CESSNA AIRCRAFT
COMPANY
SINGLE ENGINE
STRUCTURAL REPA
IR MANUAL
to an 8 ½ by 11 inch loose leaf page and represents a frame. Horizontal rows are lettered from A
at the top to L at the bottom. Vertical columns are numbered 1 to 24. The combination of a letter
and a number id
entifies a frame (image) in the aerofiche card. The List of Chapters provides a quick
reference to information contained in the aerofiche.
5. Using the Stru
ctural Repair Manual or Aerofiche
A. Division of Subject Matter.
(1) Structural repair information is divided into chapters in accordance with Air Transport Association
Specification
100. Each Chapter is further subdivided to provide individual or related structural
member presentation.
(2) Chapter 51 provides general structural information required to perform a repair. Also included
in Chapter 51
are general repair procedures that may be accomplished in noncritical areas.
B. Effectivity Page.
(1) A list of effective pages is provided with each chapter. All pages listed are active and shall appear
in sequence as
recorded in the Effectivity Page.
(2) The Effectivity Page contains tabular listing of ATA number, page and date of each page in that
chapter. A change in the chapter requires a revision to the chapter’s Effectivity Page. The date
corresponds
to the date that appears on the individual page which defines when that page was
issued.
C. Page Numbering System.
(1) The Structur
al Repair Manual or corresponding aerofiche page numbering system consists of
the Air Transport Association Specification 100 three element numbers separated by dashes.
The page number and date are printed immediately to the right of the three element number. The
three elemen
t number is assigned to a component, with the first set of numbers corresponding
to the ATA-100 assigned chapter number.
(2) The page number complies with Air Transport Association Specification 100 for subdividing a
Structural
Repair Manual. Blocks of sequential page numbers are used to identify:
Pages 1 Through 100 - Structural Identification
Pages 101 Through 199 - Allowable Damage
Pages 201 thr
ough 999 - Repair Procedures
(3) The date which appears below the page number signifies when the page was issued. If no
revisions to that page have occurred, the date signifies original date.
(4) Illustratio
ns use the same figure numbering as the page block in which they appear. For example:
Figure 202 would be the second figure in a repair procedure.
6. Revision (Ma
nual)
A. Regular Revision.
(1) Pages to be removed or inserted in the Structural Repair Manual are controlled by the Effectivity
Page. Pages a
re listed in sequence by the three element number and then by page number.
When two pages display the same three element number and page number, the page displaying
the most recent Date of Page Issue shall be inserted into the Structural Repair Manual. The date
column on th
e corresponding chapter Effectivity Page shall verify the active page.
B. Temporary Revision.
(1) For paper publications:
(a) Temporary re
vision pages are filed in the Structural Repair Manual by replacing existing
pages in the manual. File the temporary revision cover page according to the filing
instructions on the Temporary Revision Cover Page.
(2) For aerofich
e publications:
(a) 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 maintai
ned in a notebook or binder near the aerofiche library for quick reference.
INTRODUCTION Page 2
© Cessna Aircraft Company Jun 1/2005
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