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 (b) P42 5-Volt Lighting Main Instrument Panel
 1) 5V AC SEC
 S 864-098
 (5)  Make sure the indicator lights are on.
 ú
 ú  S 864-133
 ú  (6)  AIRPLANES WITH THE HONEYWELL HG480B42 ADC;
 ú  Set the LIGHTS switch on the center instrument panel, P2, to the
 ú  TEST position.
 ú
 ú  S 864-134
 ú  (7)  Set the TEST SELECT switch on the DADC to the FUNCTION position.
 ú
 ú  S 864-135
 ú  (8)  Push and hold the PUSH TO TEST switch on the ADC.
 ú  (a) Make sure the TEST VALID WHEN LIT light on the ADC comes on in
 ú  approximately 30 seconds.
 ú  (b) Make sure that you see these values on the air data indicators:
 ú 
        ú
 NOTE: The TAT/SAT/TAS indicator receives input from the No. 1____
 ú  ADC.
 ú  1) Altitude 10,000 +/-40 feet
 ú  2) Mach 0.785 +/-0.01
 ú  3) Airspeed 440 +/-2 knots
 ú  4) Total Air Temperature +0.1 +/-2 degrees C
 ú  5) Static Air Temperature -29.4 +/-2 degrees C
 ú  6) True Airspeed 477.8 +/-6 knots
 ú 
        ú
 NOTE: To change the mode of the TAT/SAT/TAS indicator push____
 ú  the switch on the front of the indicator.

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 ú ú S 864-136 ú (9) Set the TEST SELECT switch to the SLEW position. ú ú S 864-137 ú (10) Push and hold the PUSH TO TEST switch. ú (a) Make sure the TEST VALID WHEN LIT light comes on. ú (b) Make sure the VSI indicators slew to -600 ft/min. ú ú S 864-138 ú (11) Set the TEST SELECT switch to the FAIL WARN position. ú ú S 864-139 ú (12) Push and hold the PUSH TO TEST switch. ú (a) Make sure the TEST VALID WHEN LIT light comes on. ú (b) Make sure warning flags for the Air Data indicators are in ú view. ú ú S 864-140 ú (13) AIRPLANES WITH THE HONEYWELL HG480E1 ADC; ú Set the LIGHTS switch on the pilot's instrument panel, P2, to the ú TEST position. ú ú S 864-141 ú (14) Make sure all parts of the TAT/SAT/TAS indicator flash. ú ú S 864-142 ú (15) Set the BARO correction on the altimeters to 29.92 inches Hg. ú ú S 864-143 ú (16) Momentarily set the self-test switch on the ADC to the TEST ú position. ú ú S 864-144 ú (17) Make sure the ADC front panel shows 88 for three seconds and then ú shows AA. ú         ú
NOTE: The test will continue for 60 seconds.
____ The off flag will be
 ú  in view during the test. 50 seconds after the output is in a
 ú  stable condition, the ADC front panel will flash. This shows
 ú  the end of the test is near. Momentarily set the self-test
 ú  switch to the TEST position again, and the outputs will stay
 ú  for 60 seconds.
 ú  If failures are found with the ADC or the sensor inputs, the
 ú  ADC front panel will flash FF. The failure code will then be
 ú  shown.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 ú
 ú  S 864-145
 ú  (18) Make sure that you see these values on the air data indicators:
 ú 
        ú
　
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