Honeywell 1152682-2 - Page 47

COMPONENT MAINTENANCE MANUAL
1152682
Page 114
Oct 27/06
© Honeywell International Inc. Do not copy without express permission of Honeywell.
23-24-02
2 Activate the ELT by using a quick throwing motion in the direction of the
arrow, followed by a quick motion in the reverse direction. Verify the unit has
activated by observing that the LED on the control panel is blinking (signifying
activation).
3
After verifying operation, set the switch on the control panel of the transmitter
unit to “OFF”.
3. Connector Pin-Outs for RESCU 406AFN
Connector pin-outs are given in Tables 102 to 105.
TABLE 102. TRANSMITTER UNIT P/N 1152862-2 CONNECTOR J1 PIN-OUTS
Pin Pin Label (I/O) Description Requirements
1NC
2 NC Input Used to put transmitter unit into TEST
mode.
Optional
3NC
4NC
5NC
6NC
7NC
8 ELTON1 Output Contact closure to ground during
TRANSMIT mode. If not, open circuit.
Optional
9 RFTEST Input Used for factory testing only. This
input must be open circuit during
usual operation.
Optional
10 NC
11 DC RETURN Output DC ground supplied by the chassis of
the transmitter unit.
Required
12 ELTON2 Output Contact closure to ground during
TRANSMIT mode. At other times,
open circuit.
Optional
13 LEDDRIVE Output Pulsed output to drive LED. Optional
14 JAA G SWITCH Input Contact closure to G SW SENSE to
make selection of JAA G-Switch.
Required if
aircraft is
operated under
JAA regulations.
15 FAA G SWITCH Input Contact closure to G SW SENSE to
make selection of FAA G-Switch.
Required if
aircraft is
operated under
FAA regulations.
16 G SW SENSE Output Has function as contact closure for
JAA G SWITCH or FAA G SWITCH.
Required