CHAPTER 01-00 – INTRODUCTIONp. 25
+Introductionp. 29
+4. Manual Configurationp. 30
+CHAPTER 03-00 – GENERAL DESCRIPTION OF THE AIRCRAFTp. 35
+General Description of the Aircraftp. 39
+CHAPTER 04-00 – AIRWORTHINESS LIMITATIONSp. 43
+Airworthiness Limitationsp. 47
+1. Airworthiness Limitationsp. 49
+CHAPTER 05-00 – TIME LIMITS AND MAINTENANCE CHECKSp. 51
+05-10 – Time Limitsp. 55
+4. Component Time Limitsp. 56
+05-20 – Scheduled Maintenance Checksp. 59
+05-20 – Scheduled Maintenance Checks – Maintenance Practicesp. 61
+4. Maintenance of Checklist Zonesp. 63
+CHAPTER 06-00 – DIMENSIONS AND AREASp. 79
+Dimensions and Areasp. 83
+CHAPTER 11-00 – PLACARDS AND MARKINGSp. 87
+Description and Operationp. 91
+2. Replace Plastic Placardsp. 91
+11-20 Exterior Placards and Markingsp. 93
+11-30 Interior Placards and Markingsp. 95
+Maintenance Practicesp. 101
+CHAPTER 12-00 – SERVICINGp. 103
+servicingp. 107
+12-10 – Replenishingp. 109
+2. Fuel Systemp. 109
+3. Fuel Contamination Testp. 111
+4. Engine Oil Systemp. 112
+12-20 – Scheduled Servicingp. 117
+CHAPTER 20-00 – STANDARD PRACTICESp. 121
+20-10 – Standard Practices – Airframep. 125
+2. Bolt and Nut Types Used in the Aircraftp. 125
+3. Standard Torque Valuesp. 126
+20-70 – Enginesp. 129
+CHAPTER 24-00 – ELECTRICAL POWERp. 133
+Description and Operationp. 137
+2. Electrical System Description and Operationp. 137
+24-30 – DC Generationp. 143
+1. Generalp. 143
+2. Description and Operationp. 143
+Troubleshootingp. 145
+Maintenance Practicesp. 147
+4. Remove/Install an Alternatorp. 149
+5. Remove/Install a Voltage Regulatorp. 151
+8. Removal/Installation of EMI Filterp. 154
+24-31 – Battery Systemsp. 159
+Troubleshootingp. 161
+CHAPTER 25-00 – EQUIPMENT AND FURNISHINGSp. 163
+Nose Forward ballast – Description and Operationp. 167
+Nose Forward Ballast – Maintenance Practicesp. 169
+2. Remove/Install the Ballast Plate Assemblies and Clampsp. 169
+CHAPTER 27-00 – FLIGHT CONTROLSp. 173
+27-20 – Flight Controls – Rudderp. 177
+Maintenance Practicesp. 183
+2. Rudder Control System Test for Correct Range of Movementp. 183
+3. Rudder Control System Adjustmentsp. 184
+4. Remove/Install the Rudder Control Cablesp. 187
+5. Rudder System Control Forces Testp. 193
+27-21 – Flight Controls – Rudder Trimp. 203
+Maintenance Practicesp. 205
+3. Rudder Trim Rigging Procedurep. 206
+27-30 Flight Controls – Elevatorp. 215
+Maintenance Practicesp. 217
+2. Elevator Control System Test for Correct Range of Movementp. 217
+3. Elevator Control System Adjustmentsp. 219
+4. Remove/Install the Variable Elevator Stop Assemblyp. 220
+5. Test/Adjust the Variable Elevator Stopp. 222
+27-50-00 – Flaps – Maintenance Practicesp. 235
+CHAPTER 28-00 – FUELp. 237
+Description and Operationp. 241
+3. Operationp. 241
+28-20 – Fuel Distribution – Description and Operationp. 245
+2. Fuel Distribution System Componentsp. 245
+Maintenance Practicesp. 249
+2. Clean/Examine a Fuel Sediment Bowlp. 249
+4. Remove/Install a Fuel Booster Pumpp. 251
+6. Remove/Install the FUEL PUMP Switch (Pre-SB D42L-28-01)p. 256
+7. Remove/Install the Illuminated FUEL PUMP Switch and the Current Monitor (Post-SB D42L-28-01 – Optional Installation)p. 257
+CHAPTER 30-00 – ICE PROTECTION SYSTEMp. 265
+Description and Operationp. 269
+CHAPTER 31-00 – INDICATING SYSTEMSp. 273
+Decription and Operationp. 277
+31-10 – Instrument and Control Panels – Description and Operationp. 279
+31-40 – Central Computers – Description and Operations
+Central Computer – Maintenance Practicesp. 285
+2. Remove/Install the GEA 71 Processorp. 285
+3. G1000 System Software Load Procedurep. 286
+CHAPTER 32-00 – LANDING GEARp. 289
+32-60 – Position and Warning – Description and Operationp. 293
+Position and Warning – Maintnance Practicesp. 295
+CHAPTER 51-00 – STANDARD PRACTICES – STRUCTURESp. 301
+51-80 – Electrical Bonding – Description and Operationp. 305
+Electrical Bonding – Maintenance Practicesp. 307
+2. Test the Electrical Bonding Systemp. 307
+CHAPTER 55-00 – STABILIZERSp. 313
+55-40-00 – Rudder and Trim Tab – Description and Operationp. 317
+Maintenance Practicesp. 319
+2. Remove/Install the Rudder Trim Sealp. 319
+CHAPTER 61-00 – PROPELLERp. 321
+Description and Operationp. 325
+61-10 – Propeller Assembly – Description and Operationp. 327
+2. Description and Operation of MT Propellerp. 327
+Troubleshootingp. 331
+Maintenance Practicesp. 333
+2. Remove/Install the MT Propellerp. 333
+3. Propeller Blade Tracking Testp. 336
+61-20 – Propeller Control – Description and Operationp. 339
+2. Description and Operationp. 339
+Troubleshootingp. 343
+Propeller Control – Maintenance Practicesp. 345
+2. Remove/Install the Propeller Governorp. 345
+3. Remove/Install the Propeller Un-Feathering Accumulatorp. 348
+CHAPTER 71-00 – POWER PLANTp. 361
+Description and Operationp. 367
+2. Description and Operationp. 368
+Troubleshootingp. 373
+Power Plant – Maintenance Practicesp. 375
+2. Remove the Engine (Without the Engine Mount)p. 375
+3. Install the Engine (Without the Engine Mount)p. 382
+4. Engine Test – Generalp. 390
+6. Measure/Adjust Engine Parametersp. 393
+71-10-00 – Cowling – Description and Operationp. 405
+Troubleshootingp. 409
+Cowling – Maintenance Practicesp. 411
+2. Remove/Install the Engine Cowlingsp. 411
+3. Remove/Install the Winter Kit bafflesp. 414
+4. Cleaning and Paintingp. 415
+71-20 – Engine Mounting – Description and Operationp. 417
+Troubleshootingp. 419
+Maintenance Practicesp. 421
+2. Remove/Install an Engine Mountp. 421
+71-50 – Electrical Cables in the Engine Compartment – Description and Operationp. 423
+71-60 – Air Intakes – Description and Opeartionp. 427
+2. Descriptionp. 427
+Troubleshootingp. 431
+Maintenance Practicesp. 433
+2. Remove/Install an Air Filterp. 433
+3. Remove/Install an Alternate Air Valvep. 434
+4. Remove/Install an Alternate Air Control Inner Cablep. 436
+5. Adjust an Alternate Air Valve Control Cablep. 441
+71-70 – Engine Drains – Description and Operationp. 445
+2. Descriptionp. 445
+3. Operationp. 446
+A. Engine Driven Fuel Pump Drainp. 446
+Troubleshootingp. 449
+Maintenance Practicesp. 451
+2. Remove/Install the Engine Driven Fuel Pump Drainp. 451
+3. Remove/Install Fuel Flow Divider Drainp. 452
+4. Remove/Install the Induction Manifold Drainp. 453
+CHAPTER 72-00 – ENGINEp. 455
+Description and Operationp. 459
+2. Descriptionp. 459
+Troubleshootingp. 463
+Engine – Maintenance Practicesp. 465
+2. Cylinder Compression Testp. 465
+CHAPTER 73-00 – ENGINE FUEL AND CONTROLp. 469
+Description and Operationp. 473
+2. Description and Operationp. 473
+Troubleshootingp. 477
+Maintenance Practicesp. 479
+2. Remove/Install the Fuel Injectorp. 479
+CHAPTER 74-00 – IGNITIONp. 485
+Description and Operationp. 489
+3. Ignition System Componentsp. 490
+4. Operationp. 492
+Troubleshootingp. 495
+Maintenance Practicesp. 497
+2. Remove/Install an Engine Ignition Switchp. 497
+3. Remove/Install a Start Booster Control Unitp. 499
+CHAPTER 75-00 – AIRp. 503
+Description and Operationp. 507
+Maintenance Practicesp. 509
+2. Remove/Install a Component of the Baffle Assemblyp. 509
+CHAPTER 76-00 – ENGINE CONTROLSp. 519
+Description and Operationp. 523
+2. Description and Operationp. 523
+Troubleshootingp. 529
+Maintenance Practicesp. 531
+2. Remove/Install a Throttle Control Bowden Cablep. 531
+3. Remove/Install a Mixture Control Bowden Cablep. 537
+4. Throttle/Mixture Control Range of Movement Testp. 543
+CHAPTER 77-00 – ENGINE INDICATING SYSTEMSp. 549
+Description and Operationp. 553
+77-40 – Engine Indicating System – Description and Operationp. 555
+2. Description and Operationp. 555
+Troubleshootingp. 557
+Maintenance Practicesp. 559
+CHAPTER 78-00 – EXHAUSTp. 579
+Description and Operationp. 583
+Troubleshootingp. 585
+Maintenance Practicesp. 587
+2. Remove/Install an Engine Exhaust Systemp. 587
+CHAPTER 79-00 – OILp. 593
+Description and Operationp. 597
+Troubleshootingp. 599
+Maintenance Practicesp. 601
+2. Remove/Install an Engine Oil Coolerp. 601
+CHAPTER 80-00 – STARTINGp. 603
+Description and Operationp. 607
+2. Descriptionp. 607
+Troubleshootingp. 611
+Maintenance Practicesp. 613
+2. Remove/Install an Engine Start Relayp. 613
+3. Remove/Install an Engine Starterp. 614
+CHAPTER 92-00 – WIRING DIAGRAMSp. 619
+Wiring Diagramsp. 623
This Diamond DA42 L360 Aircraft Maintenance Manual Supplement gives a licensed A&P mechanic or maintenance organization all the data required to maintain the Lycoming IO-360 engine installation. It includes detailed removal/installation steps for major components like the engine, propeller, fuel pumps, alternator, and starter. Step-by-step procedures cover system adjustments, rigging checks, and functional tests. Comprehensive wiring diagrams (Chapter 92) and electrical schematics support accurate troubleshooting of the G1000 avionics and aircraft systems.
The supplement lists all mandatory Service Bulletins and Temporary Revisions applicable to the DA42 L360, ensuring your maintenance records remain current. It provides torque tables for AN, DIN, and LN fasteners, engine-specific torque values, and the airworthiness limitations required by TCCA and FAA regulations (Secs. 43.16 and 91.403). With this manual, you can confidently perform everything from a 25-hour engine check to a 2000-hour structural inspection.
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Why This Manual Is Essential
This Diamond DA42 L360 AMM Supplement is not a generic manual; it is the specific document required to maintain the STC-modified aircraft. Without it, you lack the correct procedures for the Lycoming engines, the MT propellers, the revised fuel and ignition systems, and the unique variable elevator stop. This manual protects your aircraft’s airworthiness, ensures compliance with all mandatory inspections, and provides the precision required for safe aircraft operation.
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Your purchase provides a single, high-quality PDF file exactly as published by Diamond Aircraft Industries. Download it immediately after payment, view it on any computer, tablet, or smartphone, and print specific sections for use in the hangar or workshop. No physical shipping, no waiting, and no handling fees.
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