Service difficulty report · Warning Light · Boeing 737890

Difficulty date
March 27, 2016
Submitted
March 29, 2016
Operation
Air carrier
Aircraft
N530AS
Make and model
Boeing 737890
Aircraft serial
36578
Aircraft time
23,519 hours, 7,036 cycles
Part
Warning Light
Condition
False Activation
Location
Nr 2 Engine
Stage of operation
TX
How discovered
O
Nature of condition
N
Precautionary procedure
D

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

NR 2 ENGINE CONTROL LIGHT ILLUMINATED ON GROUND. ACFT GROUNDED. REF FIM 73-06, TASK 801, PERFORMED ELECTRONIC ENGINE CONTROL BITE TEST ON NR 2 ENGINE ELECTRONIC ENGINE CONTROL, BITE TEST PASSED. ENGINE CONTROL NORMAL. ACFT OK FOR SERVICE. ENGINEERING REQUEST, ACCOMPLISHED DEU BITE & ELECTRONIC ENGINE CONTROL BITE REF FIM 31-62, TASK 801 & 73-00, TASK 801. NR 1 DEU LOGGED 31-61033 DU-CU LOW BRIGHTNESS, 31-61036 DU-CL LOW BRIGHTNESS, 31-68861 NO CAPTAIN DATA, & 31-65050 ALTITUDE DISAGREE. NR 2 DEU LOGGED 31-61033 DU-CU LOW BRIGHTNESS, 31-61036, DU-CL LOW BRIGHTNESS, 31-68862 NO CAPTAIN DATA, 31-65050, ALTITUDE DISAGREE, 31-61012, DU-LIB FAIL, & 31-61011, DU-LOB FAIL. NR 2 ELECTRONIC ENGINE CONTROL LOGGED 75-10582, TBV DEMAND & POSITION SIGNALS DISAGREE. ACCOMPLISHED FIM 75-23, TASK 801. ELECTRONIC ENGINE CONTROL BITE CHECK NORMAL. ACCOMPLISHED ACTUATORS TEST 3 TIMES, NO DEFECTS NOTED. TBV TORQUE MOTOR RESISTANCE NOMINAL AT 16 OHMS. DISCONNECTED, INSPECTED & CLEANED DP0907, TBV, DP0909 & DP0505, ELECTRONIC ENGINE CONTROL AND DP 0501, HMU, NO DEFECTS NOTED. SOCKET, PIN RETENTION TEST NORMAL REF AMM 70-70-01 AND SSM 75-31-22. INSPECTED CONNECTORS ON PREVIOUSLY MENTIONED UNITS, NO DEFECTS NOTED. RANG WIRING BETWEEN DP0907 & DP0909, DP0505 & DP0501, NO DEFECTS NOTED. AFTER CONNECTOR CLEANING, ACCOMPLISHED ELECTRONIC ENGINE CONTROL BITE, ACTUATORS TEST AND IDLE ENGINE RUN. NO DEFECTS NOTED, ALL INDICATIONS NORMAL. TBV DEMAND & POSITION DIFFERENCE WAS ONLY 7 PERCENT.