Diamond Aircraft DA 40 D Specifiche tecniche

•

Diamond

AIRCRAFT

AIRPLANE FLIGHT MANUAL

DA40D

: Normal, Utility

: JAR-23

Airworthiness Category

Requirement

Serial Number

Registration

= ltB

-,s:c;;;c

/1/S

·~

,r'(j

))f.3G)!

Doe. No. : 6.01.05-E

Date

Issue :

November 2002

Signature

Authority

Stamp

Date

approval

This Flight Manual has been verified

for

EASA by the Austrian Civil Aviation Authority

Austro Control (ACG)

Primary Certification Authority (PCA) in accordance with the

valid Certification Procedures and approved by EASA with approval

no.2004

,,z

:szc;.

This Flight Manual has been approved by EASA on behalf ofCAAC-AAD.

DIAMOND

AIRCRAFT

INDUSTRIES

GMBH

N.A.

OTTO·STR. 5

A-2700

WIENER

NEUSTADT

AUSTRIA

Page 0 •

Rev.

DA40

DAFM

Diamond

T4P'

AIRCRAFT Introduction '

Intentionally left blank.

Page

Revision 6 31-Jul-2013 Doe. # 6.01.05-E

DA40DAFM

•Diamond

AIRCRAFT

TEMPORARY REVISION

TR-17-03

Change

Type Design Responsibility

This Temporary Revision TR-17-03

approved and

valid

conjunction with the latest

revision

the DA

400

Airplane Flight Manual until this Temporary Revision has been

incorporated into the Airplane Flight Manual.

The limitations and information contained herein either supplement or,

the case

conflict, override those in the Airplane Flight Manual or its previous Temporary Revisions.

The technical information contained

this document has been approved the Minister

Transportation

Doe. No. Chapter Affected Page

6.01.05-E Cover Page, Forward Cover Page, 0-0

Instruction

-Print this document on yellow paper (single-sided).

-Insert this cover page as the first page

the AFM.

-Insert the other pages

this TR in front

the corresponding AFM pages.

Doe. #.: 6.01.05-E

TR-17-03 November 15, 2017 Cover Page

•Diamond

AIRCRAFT

AIRPLANE FLIGHT MANUAL

DA40D

Airworthiness Category: Normal, Utility

Applicable Airworthiness Requirement: AWM

523

Serial Number:

Registration

Doe. No.: 6.01.05-E TR-17-03

Date of Issue:

November 2017

DA40D

AFM

This temporary revision to the

40D AFM 6.01.05-E must

inserted into the

front ofthe manual and carried

the aircraft at

all

time.

Signature:

Authority:

d:f!l_Ch;ef

Fl;ghtTe•t

for

l.Jit'"'ctor,

National

Aircraft

Certification Transport Canada Civil Aviation

TRANS?ORT

CANADA

Date ofapproval:

.Ne.,.._,~~~-

.2-';

15 November 2017

This temporary revision

prepared

identify that the type design holder for the

400

has been transferred to Diamond Aircraft Industries

Inc.

from Diamond Aircraft Industries

GmbH

and

that Transport Canada

now responsible for the continuing airworthiness of

the aircraft.

Diamond Aircraft Industries

Inc.

now responsible for the content

and

publishing of the

AFM for the

400

aircraft. A new AFM

being prepared that will replace the manual

prepared by Diamond Aircraft Industries GmbH. All contents of the AFM,

Doe.

No.

6.01.05-E are applicable

and

remain the requirements to operate the

400

aircraft

properly.

DA40DAFM

•Diamond

AIRCRAFT

This airplane

may

only be operated

accordance with the procedures and operating

limitations

the Airplane Flight Manual, 6.01.05-E.

Any questions

concerns regarding the AFM for the DA 40D aircraft please contact:

Diamond Aircraft Industries Inc.

1560 Crumlin Sideroad

London, Ontario, Canada N5V 1

http://www.diamondair.com/

For more information contact:

Diamond Aircraft Industries Inc.

Technical Publications

+1-519-457-4000

[email protected]

this manual

any portion thereof

by any means without the express written permission

DIAMOND

AIRCRAFT INDUSTRIES INC. is prohibited.

by DIAMOND AIRCRAFT INDUSTRIES INC.,

London, Ontario

Doe. #.: 6.01.05-E

TR-17-03 November 15, 2017 0-0

DA40

D AFM

IliA

Diamond

AIRCRAFT

Temporary Revision

Removal

Pilot Gust

Lock Mount

TEMPORARY REVISION

TR-MAM 40-1020

Removal of Pilot Gust Lock Mount

ThisTemporaryRevision TR-MAM 40-1020 is approved

conjunction with the Mandatory

Design ChangeAdvisoryMAM40-1020and is valid

conjunction with the latestrevision

the DA40DAirplane FlightManual until this temporaryrevision hasbeen incorporated

into the Airplane Flight Manual.

The limitations and information contained herein either supplement or,

the case

conflict, override those

the Airplane Flight Manual.

Doe. No. Chapter Affected Pages

6.01.05-E 8 8-7a

Instruction

-Print

this document on yellow paper (single sided).

-Insert

this

cover

page as the first page

the AFM.

-Insert

the otherpages

thisTemporaryRevision

front

ofthe

corresponding AFM

pages.

Doe.#

6.01.05-E TR-MAM 40-1020 13-Sept-2018 Cover Page

DA40

D AFM

~Diamond

V4"'

AIRCRAFT

Temporary Revision

Emergency Egress

Hammer

TEMPORARY REVISION

TR-OAM-40-401

Emergency Egress Hammer

This Temporary Revision TR-OAM-40-401 is approved

conjunction with the Optional

Design ChangeAdvisory OAM-40-401 and is valid

conjunction with the latest revision

the

DA40

DAirplane FlightManual until this TemporaryRevision hasbeen incorporated

into the Airplane Flight Manual.

The limitations and information contained herein either supplement or,

the case

conflict, override those in the Airplane Flight Manual.

The technical information contained

this document has been approved under the

authority

DOA No. EASA.21J.052.

Doe. No. Chapter Affected Pages

1 1-3b

4A-4a

6.01.05-E 6 6-18a

7 7-14a

Instruction

-Print

this document on yellow paper (single-sided).

-Insert

this cover page as the first page of the AFM.

-Insert

theotherpages

ofthis

TemporaryRevision

front

ofthe

corresponding AFM

pages.

Doe. No. 6.01.05-E TR-OAM-

40-401 06-Dec-2016

COVER

PAGE

DA40

DAFM

4'ADiamond

AIRCRAFT

TEMPORARY REVISION

TR-MAM-40-816

Temporary Revision

Alternate Means for

Fuel Quantity

Alternate Means for Fuel Quantity Measurement

ThisTemporary Revision TR-MAM-40-816is approved

conjunctionwith the Mandatory

Design ChangeAdvisory MAM 40-816 and is valid in conjunction with the latest revision

the

DA40

DAirplane FlightManual untilthisTemporary Revision hasbeen incorporated

into the Airplane Flight Manual.

The limitations and information contained herein either supplement or,

the case

conflict, overridethose

theAirplaneFlightManual orits previousTemporary Revisions.

The technical information contained

this document has been approved under the

authority

DOA No. EASA.21J.052.

Doe. No. Chapter Affected Pages

6 6-24a

6.01.05-E 7 7-32a thru 7-32d

Instruction

-Print

this document on yellow paper (single-sided).

-Insert

this cover page as the first page

the AFM.

-Insert

the other page

this TR

front

the corresponding AFM page.

Doe. # 6.01.05-E TR-MAM-40-816 18-Nov-2015 Cover Page

DA40

DAFM

Temporary Revision

RG·35AXC

Main Battery

TEMPORARY REVISION

TR-OAM 40-384

Concorde RG-35AXC -Main Battery

This Temporary Revision TR-OAM 40-384 is approved

conjunction with the Optional

Design Change Advisory OAM 40-384 and is valid

conjunction with thelatestrevision

ofthe

40 DAirplaneFlightManual until thistemporaryrevision hasbeen incorporated

into the Airplane Flight Manual.

The limitations and information contained herein either supplement or, in the case

conflict, override those in

the

Airplane Flight Manual.

The technical information contained in this document has been approved under the

authority

DOA No. EASA.21J.052.

Doe. No. Chapter Affected Pages

6.01.05-E 1 1-3a

6 6-16a

Instruction

-Print

this document on yellow paper (single sided).

-Insert

this cover page

the first page

the AFM.

-Insert

theotherpages

thisTemporary Revision in front

ofthe

corresponding AFM

pages.

Doe.#

6.01.05-E TR-OAM 40-384 02-Sep-2014 Cover Page

DA40 DAFM

4ia0iamond

AIRCRAFT

Temporary

Revision

Entering

and

Exiting

the

Airplane

TEMPORARY REVISION

TR-MAM 40-766

Entering and Exiting the Airplane

ThisTemporary Revision TR-MAM40-766is approved

conjunctionwith theMandatory

Design Change Advisory MAM 40-766 and is valid in conjunction with the latestrevision

the

DA40

DAirplaneFlightManualuntilthisTemporaryRevision hasbeenincorporated

into the Airplane Flight Manual.

The limitations and information contained herein either supplement or, in the case

conflict, overridethosein theAirplaneFlightManual

itspreviousTemporaryRevisions.

The technical information contained in this document has been approved under the

authority

DOA No. EASA.21J.052.

Doe. No.

Chapter

Affected

Page

6.01.05-E 4A 4A-13a

Instruction

-Print

this document on yellow paper (single-sided).

-Insert

this cover page as

the

first page

the AFM.

-Insert

the other pages

this TR

front

the corresponding AFM pages.

Doe. # 6.01.05-E TR-MAM 40-766 05-Jul-2014 Cover Page

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