Diamond Aircraft DA 40 NG Manuale utente

AIRCRAFT

DA 40 NG

AIRPLANE MAINTENANCE MANUAL

AIRCRAFT

Introduction DA 40 NG AMM

This document is protected by copyright. All associated rights, in particular those of translation,

reprinting, radio transmission, reproduction by photo-mechanical or similar means and storing indata

processing facilities, in whole or part, are reserved.

Diamond Aircraft Industries GmbH

N. A. Otto-Str. 5

A-2700 Wiener Neustadt

Austria

Phone: +43-2622-26700

Fax: +43-2622-26780

E-mail: [email protected]

AIRCRAFT

DA 40 NG AMM Table of Contents

Doc # 6.02.15

Rev. 3 CONTENTS Page i

01 Sep 2017

TABLE OF CONTENTS

Ch/Sect Title

01-00 Introduction

02-00 Organization and Handling of the Manual

03-00 General Description of the Airplane

04-00 Airworthiness Limitations

05-00 Time Limits and Maintenance Checks

05-10 Time Limits

05-20 Scheduled Maintenance Checks

05-21 Flight-Line Checks

05-25 Drain Holes Inspection Checklist and Report

05-28 Maintenance Checklist DA 40 NG

05-50 Unscheduled Maintenance Checks

06-00 Dimensions and Areas

07-00 Lifting and Shoring

07-10 Jacking

08-00 Weighing and Levelling

08-10 Weighing

08-20 Levelling

09-00 Towing and Taxiing

09-10 Towing

09-20 Taxiing

10-00 Parking, Mooring, Storage and Return to Service

10-10 Parking and Storage

10-20 Mooring

10-30 Return to Service

11-00 Placards and Markings

11-20 Exterior Placards and Markings

11-30 Interior Placards and Markings

12-00 Servicing

12-10 Replenishing

12-20 Scheduled Servicing

12-30 Unscheduled Servicing

20-00 Standard Practices

20-10 Standard Practices - Airframe

20-30 Standard Practices - Electrical

20-70 Standard Practices - Engine

AIRCRAFT

Table of Contents DA 40 NG AMM

Page ii

01 Sep 2017 CONTENTS Doc # 6.02.15

Rev. 3

21-00 Air Conditioning, Heating and Ventilation

21-50 Cooling

21-51 Cooling (OÄM 40-316/i or later installed)

22-00 Auto Flight

22-10 Autopilot, GFC 700

22-11 Autopilot, KAP 140

23-00 Communications

23-10 Speech Communication with G1000 System Installed

23-11 Speech Communication with Conventional Cockpit Installed

23-50 Audio Integrating with G1000 System Installed

23-51 Audio Integrating with Conventional Cockpit Installed

23-60 Static Discharging

24-00 Electrical Power

24-30 DC Generation

24-31 Battery System

24-32 Emergency Battery System

24-33 Additional Alternator

24-40 External Power

24-60 DC Electrical Load Distribution

25-00 Equipment/Furnishings - General

25-10 Flight Compartment

25-60 Emergency

26-00 Fire Protection

27-00 Flight Controls

27-10 Flight Controls - Ailerons and Tabs

27-20 Flight Controls - Rudder

27-30 Flight Controls - Elevator

27-38 Flight Controls - Elevator Trim

27-39 Stall Warning System

27-50 Flight Controls - Flaps

28-00 Fuel System

28-10 Fuel Storage System

28-20 Fuel Distribution System

28-40 Fuel Quantity Indicating

31-00 Indicating Systems

31-10 Instrument and Control Panels with G1000 System Installed

31-11 Instrument and Control Panels with Conventional Cockpit Installed

31-20 Independent Instruments

31-40 Central Computers

31-51 Central Warning System with Conventional Cockpit Installed

AIRCRAFT

DA 40 NG AMM Table of Contents

Doc # 6.02.15

Rev. 3 CONTENTS Page iii

01 Sep 2017

32-00 Landing Gear

32-10 Main Landing Gear

32-20 Nose Landing Gear

32-40 Wheels and Brakes

33-00 Lights

33-10 Lights - Flight Compartment

33-40 Exterior Lights

34-00 Navigation

34-10 Flight Environment Data

34-20 Attitude and Direction with G1000 System Installed

34-21 Attitude and Direction with Conventional Cockpit Installed

34-22 Magnetic Compass with Conventional Cockpit Installed

34-25 Gyro Instruments with Conventional Cockpit Installed

34-30 Landing and Taxiing Aids with G1000 System Installed

34-31 Landing and Taxiing Aids with Conventional Cockpit Installed

34-40 Independent Position Determining with G1000 System Installed

34-41 Stormscope System with G1000 System Installed

34-42 Traffic Advisory System (TAS)

34-50 Dependent Position Determining with G1000 System Installed

34-51 Dependent Position Determining with Conventional Cockpit Installed

34-52 VOR/Localizer/Glideslope (VOR/LOC/GS) with Conventional Cockpit Installed

34-56 Transponder (XPDR) with Conventional Cockpit Installed

51-00 Standard Practices and Structure

51-10 Investigation

51-20 Repair Processes

51-30 Materials

51-40 Fasteners

51-60 Control Surface Balancing

51-80 Electrical Bonding

52-00 Doors

52-10 Canopy and Passenger Door

52-40 Access Panels

53-00 Fuselage

53-10 Fuselage Structure

55-00 Stabilizers

55-10 Horizontal Stabilizer

55-20 Elevator

55-30 Lower Fin

55-40 Rudder

AIRCRAFT

Table of Contents DA 40 NG AMM

Page iv

01 Sep 2017 CONTENTS Doc # 6.02.15

Rev. 3

56-00 Windows

56-10 Flight Compartment Windows

57-00 Wings

57-10 Wing Structure

57-50 Flaps

57-60 Aileron

61-00 Propeller

61-10 Propeller Assembly

61-20 Propeller Control

71-00 Power Plant

71-10 Engine Cowling

71-20 Engine Mounting

71-50 Electrical Cables in the Engine Compartment

71-60 Air Intakes

71-70 Engine Drains

72-00 Engine

73-00 Engine Fuel and Control

75-00 Liquid Cooling System

76-00 Engine Controls

77-00 Engine Indicating with G1000 System Installed

77-01 Engine Indication with Conventional Cockpit Installed

77-40 Engine Indicating System with G1000 System Installed

77-41 Engine Integrated Instrument System with Conventional Cockpit Installed

78-00 Exhaust

79-00 Oil

80-00 Starting

81-00 Turbo Charger

92-00 Wiring Diagrams

AIRCRAFT

DA 40 NG AMM Record of Revision

Doc # 6.02.15

Rev. 3 ROR Page v

01 Sep 2017

Record of Revision

1. Record of Revision

Use this check list to record and control all of the revisions which you put inthis Airplane Maintenance

Manual(AMM). Put theaffectedpages oftherevisioninto theAMMas soonas youget them.Remove

and destroy the pages which are superseded. Complete the table below when you have put the

revision in the AMM.

Revision

Number Date

Issued Inserted

On Inserted

Original 01 Apr 2010

1 15 Jun 2011

2 15 Apr 2013

3%01 Sep 2017%

Revision

Number Date

Issued Inserted

On Inserted

AIRCRAFT

Record of Revision DA 40 NG AMM

Page vi

01 Sep 2017 ROR Doc # 6.02.15

Rev. 3

2. Record of Incorporated Temporary Revisions

The following Temporary Revisions are incorporated into the DA 40 NG AMM by Revision 1:

Temporary Revision Number Description of Temporary Revision

AMM-TR-MÄM 40-434 Cowling Redesign

AMM-TR-MÄM 40-434/a Cowling Redesign

AMM-TR-MÄM 40-434/b &

AMM-TR-MÄM 40-549 Cowling Redesign

AMM-TR-MÄM 40-436 Shock Mount Installation Torques

AMM-TR-MÄM 40-440 Safety Harnesses

AMM-TR-MÄM 40-442 New Governor Speed Settings

AMM-TR-MÄM 40-468 Fuel Pulsation Damper

AMM-TR-MÄM 40-481 Safety Walk Adhesive Strips

AMM-TR-MÄM 40-524 Maintenance Program Phase 1

AMM-TR-MÄM 40-525 Maintenance Interval GFC 700

AMM-TR-MÄM 40-526 Landing Gear Special Torque Values and Corrections

AMM-TR-MÄM 40-535 Gearbox Oil Inspection

AMM-TR-OÄM 40-310 Exhaust Muffler

AMM-TR-OÄM 40-314/c Additional Alternator

AMM-TR-OÄM 40-316 Recirculating Air - Cabin Cooling (RACC)

AMM-TR-OÄM 40-317 Coated Safety Walk

AMM-TR-OÄM 40-321 Conventional Cockpit DA 40 NG Club

AMM-TR-OÄM 40-326/a Emergency Axe

AMM-TR-OÄM 40-327 Sun Visor for Tall Canopy

AMM-TR-OÄM 40-329 DA 40 NG Retrofit, G1000 with Autopilot KAP 140

AMM-TR-OÄM 40-330 DA 40 NG Retrofit, G1000 without Autopilot GFC 700

AMM-TR-OÄM 40-331 Short Baggage Extension

AMM-TR-OÄM 40-333 DA 40 NG without Autopilot GFC 700

AIRCRAFT

DA 40 NG AMM Record of Revision

Doc # 6.02.15

Rev. 3 ROR Page vii

01 Sep 2017

The following Temporary Revisions are incorporated into the DA 40 NG AMM by Revision 2:

Temporary Revision Number Description of Temporary Revision

AMM-TR-MÄM 40-502/a &

AMM-TR-MÄM 40-506/a Replacement of Charged Air Hoses with Tube

AMM-TR-MÄM 40-505 Firewall Reinforcements on Engine Mount Holes

AMM-TR-MÄM 40-519 &

AMM-TR-MÄM 40-520 Breather Line with Additional Outlet

AMM-TR-MÄM 40-534 Propeller Shipping Plug Removal

AMM-TR-MÄM 40-537 Fuel Drain Valve Mounting Torque

AMM-TR-MÄM 40-551 Alternator Regulator E4A-91-200-000

AMM-TR-MÄM 40-568/a Alternative Engine Shock Mount

AMM-TR-MÄM 40-574/a &

AMM-TR-OÄM 40-334/b &

AMM-TR-MÄM 40-631

1280 kg Maximum Landing Mass

and/or Landing Gear with

Large or Small Tires

AMM-TR-MÄM 40-607/a Adaption of Engine Time Limits

AMM-TR-MÄM 40-629 Rudder Control Cable Installation

AMM-TR-MÄM 40-630 Turbo Connector and Worm Drive Clamps

AMM-TR-MÄM 40-632 New AE 300 Gearbox

AMM-TR-MÄM 40-634 Snow and Ice Removal

AMM-TR-MÄM 40-636 Additional Greases

AMM-TR-MÄM 40-639 Charged Air Hoses SG5-0

AMM-TR-OÄM 40-314/e Additional Alternator

AMM-TR-OÄM 40-316/a Recirculating Air-Cabin Cooling

AMM-TR-OÄM 40-339 Foot Step Rear Option

AMM-TR-OÄM 40-340 Avidyne/Ryan TAS 600 Series

AMM-TR-OÄM 40-341 Whelen LED Position Lights

AIRCRAFT

Record of Revision DA 40 NG AMM

Page viii

01 Sep 2017 ROR Doc # 6.02.15

Rev. 3

The following Temporary Revisions are incorporated into the DA 40 NG AMM by Revision 3:%

Temporary Revision Number%Description of Temporary Revision%

AMM-TR-MÄM 40-561%New GFC 700 Autopilot Hardware%

AMM-TR-MÄM 40-619%Passenger Door Improvement%

AMM-TR-MÄM 40-635%Adjust Taxi Light Procedure%

AMM-TR-MÄM 40-638%Cold Weather Operation%

AMM-TR-MÄM 40-647%Engine Oil Quick Drain%

AMM-TR-MÄM 40-650%Fuel Filter Element Check Valve%

AMM-TR-MÄM 40-654%Trouble Shooting Fuel System%

AMM-TR-MÄM 40-655/a%Governor Nut Torque%

AMM-TR-MÄM 40-658/a%Coolant Tank Pressure Relief Valve Test%

AMM-TR-MÄM 40-661%Coolant System Pressure Test%

AMM-TR-MÄM 40-678%Removal of Checklist Items%

AMM-TR-MÄM 40-709%Stall Warning System%

AMM-TR-MÄM 40-728%Lubrication Schedule%

AMM-TR-MÄM 40-743%Protective Pads for Charged Air Hoses%

AMM-TR-MÄM 40-763%Coolant Water Tank with Threaded Cap and Larger%

Filler Neck%

AMM-TR-MÄM 40-785%Replacement of Passenger Door Hinges%

AMM-TR-MÄM 40-792%Additional Elevator Mass%

AMM-TR-MÄM 40-806/a%Silicate Cartridge%

AMM-TR-MÄM 40-808%Inspection of NLG Elastomer Pack Center Tube%

AMM-TR-MÄM 40-820%Flexible Charge Air Hose%

AMM-TR-MÄM 40-822%Inspection of MLG Strut%

AMM-TR-MÄM 40-824%New Type 6 Lubricants%

AMM-TR-MÄM 40-840%Main Landing Gear Adaptions%

AMM-TR-MÄM 40-841%Fuel Tank Maintenance%

AMM-TR-MÄM 40-846%Door Handle Improvement%

AMM-TR-MÄM 40-847%Fuel Filter Assembly%

AMM-TR-MÄM 40-853/c & -873%Turbo Charger V-Clamp%

AMM-TR-MÄM 40-860%Vent Line Routing%

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