BENDIXKing KI 300, Руководство по установке

Страница: 46 / 50

____________________________________________________________________________
89000004-101 KI 300 Installation Manual
Rev 1 5-4
© Honeywell International Inc. Do not copy without express permission of Honeywell.
12. Loop the excess wire into the cavity co-located with the battery connector. Do not run
the excess wire adjacent to, over, or under the battery pack itself.
13. Insert the battery pack into the battery cavity with the label facing the battery cover.
14. Replace the battery cover, tighten the screws firmly into position. Take care to ensure
that the battery wires are fully contained within the battery compartment, and do not
get pinched under the battery cover plate.
15. Re-install the unit following the procedures defined in this manual.
16. Note the date of battery replacement in the aircrafts log book. The age of the battery
is determined by the placed-in-service date, not manufacture date.
17. New battery packs will not have full charge. The battery pack should be fully charged
prior to re-entry into service.
5.4 Airspeed and Altimeter Test & Calibration
Both the airspeed and attitude sensors have the ability to be tested and calibrated in the field. Greater
accuracy will be obtained by allowing the unit to fully stabilize in the on-state for a period of
approximately 5 - 10 minutes prior to determining any required adjustments.
5.4.1 Altimeter System Test and Inspection
This procedure should only be performed utilizing a calibrated air-data test set. The physical connection
(pitot and static) of the air-data test set is identical to that of traditional mechanical instruments. No
vibration is required to be applied to the unit during testing or calibration.
NOTE
THE KI 300 MUST BE CALIBRATED EVERY 24 MONTHS PER CFR 91.411.
CAUTION
IF OTHER INSTRUMENTS ARE CONNECTED TO THE PITOT STATIC SYSTEM THAT CANNOT HANDLE
AN AIRSPEED INPUT OF 400 KTS, THE KI 300 MUST BE REMOVED FROM THE AIRCRAFT AND THE
AIRSPEED TRIM PROCEDURE MUST BE COMPLETED ON THE BENCH.
5.4.2 Airspeed Trim Procedure
1. Connect the pitot-static test set to the aircraft static system. The KI 300 must be connected to
the aircraft static system.
2. Apply power to the KI 300 while holding the pushbutton down in order to enter setup mode and
allow the internal encoder to stabilize.