Diamond DA 40 Specifiche tecniche
Introduction DA 40 AFM
Page 0 - 0 Revision 6 15-Sep-2004 Doc. # 6.01.01-E
FOREWORD
We congratulate you on the acquisition of your new DIAMOND STAR.
Skillfuloperationofanairplaneincreasesbothsafetyandtheenjoymentofflying.Please
take the time therefore, to familiarize yourself with your new DIAMOND STAR.
This airplane may only be operated in accordance with the procedures and operating
limitations of this Airplane Flight Manual.
Before this airplane is operated for the first time, the pilot must familiarize himself with
the complete contents of this Airplane Flight Manual.
In the event that you have obtained your DIAMOND STAR second-hand, please let us
know your address, so that we can supply you with the publications necessary for the
safe operation of your airplane.
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 in data processing facilities, in whole or part, are reserved.
Copyright © by: DIAMOND AIRCRAFT INDUSTRIES GMBH
N.A. Otto-Strasse 5
A-2700 Wiener Neustadt, Austria
Phone. : +43-2622-26700
Fax : +43-2622-26780
DA 40 AFM Introduction
Doc. # 6.01.01-E Rev. 8 01-Dec-2010 Page 0 - 1
0.1 APPROVAL%
The content of approved chapters is approved by EASA. All other content is approved%
byDAIundertheauthorityofEASADOANo.EASA.21J.052inaccordancewithPart21.%
0.2 RECORD OF REVISIONS
All revisions of this manual, with the exception of -
CTemporary Revisions,
Cupdates of the modification level (Section 1.1),
Cupdated mass and balance information (Section 6.3),
Cupdates of the Equipment Inventory (Section 6.5), and
Cupdates of the List of Supplements (Section 9.2)
must be recorded in the following table.%
The new or amended text is indicated by a vertical black line at the left hand side of the
revised page, with the revision number and date appearing at the bottom of the page.
NOTE
If pages are revised which contain information valid for your
particular serial number (modification level of the airplane,
weighing data, Equipment Inventory, List of Supplements),
then this information must be transferred to the new pages
in hand-writing.
Temporary Revisions, if applicable, are inserted into this manual. Temporary Revisions
are used to provide information on systems or equipment until the next 'permanent'
RevisionoftheAirplaneFlightManual.Whena'permanent'RevisioncoversaMandatory
orOptionalDesignChangeAdvisory(MÄMorOÄM),thenthecorrespondingTemporary
Revision is superseded. For example: Revision 5 covers OÄM-40-061, therefore the
Temporary Revision TR-OÄM-40-061 is superseded by the 'permanent' Revision 5.
Introduction DA 40 AFM
Page 0 - 2 Rev. 8 01-Dec-2010 Doc. # 6.01.01-E
Rev.
No. Reason Chapte
rPage(s) Date of
Revision Approval Date of
Approval Date Inserted Signature
1 corrections all all 26-Sep-2000
[approved by
Ing. Andreas
Winkler for
ACG]
09-Oct-2000
2
OÄM 40-060
(White Wire
optional)
OÄM 40-068
(Essential Bus)
OÄM 40-073
(LASAR
optional)
corrections
0 0-2, 0-4 thru 0-7
19-Dec-2000
approved by
Ing. Andreas
Winkler for
ACG]
25-Jan-2001
11-16
22-1, 2-7 thru 2-9,
2-13 thru 2-19
33-7, 3-8, 3-19,
3-20, 3-25, 3-26
4A 4A-3 thru 4A-8,
4A-14, 4A-15
4B 4B-4 thru 4B-6
66-1, 6-2,
6-12 thru 6-14
77-1, 7-8, 7-14,
7-28 thru 7-38
3
OÄM 40-064
(Night VFR)
OÄM 40-069
(control surf.
gust lock)
OÄM 40-070
(tow bar)
corrections
0 0-2 thru 0-7
05-Feb-2001
[approved by
Ing. Andreas
Winkler for
ACG]
02 Jul 2001
11-2
22-1, 2-8, 2-9, 2-12,
2-15 thru 2-20
3 3-1, 3-25 thru 3-27
4A 4A-1,
4A-8 thru 4A-31
5 5-7, 5-14, 5-16
66-7, 6-9,
6-12 thru 6-14
7 7-32, 7-35, 7-36
8 8-1 thru 8-9
DA 40 AFM Introduction
Rev.
No. Reason Chapte
rPage(s) Date of
Revision Approval Date of
Approval Date Inserted Signature
Doc. # 6.01.01-E Rev. 8 01-Dec-2010 Page 0 - 3
4
OÄM 40-067
(IFR)
corrections
all all 09 Apr 2001
[approved by
Ing. Andreas
Winkler for
ACG]
02 Jul 2001
5
OÄM 40-061
(KAP 140
autopilot)
OÄM 40-073
(SlickSTART)
OÄM 40-081
(door lock)
OÄM 40-085
(KX 155A
as COM 1)
OÄM's 40-092
thru 40-094
(Mikrotechna
ASI, altimeter,
VSI)
MÄM 40-039/a
(VM 1000)
MÄM 40-048
(RH emerg.
window)
corrections
0 0-1 thru 0-8
09 Sep 2001
[approved by
Ing. Andreas
Winkler for
ACG]
09 Sep 2001
1 1-2, 1-5, 1-14
22-1, 2-16, 2-22,
2-23, 2-24
33-13, 3-18, 3-22,
3-23, 3-24, 3-31,
3-36
4A 4A-8, 4A-10, 4A-22,
4A-23, 4A-26
4B 4B-1, 4B-8
6 6-5, 6-8 thru 6-17
77-13, 7-14, 7-33,
7-35
88-10
9 9-3, 9-4, 9-5
Introduction DA 40 AFM
Page 0 - 4 Rev. 8 01-Dec-2010 Doc. # 6.01.01-E
Rev.
No. Reason Chapter Page(s) Date of
Revision EASA Approv-
al No. ACG
Compliance Date
Inserted Signature
6type certifi-
cation in China 0 0-0, 0-5, 0-6 15 Sep 2004 2004-12326 [Ing. Andreas
Winkler for
ACG]
7
MÄM-40-
-047, -069,
-075, -078,
-096, -099,
-123e, -133,
-141, -174,
-175;
OÄM-40-
-063/b, -071/c,
-077, -078,
-080, -083/a,
-090, -091,
-097, -098,
-103, -104,
-105, -106,
-111, -112,
-114, -115,
-117, -117/a,
-119, -120,
-121, -122,
-124, -127,
-128, -138,
-140, -154,
-165, -167,
-168, -179,
-181, -183,
-185, -186,
-190, -198,
-200, -206,
-237, 250/a;
RÄM-40-
-014;
corrections;
double-sided
layout
all all except cover
page 15 Jul 2006
Revision No. 7
%of the AFM%Doc. No.%6.01.01-E is%approved%under the%authority of%DOA No.%EASA.21J.052%
[11 Aug 2006
Dipl.-Ing.
(FH)
Manfred
Reichel
for DAI]
DA 40 AFM Introduction
Rev.
No. Reason Chapter Page(s) Date of
Revision EASA Approv-
al No. ACG
Compliance Date
Inserted Signature
Doc. # 6.01.01-E Rev. 8 01-Dec-2010 Page 0 - 5
8%
MÄM-40-%-176, -227/a,%-313, -344,%-360/a, -378,%-401, -415,%-428, -446;%
%
OÄM-40-%-217, -251,%-253/b, 258,%-267, -277/a,%-279, 283/a,%-284, -289,%-326, -327;%
%corrections%
%
all%all except cover%page%01 Dec 2010%
Revision No. 8%of the AFM%Doc. No.%6.01.01-E is%approved%under the%authority of%DOA No.%EASA.21J.052%
%%%
Introduction DA 40 AFM
Page 0 - 6 Rev. 8 01-Dec-2010 Doc. # 6.01.01-E
0.3 LIST OF EFFECTIVE PAGES
Ch. Page Date
0 0-0 15-Sep-2004
0-0a 15-Sep-2004
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DA 40 AFM Introduction
Doc. # 6.01.01-E Rev. 8 01-Dec-2010 Page 0 - 7
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Introduction DA 40 AFM
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