DA 40 F
TEMPORARY REVISION
AMM-TR-V.M-40-002
DA 40 F
(Lycoming O-360-A4M Engine and
Fixed Pitch Propeller)
This Temporary Revision AMM-TR-V.M-40-002 is approved in conjunction with the Variant Design Change Advisory V.M 40-002 and is valid in conjunction with the Airplane Maintenance Manual (AMM) Revision 4 until this Temporary Revision has been incorporated into the AMM.
The limitations and information contained herein either supplement or, in case of conflict, override those in the AMM.
The technical information contained in this document has been approved under the authority of DOA No. EASA.21J.052.
Affected Pages
See table on reverse side.
Instruction
) Print this document double-sided on yellow paper (odd pages and 'a' pages on front sides, even pages and 'aa' pages on reverse sides).
) Insert this cover page as the first side of the AMM.
) Insert the other pages of this Temporary Revision in front of the corresponding AMM pages.
Doc # 6.02.01 Page 1
COVER
DA 40 Series AMM
Affected Pages
DA 40 F
Doc. No. Section Affected Pages Section Affected Pages
6.02.01 02-00 1a, 1aa 71-62 1-4, 101-102, 201-210
03-00 2a, 2aa, 4a, 4aa 71-70 1a, 1aa
05-10 3a, 3aa 71-72 1-2, 101-102, 201-202
05-20 7a, 7aa, 14a-14h, 21a, 21aa 72-00 1a, 1aa, 202a, 202aa
11-30 05a, 05aa 73-CONT. 1a, 1aa
12-10 1a, 1aa 73-00 1a, 1aa
21-00 101a, 101aa 73-02 1-4, 101-102, 201-208
24-60 5a, 5aa, 9, 10 75-CONT. 1a, 1aa
28-00 1a, 1aa, 2a, 2aa 75-00 1a, 1aa
28-10 3a, 3aa 75-02 1-2, 201-202
28-40 3a, 3aa 76-CONT. 1a, 1aa
31-10 1a, 1aa, 15a, 15aa 76-00 1a, 1aa
31-20 5, 6, 201a, 201aa 76-02 1-8, 101-102, 201-218
61-CONT. 1a, 1aa, 3a, 3aa 77-CONT. 2a, 2aa
61-00 1a, 1aa, 3, 4 77-00 1a, 1aa
61-10 1a, 1aa 77-40 1a, 1aa
61-12 1, 2, 101, 102, 201-204 77-42 1-10, 101-102, 201-214
71-CONT. 1a, 1aa, 3a, 3aa, 7a, 7aa, 8a, 8aa 78-CONT. 1a, 1aa
71-00 1a, 1aa 78-00 1a, 1aa
71-02 1-6, 101-102, 201-248 78-02 1, 2, 101-102, 201-208
71-10 1a, 1aa 79-CONT. 1a, 1aa
71-12 1-2, 101-102, 201-204 79-00 1a, 1aa
71-60 1a, 1aa 79-02 1-2, 101-102, 201-208
DA 40 F
CHAPTER 02
ORGANIZATION AND HANDLING OF THE MANUAL
Add the following paragraph:
NOTE: There are different models of Lycoming engines used for the DA 40 series airplanes.
Instructions given for the 'Lycoming version' in the AMM are applicable to all DA 40 aircraft powered by a Lycoming engine. Specific changes apply to the Lycoming O-360-A4M engine model and are listed referring to the engine model number.
Doc # 6.02.01 Page 1a
02-00-00
DA 40 Series AMM
DA 40 F
Intentionally left blank
DA 40 F
2. Description
The DA 40 is powered by one of the following engines:
The paragraph is amended to read:
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