Diamond DA42 L360 Aircraft Maintenance Manual Supplement – D42L-AMM-001 Rev 5 (2012) PDF

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)

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.

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.

Instant PDF Delivery

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.