SDR 2025F00234

Service difficulty report · Wire Harness · Urocop EC155B

Difficulty date
August 30, 2025
Submitted
October 7, 2025
Operation
General aviation
Aircraft
N100GN
Make and model
Urocop EC155B
Aircraft serial
6847
Aircraft time
1,947 hours, 4,163 cycles
Engine
Tmeca ARRIEL2C2
Engine time
1,947 hours, 2,787 cycles
Part
Wire Harness
Condition
Burned
Location
Zone 100
Part time
1,947 hours, 4,163 cycles
Stage of operation
TX
How discovered
V
Nature of condition
B
Precautionary procedure
H, E

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

What was found

AIRCRAFT LANDED NORMALLY ON THE ROOFTOP HELIPAD AT 7XA7 WITH NO ABNORMAL INDICATIONS ON CAD OR VEMD IN FLIGHT OR UPON LANDING. ENGINES WERE BROUGHT TO IDLE, PASSENGERS WERE BRIEFED AND LOADED, BAGGAGE SECURED, AND DOORS CLOSED. SHORTLY AFTER ACTIVATION OF THE STEP SWITCH FROM THE OPEN TO CLOSED POSITION, A FLASHING GOV LIGHT APPEARED ON THE #1 SIDE OF THE CAD FOLLOWED BY FLICKERING OF THE LG PUMP LIGHT. THE VEMD VEHICLE PAGE DISPLAYED ENGINE STOP DATA WITH ALL FIELDS SHOWING ZERO, WHILE BOTH GENERATORS WENT OFFLINE. SMOKE WAS OBSERVED INSIDE THE COCKPIT. FLIGHT CREW SHUT DOWN ENGINES, GENERATORS, AND ALL SYSTEMS, THEN EVACUATED PASSENGERS AND REMOVED CARGO. IMMEDIATELY AFTER SHUTDOWN, SMOKE WAS OBSERVED FROM THE LEFT STEP FAIRING, WHICH DISSIPATED FOLLOWING COMPLETE DEPOWERING OF THE AIRCRAFT. PIC CONCURRED WITH PREVIOUSLY NOTED CAUTIONS EXCEPT FOR NOT OBSERVING THE #2 GEN LIGHT; BOTH GOV LIGHTS WERE CONFIRMED. #1 WAS BLINKING, #2 SOFT FAILURE. MAINTENANCE PERSONNEL OPENED PANELS REVEALING BURN MARKS AND SLAG JUST TO THE LEFT STEP COMPARTMENT, WITH EXTENSIVE WIRING HARNESS DAMAGE CONCENTRATED IN ABOUT A ONE-FOOT SECTION. ADDITIONAL INSPECTION CONFIRMED THREE CIRCUIT BREAKERS HAD TRIPPED.

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