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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本文鏈接地址：鉆石40飛機維護手冊 DA 40 SERIES AMM 6(30)