EDIATec ECW100 설치 매뉴얼 - 페이지 4
{카테고리_이름} EDIATec ECW100에 대한 설치 매뉴얼을 온라인으로 검색하거나 PDF를 다운로드하세요. EDIATec ECW100 14 페이지. Collision warning unit
EDIATec ECW100에 대해서도 마찬가지입니다: 운영 매뉴얼 (15 페이지)
페이지 인쇄
4. General Advice on Installation
Installation and operation must be on the basis of non-interference with and no
hazard to the existing suite of other certified equipment necessary for safe
flying operation, or installed to comply with official requirements. Installation
and operation must comply with official regulations and requirements. When
ECW100 is permanently installed in an aircraft in Switzerland, the installation must
comply with the "FLARM and TR-DVS Installation Policy" published by the Swiss Civil
Aviation Authority (FOCA). In Germany, an installation as portable device is possible in
gliders and motor-gliders; if an installation in powered aircraft is considered, European
Commission Regulation (EC) No 1702/2003 must be respected.
ECW100 must be secured in such a position that the pilot has the display LEDs in direct
view, and can hear the acoustic warning tone and operate the control buttons. ECW100
must not obstruct the piloting operation and in particular it must not hinder his field of
view. These requirements must be maintained at all times during conditions of strong
turbulence and acceleration. ECW100 is not suited for use in conjunction with night vision
systems, night flying (no dimmers) or in pressurized cabins.
Ideally, ECW100 will be installed in a 57 mm hole in the instrument panel. If possible,
ECW100 should be so installed that the pilot does not inadvertently touch the push-
buttons during cockpit ingress and egress. Cables must not be folded or under tension.
The installation must allow adequate space for cable connectors and the internal
antenna.
ECW100, the radio antenna and the GPS antenna should each be installed at least 25 cm
away from the magnetic compass, more if possible.
After installation, an appropriate entry should be made in the aircraft technical
logs and a check made that the installation is in no way detrimental to the
performance of mechanical, electrical or magnetic (e.g. compass) performance
of other aircraft systems (e.g. radio).
The unit serial number and software version should be recorded in the aircraft technical
log. In the case of a permanent installation, the "Means of Compliance" should be
confirmed in the aircraft technical log, and an "AFM Supplement" carried in the aircraft.
The following remark is to place at the instrument panel by the ECW100:
For Situation Awareness only
Page 4