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N: New
R: Revised
D:
Deleted
Chap Sect
TITLE
LOEP
LOEP
LOEP
LOEP
LOEP
LOEP
LOEP
TOG
TOG
TOG
HIGHLIGHTS
HIGHLIGHTS
SB LIST
INTRO
INTRO
INTRO
INTRO
lr\ITRO
INTRO
lf\ITRO
INTRO
INTRO
lf\ITRO
GLOSSARY
HOW TO USE
HOW TO USE
HOW TO USE
HOW TO USE
OPTIONAL
OPTIONAL
OPTIONAL
OPTIONAL
O ~ : i - 1 0 GENE
O ~ : i 1 0 GENE
0 ~ > - 1 0 TABLE
O ~ : i - 1 0 TABLE
O ~ : i 1 0 00 REP
0 ~ - 1 0 00 REP
O ~ : i 1 0 00
ATA
21 52
Ot:i 1 0 00
ATA
21 53
0 ~ 5 1 0 00 ATA 22 30
Page
1
2
3
4
5
6
7
1
2
3
1
2
1
1
2
3
4
5
6
7
8
9
10
1
1
2
3
4
1
2
3
4
1
2
1
2
1
2
1
1
1
M INTEN NCE PROGR M
LIST OF EFFE TIVE P GES
Type Date Chap Sect Page Type
Date
N
2012.07.02
05 10 00
ATA
22 30
2 2011.06.09
N 2012.07.02
05 10 00
ATA
23 52 1
2009.05.14
N
2012.07.02
05 10 00 ATA 23 71 1
2010.10.11
N
2012.07.02
05 10 00 ATA 24 20 1 2010.10.11
N 2012.07.02 . 05 10 00
ATA
24 20 2 2010.10.11
N 2012.07.02
05 10 00
ATA
24 30 1 2003.01.03
N
2012.07.02
05 10 00
ATA
24 31 1 2007.01.09
N
2012.07.02
05 1 0 00
ATA
25 00 1
2008.01.28
N
2012.07.02
05 10 00
ATA
25 10 1
2005.04.21
N
2012.07.02 05 10 00
ATA
25 62 1
2006.04.07
N 2012.07.02
05 10 00
ATA
25 62 2
2006.04.07
N
2012.07.02
05 10 00 ATA 25 64 1
2007.04.30
N
2012.07.02
05 10 00 ATA
25 64
2 2007.04.30
2012.03.22
05 10 00
ATA
25 64
3
2007.04.30
2012.03.22
05 10 00
ATA
25 64 4
2007.04.30
2012.03.22
05 10 00
ATA
25 64
5
2007.04.30
2012.03.22
05 10 00
ATA
25 64
6
2007.04.30
2012.03.22
05 10 00
ATA
25 64 7 2007.04.30
2012.03.22
05 10 00
ATA
25 66
1
2012.03.22
2012.03.22
05 10 00 ATA
25 66
2 2012.03.22
2012.03.22
05 10 00 ATA 25 66
3
2012.03.22
2012.03.22
05 10 00 ATA 25 66 4 2012.03.22
2012.03.22
05 10 00
ATA
25 66
5
2012.03.22
2012.03.22
05 10 00
ATA
25 66
6
2012.03.22
2004.03.25
05 10 00
ATA
25 69
1 2008.09.01
2006.04.07
05 10 00 ATA 25 69 2 2008.09.01
2006.04.07
05 10 00 ATA 25 69
3
2008.09.01
2006.04.07
05 10 00 ATA 25 81
1 2007.01.09
2006.04.07
05 10 00 ATA 25 81
2
2007.01.09
2003.01.03
05 10 00 ATA 26 13 1 2003.01.03
2003.01.03
05 10 00
ATA
26 21 1 R 2012.07.02
2003.01.03
05 10 00 ATA 26 21
2 R 2012.07.02
2003.01.03
05 10 00 ATA 26 22 1
2005.04.21
2012.03.22
05 10 00 ATA 28 10 1 2011.06.09
2012.03.22
05 10 00
ATA
28 20 1 2011.06.09
2004.03.25
05 10 00 ATA 28 20 2 2011.06.09
2004.03.25
05 10 00
ATA
28 41 1 2008.09.01
N
2012.07.02
05 10 00 ATA 28 93 1
2003.01.03
N
2012.07.02
05 1 0 00 ATA 29 1 0
1 2010.10.11
2007.01.09
05 10 00 ATA 29 10 2 2010.10.11
2008.01.28
05 10 00 ATA 29 10 3
2010.10.11
2011.06.09
05 10 00 ATA 29 10
4
2010.10.11
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~ J : 1 9 C O P T E R
M INTEN NCE
PROGR M
Chap Sect
Page
Type
Date
Chap Sect
Page
Type Date
05 20 01
ATA
28 10 1 2006.04.07 05 20 01
ATA
36 10 1 2004.03.25
05 20 01
ATA
28 11
1
R
2012.07.02
05 20 01
ATA
36 10 2
2004.03.25
05 20 01
ATA
28 20
1
2009.05.14
05 20 01 ATA 39 11
1 2003.01.03
05 20 01 ATA 28 30
1
2003.01.03
05 20 01 ATA 45 11
1
2010.10.11
05 20 01 ATA 28 40
1
2008.09.01
05 20 01 ATA
45 11
2
2010.10.11
05 20 01 ATA 28 41
1
2003.01.03
05 20 01 ATA 47 50
1
2011.06.09
05 20 01 ATA 28 91
1
2003.01.03
05 20 01 ATA 52 10
1
2003.01.03
05 20 01 ATA 28 92
1
2003.01.03
05 20 01
ATA 52 11
1 2012.03.22
05 20 01 ATA 28 93
1
2003.01.03
05 20 01 ATA52 11
2
2012.03.22
05 20 01 ATA 29 00
1
2005.04.21
05 20 01 ATA 52 12
1
2003.01.03
05 20 01 ATA 29 10
1
2005.04.21
05 20 01 ATA 52 13
1
2003.01.03
05 20 01 ATA 29 10
2
2005.04.21
05 20 01 ATA 52 14
1
2003.01.03
05 20 01 ATA 29 20
1
2003.01.03
05 20 01 ATA 52 30
1
2003.01.03
05 20 01
ATA
30 20
1
2011.06.09
05 20 01 ATA 53 00
1
2011.06.09
05 20 01 ATA 30 20
2
2011.06.09
05 20 01 ATA 53 00
2
2011.06.09
05 20 01
ATA
30 20 3
2011.06.09
05 20 01 ATA 53 10
1
2011.06.09
05 20 01
ATA
30 30
1
2003.01.03
05 20 01
ATA
53 10
2
2011.06.09
05 20 01 ATA 30 41
1
2003.01.03
05 20 01 ATA 53 10
3
2011.06.09
05 20 01 ATA 30 42
1
2012.03.22
05 20 01 ATA 53 10
4
2011.06.09
05 20 01 ATA 30 60
1
2007.09.20
05 20 01 ATA 53 20
1
2004.03.25
05 20 01 ATA 30 60
2
2007.09.20
05 20 01 ATA 53 40
1
2005.04.21
05 20 01 ATA 30 61
1
2003.01.03
05 20 01
ATA
53 40
2
2005.04.21
05 20 01 ATA 30 80
1
2007.01.09
05 20 01 ATA 53 50
1
2011.06.09
05 20 01 ATA 31 32
1
2008.09.01
05 20 01 ATA 53 50
2
2011.06.09
05 20 01 ATA 31 32
2
2008.09.01
05 20 01 ATA 55 10
1
R
2012.07.02
05 20 01
ATA
31 50 1 2003.01.03 05 20 01
ATA
55 10 2
R
2012.07.02
05 20 01 ATA 32 00
1
2003.01.03
05 20 01 ATA 56 10
1
2003.01.03
05 20 01 ATA 32 12
1
2003.01.03
05 20 01 ATA 56 20
1
2008.09.01
05 20 01 ATA 32 22
1
2003.01.03
05 20 01 ATA 62 10
1
2011.06.09
05 20 01 ATA 32 30
1
2010.10.11
05 20 01 ATA 62 10
2
2011.06.09
05 20 01 ATA 32 30
2
2010.10.11
05 20 01 ATA 62 10 3
2011.06.09
05 20 01 ATA 32 30 3
2010.10.11
05 20 01 ATA 62 10
4
2011.06.09
05 20 01
ATA
32 40
1
2010.10.11
05 20 01 ATA 62 10
5
2011.06.09
05 20 01 ATA 32 40
2
2010.10.11
05 20 01 ATA 62 10 6
2011.06.09
05 20 01
ATA
32 50
1
2003.01.03
05 20 01 ATA 62 10
7
2011.06.09
05 20 01 ATA 32 70
1
2003.01.03
05 20 01 ATA 62 35
1
2012.03.22
05 20 01 ATA 32 91
1
2008.01.28
05 20 01 ATA 62 35
2
2012.03.22
05 20 01 ATA 33 10
1
2003.01.03
05 20 01 ATA 62 35 3
2012.03.22
05 20 01
ATA
33 20 1 2003.01.03 05 20 01
ATA
62 35 4 2012.03.22
05 20 01
ATA
33 40
1
2003.01.03
05 20 01 ATA 62 35
5
2012.03.22
05 20 01 ATA 33 43
1
2007.09.20
05 20 01 ATA 62 35 6
2012.03.22
05 20 01
ATA
33 43
2
2007.09.20
05 20 01 ATA 62 36
1
2006.04.07
05 20 01 ATA 33 45
1
2008.09.01
05 20 01 ATA 62 36
2
2006.04.07
05 20 01 ATA34 11
1
R
2012.07.02
05 20 01 ATA 63 10
1
2012.03.22
05 20 01 ATA 34 21
1
2003.01.03
05 20 01 ATA 63 20
1
2012.03.22
05 20 01 ATA 34 22
1
2003.01.03
05 20 01 ATA 63 20
2
2012.03.22
05 20 01
ATA
34 23
1
2003.01.03
05 20 01 ATA 63 20
3
2012.03.22
05 20 01 ATA 34 42
1
2011.06.09
05 20 01 ATA 63 21
1
2005.04.21
05 20 01 ATA 34 42
2
2011.06.09
05 20 01 ATA 63 23
1
2011.06.09
05 20 01
ATA
35 30
1
2009.05.14
05 20 01 ATA 63 23
2
2011.06.09
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~ Y R 9 C O P T E R
MAINTENANCE PROGRAM
Chap/Sect
Page
Type
Date
Chap/Sect
Page
Type
Date
05 20 02
5
H 5 R 2012.07.02 05 20 02 2000 H 1 2007.09.20
05 20 02 500 H
6
R
2012.07.02
05 20 02 2000 H
2
2007.09.20
05 20 02 500 H
7 R
2012.07.02
05 20 02 2500 H
1
2010.10.11
05 20 02 500 H
8
R
2012.07.02
05 20 02 3000 H
1
2008.09.01
05 20 02 500 H
9
R
2012.07.02
05 20 02 3000 H
2
2008.09.01
05 20 02 500 H
1
R
2012.07.02
05 20 02 3000 H
3
2008.09.01
05 20 02 500 H
R
2012.07.02
05 20 02 3000 H
4
2008.09.01
05 20 02 500 H
12 R
2012.07.02
05 20 02 3500 H
1
2012.03.22
05 20 02 500 H
13
R
2012.07.02
05 20 02 3750 H
1
2003.01.03
05 20 02 500 H
14
R
2012.07.02
05 20 02 4500 H
1
2010.10.11
05 20 02 500 H
15
R
2012.07.02
05 20 02 7500 H
1
2011.06.09
05 20 02 500 H
16
R
2012.07.02
05 20 02 7500 H
2
2011.06.09
05 20 02 500 H
17
R
2012.07.02 05 20 02 7500 H
3
2011.06.09
05 20 02 500 H
18
R
2012.07.02
05 20 02 7500 H
4
2011.06.09
05 20 02 500 H
19
R
2012.07.02
05 20 02 7500 H
5
2011.06.09
05 20 02 500 H
2
R
2012.07.02
05 20 02 7500 H
6
2011.06.09
05 20 02 500 H
21
R
2012.07.02
05 20 02 7500 H
7
2011.06.09
05 20 02 500 H
22
R
2012.07.02
05 20 02 7500 H
8
2011.06.09
05 20 02 500 H
23
R
2012.07.02
05 20 02 7500 H
9
2011.06.09
05 20 02 500 H
24
R
2012.07.02
05 20 02 7500 H
1
2011.06.09
05 20 02 500 H
25
R
2012.07.02
05 20 02 7500 H
2011.06.09
05 20 02 500 H
26
R
2012.07.02
05 20 02 7500 H
12
2011.06.09
05 20 02 500 H
27
R
2012.07.02
05 20 02 7500 H
13
2011.06.09
05 20 02 500 H
28
R
2012.07.02
05 20 02 7500 H
14
2011.06.09
05 20 02 500 H
29
R
2012.07.02
05 20 02 7500 H
15
2011.06.09
05 20 02 500 H 30 R 2012.07.02 05 20 02 7 D 1 2004.03.25
05 20 02
5
H
31
R
2012.07.02
05 20 02 7 D
2
2004.03.25
05 20 02 500 H
32
R
2012.07.02
05 20 02 8 D
1
2003.01.03
05 20 02 500 H
33
R
2012.07.02
05 20 02 1 M
1
2011.06.09
05 20 02 500 H
34
R
2012.07.02
05 20 02 1 M
2
2011.06.09
05 20 02 500 H
35
R
2012.07.02
05 20 02 1 M
3
2011.06.09
05 20 02 500 H
36
R
2012.07.02
05 20 02 2 M
1
2011.06.09
05 20 02 500 H
37
R
2012.07.02
05 20 02 2 M
2
2011.06.09
05 20 02 500 H
38
R
2012.07.02
05 20 02 2 M
2011.06.09
05 20 02 500 H
39
R
2012.07.02
05 20 02 3 M
1
2009.05.14
05 20 02 500 H
4
R
2012.07.02
05 20 02 3 M
2
2009.05.14
05 20 02 520 H
1
2003.01.03
05 20 02 6 M
1
2011.06.09
05 20 02 550 H
1
2008.09.01
05 20 02 6 M
2
2011.06.09
05 20 02 600 H
1
2005.04.21 05 20 02 6 M 3 2011.06.09
05 20 02 800 H
1
2003.01.03
05 20 02 6 M
4
2011.06.09
05 20 02 800 H
2
2003.01.03
05 20 02 6 M
5
2011.06.09
05 20 02 1000 H
1
R
2012.07.02
05 20 02 6 M
6
2011.06.09
05 20 02 1000 H
2
R
2012.07.02
05 20 02 6 M
7
2011.06.09
05 20 02 1000 H
R
2012.07.02
05 20 02 6 M
8
2011.06.09
05 20 02 1000 H
4
R
2012.07.02
05 20 02 6 M
9
2011.06.09
05 20 02 1500 H
1
2010.10.11
05 20 02 6 M
1
2011.06.09
05 20 02 1500 H
2
2010.10.11
05 20 02 1 y
1
2010.10.11
05 20 02 1500 H
3
2010.10.11
05 20 02 1 y
2
2010.10.11
05 20 02 1500 H
4
2010.10.11
05 20 02 1 y
3
2010.10.11
05 20 02 1500 H
5
2010.10.11
05 20 02 1
y
4
2010.10.11
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M INTEN NCE PROGR M
Chap Sect
Page
Type
Date Chap Sect
Page Type
Date
05 20 03
T
62 35 3 2011.06.09
05 20 03
T
62 36 1
2003.01.03
05 20 03
T
63 20
1
2006.04.07
05 20 03 T 63 20
2
2006.04.07
05 20 03
T
63 25 1
2005.04.21
05 20 03
T
63 28
1
2005.04.21
05 20 03
T
63 30 1
2003.01.03
05 20 03
T
64 10
1
2003.01.03
05 20 03
T
64 20 1
2007.04.30
05 20 03 T 64 20
2 2007.04.30
05 20 03 T 64 20
3
2007.04.30
05 20 03 T 65 10 1
2004.03.25
05 20 03
T
65 20
1 2007.04.30
05 20 03 T 65 20
2
2007.04.30
05 20 03
T
67 30 1
2007.09.20
05 50 GENE 1
2003.01.03
05 50 00 REP 1 N 2012.07.02
05 50 00 T 28 20 1
2003.01.03
05 50 00 T 28 93 1 2003.01.03
05 50 00
T
30 20
1 2007.09.20
05 50 00
T
30 61
1 2003.01.03
05 50 00
T
32 70
2003.01.03
05 50 00 T 33 20
2003.01.03
05 50 00 T 62 10
R
2012.07.02
05 50 00
T
62 36
1 2003.01.03
05 50 00
T
63 23 1 2005.04.21
05 50 00 T 64 10
1 R 2012.07.02
05 50 00
T
65 10 1 2005.04.21
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~ - B 9 C O P T E R
M INTEN NCE
PROGR M
TABLE OF CONTENTS
Title age
TRANSMITIAL
L IT R . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . .
1 INSTRUCTIONS
...........................................................................................
2 OUTLINE OF THE REVISION . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . 1
3 DETAILED DESCRIPTION . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . 1
LIST OF SERVICE BULLETINS INCORPORATED
.. .. .. . .. .. .. .. .. .. .. . .. .. .. . .. .. .. .. .. ..
.. ..
INTRODUCTION
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
GENERAL
..................................................................................................
1 1
Scope of the Maintenance Program
...........................................................
1.2 Classification of the information
.................................................................
1 3
Airworthiness Limitations
.........................................................................
1.4
Adaptation of the PRE by the Operator .. . .. .. .. .. .. .. ..
.. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. 2
1 5
Changes
in
the PRE . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . 2
1.6 Feedback
of
Information from the Operator to the Manufacturer . . . . . . .
. . . . . . . . . . . . . . . . . . . . . 2
1 7 Effectivity - Responsibility . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . 2
2 DEFINITIONS . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . 3
2 1 Aircraft Maintenance. . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . 3
2.2 Types of Maintenance . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . 3
2 2 1 PREVENTIVE MAINTENANCE . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . 3
2.2.2 CORRECTIVE MAINTENANCE . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . 3
2.2.3 REMEDIAL MAINTENANCE . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . 3
2.3 Maintenance Procedures . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 3
2 3 1 Hard Time Maintenance . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . 4
2.3.2
On
Condition Maintenance: OC ( On Condition ) or CHK ( Inspection
Check ) . . . 4
2.3.3 Condition Monitoring . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . 5
2.4 Particular and Severe Operating Conditions . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . 5
2 4 1 Definitions: . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . 5
2.5 Maximum compliance interval for maintenance operations . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6
2 5 1 Definition of the margins .. .. . .. .. .. .. .. .. . ..
.. . .. . .. . .. .. .. .. .. .. . .. .. . .. .. . .. .. .. . .. ..
.. 6
2.5.1.1 lntetals classified as 2-star intervals .. .. .. .. ..
.. .. .. .. .. .. .. .. .. .. .. .. . .. .. . 6
2.5.1.2
lnte als
classified
as
1-star intervals .. .. .. .. . .. .. . .. .. . .. .. .. .. .. ..
.. .. . .. . 7
2.5.22 5 1 ~ u m m a ~ t ~ r ~ ~ ~ ~ ~ ~ ~ . ~ i ~ i . ~ ~ . ~ ~
. ~ ~ ~ ~ . ~ ~ ~ . ~ . ~ i ~ ~ .. ~ ~ ~ ~ t . ~ ~ : : : : : : : :
: : : : : : : : : : : : : : : : : : : : : : : : : :
2.5.3 Use of the margins . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . 8
2.6 Authorization to
in
tall and transfer a component (part or assembly) from one
aircraft
version to another aircraft version . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . 9
2 6 1
Components not Subject to In-Service Monitoring .. . .. .. .. ..
. .. .. .. . .. . .. .. .. .. .. .. .. 9
2.6.2 Components Subject to In-Service Monitoring .. .. .. .. ..
.. . .. . .. .. .. .. . .. .. ..
..
.
.. ..
.. . 9
2.6.2.1 Transfer Authorization . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . 9
2.6.2.2 Components Subject to a Service Life Limit (SLL) . . . .
. . . . . . . . . . . . . . . . . . . . . . 9
2.6.2.3 Components Subject to an Operating Time Limit (OTL) . .
. . . . . . . . . . . . . . . . . . . 9
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Title
Page
1 INTRODUCTION
2
PRESENTATION OF THE INFORMATION
3
AIRCRAFT MAINTENANCE
3 1 Scheduled Maintenance Operations Classified by
Chapter/Section: Section 05 20 01 2
3 2
Scheduled Maintenance Operations Classified according to the
Recommended Inspection
Schedule: Section
05 20 02 2
3 3
Unscheduled Maintenance Operations e.g. : After Component
Replacement) : Section
05 20 03 2
3 4
Daily Checks . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . .
3
3 5
Additional Checks . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . .
3
3 6
Basic Inspection . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . .
3
3.7 Major Inspection G) . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . 4
4
MARGINS APPLICABLE TO MAINTENANCE INTERVALS . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
.
5
05 20 HOW TO US THE TABLES . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . 1
GENERAL PRESENTATION
2
DESCRIPTION
3
DOCUMENTATION
4
LIMIT
5
CL 1
05 50 SPECIAL MONITORING . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . 1
GENERAL
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~ - 3 9 C O P T E R
M INTEN NCE PROGR M
TR NSMITT L LETTER
1 INSTRUCTIONS
- Check that the content of the sections is in accordance with
the List of Effective Pages .
- Return the acknowledgment card.
2 OUTLINE O THE REVISION
The revision is codified as follows:
- Revision
013
frozen: 2012.07.02.
3 DETAILED DESCRIPTION
Section 05-10-00
ATA 26 21 ENGINE FIRE EXTINGUISHERS
- Modification of date code without technical modification.
Section 05-20-01/02 The scheduled maintenance operations)
ATA 26 21
ENGINE FIRE EXTINGUISHERS
~ - Modification
of
date code without technical modification.
ATA 28 11
OPT - PRESSURE REFUELLING
- 28/11/00/000/000/000
PRESSURE REFUELLING SYSTEM
Description
and
documentation modified: MET 28.11.00.503 added.
ATA 34 11 PITOT-STATIC SYSTEM INSTRUMENTS
- 34/11/00/601/000/010
AIR DATA SYSTEM
New task integrated.
ATA 55-10 HORIZONTAL STABILIZER
500 H
500 H//2 Y
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~ 3 _ 9 C O P T E R
MAINTENANCE PROGR M
TR NSMITT L LETTER
1 INSTRUCTIONS
- Check that the content of the sections is in accordance with
the List of Effective Pages .
- Return the acknowledgment card.
2 OUTLINE OF THE REVISION
The revision is codified as follows:
- Revision 012 frozen: 2012.03.22.
3 DETAILED DESCRIPTION
Section
SB
LIST
- Addition of service bulletins:
SB 05.00.88: TIME LIMITS - MAINTENANCE CHECKS - ICE AND RAIN
PROTECTION -
De-icing system slip-ring ATA 30-60).
SB
05.00.90: TIME LIMITS - MAINTENANCE CHECKS - Changes to the
maintenance intervals
of transformer-rectifiers MP/N 684-1009-200 ATA 24-30 and ATA
25-64).
Section INTRO
- Paragraph
2.6.2.1
modified.
Section 05 10 GENE
- Paragraph modified.
Section 05 1 0 00
ATA
25-66 OPT - EMERGENCY LOCATOR TRANSMITTER
- 25/66/00/000/000/115
B T T E R ~ RECHARGEABLE
Description modified.
ATA 30-60 OPT - DE-ICING SYSTEM
OTL 4 Y
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25/64/02/000/000/11 0
EMERGENCY ELECTRICAL HOIST TRANSFORMER RECTIFIER
Documentation modified.
3500 H//6 Y
ATA 25 69 OPT LIFE RAFTS
25/69/1 0/602/000/000
SPONSON MOUNTED LIFE RAFT
Title and documentation modified.
25/69/10/602/000/010
SPONSON MOUNTED LIFE RAFT
New task integrated.
ATA 26 11 ENGINE FIRE DETECTION
26/11
/00/501 /000/01 0
FIRE DETECTION
Description modified.
ATA 30 42 WINDSHIELD WIPERS
30/42/00/602/000/000
MOTOR BRUSHES
Task deleted.
ATA
34 11
PITOT STATIC SYSTEM INSTRUMENTS
34/11
/00/601 /000/01 0
STATIC PRESSURE VALVE
Task deleted.
ATA
52 11
SIDE DOORS
52/11 /01 /602/000/000
SIDE PLUG DOOR
Description modified.
ATA 62 35 MAIN ROTOR HUB/SHAFT
62/35/00/000/000/115
MAIN ROTOR HEAD/MAST
Description modified.
62/35/00/000/000/120
MAIN ROTOR HEAD/MAST
Description modified.
500 H
500 H
500 H
2 y
500 H
250 H
y
Y
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~ Q C O P T E R
65 1 0 00 000 000 340
TAIL ROTOR DRIVE
Description modified.
65 1
0/00/000/000/350
TAIL ROTOR DRIVE
Description modified.
65 1 0/00/000/000/360
TAIL ROTOR DRIVE
Description modified.
ATA 65 20 INTERMEDIATE GEARBOX
65/20/00/601/000/020
INTERMEDIATE GEARBOX
Description modified.
65/20/00/601/000/030
INTERMEDIATE GEARBOX
Description modified.
65/20/00/601/000/040
INTERMEDIATE GEARBOX
Description modified.
MAINTENANCE PROGR M
Y
Y
y
Y
Y
y
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-: B9COPTER
M INTEN NCE PROGR M
No
01.00.45
05.00.44
05.00.46
05.00.47
05.00.48
25.00.79
63.00.58
05.00.62
05.00.61
30.00.56
05.00.30
05.00.69
05.00.75
05.00.79
05.00.83
25.02.11
30.00.56
34.00.40
05.00.82
05.00.86
63.00.68
64.00.31
05.00.88
05.00.90
LIST OF SERVICE BULLETINS INCORPOR TED
Frozen revision
date
Subject
2006.04.07
2007.04.30
2007.04.30
2007.09.20
2008.09.01
2010.10.11
2010.10.11
2010.10.11
2010.10.11
2010.10.11
2010.10.11
2010.10.11
2010.10.11
2011.06.09
2012.03.22
2012.03.22
Main rotor blades leading edge inspection (superseded by
SB No.
05.00.46)
ATA
62-1 0)
Checking the TGB for angular play ATA 64-20)
Main rotor blades leading edge and blade tip fairing check
ATA 62-1 0)
X-Ray inspection of MGB suspension bars ATA 63-32)
Ventilation flap control tangential bar
ATA
76-20)
Mechanical release control unit (Sling installation)
ATA
25-81)
Engine-to-MGB 23000 rpm input coupling
ATA
63-28)
Check and replacement of engine fire extinguishers
ATA
26-21)
Tail
boom - Check of the skin at frame 9000 or 9900 ATA
53-1 0)
Heater mat wiring modification
ATA
30-20)
Addition of a calendar time limit for the dynamic assemblies
which are
maintained: - According to On-Condition procedures. - According
to
their TBO
ATA
60-00)
Main Rotor Servo-control Attachment Bolts
ATA
67-30)
TIME LIMITS - MAINTENANCE CHECKS - Addition of a periodic
check
of the engine fuel flow control
ATA
76-00)
LANDING GEAR - Check of the landing gear hydraulic unit ATA
32-30)
TIME LIMITS - MAINTENANCE CHECKS - Side plug doors ATA
52-11)
EQUIPMENT AND FURNISHINGS - Check
of
the inflation control system
of the optional life-raft installation ATA 25-69)
ICE AND RAIN PROTECTION - Heater mat wiring modification
ATA
30-20)
NAVIGATION - Maintenance
of
radar antenna slaving units
ATA
34-42)
TIME LIMITS - MAINTENANCE CHECKS - Emergency floatation
gear:
Untimely deployment
ATA
25-62)
TIME LIMITS - MAINTENANCE CHECKS - Alternator bearings
ATA
24-20)
MAIN ROTOR DRIVE - Rotor brake control lever improved rotor
brake
control lever operation corresponds
to MOD
0726696 ATA 63-23)
TAIL ROTOR - Maintenance applicable
to
the TRH pitch control
rod
bearing
in
the event of a hydraulic fluid leak
ATA
64-20)
TIME LIMITS - MAINTENANCE CHECKS - ICE AND RAIN
PROTECTION - De-icing system slip-ring
ATA
30-60).
TIME LIMITS - MAINTENANCE CHECKS - Changes
to
the maintenance
intervals of transformer-rectifiers MP/N 684-1009-200 ATA 24-30
and
ATA 25-64).
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~ 3 9 C O P T E R
M INTEN NCE PROGR M
INTRODUCTION
1 GENERAL
1 1 Scope of the Maintenance
Program
The Maintenance Program
(PRE) is
drawn
up by
the aircraft manufacturer
and
it gives
all
the
maintenance operations that are to
be
performed by the operator.
It
specifies the mandatory limitations
and
operations to ensure that the aircraft airworthiness
is
maintained,
as
well
as
all the
operations
and
intervals, recommended
by the
manufacturer
and designed
to
ensure the operational availability of the aircraft,
irrespective of its varied
operating missions.
1 2 Classification of the information
The
intervals specified
in
this
PRE
are
classified according
to
their importance into three
categories coded with stars (*):
**
Intervals
are
considered
to
be
mandatory. They
are
specified
in
the
Airworthiness
Limitations section.
No
margins
are
permissible.
Any changes to
an
interval can
be
negotiated only with the Manufacturer (EUROCOPTER)
and the EASA
(European Aviation Safety Agency).
*
Intervals beyond the margin
can be
adjusted subject
to
the approval
of
the Manufacturer
(EUROCOPTER)
and
supervisory authorities. The permissible margin complies
with
Paragraph 2.5, unless
No
margin permissible
is
specified.
Intervals beyond the margin with
no
distinctive signs
can be
adjusted subject
to
the
approval
of the
Manufacturer (EUROCOPTER), providing compliance with the
applicable
local authorities' regulations
is
ensured. The adjusted margin complies with Paragraph 2.5.
NOTE
The
*
or
**
classification can also be used
in
other manuals
(e.g. the
Maintenance Manual
(MET)).
In
this case,
it
applies
to
the procedure.
For example, a procedure
can
be classified **
with
an
interval not classified
**
.
1 3 Airworthiness Limitations
The airworthiness limitations are always subject
to
approval by the European Airworthiness
Authorities.
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G ~ 3 9 C O P T E R
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The operating time limits specified for the components guarantee
flight safety with respect to
the
stress to which they are subjected. These limits
do
not constitute a commercial warranty.
It may be
necessary
to
remove
the
components before
the
listed time, based
on
other criteria
such as wear, fretting, corrosion ..
The only warranty applicable to the helicopter and to the
components is that included in the
purchase agreement.
2 DEFINITIONS
2 1 Aircraft Maintenance
THE INITIAL
DATE
FOR AIRCRAFT AIRFRAME
AGING IS THE DATE THAT IS MARKED ON THE
IDENTIFICATION PLATE OF THE HELICOPTER
Maintenance covers
all the
operations intended to maintain
the
aircraft airworthiness, flight
readiness
and
performance in the course
of time.
It
includes monitoring, servicing
and the
repair of aircraft components
as
defined in
the
different
manuals, taking into account
all the
information that
the
aircraft manufacturer may need
to
pass
on
to
the operator Service Bulletins, Service
Telex,
Information
Telex,
Service Letters
... .
2 2 Types of
Maintenance
2 2 1
PREVENTIVE MAINTENANCE
Which
means all
scheduled, usually recurrent, actions
to
check
and
maintain a given
operational level.
2 2 2 CORRECTIVE MAINTENANCE
Which
means all the actions carried out further to a failure or a
fault to restore the initial
operational level.
2 2 3 REMEDIAL MAINTENANCE
Which
means
all
the
actions designed
to
correct
an
anomaly and enable all or part of
the
preventive
and
corrective maintenance associated
with
this anomaly to
be
discontinued.
2 3 Maintenance Procedures
There
are
three
main
maintenance procedures:
- hard time maintenance,
-
on
condition maintenance,
- condition monitoring.
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~ B C O P T E R
MAINTENANCE PROGRAM
defects that might affect the surface, the protection
and
paint coat of
the
components.
These defects must
be
examined
and
repaired immediately
in
compliance with the
applicable directives (criteria, then reconditioning).
Components and assemblies subject
to
OC maintenance are listed in Section
05.1 0.00.
The inspection intervals and the MET work cards
on
which the inspections are detailed,
are given
in
Section 05.20.01/02/03 of this
PRE.
The airworthiness inspection checks
are
marked
**
(two stars)
in
Section
05.20.01/02/03
and
called CHK
in
Section 05.99.00 of this
PRE.
2.3.3 Condit ion Monitoring
Remedial action
is
taken
on
a component subject
to
condition monitoring only after a
fault has been detected
on
it (without affecting flight safety).
The fault may be evidenced during a maintenance operation or
in
service. These
components are not therefore listed
in
a special chapter of this PRE.
2.4 Particular and Severe Operating Conditions
Certain climatic conditions are considered
to be
particular operating conditions.
They basically relate
to
operation:
-
in
damp tropical atmosphere
-
in
salt-laden atmosphrere
-
in
sand- and/or dust-laden atmosphere
-
in
cold weather
-
in
very cold weather
The limitations
and
maintenance procedures pertaining
to each
type of operating conditions
are covered with
all the
other tasks (refer
to
Sections 05.10.00
and
05.20.01 /02/03). The
particular operating condition
is
specified
in
the relevant task.
In these operating conditions,
in
addition to the routine maintenance operations, it is
necessary to apply the recommended preventive procedures
as
per Work Card 05.52.00.301.
As
no particular interval is specified, the operator will repeat
these procedures according to
his own
experience gained
in
corresponding conditions.
2.4.1
Definitions:
Damp tropical atmosphere:
Helicopters operating
in the
following conditions: combinations
of high
temperatures
and
high humidity levels (from +
28
C
and 75 %
relative humidity).
Salt-laden atmosphere:
Helicopters operating
in the
following conditions:
- Helicopters based
on
a ship or based less than 1
km
inland for more than 50 of
the time,
or
- Flying offshore at low altitude (below 1 000 feet) for more
than 5 of the time.
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YJ39COPTER
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2.5.1.2
2.5.1.3
Specific case:
Not applicable.
Intervals classified
as
1-star intervals
General
rule:
A margin
of 10%
limited:
-
to 300 H, for intervals expressed in flight hours,
-
to
6 months, for intervals expressed
in
calendar time,
- Not limited, for intervals expressed
in
a number
of
cycles or operations.
Important: This margin
of 10%
is
not
specified
in the
tasks concerned.
Specific case:
-
If
a specific margin
is
defined,
it is
specified
in the
task concerned.
-
If the
margin
is
equal
to
0, a no margin permissible annotation
is
specified
in
the task concerned.
Intervals classified
as
intervals with
no
star
General
rule:
A margin
of 10%
limited:
- to
300 H,
for intervals expressed
in
flight hours,
-
to
6 months, for intervals expressed
in
calendar time,
- Not limited, for intervals expressed in a number
of
cycles or operations.
Important: This margin
of
10% is
not
specified in the tasks concerned.
Specific case:
Not
applicable.
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The
next application
of
this same maintenance operation A shall
be
carried out
at the
latest
at
X + Y i.e. 600 +
60
660 H.
In
all
cases, the interval between two maintenance operations shall not
exceed the
maximum interval i.e. X +
Y
This principle is identical for intervals expressed
in
calendar time or cycles.
2 6 Authorization to install and transfer a component part or
assembly) from one
aircraft version to another aircraft version
2 6 1
Components not Subject
to
In-Service Monitoring
2.6.2
2.6.2.1
2.6.2.2
2.6.2.3
2.6.2.4
Transfer of components not subject
to
in-service monitoring
is
authorized between any
versions;
in
particular, the mixability
of
such
components
is
thus authorized between civil
and
military versions.
Components Subject to In-Service Monitoring
Transfer Authorization
Transferring a component (part
or
assembly) listed
in the
PRE
from an
aircraft
version x to
an
aircraft version y
is
authorized only if the following conditions are
met
simultaneously:
- the aircraft versions x
and
y
are
those
in
the following list of SUPER
PUMA
versions:
AS
332
C,
332
C1,
332
L,
332 L
1,
332 L2 and
EC225.
The installation of components from any other aircraft version
or type is prohibited,
- the part number of the component
to be
transferred
is
listed both
in
the
PRE of
version
x and
in
the
PRE
of version
y ,
-
no
temporary limitation for the component to be transferred is
assigned in the
PRE
of version x or
in
the
PRE
of version
y ,
- it
is
prohibited
to
install version-specific
MOX
parts (parts resulting
from
a version
PUMA),
- it
is
prohibited
to
install version-specific
KUH [P]
or GTV parts.
Components Subject
to
a Service
Life
Limit
(SLL)
The transfer rules are defined
in
AIRWORTHINESS LIMITATIONS Section 05-99-00
of
this
PRE.
Components Subject
to an
Operating Time Limit (OTL)
Transfers
are
only authorized when the OTL limits are
the
same
and
final for each
of the versions.
The flight hours, cycles or calendar time
to be
logged
on
the new
version must
be
added to the flight hours already logged.
Components Subject to a Time Between Overhauls (TBO)
Transfers
are
only authorized when the TBO limits are
the
same
and
final for
each of the versions.
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GLOSS RY
ABBREVIATIONS USED
A Basic inspection with a calendar interval
ALF:
ALL MP/N:
BFF:
C
CHK:
CSS:
CT:
D
E
EXC:
FC
G:
H
HT
INF:
M
MCM:
MEM:
MET:
MP/N:
NO
NOT
OC:
OpC:
OPT:
OTL:
S
SLL:
S/N:
T
TA
TBO
TSI
TSM
U
Y
:
:
Check After the Last Flight of the day
All part numbers
Check Before the First Flight
of
the day
Major inspection with a calendar interval
Airworthiness inspections
Chapter/Section/Subject
Work Card
Day
Maintenance due time
Except, except for
Functional Check
Major inspection with
an
interval
in
hours
Hour
Hard Time
Infinite service life
Month
Component Maintenance Manual
Engine Maintenance Manual
Maintenance Manual
Manufacturer's Part Number
Not Described
Non destructive Testing
On Condition Maintenance
Operational Check
Optional
Operating Time Limit
Supplementary inspection
Service Life Limit
Serial Number
Basic inspection with
an
interval
in
hours
Turn around check
Time Between Overhauls
Time Since Installation
Time Since Manufacture
Operating cycle
Year
Or - (See Section HOW TO USE THE PRE )
And
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M INTEN NCE PROGR M
HOW T USE THE PRE
GENERAL LAYOUT
The Maintenance Program PRE) is made
up
of the following sections:
05 1
0-00 Intervals
This section lists the components subject to an Operating Time
Limit OTL) or to a
limited Time Between Overhauls TBO) together with their
corresponding intervals.
This section also lists the assemblies subject to On-Condition
maintenance OC).
05-20-00 Maintenance Operations
This section lists the maintenance operations and their
intervals
in
all the aircraft
operating conditions. It includes three sub-sections:
- 05-20-01 scheduled maintenance operations classified by
Chapter/Section),
- 05-20-02 scheduled maintenance operations classified by
intervals),
- 05-20-03 unscheduled maintenance operations classified by
Chapter/Section).
For maintenance operations to
be
performed after incidents or during storage, refer to
the Maintenance Manual MET Chapter 05) or the Storage Manual
MST) respectively.
Refer to the Engine Handbook for maintenance operations to be
performed on the
power plant.
05-50-00 Special Monitoring
This section groups all the maintenance actions that are to be
taken subsequent to
certain incidents or anomalies.
05-99-00 Airworthiness Limitations
This section lists all the components subject to a mandatory
airworthiness limit SLL or
CHK) which must be applied in addition to the indications given
in the other sections of
this manual.
The aircraft maintenance is to be carried out using all this
information making reference to the
Work Cards in the Maintenance Manuals specifying the operating
procedures.
NOTE
When applicable, depending on its necessity, the
operational procedure may
be
classified according
to the star codes defined in the Introduction to this
section.
In
addition to the information contained in the PRE, the aircraft
manufacturer may require
additional monitoring operations or the embodiment of
modifications.
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~ ~ o p t e r
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PROGRAM
The effectivity (helicopter type
and
version)
is
indicated on
the
TITLE page
and
repeated at the
bottom of each page of
the
PRE.
4 MODIFYING AND UPDATING THE PRE
Each time he receives a revision
from
the aircraft manufacturer, the operator must update his
documentation. To this end, he will use the LIST OF EFFECTIVE
PAGES given in both the
MAINTENANCE PROGRAM and AIRWORTHINESS LIMITATIONS sections. The
date indicated at
the bottom of each page in each section
must
correspond to that indicated in these lists.
There are different types of Revisions: the Temporary Revision
(TR), the Normal Revision (NR)
and the Customer Complement (CC).
4 1
Temporary Revision TR): Printed on yellow paper
4.1.1 General
EUROCOPTER may need to change points they consider to
be
important
in
the manual
between two normal revisions,
and
they do this by issuing Temporary Revisions.
The Temporary Revision covers crucial information that must be
passed on rapidly and
cannot wait until the next Normal Revision
NR).
Several TRs may be issued between
two NRs.
The new DUs, whether revised or deleted, are issued
in
full on yellow paper. Changes
are identified by thick vertical lines
in
the right margin. TRs are identified by the number
of the next NR followed by a letter taken in alphabetical
order
and
by a date: e.g.: 003b
identifies the second
TR
of the NR 002.
4.1.2 Content and Application
The Temporary Revision
is
made
up
of a Highlights unit, a List of Effective Pages
LOEP-TR and one or more Document Units.
The Highlights unit lists the major points covered by the TR.
This information is issued
for each new TR.
The LOEP-TR identifies the new DUs, those revised and those
deleted by the Temporary
Revision. The date marked on the DU
is
that of the TR
by
which
it
was modified. This
list
is
to be inserted at the beginning of the corresponding manual and,
when necessary,
it
supersedes that issued previously. This list must
be
kept until the next NR.
The new DUs, those revised and those deleted:
- the new DU on yellow paper is to be inserted directly in the
manual,
-
the
revised DU on yellow paper entirely supersedes the related DU
issued on white
paper. The
DU on
white paper
is
to
be
removed from the manual.
- the DU that
is
to
be
deleted by the
TR is
issued on a single yellow page marked
DELETED . This page supersedes all the white pages of the
Document Unit in
question and the white pages are to be removed from the
manual.
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M INTEN NCE PROGR M
OPTION L EQUIPMENT
1 COMPATIBILITY INCOMPATIBILITY
A system designed for specific operational requirements may
sometimes impede other functions.
This incompatibility may be encoutered at two different
levels:
In operation. The operating incompatibility of optional
equipment is specified
in
the Flight Manual.
On installation on the aircraft:
- either provision is ensured on the helicopter for two optional
systems but they cannot be
installed at the same time: installation incompatibility.
- or two optional systems can
be
installed at the same time provided that at least one of the
systems is modified: compatibility subject to certain
conditions.
The following table lists the approved optional equipment and
specifies any incompatibility,
capabilities subject to conditions and indicates when
consequences on the helicopter operation are
specified in a Flight Manual Supplement.
2 TABLE OF THE APPROVED OPTIONAL EQUIPMENT INSTALLATIONS
INSTALLATION
CONDITIONAL
ITEM
DESCRIPTION
INCOMPATIBILITY WITH
INSTALLATION
INCOMPATIBILITY WITH
Pilot's and Copilot s
47
Comfortable Seats
4CC Ice Detector
5 6
5
LEIGH Ice Detector
4
6
6
ROSEMOUNT Ice Detector
5
4
9
Ice-Trap System
16
SFIM Three-Axis Coupler
18
Installation
18
SFIM Four-Axis Coupler
16
Installation
26
Emergency Flotation Gear
27, 28
31 (1)
with External Fuel Tanks
27
Emergency Flotation Gear
26, 45, 46
31
( 1)
without External Fuel Tanks
28
Life Rafts in Sponsons
26, 45, 46
31
Skis Installation
(2) 36, 37 (1)
32
Semi-Retractable Main
Landing Gear
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M INTEN NCE PROGR M
INSTALLATION
CONDITIONAL
ITEM
DESCRIPTION
INCOMPATIBILITY WITH
INSTALLATION
INCOMPATIBILITY WITH
58 LOCATOR Searchlight
72
36, 37 1)
59
Incandescent Flares
60 Public Address System
36,
37
1)
61 600-Liter Cabin Fuel Tank 49, 54, 56, 57, 74, 75, 76,
39,
40,
41
(3)
77, 78
55, 76, 77
74, 75 (5)
62
Abseiling Installation
50, 53, 72, 73, 75, 81, 82
54 (6)
51, 57
70
Reinforced Soundproofing
71
71
De Luxe Reinforced 70
Soundproofing
72
LH
Stairway Door
58,
62, 79, 80
73
RH Two-Panel Hinged Door
55, 56, 62, 79, 80
74
24-Utility Seats Installation
49, 50, 53, 56,
57,
75, 76,
48, 54, 61
(5)
77, 78, 79, 80, 81, 82
75
18-Crashworthy Utility Seats
49, 50, 53, 56, 57, 74, 76,
48, 54, 61
(5)
Installation
77, 78, 79, 80, 81, 82
76-77
20 and 19 Comfortable Seats
49, 50,
53,
56, 57, 74, 75,
48, 54, 61
(4)
Installation
78,
80, 81
82
78
18-Comfortable Seats
+
Toilet
49,
50,
53,
56,
57, 74,
75, 48, 54,
61
(4)
Installation
76,
77, 81
82
79
Baggage Hold Compatible
57, 72, 73, 7
4,
75, 79, 81,
with 20-Seats Installation
82, 83
80 Baggage Hold Compatible with
57, 72, 73, 74, 75, 79, 81
18-Seats + Toilet Installation
82,
83
81 10-12 VIP Seat Installation
48, 49, 50, 53, 54, 55, 56,
57, 61 62, 74, 75,
76,
77,
78, 79, 82
83 Aft Stairway Door 57, 70, 80
Legend:
1 ): Compatibility not demonstrated.
2): Incompatible with the tie-down function
in
the main landing gear wheel hub.
3): Incompatible with pressure refueling system.
4)
Compatible after removal of the front or rear seats.
5) Compatible after removal of the front seats.
6)
Compatible after re-arranging the seats.
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G
~ B C O P T E R
MAINTENANCE PROGR M
GENER L
1 INTRODUCTION
This section lists the components and assemblies subject to
an
operating time limit OTL) or a
limited time between overhauls TBO) together with the
corresponding intervals.
This section also lists the assemblies that are subject
to on
condition maintenance OC). The
inspection intervals of these assemblies are specified
in
this
PRE in
section 05.20.01/02.
The components are presented according
to ATA
standard 100 breakdown.
2 INTERVALS
For each component mentioned
in
this Section, the interval limit applies
to
the part number(s)
listed
and to all
successive dash numbers.
The
operator must confirm the validity of the installation of dash
numbers with the EUROCOPTER
Customer Service Technical Support Department.
For
particular operating conditions, refer
to
the information given
in
Section INTRODUCTION
paragraph 2.4.
2 1
Operating
Time
Limit OTL)
Refer to Section INTRODUCTION, of this
PRE
for the definition of the operating time limit.
It may
be
expressed
in
flight hours, as a calendar time limit or as a number of
cycles/utilizations.
When several limits are indicated, the component
in
question must
be
removed
at
the first
limit reached.
2 2
Time Between Overhauls TBO)
Refer
to
Section INTRODUCTION, of this
PRE
for
the
definition
of
time between overhauls.
It
may
be
expressed
in
flight hours,
as
a calendar time limit or
as
a number
of
cycles/utilizations.
When several limits
are
indicated, the component
in
question must
be
removed at the first
limit reached.
A TBO applies to all the components of the assembly
indicated.
3 INITIAL DATE OF EQUIPMENT AGING
Generally, the date
to be
taken into account
is
the date of first installation or first depreservation
of
the
equipment. This date
is to be
recorded
on
the equipment
log card
(FME).
In
some cases, the date
to be
taken into account
is
the date since manufacture recorded
on
the
equipment
log
card FME). In this case, the statement time since manufacture is
indicated
in
the
DESCRIPTION column
in
this
PRE
section.
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M INTEN NCE
PROGR M
HOW TO USE THE T BLES
1 GENERAL PRESENTATION
Description, documentation
Part number
Limit
CL
The parts, assemblies and components with a utilization or
an
operating time limit are listed
in
these tables according to the Chapter-Section-Subject breakdown
of the ATA Specification 100 in
accordance with which the aircraft technical publications are
produced).
2 DESCRIPTION PUBLICATION
The components subject to a limitation (OC, TBO, OTL) are listed
in this column.
3 PART NUMBER
3 1 General
This column gives the manufacturer s part number for the
component
in
question.
When applicable, the IPC gives the correspondence between the
manufacturer s part number
and the EUROCOPTER identification number (704A.
..
).
These part numbers are also those which are used in all the
support publications (MMA, IPC,
SBT,
etc.) and those which
can
be allocated a suffix used for spares purposes to indicate
the
installation of an optional equipment item or of a specific
configuration.
Example
The limitation given for the part number 332A33-0001-04 is also
effective for
the assembly 332A33-0001-04M1.
3 2 Presentation
Components with the same description but with different part
numbers are identified in the
following way:
MAIN OIL PUMP
4
TL:
TYPE OF LIMIT
This column defines the type of limitation:
o
on condition maintenance
31-751
03-4034-5
7034-400
7034-500
7034-600
TBO
3000 H
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G
YB COPTER
M INTEN NCE PROGR M
05 10 00 REPERTORY
Chap/Sect
Description
age
21 52 ........................ OPT
AIR
CONDITIONING.................................................
1
21 53 ........................ OPT FREON POD MOUNTED AIR
CONDITIONING................... 1
22 30
........................
MOVEMENT CONTROL . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
23 52
........................
OPT UNIT CONTROL CENTRALIZED .
........ .......
... . . .. . . . ... . . ... 1
23 71 ........................ OPT COCKPIT VOICE
RECORDER..................................... 1
24 20
........................
AC GENERATING SYSTEM . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . 1
24 30
........................ DC
GENERATING SYSTEM . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . 1
24 31 ........................ BATTERY . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . 1
25 00
........................
EQUIPMENT
AND
FURNISHING . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . 1
25 1 0 ........................ COCKPIT... . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . 1
25 62 ........................ OPT EMERGENCY FLOATATION GEAR . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
25 64 ........................ OPT HOIST.. . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . 1
25 66 ........................ OPT EMERGENCY LOCATOR
TRANSMITTER........................ 1
25 69
........................
OPT LIFE RAFTS . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
25 81 ........................ OPT SLINGS AND ACCESSORIES . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
26 13
........................
MGB FIRE DETECTION SYSTEM . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . 1
26 21 ........................ ENGINE FIRE EXTINGUISHERS . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . 1
26 22 ........................ CABIN FIRE EXTINGUISHERS . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . 1
28 10
........................
STOR
AGE.....................................................................
1
28 20 ........................ FUEL DISTRIBUTION SYSTEM
............................................ 1
28 41 ........................ FUEL FLOWMETER . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . 1
28 93
........................
OPT FUEL
ICE
TRAP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . 1
29 10
........................
MAIN HYDRAULIC SYSTEM . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . 1
29 20
........................
AUXILIARY HYDRAULIC SYSTEM . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . 1
30 20 ........................
AIR
INTAKES . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . 1
30 42 ........................ WINDSHIELD WIPERS . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . 1
30 60 ........................ OPT DE ICING SYSTEM . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . 1
31 20 ........................
CHRONOGRAPH.............................................................
1
32 12 ........................ RETRACTABLE MAIN LANDING GEAR . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1
32 22
........................
NOSE LANDING GEAR . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
32 40 ........................ WHEELS AND BRAKES . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . 1
32 91 ........................ OPT SKIS . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . 1
33 20 ........................ OPT PASSENGER COMPARTMENT
LIGHTING . . . . . . . . . . . . . . . . . . . . . . . 1
33 43
........................
LANDING LIGHT . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . 1
33 45
........................
OPT SEARCHLIGHT . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
34 42 ........................ RADAR . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . 1
34 43 ........................ OPT NAVIGATION COMPUTER . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . 1
35 30 ........................ PROTECTION AGAINST
SMOKE.......................................... 1
36 1 0 ........................ P2 SUPPLY SYSTEM . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . 1
45 11 ........................ OPT
HUMS/CVFDR........................................................
1
47 50
........................
OPT FUR INSTALLATION . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . .. . . . . 1
55 10 ........................ HORIZONTAL STABILIZER . .
...
. ..... ... . . . .
...
.. . ....... .. . . . .....
...
.
...
. 1
62 35
........................ MAIN
ROTOR HUB/SHAFT . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . 1
62 37 ........................ BLADE PITCH CHANGE
ROD
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . 1
63 10
........................
ENGINE TO MGB
COUPLING..............................................
1
63 20 ........................ MAIN GEARBOX . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . 1
63 21
........................ OIL FILTER . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 1
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Description, document tion
21 52
OPT AIR CONDITIONING
21/52/00/201/000/000
REGULATION FILTER FILTER ELEMENT
M T 21 52 00 201
Regulation filter
2
08ZE4.
Fitted
to
the air-conditioning units 3502A03
and 3502A04.
No
margin permissible.
21/52100/402/000/000
TURBO FAN COOLING UNIT
M T
21 52 00 402
Part number
CN15-05UJ
3202A0101
3202A0201
320280101
320280201
MAINTENANCE PROGRAM
T
21 52
TL
Limit
CL
OTL
1200 H
T8
1200 H
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~ o p t e r
MAINTENANCE PROGRAM
T
21 53
Description document tion Part number
Limit
21 53
OPT
FREON
POD MOUNTED
AIR CONDITIONING
21/53/00/401/000/005
R22/R134A COLD AIR UNIT
788AA01 0101
788A040101
oc
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~ 1 9 C O P T E R
Description document tion
Part number
22 30
MOVEMENT CONTROL
22/30/00/000/000/000
AUTOPILOT HYDRAULIC UNIT DISTRffiUTOR
30245
30245-001
22/30/00/000/000/005
AUTOPILOT HYDRAULIC UNIT DISTRffiUTOR
A84122-1
010-60666
22130/00/000/000/020
AUTOPILOT HYDRAULIC
UNIT
TRIM ELECTROVALVE
30010
22/30/00/000/000/021
67-770-1
67-770-2
AUTOPILOT HYDRAULIC UNIT SERVODISTRIBUTOR
30550-401
30550-501
22/30/00/000/000/022
AUTOPILOT HYDRAULIC UNIT SERVODISTRIBUTOR
A21495
A84 2
A84121-1
M T
22 30 10 403
22/30/1 0/401/000/000
HYDRAULIC UNIT
FILTER
FILTER ELEMENT
CG0140093411
NOO
M T
22 30 10 401
This filter cannot
be
cleaned. It must be
replaced if clogging
is
detected.
MAINTENANCE PROGRAM
T 22 30
T imit
CL
TBO 6000 H
TBO 6000 H
II
15
Y
TBO 6000 H
TBO 6000 H
TBO 6000 H
II
15 Y
OTL
3000 H
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MAINTENANCE PROGRAM
Description, document tion
Part number TL
23-52
OPT
-
UNIT CONTROL
CENTR LIZED
23/52/00/000/000/000
ETC 40XXF INSTALLATION, GPS/PTTI INTERFACE
C RD
- BATTERY
MET 23 52 XX 401
itted to the interface card 222-7012-201.
The operating time limit must
not
exceed
the
life
limit since manufacture.
No margin permissible.
23/52/00/000/000/0 10
222-3025-905 OTL
ETC 40XXF INSTALLATION, GPS/PTTI INTERFACE C RD - BATTERY
MET 23 52 XX 401
itted to the interface card 222-7012-201.
Life
limit since manufacture.
No margin permissible.
222-3025-905 OTL
T
23-52
Limit
CL
1
y
5 y
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~ ~ B f C O P T E R
Description document tion
Part number
23 71
OPT COCKPIT VOICE RECORDER
23 71 01 /40 1 000/005
COCKPIT VOICE RECORDER
M T 23 71 XX 401
93A1 00-31
93A100-80
MAINTENANCE PROGRAM
ATA
23 71
T Limit
CL
TBO
4000 H
I
I
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Description document tion
24 30
DC
GENER TING SYSTEM
24/30/00/402/000/000
TRANSFORMER RECTIFIER
MAINTENANCE PROGRAM
ATA 24 30
Part number
T
imit
CL
684-1009-200
oc
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~ ~ p t r
Description
document tion
24 31 B TTERY
24/31/00/000/000/010
4 AH BATTERY
24/31/00/000/000/21 0
STANDBY BATTERY
Part number
40208-1
40208-5
40408
EEOOOS 011
EEOOOS 0111
MAINTENANCE PROGRAM
ATA 24 31
TL Limit
CL
oc
oc
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MAINTENANCE PROGR M
T 25 00
Description, documentation
Part number
imit
25 00 EQUIPMENT
ND
FURNISHING
25/00/00/000/000/000
BELT HARNESS STRAPS MEDICAL INSTALLATION STRAPS
Life limit since manufacture.
Pilot, copilot, passenger and operator seat
belt and harness straps - Medical installation
straps.
For seat belts
and
harnesses fitted with
buckles manufactured by ANJOU refer to the
AIRWORTHINESS LIMITATIONS chapter.
Margin: 6 months
ALL MP/N OTL
10 y
*
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Description, document tion
Part number
25-10
COCKPIT
25 1 0 00 000 000 01
0
PILOT S
AND
COPILOT S
SEAT SHOCK ABSORBERS
No margin permissible.
25/1 0/00/000/000/020
251 1 02900-01
251 1 02900-02
3RD CREW MEMBER S SEAT SHOCK ABSORBER
2510107900
2510107901
No margin permissible.
MAINTENANCE PROGRAM
ATA 25-10
TL Limit
CL
OTL
5
y
OTL
5 y
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Description
document tion
Part number
25 62 PT EMERGENCY FLOTATION GEAR
25/62/00/401/000/000
FORWARD CYLINDER
M T
25 62 00 401
Return the equipment to an approved repair
station for overhaul and replacement of the
unequipped bottle.
Interval starting from the date of manufacture.
No margin permissible.
25/62/00/401/000/020
FT CYLINDER
M T
25 62 00 401
Return the equipment to an approved repair
station for overhaul and replacement of the
unequipped bottle.
Interval starting from the date of manufacture.
No margin permissible.
202458-0
202458-1
202458-2
202458-3
158562-0
158562-1
158562-2
158562-3
MAINTENANCE PROGRAM
TL
Limit
L
OTL
15
OTL
15
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Description document tion
25 64 O PT HOIST
25 64 00 000 000 020
HYDRAULIC HOIST 50 M CABLE
M M 25 62 21
M M 25 64 96
Life limit since manufacture in the original
packaging.
Normal climatic conditions.
No margin permissible.
25 64 00 000 000 021
HYDRAULIC HOIST 50 M CABLE
M M
25 62 21
MCM 25 64 96
Life limit since manufacture in the original
packaging.
Tropical and damp atmosphere.
No margin permissible.
25 64 00 000 000 022
HYDRAULIC HOIST 50 M CABLE
M M
25 62 21
MCM 25 64 96
Life limit since manufacture in the original
packaging.
Salt atmosphere.
No margin permissible.
Part number
709070
709070-100
709070
709070-100
709070
709070-100
MAINTENANCE PROGRAM
T 25 64
TL
Limit
L
OT
9 y
OT
7 y
OT
7 y
-
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Description, document tion
25/64/00/000/000/027
HYDRAULIC HOIST
50
CABLE
MCM 25 62 21
MCM 25 64 96
The operating time limit must not exceed the
life limit since manufacture.
Salt-laden atmosphere.
No margin permissible.
25/64/00/000/000/028
HYDRAULIC HOIST
50
M CABLE
MCM 25 62 21
MCM 25 64 96
The operating time limit must not exceed the
life limit since manufacture.
Sand-laden atmosphere.
No margin permissible.
25/64/00/402/000/000
HYDRAULIC HOIST
50
M
M T 25 64 00 402
With hydraulic motor.
No margin permissible.
25/64/00/403/000/005
HYDRAULIC HOIST SQUIB
MET 25 64 00 403
Life limit since manufacture n the original
Part number
709070
709070-100
709070
709070-100
76360-100
76360-110-01
76360-200
76360-210-01
76363-200-A
20CF4D
MAINTENANCE PROGRAM
ATA
25 64
TL
imit
CL
OTL 2 Y
II 500 U
OTL 2 Y
II
500 U
TBO 4 Y
II 1000 U
OTL
5 y
