STEMME S6 User manual

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
Issued: December 2010
STEMME
c2010
STEMME TSA-M
MODELS: S6
S6-RT
Doc.-No. P500-006.000 Rev. 9

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
Revision
Number
Date of
Revision
Revised
Chapters Descriptions of RevisionsDate
Inserted By
RECORD OF REVISIONS
0
1
2
3
4
5
6
7
8
9
20.12.2010
18.03.2011
28.06.2011
04.07.2011
26.09.2011
01.11.2011
18.11.2011
28.02.2012
16.03.2012
04.05.2012
--
26, 31, 91
05, 06, 21, 91
05, 11, 12, 53,
91
06, 11, 12, 20,
28, 57, 71
24, 71, 91
all
04
10, 11
05, 11, 12, 28,
31, 32, 57, 71,
72, 75
First complete Issue
Installation Fire Warning
Introduction Cabin Heating
(Option)
Introduction Aerotow Equipment
(Option)
Flap Setting Cruise -4.0°,
Documentary Changes
Introduction Solar Panel
(Option)
Introduction Retractable Landing
Gear, 900 kg MTOW (Model S6-RT),
Documentary Changes
(incl. change of header all pages)
100h TBO Front Gear Box
Introduction Wing Folding Device
(Option)
Documentary Changes, Corrections

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
Revision
Number
Date of
Revision
Revised
Chapters Descriptions of RevisionsDate
Inserted By
RECORD OF REVISIONS
0
1
2
3
4
5
6
7
8
9
20.12.2010
18.03.2011
28.06.2011
04.07.2011
26.09.2011
01.11.2011
18.11.2011
28.02.2012
16.03.2012
04.05.2012
--
26, 31, 91
05, 06, 21, 91
05, 11, 12, 53,
91
06, 11, 12, 20,
28, 57, 71
24, 71, 91
all
04
10, 11
05, 11, 12, 28,
31, 32, 57, 71,
72, 75
First complete Issue
Installation Fire Warning
Introduction Cabin Heating
(Option)
Introduction Aerotow Equipment
(Option)
Flap Setting Cruise -4.0°,
Documentary Changes
Introduction Solar Panel
(Option)
Introduction Retractable Landing
Gear, 900 kg MTOW (Model S6-RT),
Documentary Changes
(incl. change of header all pages)
100h TBO Front Gear Box
Introduction Wing Folding Device
(Option)
Documentary Changes, Corrections

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
CHAPTER 00
INTRODUCTION

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
CHAPTER 00
INTRODUCTION

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
00- TOC
Page 01
TABLE OF CONTENTS
Chapter
Section
Title Subject Page
INTRODUCTION .............................................................................................00-00-00 1
General 00-00-00 1
List of Vendor Technical Publications 00-00-00 1
Structure of Maintenance Manual 00-00-00 2
Using the Maintenance Manual 00-00-00 4
List of Chapters 00-00-00 7
List of Effective Pages 00-00-00 9
Applicable Service Bulletins 00-00-00 11
Nov 18/11

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
00- TOC
Page 01
TABLE OF CONTENTS
Chapter
Section
Title Subject Page
INTRODUCTION .............................................................................................00-00-00 1
General 00-00-00 1
List of Vendor Technical Publications 00-00-00 1
Structure of Maintenance Manual 00-00-00 2
Using the Maintenance Manual 00-00-00 4
List of Chapters 00-00-00 7
List of Effective Pages 00-00-00 9
Applicable Service Bulletins 00-00-00 11
Nov 18/11

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
INTRODUCTION
1. General
This maintenance manual provides necessary for the maintenance of the S6 information to the
maintenance personnel. It contains detailed descriptions of the systems, troubleshooting, and
maintenance practices.
In this handbook are only contained maintenance practices about jobs, which are to be practiced at the
aircraft itself: e.g. removal and installation of components.
The maintenance instructions for engine and propeller are given by their own Maintenance Manuals.
Maintenance, repairs and inspections must be accomplished in accordance with the instructions given
in this Maintenance Manual (MM).
2. List of Vendor Technical Publications
A. Use the MM in conjunction with vendor technical publications listed in the table 01.
No.
Manual No./Part No.
Manual Title
Vendor
1
Doc-No.
P400-006.000 / E / FAA
latest Revision
Airplane Flight Manual TSA-M
Model: S6 STEMME AG
2
Doc-No.
P400-006.001 / E / FAA
latest Revision
Airplane Flight Manual TSA-M
Model: S6-RT STEMME AG
3
Doc-No.
P530-901.500
latest Revision
Illustrated Parts Catalog STEMME S6 STEMME AG
4
Doc-No.
A35-10SMRE
latest Revision
Small Repairs of Composite Material
Parts for STEMME Aircraft STEMME AG
5
ROTAX Part. No. 809606,
Rev. 1, September 01/2007, or
a later Revision
Maintenance Manual (Line) for ROTAX
914 Series ROTAX Aircraft Engines
6
ROTAX Part. No. 809603,
Rev. 1, January 01/2008, or a
later Revision
Maintenance Manual (Heavy) for ROTAX
912 and 914 Series ROTAX Aircraft Engines
Table 1 - List of Vendor Technical Publications
00-00-00 Page 01
Nov 18/11

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
INTRODUCTION
1. General
This maintenance manual provides necessary for the maintenance of the S6 information to the
maintenance personnel. It contains detailed descriptions of the systems, troubleshooting, and
maintenance practices.
In this handbook are only contained maintenance practices about jobs, which are to be practiced at the
aircraft itself: e.g. removal and installation of components.
The maintenance instructions for engine and propeller are given by their own Maintenance Manuals.
Maintenance, repairs and inspections must be accomplished in accordance with the instructions given
in this Maintenance Manual (MM).
2. List of Vendor Technical Publications
A. Use the MM in conjunction with vendor technical publications listed in the table 01.
No.
Manual No./Part No.
Manual Title
Vendor
1
Doc-No.
P400-006.000 / E / FAA
latest Revision
Airplane Flight Manual TSA-M
Model: S6 STEMME AG
2
Doc-No.
P400-006.001 / E / FAA
latest Revision
Airplane Flight Manual TSA-M
Model: S6-RT STEMME AG
3
Doc-No.
P530-901.500
latest Revision
Illustrated Parts Catalog STEMME S6 STEMME AG
4
Doc-No.
A35-10SMRE
latest Revision
Small Repairs of Composite Material
Parts for STEMME Aircraft STEMME AG
5
ROTAX Part. No. 809606,
Rev. 1, September 01/2007, or
a later Revision
Maintenance Manual (Line) for ROTAX
914 Series ROTAX Aircraft Engines
6
ROTAX Part. No. 809603,
Rev. 1, January 01/2008, or a
later Revision
Maintenance Manual (Heavy) for ROTAX
912 and 914 Series ROTAX Aircraft Engines
Table 1 - List of Vendor Technical Publications
00-00-00 Page 01
Nov 18/11

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
3. Structure of the Maintenance Manual
The MM has been prepared in accordance with the Air Transport Association (ATA) Specification
Number 100 for Manufacturers Technical Data.
A. Division of Subject Matter
The MM is divided into 5 major sections. Each of these sections is subdivided into chapters. A list
of effective pages and the table of contents are provided at the beginning of each MM chapter.
(1) General Ch. 05 - 12
(2) Airframe Systems Ch. 20 - 37
(3) Structures Ch. 51 - 57
(4) Propeller Ch. 61
(5) Power Plant Ch. 71 - 80
Each chapter is separated by a cover sheet with the chapter number and the title.
B. The Page Numbering System
(1) The page numbering system consists of three-element numbers separated by dashes.
The first element of the division identify a system:
e.g. 27 –Flight Controls (a chapter)
The following element designate a subsystem in the system:
e.g. 27-30 Elevator (a section)
If a system consists of several subsystems, further sections are added:
e.g. 27 - 31 Elevator Trim control (a further section)
The last element permits the identification of the individual units in a system or subsystem.
However, this is used if it is necessary.
Example
27 - 10 - 00
Chapter/ Section/ Subject/
System Subsystem Unit
(here Flight- (here
Controls) Ailerons)
(2) When the chapter/system element number is followed with zeros in the section/subsystem
and subject/unit element number (28-00-00), the information is applicable to the entire
system.
:
00-00-00 Page 02
Nov 18/11
00-00-00 Page 03
No.
Manual No./Part No.
Manual Title
Vendor
7
ROTAX Part. No. 899470,
Rev. 0, December 01/2007, o r
a later Revision
Illustrated Parts Catalog ROTAX 912
A/F/S/UL/ULS/ULSFR and 914 F/UL ROTAX Aircraft Engines
8
ROTAX Part. No. 899643,
Rev. 01, February 01/2008, or
a later Revision
Operator’s Manual for ROTAX 914 Series ROTAX Aircraft Engines
9 E-118, Issue No. 33, September
18th, 2007 or a later Issue
Operation & Installation Manual,
Electrically Controlled Variable Pitch
Propeller
mt-Propeller Entwicklung
GmbH
10 Garmin p/n 190-00356-02,
latest revision 400W series Installation Manual Garmin International
11 Garmin p/n 190-00180-00,
latest revision GI-102A/GI-106A Installation Manual Garmin International
12 Garmin p/n 190-00149-01,
latest revision GMA340 Audio Panel Installation Manual Garmin International
13 Garmin p/n 190-00207-02,
latest revision
GTX 330/GTX330D Transponder
Installation Manual Garmin International
14 --- Operating Manual for Aero tow Release,
Type Tail Clutch E22 (german)
TOST GmbH,
Flugzeuggerätebau
München
Table 1 - List of Vendor Technical Publications (Continued)
Nov 18/11

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
3. Structure of the Maintenance Manual
The MM has been prepared in accordance with the Air Transport Association (ATA) Specification
Number 100 for Manufacturers Technical Data.
A. Division of Subject Matter
The MM is divided into 5 major sections. Each of these sections is subdivided into chapters. A list
of effective pages and the table of contents are provided at the beginning of each MM chapter.
(1) General Ch. 05 - 12
(2) Airframe Systems Ch. 20 - 37
(3) Structures Ch. 51 - 57
(4) Propeller Ch. 61
(5) Power Plant Ch. 71 - 80
Each chapter is separated by a cover sheet with the chapter number and the title.
B. The Page Numbering System
(1) The page numbering system consists of three-element numbers separated by dashes.
The first element of the division identify a system:
e.g. 27 –Flight Controls (a chapter)
The following element designate a subsystem in the system:
e.g. 27-30 Elevator (a section)
If a system consists of several subsystems, further sections are added:
e.g. 27 - 31 Elevator Trim control (a further section)
The last element permits the identification of the individual units in a system or subsystem.
However, this is used if it is necessary.
Example
27 - 10 - 00
Chapter/ Section/ Subject/
System Subsystem Unit
(here Flight- (here
Controls) Ailerons)
(2) When the chapter/system element number is followed with zeros in the section/subsystem
and subject/unit element number (28-00-00), the information is applicable to the entire
system.
:
00-00-00 Page 02
Nov 18/11
00-00-00 Page 03
No.
Manual No./Part No.
Manual Title
Vendor
7
ROTAX Part. No. 899470,
Rev. 0, December 01/2007, o r
a later Revision
Illustrated Parts Catalog ROTAX 912
A/F/S/UL/ULS/ULSFR and 914 F/UL ROTAX Aircraft Engines
8
ROTAX Part. No. 899643,
Rev. 01, February 01/2008, or
a later Revision
Operator’s Manual for ROTAX 914 Series ROTAX Aircraft Engines
9 E-118, Issue No. 33, September
18th, 2007 or a later Issue
Operation & Installation Manual,
Electrically Controlled Variable Pitch
Propeller
mt-Propeller Entwicklung
GmbH
10 Garmin p/n 190-00356-02,
latest revision 400W series Installation Manual Garmin International
11 Garmin p/n 190-00180-00,
latest revision GI-102A/GI-106A Installation Manual Garmin International
12 Garmin p/n 190-00149-01,
latest revision GMA340 Audio Panel Installation Manual Garmin International
13 Garmin p/n 190-00207-02,
latest revision
GTX 330/GTX330D Transponder
Installation Manual Garmin International
14 --- Operating Manual for Aero tow Release,
Type Tail Clutch E22 (german)
TOST GmbH,
Flugzeuggerätebau
München
Table 1 - List of Vendor Technical Publications (Continued)
Nov 18/11

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
(3) When the section/subsystem element number is followed with zeros in the subject/unit
element number (28-20-00), the information is applicable to subsystem within the system.
(4) The subject/unit element number is used to identify information applicable to units within
the subsystems.
This breakdown of the chapters provides a good overview and facilitates exchange of revised
pages. Since the most of systems are relatively simple and noncomplex, the third element is
used only at more complicated systems, i.e. if it appears necessary to treat a unit or device in
greater detail.
(5) All maintenance data given in the MM is separated into specific types of information.
That facilitates work with the manual. For this purpose, page number blocks are reserved
depending on type of information.
Page 1 - 99 Description and Operation
Page 101 - 199 Troubleshooting
Page 201 - 299 Maintenance Practices
Page 301 - 399 Servicing
Page 401 - 499 Removal/Installation
Page 501 - 599 Adjustment/Test
Page 601 - 699 Inspection/Check
Page 701 - 799 Cleaning/Painting
Page 801 - 899 Repairs
A page number as an example:
Page 301 First page with service instructions
12 - 17 - 00
14.11.08 Publication date
Servicing Battery
(6) Figures are numbered consecutively within each topic.
Example: Fig. 201 1. Illustration for maintenance
Fig. 202 2. Illustration for maintenance etc.
C. Page Order
(1) In the Front of the Manual:
Title
Record of Revisions
Record of Temporary Revisions
Introduction
(2) Each chapter begins with:
Title
Table of Contents
D. Figures
The figures within the sections of a chapter are numbered in accordance with the appropriate
page number block. Numbering is beginning by one (1) and continuous.
4. Using the Maintenance Manual
A. To obtain information about a specific system, refer to the List of Effective Chapters in front of
manual in order to find the corresponding chapter number here.
In the table of contents of the respective chapter, one then finds closer information about the
arrangement of material.
B. Effectivity and Effectivity Block
This Maintenance Manual is "customized". It includes the following effectivity identification
system to show modification and/or configurational differences.
(1) The MM starts with a List of Effective Chapters. Each chapter is listed with the date of issue
or revision.
(2) To identify the aircraft an effectivity statement (i.e. Garmin Avionics) or a six-digit numeric
indicator is shown in the effectivity column in the table of contents if applicable.
(a) The six-digit numeric indicator begins with the last three digits of the lowest assigned
number, to indicate first effectivity, and ends with the last three digits of the highest
assigned number, to indicate last effectivity, of an unbroken sequence of assigned
numbers. A hyphen is shown between the numbers. Open ended effectivity is
indicated by "999" in the last effectivity if applicable. For example: 023-999 indicates
aircraft 023 and subsequent.
(3) Effectivity Block
The system provides further direct annotation of the applicability on pages. On pages not
applicable for all models of the aircraft type, all serial numbers or equipment variants at the
bottoms left-hand corner a effectivity block appears. The effectivity identification placed
in this block may be a six-digit numeric indicator (Ref. to (2)(a)) or an effectivity
statement. (Refer to Figure 01)
All information appearing on that page applies only to the aircraft noted in the
effectivity block, respectively for aircraft equipped with mentioned item.
NOTE: Pages with no effectivity block may be followed by pages which have
effectivity blocks and vice versa and bear identical page numbers.
NOTE: The contents of pages with effectivity block extends or subsitutes the
contents of pages with identical page numbers with no effectivity block.
00-00-00 Page 0400-00-00 Page 05
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MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
(3) When the section/subsystem element number is followed with zeros in the subject/unit
element number (28-20-00), the information is applicable to subsystem within the system.
(4) The subject/unit element number is used to identify information applicable to units within
the subsystems.
This breakdown of the chapters provides a good overview and facilitates exchange of revised
pages. Since the most of systems are relatively simple and noncomplex, the third element is
used only at more complicated systems, i.e. if it appears necessary to treat a unit or device in
greater detail.
(5) All maintenance data given in the MM is separated into specific types of information.
That facilitates work with the manual. For this purpose, page number blocks are reserved
depending on type of information.
Page 1 - 99 Description and Operation
Page 101 - 199 Troubleshooting
Page 201 - 299 Maintenance Practices
Page 301 - 399 Servicing
Page 401 - 499 Removal/Installation
Page 501 - 599 Adjustment/Test
Page 601 - 699 Inspection/Check
Page 701 - 799 Cleaning/Painting
Page 801 - 899 Repairs
A page number as an example:
Page 301 First page with service instructions
12 - 17 - 00
14.11.08 Publication date
Servicing Battery
(6) Figures are numbered consecutively within each topic.
Example: Fig. 201 1. Illustration for maintenance
Fig. 202 2. Illustration for maintenance etc.
C. Page Order
(1) In the Front of the Manual:
Title
Record of Revisions
Record of Temporary Revisions
Introduction
(2) Each chapter begins with:
Title
Table of Contents
D. Figures
The figures within the sections of a chapter are numbered in accordance with the appropriate
page number block. Numbering is beginning by one (1) and continuous.
4. Using the Maintenance Manual
A. To obtain information about a specific system, refer to the List of Effective Chapters in front of
manual in order to find the corresponding chapter number here.
In the table of contents of the respective chapter, one then finds closer information about the
arrangement of material.
B. Effectivity and Effectivity Block
This Maintenance Manual is "customized". It includes the following effectivity identification
system to show modification and/or configurational differences.
(1) The MM starts with a List of Effective Chapters. Each chapter is listed with the date of issue
or revision.
(2) To identify the aircraft an effectivity statement (i.e. Garmin Avionics) or a six-digit numeric
indicator is shown in the effectivity column in the table of contents if applicable.
(a) The six-digit numeric indicator begins with the last three digits of the lowest assigned
number, to indicate first effectivity, and ends with the last three digits of the highest
assigned number, to indicate last effectivity, of an unbroken sequence of assigned
numbers. A hyphen is shown between the numbers. Open ended effectivity is
indicated by "999" in the last effectivity if applicable. For example: 023-999 indicates
aircraft 023 and subsequent.
(3) Effectivity Block
The system provides further direct annotation of the applicability on pages. On pages not
applicable for all models of the aircraft type, all serial numbers or equipment variants at the
bottoms left-hand corner a effectivity block appears. The effectivity identification placed
in this block may be a six-digit numeric indicator (Ref. to (2)(a)) or an effectivity
statement. (Refer to Figure 01)
All information appearing on that page applies only to the aircraft noted in the
effectivity block, respectively for aircraft equipped with mentioned item.
NOTE: Pages with no effectivity block may be followed by pages which have
effectivity blocks and vice versa and bear identical page numbers.
NOTE: The contents of pages with effectivity block extends or subsitutes the
contents of pages with identical page numbers with no effectivity block.
00-00-00 Page 0400-00-00 Page 05
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MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
C. Revisions
(1) Maintenance manual revisions, result by different reasons (regulation changes, technical
changes, typographical errors and so on), will be published regularly.
This manual has been prepared in loose-leaf form for ease in inserting revisions. The ATA
format in presentation and numbering allows quick reference to data in each section. Logical
and convenient Table of Contents at the beginning of each chapter to aid in locating specific
data within that chapter.
(2) Identifying Revised Material
(a) Revisions and /or additions will be identified by a vertical black line (revision bar) along
the outside of the page opposite only that portion of the printed matter that was
changed. This also applies to illustrations.
(b) When technical changes cause unchanged text to appear on a different page(s), a
revision bar will be placed in the outside margin, opposite the chapter/section/subject,
page number and date of all affected pages, providing no other revision bar appears on
the page.
00-00-00 Page 06
D. WARNINGS, CAUTIONS, and NOTES
If maintenance operations on the airplane are practiced, general safety and maintenance rules
must be always considered.
In addition, the MM contains adjuncts to the text used to highlight or emphasize important and
critical instructions.
WARNING:
HAZARD FOR MAINTENANCE PERSONNEL!
CAUTION:
HAZARD FOR SYSTEMS AND EQUIPMENT!
NOTE:
Specific information
E. Abbreviations
Where it appears reasonable, abbreviations are used. They are conforming to a recognized
standard.
Meter
Common
Meter
Plus
PSI Desired
Value (VDC)
Unit under
test
Pin 2 (blk) Pin 4 (red) 0 4.95 to 5.0 3010016,17,18
Pin 2 (blk) Pin 1 (wht) 0 1.70 to 2.10 3010016,17,18
Pin 2 (bik) Pin 3 (grn) 0 1.70 to 2.10 3010016,17,18
Pin 3 (grn) Pin 1 (wht) 0 -0.003 to +0.003 3010016,17,18
Pin 3 (grn) Pin 1 (wht) 10 0.031 to +0.034 3010016
Pin 3 (grn) Pin 1 (wht) 30 0.028 to +0.032 3010017
Pin 3 (grn) Pin 1 (wht) 60 0.028 to +0.032 3010018
77-40-00 Page 101
Feb 26/10
EFFECTIVITY
Aircraft equipped with VM 1000 Engine Management
System
Effectivity Block
Effectivity Block
Figure 01
00-00-00 Page 07
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MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
C. Revisions
(1) Maintenance manual revisions, result by different reasons (regulation changes, technical
changes, typographical errors and so on), will be published regularly.
This manual has been prepared in loose-leaf form for ease in inserting revisions. The ATA
format in presentation and numbering allows quick reference to data in each section. Logical
and convenient Table of Contents at the beginning of each chapter to aid in locating specific
data within that chapter.
(2) Identifying Revised Material
(a) Revisions and /or additions will be identified by a vertical black line (revision bar) along
the outside of the page opposite only that portion of the printed matter that was
changed. This also applies to illustrations.
(b) When technical changes cause unchanged text to appear on a different page(s), a
revision bar will be placed in the outside margin, opposite the chapter/section/subject,
page number and date of all affected pages, providing no other revision bar appears on
the page.
00-00-00 Page 06
D. WARNINGS, CAUTIONS, and NOTES
If maintenance operations on the airplane are practiced, general safety and maintenance rules
must be always considered.
In addition, the MM contains adjuncts to the text used to highlight or emphasize important and
critical instructions.
WARNING:
HAZARD FOR MAINTENANCE PERSONNEL!
CAUTION:
HAZARD FOR SYSTEMS AND EQUIPMENT!
NOTE:
Specific information
E. Abbreviations
Where it appears reasonable, abbreviations are used. They are conforming to a recognized
standard.
Meter
Common
Meter
Plus
PSI Desired
Value (VDC)
Unit under
test
Pin 2 (blk) Pin 4 (red) 0 4.95 to 5.0 3010016,17,18
Pin 2 (blk) Pin 1 (wht) 0 1.70 to 2.10 3010016,17,18
Pin 2 (bik) Pin 3 (grn) 0 1.70 to 2.10 3010016,17,18
Pin 3 (grn) Pin 1 (wht) 0 -0.003 to +0.003 3010016,17,18
Pin 3 (grn) Pin 1 (wht) 10 0.031 to +0.034 3010016
Pin 3 (grn) Pin 1 (wht) 30 0.028 to +0.032 3010017
Pin 3 (grn) Pin 1 (wht) 60 0.028 to +0.032 3010018
77-40-00 Page 101
Feb 26/10
EFFECTIVITY
Aircraft equipped with VM 1000 Engine Management
System
Effectivity Block
Effectivity Block
Figure 01
00-00-00 Page 07
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MAINTENANCE MANUAL
STEMME TSA-M
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STEMME TSA-M
5. List of Chapters
Chapter Title Date
GENERAL
00 Introduction Mar 16/12
02 General Nov 18/11
04 Airworthiness Feb 28/12
05 Time Limits / Maintenance Checks May 04/12
06 Dimensions and Areas Nov 18/11
07 Lifting & Shoring Nov 18/11
08 Leveling and Weighing Nov 18/11
09 Towing and Taxiing Nov 18/11
10 Parking, Mooring, Storage & Return to Service Mar 16/12
11 Placards and Markings
12 Servicing
AIRFRAME SYSTEMS
20 Standard Practices Airframe Nov 18/11
21 Ventilation Nov 18/11
23 Communications Nov 18/11
24 Electrical Power Nov 18/11
25 Equipment and Furnishings Nov 18/11
26Fire Detection Nov 18/11
27 Flight Control System Nov 18/11
28 Fuel
31 Indicating/Recording Systems
32 Landing Gear
33 Lights Nov 18/11
34 Navigation Nov 18/11
STRUCTURES
51 Structures - General Nov 18/11
52 Doors Nov 18/11
53 Fuselage Nov 18/11
55 Stabilizers Nov 18/11
57 Wings
PROPELLER
61 Propeller Nov 18/11
May 04/12
May 04/12
May 04/12
May 04/12
May 04/12
May 04/12
00-00-00 Page 08
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MAINTENANCE MANUAL
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STEMME TSA-M
5. List of Chapters
Chapter Title Date
GENERAL
00 Introduction Mar 16/12
02 General Nov 18/11
04 Airworthiness Feb 28/12
05 Time Limits / Maintenance Checks May 04/12
06 Dimensions and Areas Nov 18/11
07 Lifting & Shoring Nov 18/11
08 Leveling and Weighing Nov 18/11
09 Towing and Taxiing Nov 18/11
10 Parking, Mooring, Storage & Return to Service Mar 16/12
11 Placards and Markings
12 Servicing
AIRFRAME SYSTEMS
20 Standard Practices Airframe Nov 18/11
21 Ventilation Nov 18/11
23 Communications Nov 18/11
24 Electrical Power Nov 18/11
25 Equipment and Furnishings Nov 18/11
26Fire Detection Nov 18/11
27 Flight Control System Nov 18/11
28 Fuel
31 Indicating/Recording Systems
32 Landing Gear
33 Lights Nov 18/11
34 Navigation Nov 18/11
STRUCTURES
51 Structures - General Nov 18/11
52 Doors Nov 18/11
53 Fuselage Nov 18/11
55 Stabilizers Nov 18/11
57 Wings
PROPELLER
61 Propeller Nov 18/11
May 04/12
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May 04/12
May 04/12
May 04/12
May 04/12
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MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
5. List of Chapters (continued)
Chapter Title Date
POWER PLANT
71 Power Plant
72 Engine Drive Section
74 Ignition Nov 18/11
75 Engine Cooling System
76 Engine Controls Nov 18/11
77 Engine Indicating Nov 18/11
78 Exhaust Nov 18/11
79 Oil Nov 18/11
80 Starting Nov 18/11
91 Charts and Wiring Diagrams Nov 18/11
May 04/12
May 04/12
May 04/12
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CHAPTER/
SECTION/
SUBJECT PAGE DATE EFFECTIVITY
CHAPTER/
SECTION/
SUBJECT PAGE DATE EFFECTIVITY
Titel Page
Record of Revisions
00-00-00 01 Nov 18/11
00-00-00 02 Nov 18/11
00-00-00 03 Nov 18/11
00-00-00 04 Nov 18/11
00-00-00 05 Nov 18/11
00-00-00 06 Nov 18/11
00-00-00 07 Nov 18/11
00-00-00 08 May 04/12
00-00-00 09 May 04/12
00-00-00 10 May 04/12
00-00-00 11 May 04/12
00-00-00 12 May 04/12
00-00-00 13 May 04/12
00-00-00 14 May 04/12
00-00-00 15 Nov 18/11
00-00-00 16 May 04/12
00-00-00 17 May 04/12
02-Title
02-TOC 01 Nov 18/11
02-00-00 01 Nov 18/11 S6
02-00-00 02 Nov 18/11 S6
02-00-00 03 Nov 18/11 S6
02-00-00 01 Nov 18/11 S6-RT
02-00-00 02 Nov 18/11 S6-RT
02-00-00 03 Nov 18/11 S6-RT
04-Title
04-ROR 01 Feb 28/12
04-TOC 01 Nov 18/11
04-00-00 01 Nov 18/11
04-00-01 01 Feb 28/12 S6
04-00-01 02 Nov 18/11 S6
04-00-01 03 Nov 18/11 S6
04-00-01 01 Feb 28/12 S6-RT
04-00-01 02 Nov 18/11 S6-RT
04-00-01 03 Nov 18/11 S6-RT
05-Title
05-TOC 01 Nov 18/11
05-00-00 01 Nov 18/11
05-10-00 01 May 04/12
05-10-00 02 May 04/12
05-20-00 01 Nov 18/11
05-20-00 02 Nov 18/11
05-20-00 03 Nov 18/11
05-20-00 04 Nov 18/11
05-20-00 05 Nov 18/11
05-20-00 06 Nov 18/11
05-20-00 07 Nov 18/11
05-20-00 08 May 04/12
05-20-00 09 Nov 18/11
05-20-00 10 Nov 18/11
05-20-00 11 Nov 18/11
05-20-00 12 Nov 18/11
05-20-00 13 Nov 18/11
05-20-01 01 Nov 18/11 Cabin Heating
05-20-02 01 Nov 18/11 Aerotow
05-20-03 01 Nov 18/11 S6-RT
05-20-03 02 Nov 18/11 S6-RT
05-20-03 03 May 04/12 S6-RT
05-30-00 01 Nov 18/11
05-50-00 201 Nov 18/11
05-50-00 202 Nov 18/11
05-50-00 201 Nov 18/11 S6-RT
05-50-00 202 Nov 18/11 S6-RT
06-Title
06-TOC 01 Nov 18/11
06-00-00 01 Nov 18/11
06-10-00 01 Nov 18/11 S6, 001 - 012
06-10-00 02 Nov 18/11 S6, 001 - 012
06-10-00 03 Nov 18/11 S6, 001 - 012
06-10-00 01 Nov 18/11 S6, 013 - 999
06-10-00 02 Nov 18/11 S6, 013 - 999
06-10-00 03 Nov 18/11 S6, 013 - 015
06-10-00 03 Nov 18/11 S6, 016 - 999
06-10-00 01 Nov 18/11 S6-RT
06-10-00 02 Nov 18/11 S6-RT
06-10-00 03 Nov 18/11 S6-RT
06-20-00 01 Nov 18/11
06-20-00 02 Nov 18/11
06-30-00 01 Nov 18/11
06-30-00 02 Nov 18/11
06-30-00 03 Nov 18/11
06-30-00 01 Nov 18/11 Cabin Heating
06-30-00 02 Nov 18/11 Cabin Heating
06-30-00 03 Nov 18/11 Cabin Heating
6. List of Effective Pages
00-00-00 Page 10
May 04/12

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
5. List of Chapters (continued)
Chapter Title Date
POWER PLANT
71 Power Plant
72 Engine Drive Section
74 Ignition Nov 18/11
75 Engine Cooling System
76 Engine Controls Nov 18/11
77 Engine Indicating Nov 18/11
78 Exhaust Nov 18/11
79 Oil Nov 18/11
80 Starting Nov 18/11
91 Charts and Wiring Diagrams Nov 18/11
May 04/12
May 04/12
May 04/12
00-00-00 Page 09
May 04/12
CHAPTER/
SECTION/
SUBJECT PAGE DATE EFFECTIVITY
CHAPTER/
SECTION/
SUBJECT PAGE DATE EFFECTIVITY
Titel Page
Record of Revisions
00-00-00 01 Nov 18/11
00-00-00 02 Nov 18/11
00-00-00 03 Nov 18/11
00-00-00 04 Nov 18/11
00-00-00 05 Nov 18/11
00-00-00 06 Nov 18/11
00-00-00 07 Nov 18/11
00-00-00 08 May 04/12
00-00-00 09 May 04/12
00-00-00 10 May 04/12
00-00-00 11 May 04/12
00-00-00 12 May 04/12
00-00-00 13 May 04/12
00-00-00 14 May 04/12
00-00-00 15 Nov 18/11
00-00-00 16 May 04/12
00-00-00 17 May 04/12
02-Title
02-TOC 01 Nov 18/11
02-00-00 01 Nov 18/11 S6
02-00-00 02 Nov 18/11 S6
02-00-00 03 Nov 18/11 S6
02-00-00 01 Nov 18/11 S6-RT
02-00-00 02 Nov 18/11 S6-RT
02-00-00 03 Nov 18/11 S6-RT
04-Title
04-ROR 01 Feb 28/12
04-TOC 01 Nov 18/11
04-00-00 01 Nov 18/11
04-00-01 01 Feb 28/12 S6
04-00-01 02 Nov 18/11 S6
04-00-01 03 Nov 18/11 S6
04-00-01 01 Feb 28/12 S6-RT
04-00-01 02 Nov 18/11 S6-RT
04-00-01 03 Nov 18/11 S6-RT
05-Title
05-TOC 01 Nov 18/11
05-00-00 01 Nov 18/11
05-10-00 01 May 04/12
05-10-00 02 May 04/12
05-20-00 01 Nov 18/11
05-20-00 02 Nov 18/11
05-20-00 03 Nov 18/11
05-20-00 04 Nov 18/11
05-20-00 05 Nov 18/11
05-20-00 06 Nov 18/11
05-20-00 07 Nov 18/11
05-20-00 08 May 04/12
05-20-00 09 Nov 18/11
05-20-00 10 Nov 18/11
05-20-00 11 Nov 18/11
05-20-00 12 Nov 18/11
05-20-00 13 Nov 18/11
05-20-01 01 Nov 18/11 Cabin Heating
05-20-02 01 Nov 18/11 Aerotow
05-20-03 01 Nov 18/11 S6-RT
05-20-03 02 Nov 18/11 S6-RT
05-20-03 03 May 04/12 S6-RT
05-30-00 01 Nov 18/11
05-50-00 201 Nov 18/11
05-50-00 202 Nov 18/11
05-50-00 201 Nov 18/11 S6-RT
05-50-00 202 Nov 18/11 S6-RT
06-Title
06-TOC 01 Nov 18/11
06-00-00 01 Nov 18/11
06-10-00 01 Nov 18/11 S6, 001 - 012
06-10-00 02 Nov 18/11 S6, 001 - 012
06-10-00 03 Nov 18/11 S6, 001 - 012
06-10-00 01 Nov 18/11 S6, 013 - 999
06-10-00 02 Nov 18/11 S6, 013 - 999
06-10-00 03 Nov 18/11 S6, 013 - 015
06-10-00 03 Nov 18/11 S6, 016 - 999
06-10-00 01 Nov 18/11 S6-RT
06-10-00 02 Nov 18/11 S6-RT
06-10-00 03 Nov 18/11 S6-RT
06-20-00 01 Nov 18/11
06-20-00 02 Nov 18/11
06-30-00 01 Nov 18/11
06-30-00 02 Nov 18/11
06-30-00 03 Nov 18/11
06-30-00 01 Nov 18/11 Cabin Heating
06-30-00 02 Nov 18/11 Cabin Heating
06-30-00 03 Nov 18/11 Cabin Heating
6. List of Effective Pages
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MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
CHAPTER/
SECTION/
SUBJECT PAGE DATE EFFECTIVITY
CHAPTER/
SECTION/
SUBJECT PAGE DATE EFFECTIVITY
CHAPTER/
SECTION/
SUBJECT PAGE DATE EFFECTIVITY
CHAPTER/
SECTION/
SUBJECT PAGE DATE EFFECTIVITY
12-10-00 03 May 04/12 S6-RT
12-11-00 301 Nov 18/11
12-11-00 302 Nov 18/11
12-12-00 301 Nov 18/11
12-12-00 302 May 04/12
12-13-00 301 Nov 18/11
12-13-00 302 Nov 18/11
12-14-00 301 Nov 18/11
12-14-00 302 Nov 18/11
12-15-00 301 Nov 18/11
12-16-00 301 Nov 18/11
12-17-00 301 Nov 18/11
12-20-00 01 Nov 18/11
12-21-00 01 Nov 18/11
12-21-00 02 Nov 18/11
12-22-00 301 Nov 18/11
12-22-00 302 Nov 18/11
12-22-00 303 Nov 18/11 001 - 010
12-22-00 304 Nov 18/11 001 - 010
12-22-00 303 Nov 18/11 011 - 999
12-22-00 304 Nov 18/11 011 - 999
12-22-00 305 Nov 18/11
12-22-00 306 Nov 18/11
12-22-00 307 Nov 18/11
12-22-00 308 Nov 18/11
12-22-00 309 Nov 18/11
12-22-00 310 Nov 18/11
12-22-00 311 Nov 18/11
12-22-00 312 Nov 18/11
12-22-01 301 Nov 18/11 Aerotow
12-22-02 301 Nov 18/11 S6-RT
12-23-00 701 Nov 18/11
12-23-00 702 Nov 18/11
12-23-00 703 Nov 18/11
12-23-00 704 Nov 18/11
12-23-00 703 Nov 18/11 S6-RT
12-23-00 704 Nov 18/11 S6-RT
12-24-00 701 Nov 18/11
12-30-00 301 Nov 18/11
12-50-00 701 Nov 18/11
20-Title
20-TOC 01 Nov 18/11
20-00-00 01 Nov 18/11
06-30-00 01 Nov 18/11 S6-RT
06-30-00 02 Nov 18/11 S6-RT
06-30-00 03 Nov 18/11 S6-RT
07-Title
07-TOC 01 Nov 18/11
07-00-00 01 Nov 18/11
07-10-00 201 Nov 18/11
07-10-00 202 Nov 18/11
08-Title
08-TOC 01 Nov 18/11
08-00-00 01 Nov 18/11
08-10-00 201 Nov 18/11 S6
08-10-00 202 Nov 18/11 S6
08-10-00 203 Nov 18/11 S6
08-10-00 204 Nov 18/11 S6
08-10-00 205 Nov 18/11 S6
08-10-00 206 Nov 18/11 S6
08-10-00 207 Nov 18/11 S6
08-10-00 201 Nov 18/11 S6-RT
08-10-00 202 Nov 18/11 S6-RT
08-10-00 203 Nov 18/11 S6-RT
08-10-00 204 Nov 18/11 S6-RT
08-10-00 205 Nov 18/11 S6-RT
08-10-00 206 Nov 18/11 S6-RT
08-10-00 207 Nov 18/11 S6-RT
09-Title
09-TOC 01 Nov 18/11
09-00-00 01 Nov 18/11
09-10-00 201 Nov 18/11
09-10-00 202 Nov 18/11
09-20-00 201 Nov 18/11
10-Title
10-TOC 01 Mar 16/12
10-00-00 01 Mar 16/12
10-10-00 201 Nov 18/11
10-10-01 201 Nov 18/11
10-10-01 202 Nov 18/11
10-10-01 203 Nov 18/11
10-10-01 204 Nov 18/11
10-10-01 205 Nov 18/11
10-10-01 206 Nov 18/11
10-10-02 201 Mar 16/12 Wing Folding
10-11-00 201 Nov 18/11
20-10-00 01 Nov 18/11
20-10-00 02 Nov 18/11
20-10-00 03 Nov 18/11
20-11-00 01 Nov 18/11
20-11-00 02 Nov 18/11
20-11-00 03 Nov 18/11
20-11-00 04 Nov 18/11
20-11-00 05 Nov 18/11
20-11-00 06 Nov 18/11
20-11-00 07 Nov 18/11
20-11-00 08 Nov 18/11
20-11-00 09 Nov 18/11
20-11-00 10 Nov 18/11
20-11-00 11 Nov 18/11
20-11-00 12 Nov 18/11
20-11-00 13 Nov 18/11
21-Title
21-TOC 01 Nov 18/11
21-00-00 01 Nov 18/11
21-00-00 02 Nov 18/11
21-20-00 201 Nov 18/11
21-40-00 01 Nov 18/11 Cabin Heating
21-40-00 02 Nov 18/11 Cabin Heating
21-40-00 201 Nov 18/11 Cabin Heating
21-40-00 202 Nov 18/11 Cabin Heating
21-40-00 203 Nov 18/11 Cabin Heating
23-Title
23-TOC 01 Nov 18/11
23-TOC 02 Nov 18/11
23-00-00 01 Nov 18/11
23-10-00 01 Nov 18/11 Prof. Avionics
23-10-00 02 Nov 18/11 Prof. Avionics
23-10-00 101 Nov 18/11 Prof. Avionics
23-10-00 201 Nov 18/11 Prof. Avionics
23-10-00 01 Nov 18/11 Class. Avionics
23-10-00 02 Nov 18/11 Class. Avionics
23-10-00 201 Nov 18/11 Class. Avionics
23-10-00 01 Nov 18/11 Adv. Avionics
23-10-00 02 Nov 18/11 Adv. Avionics
23-10-00 201 Nov 18/11 Adv. Avionics
23-50-00 01 Nov 18/11 Prof. Avionics
23-50-00 101 Nov 18/11 Prof. Avionics
23-50-00 102 Nov 18/11 Prof. Avionics
10-11-00 202 Nov 18/11
10-20-00 201 Nov 18/11
10-30-00 201 Nov 18/11
11-Title
11-TOC 01 Mar 16/12
11-00-00 01 Nov 18/11
11-20-00 201 Nov 18/11
11-20-00 202 Nov 18/11
11-20-00 203 May 04/12
11-20-00 204 Nov 18/11
11-20-01 201 May 04/12 Aerotow
11-20-02 201 Mar 16/12 Wing Folding
11-30-00 201 Nov 18/11 001 - 010
11-30-00 202 Nov 18/11 001 - 010
11-30-00 201 Nov 18/11 Prof. Avionics
11-30-00 202 Nov 18/11 Prof. Avionics
11-30-00 203 Nov 18/11 Prof. Avionics
11-30-00 204 Nov 18/11 Prof. Avionics
11-30-00 201 Nov 18/11 Class. Avionics
11-30-00 202 Nov 18/11 Class. Avionics
11-30-00 203 Nov 18/11 Class. Avionics
11-30-00 204 Nov 18/11 Class. Avionics
11-30-00 201 Nov 18/11 Adv. Avionics
11-30-00 202 Nov 18/11 Adv. Avionics
11-30-00 203 Nov 18/11 Adv. Avionics
11-30-00 204 Nov 18/11 Adv. Avionics
11-30-00 205 Nov 18/11
11-30-00 206 Nov 18/11
11-30-00 205 Nov 18/11 2-Panel Airbrakes
11-30-00 206 Nov 18/11 2-Panel Airbrakes
11-30-00 205 Nov 18/11 S6-RT
11-30-00 206 Nov 18/11 S6-RT
11-30-01 201 Nov 18/11 Aerotow
11-30-02 201 Nov 18/11 S6-RT
11-30-02 202 Nov 18/11 S6-RT
11-30-02 203 Nov 18/11 S6-RT
12-Title
12-TOC 01 Nov 18/11
12-TOC 02 Nov 18/11
12-00-00 01 Nov 18/11
12-10-00 01 Nov 18/11
12-10-00 02 May 04/12
12-10-00 03 May 04/12
6. List of Effective Pages (continued)6. List of Effective Pages (continued)
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