Service difficulty report · Actuator · Boeing 737924ER

Difficulty date
January 7, 2025
Submitted
January 10, 2025
Operation
Air carrier
Aircraft
N37413
Make and model
Boeing 737924ER
Aircraft serial
31664
Aircraft time
50,423 hours, 18,010 cycles
Engine
Cfmint CFM567B262
Part
Actuator
Part number
1211313010
Part serial
AU122
Condition
Faulted
Location
Nr 2 Vsv
Part time
12,047 hours, 4,477 cycles
Stage of operation
TO
How discovered
O
Nature of condition
E, A
Precautionary procedure
C

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

What was found

ON TAKE OFF ENG 2 MADE A LOUD POP AND N1 ROLLED BACK. EGT WAS SL OW TO ROLL BACK. DEBRIEFED CREW ABORTED T/O ROLL AFTER LOUD BANG AT APPROX 40KTS AND PAX REPORTED FLAME OUT OF TAILCONE MET ACFT ON RUNWAY PERFORMED VISUAL INSPECTION OF MAIN WHEELS NO DAMAGE NOTED STOWED FLAPS AND SPEEDBREAKS VISUAL INSP OF ENG2 NO DAMAGE NOTED INLET AND EXHAUST CLEAR FAN ROTATION FREE ACFT TOWED TO GATE FOLLOWED FIM 71-05 TASK 805. ENGINE STALL/SURGE, ENGINE PARAMETERS NORMAL OR NOT NORMAL, ENGINE RECOVERED OR SHUTDOWN.OVERHEAD #2 ENGINE CONTROL LIGHT ILLUMINATED. PERFORMED VSV ACTUATOR TEST. FAULT #75-30382 DISPLAYED. SEE FIM 75-31 TASK 802. PERFORMED UPTO AND INCLUDING STEP F(3)(D). EXAMINED THE PUT BACK 2 PLUGS DP0501 AND DP0601 FOR TESTING EEC PLUG TO HMU. PERFORMED RESISTANCE CHECKS ALL ELECTRICAL CONNECTOR AT THE RESISITANCE CHECKS GOOD. NO VISUAL DEFECTS NOTED. RESISTANCE CHECKS REQUIRED AS PER - DUAL CHANNEL FAULT. STEP F(4). REMOVED AND REPLACED LEFT VSV ON ENG #2 PER AMM PER 75-31 TASK 802 PERFOMED REMOVAL OF HMU PER AMM TASK 75-31-01-000-801-F00. NO FIX, OPS CHECK FAILED BUT LEAK CHECK 73-21-10-000-801-F00 GOOD.REQUIRES FURTHER TROUBLESHOOTING. POST VSV AND HMU REPLACEMENT PERFORMED POWER ASSURANCE TEST.ENG WAS ABLE TO MAKE TAKEOFF POWER WITH NO ABNORMALITIES.