Cessna T188C - Page 5

* TEMPORARY REVISION NUMBER 3
DATED 7 January 2000
MANUAL TITLE MODEL 188 & T188 SERIES 1966 THRU1984 SERVICE MANUAL
MANUAL NUMBER - PAPER COPY D2054-1-13 AEROFICHE D2054-1-13AF
TEMPORARY REVISION NUMBER PAPER COPY D2054-1TR3 AEROFICHE N/A
MANUAL DATE 25 MARCH 1983 REVISION NUMBER 1 DATE 1 AUGUST 1983
This Temporary Revision consists of the following pages, which affect existing pages in the
paper copy manual and supersede aerofiche information.
AEROFICHE AEROFICHE
SECTION
PAGE FICHE/FRAME
SECTION
PAGE FICHE/FRAME
2 24A Added
2 28A Added
17 10A Added
17 10B Added
REASON FOR TEMPORARY REVISION
To include the inspection
requirements of
Cessna Service Bulletin
SEB99-18.
To provide additional information for the stop drilling of cracks that originate at the trailing edge
of control surfaces with corrugated skins.
FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION
For Paper Publications:
File this cover sheet behind the publication's title page to identify the inclusion of the
Temporary Revision into the manual. Insert the new pages into the publication at the
appropriate locations.
Draw a line, with
a permanent red ink
marker, through any
superceded information.
For Aerofiche Publications:
Draw a line through any aerofiche frame (page) affected by the Temporary Revision with a
permanent red ink marker. This will be a visual identifier that the information on the frame
(page) is no longer
valid and the Temporary
Revision should be referenced.
For "added"
pages in a Temporary
Revision, draw a vertical
line between the applicable
frames which is
wide enough to show on the edges of the pages. Temporary Revisions should be collected
and maintained in a notebook or binder near the aerofiche library for quick reference.
COPYRIGHT © 2000
CESSNA AIRCRAFT COMPANY
WICHITA, KANSAS, USA