Service difficulty report · Wire Harness · Boeing 737890

Difficulty date
September 19, 2014
Submitted
September 23, 2014
Operation
Air carrier
Aircraft
N563AS
Make and model
Boeing 737890
Aircraft serial
35180
Aircraft time
30,536 hours, 9,319 cycles
Engine
Cfmint CFM567B27
Part
Wire Harness
Condition
Malfunctioned
Stage of operation
IN
How discovered
9
Nature of condition
O
Precautionary procedure
K

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

What was found

WHILE COMPLETING T/C 78273000, 75-30411 HPTASS SIGNAL DISAGREE. ACFT GROUNDED. PERFORMED HPTACC VALVE, EEC AND WIRE HARNESS J10, CH B AND J9, CH A, ALL RESISTANCE CK WITHIN LIMITS, AND RECEPTACLE ARE IN GOOD CONDITION, REF FIM 75-21, TASK 802. IAW PG A, STEP 5 SAME FIM FADEC 3, CH B EXCITATION CIRCUIT FOR (HPTACC) POSITION LVDT AND THE (TBV) POSITION ARE FROM A COMMON SOURCE IN THE EEC. T/S (TBV) FOUND TO BE OUT OF LIMITS IAW FIM 75-23, TASK 802. DUE TO FAULT HISTORY, CLEARED ALL FAULTS FROM NR 1 ENG EEC. BITE TEST AND VERIFIED NO FAULTS ARE CURRENT REF MM 73-21-00-740-803-F00. WE PERFORMED THE FOLLOWING TASK IN ORDER TO VERIFY NO FAULTS ON ENGINE FROM EEC. WE FIRST DID AN ACTUATORS TEST WITH NO DEFECTS NOTED REF MM 71-00-00-700-807-F00. THEN WE DID AN EEC BITE TEST REF MM 73-21-00-740-803-F00. NO DEFECTS FOUND. THEN WE PERFORMED AN ENG IDLE RUN FOR 5 MIN REF MM 71-00-00-800-808-F00. THEN WE PERFORMED ECC BITE TEST AND NO DEFECTS FOUND REF MM 73-21-00. WE DID THIS PROCEDURES THE FOLLOWING NR OF TIMES, A TOTAL OF 3 ACTUATORS TEST REF MM 71-00-00-700-807-F00, A TOTAL OF 2 ENGINE IDLE RUN 5, MIN AT A TIME, RE MM 71-00-00-800-808-F00 AND A TOTAL OF 7 EEC BITE TEST REF MM 73-21-00-740-803-F00. AT THIS TIME AND AFTER ALL TESTS, THERE HAS NOT BEEN 1 INSTANCE OF A FAULT FOR HPTACC TESTING EE REPLACEMENT AND WIRE HARNESS TESTING. ACCOMPLISHED EA -800-75, EA-13416.