Service difficulty report · Module · Boeing 737890

Difficulty date
June 4, 2016
Submitted
June 7, 2016
Operation
Air carrier
Aircraft
N560AS
Make and model
Boeing 737890
Aircraft serial
35179
Aircraft time
37,713 hours, 11,382 cycles
Part
Module
Part number
6937307300
Part serial
D05212
Condition
Failed
Location
Detection Sys
Part time
36,577 hours, 10,721 cycles
Stage of operation
CL
How discovered
O
Nature of condition
J
Precautionary procedure
A

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

What was found

AFTER DEPARTURE ON CLIMBOUT THE ENGINE NR 2 OVERHEAT LIGHT CAME ON, FOLLOWED QRH PROCEDURES. AFTER BRINGING THROTTLE TO IDLE, LIGHT WENT OUT, RETURNED TO PSP. ACFT GROUNDED. REPLACED ALL 4 NR 2 ENGINE FIRE DETECTORS AND M279 MODULE, REF AMM 26-11-01, NO HELP. AFTER 15 MIN OF IDLE ENGINE RUN, NR 2 ENGINE OVERHEAT LIGHT ON. REINSTALLED UPPER FAN DETECTOR, M1757, DUE TO FAULT DURING M279 BITE, REF FIM 26-10, TASK 801, NO HELP. ACCOMPLISHED ENGINE BLEED AIR SYS LEAK CHECK USING THE APU, REF AMM 36-11-00-700-802, NO LEAKS FOUND, OPS CHECKS GOOD AT THIS TIME. FOUND DEFECTIVE WIRING HARNESS AT FWD OF UPPER FAN, M1757, DETECTOR CAUSING NR 2 ENGINE A AND B LOOPS TO NOT TEST. ACCOMPLISHED ENGINE HIGH POWER RUN UP, REF AMM 72-00-00, DUPLICATED FAULT AFTER 10 MINS. R & R UPPER FAN DETECTOR AND EXHAUST HARNESSES, REF AMM 26-11-01-02. R & R ENGINE/APU CONTROL PANEL, REF AMM 26-00-01. REPLACED NW316 WIRE HARNESS B-LOOP, REF AMM 26-11-02. HIGH POWER ENGINE RUN FOUND NO FAULTS.