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and destroy the pages which are superseded. Complete the table below when you have put the
revision in the AMM.
A vertical bar in the left margin of the page shows the changes.
Rev.
No.
Reason Date
Issued
Inserted
On
Inserted
By
0 Initial Issue. 26 Jun 2000
% Obsolete with Rev. 5, which
is a complete re-issue.
1 Corrections. 10 Nov 2000
2 FAA certification. 15 May 2001
3 Night VFR, IFR, autopilot; corrections. 26 Jun 2001
4 DA 40 D (TAE 125 engine) inserted.
Re-issue.
09 Jan 2003
% 5 Temporary Revisions inserted.
% Corrections.
20 Sep 2007
AIRCRAFT
Record of Revisions DA 40 Series
AMM
Rev.
No.
Reason Date
Issued
Inserted
On
Inserted
By
Page x
20 Sep 2007
Doc # 6.02.01
Rev. 5
4
1. Inclusion of DA 40 D (TAE 125 engine).
2. Inclusion of Temporary Revisions:
S AMM-TR-MÄM-40-046
S AMM-TR-MÄM-40-047
S AMM-TR-MÄM-40-056
S AMM-TR-MÄM-40-057
S AMM-TR-MÄM-40-065/66
S AMM-TR-OÄM-40-071
S AMM-TR-OÄM-40-077
S AMM-TR-OÄM-40-086
S AMM-TR-OÄM-40-090
S AMM-TR-OÄM-40-091
S AMM-TR-OÄM-40-097
S AMM-TR-OÄM-40-098
S AMM-TR-OÄM-40-099
S AMM-TR-OÄM-40-101/102
S AMM-TR-OÄM-40-103
S AMM-TR-OÄM-40-104
S AMM-TR-OÄM-40-112
S AMM-TR-OÄM-40-117
S AMM-TR-OÄM-40-119
S AMM-TR-OÄM-40-120
S AMM-TR-OÄM-40-121
S AMM-TR-OÄM-40-122
S AMM-TR-OÄM-40-127
S AMM-TR-OÄM-40-128
S AMM-TR-OÄM-40-138
3. Corrections.
09 Jan 2003
(re-issue)
AIRCRAFT
DA 40 Series
AMM
Record of Revisions
Rev.
No.
Reason Date
Issued
Inserted
On
Inserted
By
Doc # 6.02.01
Rev. 5
Page xi
20 Sep 2007
% 5
% 1. Inclusion of Temporary Revisions:
% S AMM-TR-MÄM-40-075
% S AMM-TR-MÄM-40-089
% S AMM-TR-MÄM-40-093
% S AMM-TR-MÄM-40-098
% S AMM-TR-MÄM-40-099
% S AMM-TR-MÄM-40-102
% S AMM-TR-MÄM-40-107
% S AMM-TR-MÄM-40-113/a
% S AMM-TR-MÄM-40-116
% S AMM-TR-MÄM-40-119
% S AMM-TR-MÄM-40-121
% S AMM-TR-MÄM-40-124
% S AMM-TR-MÄM-40-126
% S AMM-TR-MÄM-40-128
% S AMM.TR-MÄM-40-129
% S AMM-TR-MÄM-40-136/b
% S AMM-TR-MÄM-40-138
% S AMM-TR-MÄM-40-142/a
% S AMM-TR-MÄM-40-149
% S AMM-TR-MÄM-40-151
% S AMM-TR-MÄM-40-156
% S AMM-TR-MÄM-40-161
% S AMM-TR-MÄM-40-169
% S AMM-TR-MÄM-40-172
% S AMM-TR-MÄM-40-203
% S AMM-TR-MÄM-40-215
% S AMM-TR-MÄM-40-222
% S AMM-TR-MÄM-40-225
% S AMM-TR-MÄM-40-258
% S AMM-TR-MÄM-40-262/a
% S AMM-TR-MÄM-40-280
% S AMM-TR-OÄM-40-118
% S AMM-TR-OÄM-40-137
% S AMM-TR-OÄM-40-179
% S AMM-TR-OÄM-40-205
% S AMM-TR-OÄM-40-244
% S AMM-TR-OÄM-40-247 & 40-284
% S AMM-TR-OÄM-40-251
% S AMM-TR-OÄM-40-259
% S AMM-TR-OÄM-40-267
%
% 2. Corrections
%
20 Sep 2007
(re-issue)
AIRCRAFT
Record of Revisions DA 40 Series
AMM
Rev.
No.
Reason Date
Issued
Inserted
On
Inserted
By
Page xii
20 Sep 2007
Doc # 6.02.01
Rev. 5
AIRCRAFT
DA 40 Series
AMM
List of Effective Pages
Doc # 6.02.01
Rev. 5
Page 1
20 Sep 2007
LIST OF EFFECTIVE PAGES
1. General
I The list of effective pages uses these abbreviations:
) TOC = Table of Contents.
I ) ROR = Record of Revisions
I ) LOEP = List of Effective Pages
All Sections have a Title Page and a Table of Contents. The TOC can have one page or it can have
many pages.
In the List of Effective Pages, gray shaded areas show you changes to the list. They do not show you
changes to the related pages.
Each revision to the Airplane Maintenance Manual will have a new List of Effective Pages.
Front
Matter
Page Revision Date
TOC i 20 Sep 2007
TOC ii 20 Sep 2007
TOC iii 20 Sep 2007
TOC iv 20 Sep 2007
TOC v 20 Sep 2007
TOC vi 20 Sep 2007
TOC vii 20 Sep 2007
TOC viii 20 Sep 2007
ROR ix 20 Sep 2007
ROR x 20 Sep 2007
ROR xi 20 Sep 2007
ROR xii 20 Sep 2007
LOEP 1 20 Sep 2007
LOEP 2 20 Sep 2007
LOEP 3 20 Sep 2007
LOEP 4 20 Sep 2007
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钻石40系列AMM 1(3)
