Diamond DA 40 Flight Manual page 6

Introduction
Rev.
Reason Chapter
No.
type certifi-
6
cation in China
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,
%
7 -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
Page 0 - 4
Page(s)
0 0-0, 0-5, 0-6 15 Sep 2004
all except cover
all 15 Jul 2006
page
Rev. 8 01-Dec-2010
Date of EASA Approv-
Revision al No.
2004-12326
Revision No. 7
of the AFM
Doc. No.
6.01.01-E is
approved
under the
authority of
DOA No.
EASA.21J.052
DA 40 AFM
ACG Date
Compliance Inserted
[Ing. Andreas
Winkler for
ACG]
[11 Aug 2006
Dipl.-Ing.
(FH)
Manfred
Reichel
for DAI]
Doc. # 6.01.01-E
Signature