EasyManua.ls Logo

Honeywell 1152682-2 - Page 54

Honeywell 1152682-2
104 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
COMPONENT MAINTENANCE MANUAL
1152682
Page 121
Oct 27/06
© Honeywell International Inc. Do not copy without express permission of Honeywell.
23-24-02
4. Fault Isolation for RESCU 406AFN
A. Use the Fault Isolation charts that follow as a troubleshooting guide at the same time as the
Installed System Tests. If the results of one of those tests are unsatisfactory, use the Fault Isolation
Flowcharts (Figures 103 to 105) to isolate the system component that is the problem.
F LEDDRIVE Input With 28 V dc connected to pin N, one
of LIGHT or LEDDRIVE is necessary
to drive LED indicator. With
LEDDRIVE connected, LED will have
a blinking ON indicator.
Required if 28 V
dc not used
G RESET2 Output To transmitter unit, to send the
position of the 3-position functional
switch.
Required
H EXTL WARNING Output Contact closure to ground, when
transmitter sends. Connected
internally to pin C.
Optional
J DC GROUND Input To aircraft dc ground Required
K 5 VAC PANEL
LIGHT
Input Necessary if panel backlit used.
Connect to 0 – 5 V ac 400 Hz.
Optional
L AC GROUND Input Necessary if 5 V ac is connected. Optional
M LIGHT TEST Input Supplies contact closure to ground, to
operate LED indication. Available only
if 28 V dc is connected to pin N.
Optional
N 28 VDC Input Supplies Light Test to do a test of LED
or ON LED indication show
constantly.
Optional
P LIGHT Input LIGHT or LEDDRIVE signal is
necessary from transmitter unit to
drive LED. With LIGHT, LED ON
indication is constant. With
LEDDRIVE, ON indication blinks.
Optional
R ELTONPULSE Input From transmitter unit, momentary
contact closure to ground. Used on
B737NG
Optional
S MC STEADY
STATE
Output From pin U. Used on B737NG. Optional
T MC PULSE Output From pin R, ELTONPULSE.
Momentary 50 millisecond pulse to
ground. Used on B737NG.
Optional
UELTON MC
INPUT
Input From transmitter unit. Contact closure
to ground with transmitter unit started.
Used on 737NG.
Optional
V LINK2 Input/
Output
Connected to pin B. Optional
TABLE 105. REMOTE PANEL CONNECTOR J1 PIN-OUTS (Cont’d)
Pin Pin Label (I/O) Description Requirements

Related product manuals