Instructions for Continued Airworthiness Owner's manual
EDM-900/930 Instructions for Continued Airworthiness Rev E
Date 5-24-2014 Page 3 of 6
Revision History
Revision
Date Description Affected Pages
IR 12/ 15 /2011
CompleteDocument
1 thru 6
A 2/07/2012
AddedPenetrationofAircraftPressureVesselitem9
Page 5
B
4/23/2012 Revised items 5 and 9 Page 5
C 5/16/2012 Deleted old items 3 and 12. Revised old items 4, 5,
8, and 14 (new items 3, 4, 7, and 13
Pages 5 and 6
D 7/15/2012 Clarified acronyms in item 2. Corrected
typographical errors in revision log, items 2, 4, 5, 6,
and 7. Reworded items 4 and 14 for clarity. Added
Rev. D to all pages.
Pages 1
through 6
E 5-24-14 Reorganized and rewrote complete document All
List of Effective Pages
This document is controlled and revised as a complete unit and does not contain pages of
various revisions. All pages are of the same revision as indicated on the cover page and
also indicated at the bottom of each subsequent page. The effective pages consist of the
sections as noted in the Table of Contents.
Distribution of Revisions
Notification of changes to this ICA will be sent to all EDM-900/930 owners on record.
The changed document will be available at JPInstruments.com. Paper copies will be
available on request, contact J.P.Instruments at 714-557-3805.
1.0 Introduction
This document contains the
instructions
for
continued airworthiness
(ICA). This ICA was written in
the format contained in the GAMA Specification No. 2 which was specified by FAA Order
8110.54A. This ICA conforms to the requirements specified by Part 23, Appendix G and FAA
Order 8110.54A. The FAA guidance includes sections that are not applicable to the EDM-
900/930 system, only
applicable
sections have been addressed in this document.
2.0 System Description
The EDM-900/930 is a combined electronic indicating system which simultaneously displays to
the pilot powerplant and aircraft systems operating parameters. It replaces all previous primary
digital and/or analog instruments: This system performs monitoring tasks only; it does not
perform any engine or aircraft system controlling functions.