Service difficulty report · Wire Harness · Boeing 737824

Difficulty date
September 28, 2026
Submitted
September 29, 2026
Operation
Air carrier
Aircraft
N33289
Make and model
Boeing 737824
Aircraft serial
31607
Aircraft time
67,894 hours, 25,284 cycles
Engine
Cfmint CFM567B262
Engine time
2,841 hours, 1,343 cycles
Part
Wire Harness
Part number
3250299080
Condition
Faulted
Location
Nr 2 Engine
Stage of operation
DE
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

REPLACE NR 2 ENG MW0311 HARNESS IAW AMM 73-21-06-400-802-F00, BEFORE DEPARTING SFO DUE HISTORY OF NO BLEED ON NR 2 ENGINE. STARTED REMOVAL OF MW0311 HARNESS FROM FIREWALL DOWN TO STRUT FAIRING. REMOVED AND INSTALLED MW0311 IAW AMM 73-21-06-400-802-F00 . REF AMM 73-21-06-400-802-F00, & POWER PLANT TEST REF TABLE 71-00-00-800-811-F00, FOR FFCC VIBRATION SENSOR. PERFORMED E2 FADEC SYSTEM TEST, EEC TEST PASSED, ACTUATOR TEST PASSED, EEC DISCRETES TESTED OK. PERFORMED FFCC VIBRATION SENSOR TEST, AVM OPS TESTED OK. UP TO HIGH POWER RUN. REQUIRES 70% N1 FOR 2 MINUTES. VIBRATION INDICATION TO BE READING. IAW AMM 73-21-06-400-802-F00, PERFORMED E2 HIGH POWER RUN AT 70% N1 FOR 2 MIN, VIB INDICATION IS SHOWN THROUGH OUT RUN AT POWER, IDLE, AND 0.0 ENGINE OFF. REF AMM 73-21-06-400-802-F00.