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
6
type 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]
Summary of Contents for DA 40
Page 1: ......
Page 37: ...DA 40 AFM General Doc 6 01 01 E Rev 8 01 Dec 2010 Page 1 21 1 7 THREE VIEW DRAWING ...
Page 182: ...Performance DA 40 AFM Page 5 12 Rev 8 01 Dec 2010 Doc 6 01 01 E ...
Page 184: ...Performance DA 40 AFM Page 5 14 Rev 8 01 Dec 2010 Doc 6 01 01 E ...
Page 186: ...Performance DA 40 AFM Page 5 16 Rev 8 01 Dec 2010 Doc 6 01 01 E ...
Page 190: ...Performance DA 40 AFM Page 5 20 Rev 8 01 Dec 2010 Doc 6 01 01 E ...
Page 288: ...Handling DA 40 AFM Page 8 6 Rev 8 01 Dec 2010 Doc 6 01 01 E ...