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Tank Contents: max 20 US/gal
ma x
ma x
3 10
2 25 5 10 3
5 3 5 5 5 3
5
5
3 10
5 5
3
70 70 5
ANNUN . FA N /OAT
P IT OT
HE AT
F UEL
P UMP
F LAPS B AT T.
E SS . A LT. ALT.
P ROT. CONTROL
T& B DG HOR IZON
ALT. E S S.
28 V DC
A CC.
B US PWR.
I NST . STROB E POSITOI N TA X IM/ A P LA NDING FLOOD
MA S TE R A VI ONI CS
CONTROL MA S TE R
A UTO
P IL OT
GP S
IGNIT ION
I NST . 1
A NN/UN
S TA RT
NAV /COM 2 AUDIO NAV /COM 1 X PDR
A DF DME
ENGINE & FUEL
AVIONICS
LIGHTI NG
SYSTEMS
ELECTRICAL
OPS.
GROUND
ONLY
2A MAX
ISO
ALL
Mic .
Ma no eu vri ng s peed : v = 10 8 K IA S (fo r 21 60 t o 2 58 0 l bs )
Ma no eu vri ng s peed : v = 9 4 K IA S (fo r 17 16 t o 2 16 0 l bs )
T hi s ae rop la ne is c la ssi f ie d i n t he No rma l an d U t i li t y C ateg ori es
a nd a pp rov ed f o r d ay -V F R on ly, in no n-i ci ng c on di t io ns .
A l ae rob at i c man oe uv res inc . I nt e nt ion al s pi nn in g a re pro hi bi ted .
S ee Fl ig ht Ma nu al fo r o the r l i mita ti on s.
NO SM OK ING
ACK
ON ELT ON RESET
Switch Switch
LED
In-Line Connector
for RCPI
Figure 1: ELT Installation (ACK E-01)
AIRCRAFT
DA 40 Series
AMM Equipment/Furnishings
Doc # 6.02.01
Rev. 5 25-60-00 Page 5
20 Sep 2007
3. Operation
A. ACK E-01
(1) ELT
The ELT has a switch with these 3 positions:
) ON
) OFF
) ARMED
The ON position is for ground test. When the airplane is in use the switch must be in the
ARMED position.
(a) Emergency Operation
If the airplane crashes, then the accelerometer senses the crash. The accelerometer sets
the transmitter to ON. The transmitter transmits the international distress frequency. The
battery in the ELT supplies power to the transmitter. The battery can operate the ELT for
approximately 180 hours at +21 °C (70 °F) and for approximately 140 hours at -21 °C (-6 °F).
The ELT will only transmit if set to ARMED before the crash.
(b) Test
If you press the ON switch, then the following occurs:
• An LED flashes in the RCPI
• If you set the radio to 121.5 MHz, you can hear the audio sweep tone from the ELT.
(2) RCPI
The RCPI has 2 switches and a red LED. The left switch is labeled ON. When it is pressed it
does a test of the ELT. The right switch is labeled RESET. When you press the RESET switch
it stops the test of the ELT. The red LED flashes when you test the ELT.
AIRCRAFT
Equipment/Furnishings
DA 40 Series
AMM
Page 6
20 Sep 2007 25-60-00 Doc # 6.02.01
Rev. 5
B. Jolliet JE2-NG
(1) ELT
The ELT has a switch with these 3 positions:
) MANU
) OFF/RST
) AUTO
The MANU position is for ground test or in case of emergency use out of the airplane. When the
airplane is in use the switch must be in the AUTO position.
(a) Emergency Operation
If the airplane crashes, then the accelerometer senses the crash. The accelerometer sets
the transmitter to ON. The transmitter transmits the international distress frequency. The
battery in the ELT supplies power to the transmitter. The battery can operate the ELT for
minimum of 50 hours. The ELT will only transmit if set to AUTO before the crash.
(b) Test
If you switch to MANU, then the ELT starts to transmit on the international distress
frequencies 121.5 MHz and 243.0 MHz a typical modulated signal.
If you set the radio to 121.5 MHz, you can hear the audio sweep tone from the ELT.
AIRCRAFT
DA 40 Series
AMM Equipment/Furnishings
Doc # 6.02.01
Rev. 5 25-60-00 Page 7
20 Sep 2007
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
% Figure 2: ELT (ME 406, ME 406 ACE)
AIRCRAFT
Equipment/Furnishings
DA 40 Series
AMM
Page 8
20 Sep 2007 25-60-00 Doc # 6.02.01
Rev. 5
% C. ME 406, ME 406 ACE
% (1) ELT
% The ELT has a switch with these 2 positions:
% ) ON
% ) OFF/ARM
% The ON position is for ground test. When the airplane is in use the switch must be in the ARM
% position.
% (a) Emergency Operation
% If the airplane crashes, then the accelerometer senses the crash. The accelerometer sets
% the transmitter to ON. The transmitter transmits the international distress frequency and on
　
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