Service difficulty report · Connector · Boeing 737890

Difficulty date
January 16, 2016
Submitted
February 23, 2016
Operation
Air carrier
Aircraft
N570AS
Make and model
Boeing 737890
Aircraft serial
35185
Aircraft time
34,098 hours, 10,125 cycles
Engine
Cfmint CFM567B27
Part
Connector
Part number
3250455010
Condition
Loose
Location
Engine
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

REF TC 78273000, 1 ENG MAINTENANCE FAULT 73-31371, UPPER EGT SECTION READS HIGH ECONOMIC FAULT. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT. ELECTRONIC ENGINE CONTROL BITE TEST IAW AMM 73-21-00-740-801-F00 SHOWED NO FAULTS LOGGED IN THE LAST TEN STARTS. ACCOMPLISHED NR 1 ENGINE EGT CONNECTOR CLEANING IAW AMM 77-21-00-140-801. ALL CONNECTORS IN TABLE 2 CLEANED. ON CJ9 HARNESS CONNECTOR DP0912, T495S1 PROBE CONNECTOR FOUND SOCKET TENSION NON-EXISTENT. R & R NR 1 ENGINE CJ9 HARNESS IAW AMM 73-21-06-000-803-F00/73-21-06-400-803-F00. PERFORMED FADEC TEST IAW AMM 73-21-00-700-802-F00, ELECTRONIC ENGINE TEST IAW AMM 73-21-00-700-804-F00, IDENT/CONFIG TEST IAW AMM 73-21-00-700-808-F00, TEST 12, ACTUATORS TEST IAW AMM 71-00-00-700-807-F00, AND ELECTRONIC ENGINE CONTROL DISCRETES TEST IAW AMM 73-21-00-700-809-F00. ALL TESTS PASS. EGT READINGS BEFORE CLEANING: S1-57.87; S2-22.50; S3-24.37; S4-79.25. EGT READINGS AFTER CLEANING AND HARNESS REPLACEMENT: S1-23.62; S2-10.12; S3-10.87; S4-27.75.