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01-CONTENTS
Introduction
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CHAPTER 01
INTRODUCTION
1. General
This Airplane Maintenance Manual contains the data necessary to do the maintenance of the DA 40. It contains a full description of the systems, trouble shooting procedures, removal and installation procedures and maintenance instructions. It does not contain maintenance data for components removed from the airplane (maintenance Shop data).
The Airplane Maintenance Manual contains wiring diagrams for the electrical system. Use these manuals with the Airplane Maintenance Manual, and the related Service Bulletins: ) The DA 40 Illustrated Parts Catalogue. ) The DA 40 Airplane Flight Manual. ) The ELT Manufacturer’s Operator’s Manual. %) The TAE 125 Operation and Maintenance Manual, if the TAE engine is installed. %) The Textron Lycoming Operator’s Manual, if the Lycoming engine is installed. %) The Slick Maintenance Manual, if the Lycoming engine is installed. ) The mt-Propeller Owner’s Manual. %) The mt-Propeller Operation and Installation Manual for the hydraulic constant speed governor.
2. Revision Service
The manufacturer provides a revision service for the Airplane Maintenance Manual. The revision shows design changes to the airplane or changes in procedures. Each page of the manual shows the date of first issue. If the page has changed, it shows the date of the revision.
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3. Warnings, Cautions and Notes
Obey all the usual safety precautions and maintenance instructions when doing maintenance.
This Airplane Maintenance Manual also contains warnings, cautions and notes before applicable
instructions:
WARNING: A WARNING TELLS THE PERSON DOING THE MAINTENANCE THAT INJURY OR DEATH IS POSSIBLE IF THEY DO NOT FOLLOW THE INSTRUCTIONS.
CAUTION: A CAUTION TELLS THE PERSON DOING THE MAINTENANCE THAT DAMAGE TO EQUIPMENT IS POSSIBLE IF THEY DO NOT FOLLOW THE INSTRUCTIONS.
Note: A Note tells the person doing the maintenance how to make the task easier.
4. Manual Configuration
This manual is written using the regulations of the Air Transport Association of America Specification 100 (ATA 100). Each system is given a chapter number from the ATA 100. Where applicable, a chapter contains sections for each sub-system.
The Specification AECMA Simplified English has been used to write this Airplane Maintenance Manual. This is a mandatory requirement of the Air Transport Association of America Specification 100 (ATA 100).
There are only 3 sources of words available to use in Simplified English (SE).
) Approved words from the SE Guide. These have defined meanings and selected parts of speech.
) Technical names as defined in the SE Guide. Used only as Adjectives or Nouns.
) Manufacturing processes as defined in the SE Guide. Always used as Verbs.
To obtain a copy of the SE Guide contact: AECMA Gulledelle 94, B-1200 Bruxelles, Belgium. Tel: +32-2775-81-10, Fax: +32-2775-81-11.
This manual does not use the ATA 100 Aircraft Maintenance Task Oriented Support System (AMTOSS) or the ATA 100 Production Management Data Base (PMDB).
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A. The ATA100 Numbering System
The ATA100 numbering system uses 3 pairs of numbers, for example:
57-50-xx
Chapter / System Section / Subsystem Unit / Subject Number (Wings) (Flaps) (Not normally used)
The first pair of numbers show the system. System 57 is the Wings. Chapter 57 contains the data for the wings.
The second pair of numbers show the subsystem. Subsystem 50 is Flaps. Chapter 57, section 50 contains the data for the flaps installation.
The third pair of numbers show a unit. A unit could be the flap itself. Only complex systems use unit numbers.
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