SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
9-9
Troubleshooting
The pilot steps through the tests using the L AFCS button until 98 L
FLIGHT FAULT SUMMARY is displayed as shown in Figure 9--4.
Final Flight Fault Test
Figure 9--4
When the RESET button is pushed, data is displayed for the first flight
guidance computer, as shown in Figure 9--5.
Flight Fault Summary
Figure 9--5
The alphanumeric codes should be recorded for use by Honeywell
personnel in troubleshooting the problems. When the RESET button is
pushed again, the fault data for the second flight guidance computer is
displayed.