Service difficulty report · Control Module · Boeing 737890

Difficulty date
July 31, 2014
Submitted
August 5, 2014
Operation
Air carrier
Aircraft
N518AS
Make and model
Boeing 737890
Aircraft serial
35693
Aircraft time
21,182 hours, 6,351 cycles
Engine
Cfmint CFM567B27
Part
Control Module
Part number
6937307300
Part serial
D06030
Condition
Malfunctioned
Location
Ee Bay
Part time
21,172 hours, 6,339 cycles
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 OVERHEAT ILLUMINATED AFTER STARTING AND STABLIZED NO HOT START THE OVER HEAT LIGHT REMAINED ON FOR TWO MINUTES AND 53 SECS. ACFT GROUNDED. CLEANED ALL TERMINAL GROUND LUGS ON A AND B FIRE LOOPS ON NR 2 ENG IAW POWER PLANT BUILDUP MANUAL 71-00-02 AND MM 26-11-01-000-802. PERFORMED BITE TEST ON FIRE DETECTION MODULE PASSED. RAN ENG AT TAKEOFF POWER FOR 5 MIN AFTER POWER RUN 3 MIN LATER OVERHEAT LIGHT ILLUMINATED BITE TEST ON BOX FAILED. RANG LOOP A AND B NR 2 ENGINE IAW FIM 26-10, TASK 810, ALL LOOPS WITHIN LIMITS. RANG OUT WIRES FROM DP98 TO DP1510 AND DP1610 NO DEFECTS NOTED WDM 26-11-21,26-11-11. RAN ENGINE IDLE AND HI-PWR, UNABLE TO DUPLICATE DEFECT. R & R M279 CONTROL MODULE REF AMM 26-10-01 ACCOMPLISHED ENGINE FIRE SWITCH SYSTEM SHUTDOWN TEST IAW AMM 26-21-00-720-802 FOR THE NR 1 & NR 2 ENGINE, OPS TEST NORMAL. ACCOMPLISHED NR 1 & NR 2 ENGINE FIRE EXTINGUISHING BOTTLE SQUIB CIRCUIT TEST REF AMM 26-21-00-730-801, OPS TEST NORMAL. NR 2 ENG, OPS CK NORMAL ON ENGINE RUN.