
SYSTEM INSTALLATION MANUAL
89000016
10
Read the primary altimeter value. Rotate the CODE knob either clockwise or
counterclockwise until the altitude displayed on the KGX control panel matches the
aircraft primary altimeter. Press ENT and the display will move to the test altitude
screen which is the next configuration item in the configuration mode.
(b)
To complete the testing you must leave the KGX control panel displaying the encoder
altitude, and exercise the altitude on the static test set across the altitude range of the
aircraft. The display will be as shown in Figure 3081 for pressure altitude reported.
(c)
Use at least 10 test points, and verify that in each case the altitude displayed on
the primary altimeter and the altitude displayed on the KGX control panel correspond
within the 125-foot tolerance. Lightly tap the altimeter at each test point to eliminate
friction effects.
Figure 3077. (Sheet 1 of 1) Calibrate Alt Encoder Display
Figure 3078. (Sheet 1 of 1) Alt Encoder Cal Low Altitude 0ft Display
Figure 3079. (Sheet 1 of 1) Alt Encoder Cal Mid Altitude FL100 Display
Figure 3080. (Sheet 1 of 1) Alt Encoder Cal High Altitude FL300 Display
Figure 3081. (Sheet 1 of 1) Pressure Altitude Reported Display
EFFECTIVITY
ALL
Page 3058
22 Dec 2016
© Honeywell International Inc. Do not copy without express permission of Honeywell.