Honeywell BENDIX KING KMH 880 System Installation Manual page 199

B
When the Radio altitude is at 2,500 feet, the Diagnostic Computer
indicates ______ feet.
Flag the Rad. Altitude source by pulling the circuit breaker.
Verify that the Rad. Alt. Status goes INVALID.
Verify that the "TAS" flag appears on the traffic display.
Reset the circuit breaker. Verify that the "TAS" flag clears.
Rad. Altitude Source #1 Pass/Fail ______.
7. Check that the configuration
module and logic discretes are correct. Refer to supporting drawings
and documentation if necessary to confirm the following items.
The TAS and related aircraft system should be operating normally for
the following test. Connect the Diagnostic Computer to the KMH/KTA
through the RS-232 port. Run the TASDIAG Input Data program and
observe the following on the Diagnostic Computer.
Disable the WOW logic and check that the air/ground (J10-4) mode
changes from "ON-GROUND" (GND) to "AIRBORNE" (OPEN).
Pass/Fail ______.
Disable the landing gear logic and check that the gear position (J10-3)
changes from "EXTENDED (GND) to "RETRACTED (OPEN).
Pass/Fail ______.
If applicable, confirm that ADVISORY INHIBIT (J10-22) changes from
"INHIBITED" (GND) to NOT-INHIBITED (OPEN). when testing the
GPWS.
Top Antenna elements (J1-J4) indicate ______ ______ ______ _____.
The HEX value of the antenna elements should indicate between:
J1: BF H and CC H.
J2: D4 H and DF H.
J3: E5 H and ED H.
J4: 6C H and 93 H.
Bottom Antenna elements (J1-J4) indicate _____ _____ _____ _____.
Rev 0, October/2000 10609I00.ZIPCDL
KMH 880/KTA 870
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