曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專(zhuān)營(yíng)店坑蒙拐騙欺詐消費(fèi)者

% S Loosen the thumb screws on the end cap.
% S Pull the end cap away from the ELT unit.
% S Move the protective top cover up and
% backward and remove.
(3) Disconnect the co-axial cable for the antenna at
% the ELT BNC connector and all other cables.
At the ELT.
% (4) Release the clamps or the velcro strap which
hold the ELT in its mounting and remove the ELT
from the airplane.
ACK: 2 clamps.
Jolliet: 1 clamp.
% ME 406, ME 406ACE, C 406-1: velcro
% strap.
AIRCRAFT
Equipment/Furnishings
DA 40 Series
AMM
Detail Steps/Work Items Key Items/References
Page 202
20 Sep 2007 25-60-00 Doc # 6.02.01
Rev. 5
WARNING: IF THE % ELT IS MOVED TO A DIFFERENT AIRPLANE THAN WHICH IT
% WAS ORIGINALLY REGISTERED WITH, THE ELT MUST BE
% RE-REGISTERED AND THE PRODUCT LABEL RE-MARKED TO
% INDICATE THE NEW PROGRAMMING AND/OR NEW COUNTRY OF
% REGISTRY.
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
% Figure 4: Artex ME 406 ELT Installation
AIRCRAFT
DA 40 Series
AMM Equipment/Furnishings
Doc # 6.02.01
Rev. 5 25-60-00 Page 203
20 Sep 2007
B. Install the ELT
Detail Steps/Work Items Key Items/References
WARNING: IF THE % ELT IS MOVED TO A DIFFERENT AIRPLANE THAN WHICH IT
% WAS ORIGINALLY REGISTERED WITH, THE ELT MUST BE
% RE-REGISTERED AND THE PRODUCT LABEL RE-MARKED TO
% INDICATE THE NEW PROGRAMMING AND/OR NEW COUNTRY OF
% REGISTRY.
%
% (1) Move the ELT into position into its mounting. At an angle so that the locking ears at
% the end opposite the direction-of-flight
% arrow fit into the mounting tray locking
% slots.
% (2) Close and secure the clamps or the velcro straps
% which hold the ELT.
ACK: 2 clamps.
Jolliet: 1 clamp.
% ME 406, ME 406ACE, C 406-1: velcro
% strap.
(3) ACK E-01:
S Connect the cable from the RCPI to the ELT
at the in-line connector.
% S Connect the co-axial cable from the antenna
% to the BNC connector.
Jolliet JE2-NG:
S Connect the cable from the RCS to the ELT
% at the connector screws.
% S Connect the co-axial cable from the antenna
% to the BNC connector.
% ME 406, ME 406 ACE, C 406-1:
% S Feed the coax cable through the hole in the
% end cap and connect it to the ELT.
% S Fit the top cover onto the ELT unit.
S Position the end cap and connector assembly
onto the ELT and tighten the thumbscrews
securely.
% Ensure that the slots at the end of the
% cover fit over the locking ears on the
% ELT prior to fitting cover onto the
% connector end.
% (4) Do a test for the correct operation of the ELT. Refer to Paragraph 3.
AIRCRAFT
Equipment/Furnishings
DA 40 Series
AMM
Detail Steps/Work Items Key Items/References
Page 204
20 Sep 2007 25-60-00 Doc # 6.02.01
Rev. 5
% (5) Install the trim/cover to the front face of the
baggage compartment frame.
3. ELT Functional Test
% A. ACK and Jolliet
Note: Do this test only during the first 5 minutes of each hour. If you are at a location with
a control tower or other monitoring facility, tell them before you do the test.
Note: For maintenance done to FAR 91 (airplanes registered in the USA) an additional
functional test of the ELT is required. Refer to FAA Action Notice 8150.3 for more
data.
Detail Steps/Work Items Key Items/References
(1) Set the ALT/BAT switch (Lycoming version) or
ELECTRIC MASTER key switch (TAE version) to
ON.
(2) Set the AVIONIC MASTER switch to ON.
(3) Set the radio to receive on 121.5 MHz.
(4) Set the ELT to ON (ACK) or MANU (Jolliet). The
test must not last longer than 3 audio sweeps.
(5) Monitor the radio for the ELT sweep tone.
(6) Set the ELT to OFF (ACK) or OFF/RST (Jolliet).
(7) Set the AVIONIC MASTER switch to OFF.
(8) Set the ALT/BAT switch (Lycoming version) or
ELECTRIC MASTER key switch (TAE version) to
OFF.
AIRCRAFT
DA 40 Series
AMM Equipment/Furnishings
Doc # 6.02.01
Rev. 5 25-60-00 Page 205
20 Sep 2007
% B. ME 406, ME 406 ACE and C 406-1
% Note: Do this test only during the first 5 minutes of each hour. If you are at a location with
% a control tower or other monitoring facility, tell them before you do the test.
% Note: For maintenance done to FAR 91 (airplanes registered in the USA) an additional
% functional test of the ELT is required. Refer to FAA Action Notice 8150.3 for more
% data.
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：鉆石40系列AMM 1(144)