Service difficulty report · Switch · Urocop EC130B4

Difficulty date
March 24, 2013
Submitted
March 25, 2013
Operation
Air carrier
Aircraft
N854MH
Make and model
Urocop EC130B4
Aircraft serial
4433
Aircraft time
5,171 hours, 10,866 cycles
Engine
Tmeca ARRIEL2B1
Engine time
4,127 hours, 7,316 cycles
Part
Switch
Part number
024805AA
Condition
Unserviceable
Location
Console
Part time
5,171 hours, 10,866 cycles
Stage of operation
CR
How discovered
O
Nature of condition
B
Precautionary procedure
H, A

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

What was found

DURING CRUISE, . PILOT DETECTED AN ELECTRICAL ODOR, SLIGHT & DEVELOPED TO A STRONG ODOR WITH SOME MODERATE SMOKE DEVELOPMENT. FOLLOWED FLIGHT MANUAL EMERGENCY PROCEDURES, PILOT USED EMERGENCY ELECTRICAL SYS BREAKAWAY WIRED CUTOUT SWITCH TO CUT OFF ALL ELECTRICAL POWER TO ACFT. RESIDUAL SMOKE AND ODOR CLEARED. ELECTED TO LAND. EXAMINATION OF THE CONSOLE MOUNTED 30 ALPHA SWITCH PANEL CONTROL SWITCH, IDENTIFIED AS SMOKE SOURCE. DETERMINED THE ADJACENT STROBE CONTROL SWITCH HAD VISIBLE HEAT DISCOLORATION AND A SINGLE BASE PIN FOR THE SWITCH FOUND HEAT WELDED TO IT’S 30 ALPHA PCB BOARD SOCKET. A SERVICEABLE 30 ALPHA PANEL WITH SERVICEABLE SWITCHES WAS INSTALLED AND THE ACFT RETURNED TO THE MX BASE FOLLOWING A SATISFACTORY OPS CHECK. DETAIL INSPECTION OF THE DEFECTIVE SWITCH INTERNAL PCB, ONCE SWITCH WAS REMOVED, LESS THE WELDED PIN STUCK IN ITS SOCKET, MADE IT APPEAR TO BE THE LIKELY SOURCE OF THE FAILURE WITH SUBSEQUENT HEAT DAMAGE TO THE 30 ALPHA PANEL CIRCUIT BOARD.

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