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
Nov 18/11
Nov 18/11
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