Diamond DA20-A1 Aircraft Maintenance Manual Revision 15 (DA201 AMM) PDF Download

Description

Diamond DA20-A1 Aircraft Maintenance Manual Revision 15 – The Complete DA201 AMM

This is the full Diamond DA20-A1 Aircraft Maintenance Manual, Revision 15, issued as document DA 201 by Diamond Aircraft Industries Inc. of London, Ontario. The DA20-A1 AMM follows ATA Specification No. 100 and delivers the maintenance, troubleshooting, removal and installation, adjustment and inspection data needed to keep the DA20-A1 composite two-seat light aircraft in airworthy condition. Revision 15 carries the 18 June 2012 issue date and folds in the engineering changes, service bulletins and temporary revisions current at that time.

File Details

• Manual type: Aircraft Maintenance Manual (AMM)
• Manufacturer: Diamond Aircraft Industries Inc., London, Ontario, Canada
• Aircraft model: DA20-A1
• Document number: DA 201
• Revision: Revision 15
• Revision date: 18 June 2012
• Language: English
• File format: PDF
• Page count: Approximately 605 pages
• Layout standard: ATA Specification No. 100

Chapters Covered in This DA20-A1 Maintenance Manual

• 01-00 Introduction
• 02-00 Organization and Handling of the Manual
• 03-00 General Description of the Aircraft
• 04-00 Airworthiness Limitations (04-10 Life Limited Parts, 04-20 Paint Finish)
• 05-00 Time Limits and Maintenance Checks (05-10 Time Limits, 05-20 Scheduled Maintenance Checks, 05-30 General Inspections, 05-40 Unscheduled Inspections)
• 06-00 Dimensions and Areas
• 07-00 Lifting and Shoring (07-10 Lifting, 07-20 Jacking)
• 08-00 Leveling and Weighing
• 09-00 Towing and Taxiing
• 10-00 Parking and Mooring (10-10 Parking, 10-20 Mooring, 10-30 Parking Duration)
• 11-00 Required Placards (11-10 Location of Placards)
• 12-00 Servicing (12-10 Replenishing, 12-20 Scheduled Servicing, 12-30 Unscheduled Servicing)
• 20-00 Standard Practices – Airframe
• 21-00 Environmental Systems (21-20 Distribution, 21-40 Heating)
• 23-00 Communications (23-10 Speech Communication Bendix/King KX125)
• 24-00 Electrical Power (24-30 DC Generation, 24-31 Battery System, 24-50 Electric Load Distribution)
• 25-00 Equipment and Furnishings (25-10 Flight Compartment, 25-50 Baggage Compartment)
• 27-00 Flight Controls (27-10 Aileron Control Systems, 27-11 Main Column, 27-20 Rudder Control Systems, 27-30 Elevator Control System, 27-40 Elevator Trim System, 27-50 Wing Flaps)
• 28-00 Fuel (28-10 Storage Tank, 28-20 Distribution, 28-40 Indicating)
• 31-00 Indicating and Recording Systems (31-10 Instrument Panel)
• 32-00 Landing Gear (32-10 Main Landing Gear, 32-20 Nose Landing Gear, 32-40 Wheels and Brakes)
• 33-00 Lights (33-10 Interior, 33-40 Exterior)
• 34-00 Navigation and Pitot Static (34-10 Pitot Static, 34-12 Stall Warning System, 34-20 Attitude and Direction, 34-50 Position Determining Systems)
• 51-00 Structures (51-10 Repair of Composite Parts, 51-20 Repair of Metal Parts)
• 53-00 Fuselage (53-10 Main Frame, 53-11 Canopy, 53-31 Inspection Holes)
• 55-00 Stabilizers (55-10 Horizontal Stabilizer, 55-20 Elevator, 55-30 Rudder)
• 57-00 Wings (57-10 Wing Structure, 57-50 Wing Flaps, 57-60 Ailerons)
• 61-00 Propeller
• 71-00 Power Plant (71-10 Cowling, 71-20 Mounts, 71-60 Air Intakes and Guides)
• 75-00 Engine Cooling
• 76-00 Engine Controls
• 77-00 Engine Indicating
• 78-00 Exhaust
• 79-00 Oil Systems (79-21 Oil Radiator, 79-30 Indicating)
• 92-00 Wiring Diagrams (92-10 System Schematics, 92-30 Avionics Schematics)

Read as a whole, the DA201 AMM gives a technician a single controlled document for every task on the airplane. Each chapter is split into a description and function section, troubleshooting tables, then a maintenance block covering ground service, removal and installation, adjustment and test, checks and inspections, cleaning and painting, and repairs. Because the DA20-A1 is a fibreglass and carbon composite airframe with a Rotax 912 powerplant, the manual is deliberately explicit about the techniques that matter most on this aircraft – composite layup reference drawings, chamfer ratios for GFRP repairs, coin tap and light test inspection methods, delamination and disbond defect limits, and the specific torque values, service limits and lubrication intervals that keep the airframe and engine within their approved envelopes.

What This Diamond DA20-A1 AMM Lets You Do

• Run the 50, 100, 200, 1000 and 6000 hour inspection checklists with the correct engine, propeller, cabin, structure, landing gear and general inspection steps.
• Service the Rotax 912 engine – oil changes, oil filter replacement, compression tests, spark plug replacement, ignition circuit checks, carburetor heat checks and generator belt checks.
• Remove and install the propeller, spinner and hub assembly using the published torque values and track tolerance.
• Adjust, rig and safety the aileron, elevator, rudder, trim and flap control systems, including push rod eye-end setup and cable pre-tension.
• Repair the composite airframe – GFRP laminate and sandwich repairs, delamination limits, fuselage layup reference, spar repair restrictions and painting.
• Diagnose and fix the landing gear – main and nose gear removal, toe-in, camber and track adjustment, wheel bearings, brake bleeding and the parking brake valve.
• Troubleshoot the electrical system, DC generation, battery system, load distribution, lighting, avionics and instrumentation using the Chapter 92 schematics.
• Perform fuel system checks including the fuel shut off valve and check valve inspection.
• Verify weight and balance, leveling, jacking, towing, mooring and placard requirements.

Why This Revision 15 AMM Matters

Component replacement times, torque values, composite defect limits and rigging tolerances on the DA20-A1 are not guesses. Revision 15 consolidates the latest engineering data, temporary revision TR 05-01 and the incorporated service bulletins – including DA20-32-05, DA20-79-03, DA20-79-08 and DA20-74-01 – so the maintenance you perform is the maintenance the manufacturer actually published. Getting the adjustment report values, cable tensions and control surface travels right is what prevents flutter, premature wear and airworthiness findings down the line.

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Instant PDF Delivery

You receive the Diamond DA20-A1 Aircraft Maintenance Manual Revision 15 immediately after checkout as a PDF. There is nothing to ship and nothing to wait for. Open it on a laptop, tablet or phone in the hangar or at the bench, search the ATA structure for the system you need, and print the pages you want to work from. The complete DA201 AMM, ready when you are.