SDR 99ZZZX4152

Service difficulty report · Harness · Socata TB10TOBAGO

Difficulty date
October 5, 1999
Submitted
March 26, 2000
Operation
General aviation
Aircraft
N55437
Make and model
Socata TB10TOBAGO
Aircraft serial
1229
Part
Harness
Condition
Chafed
Location
Cockpit
Stage of operation
IN
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

MAIN POWER WIRING HARNESS PASSED THROUGH 2 INCH DIAMETER HOLE IN HORIZONTAL ALUMINUM INSTRUMENT PANEL SUPPORT STRUCTURE. THIS HOLE IS LOCATED BEHIND FIREWALL APROXIMATELY 10 INCHES AND APPROXIMATELY 1 INCH FROM PILOT'S SIDE OF FUSELAGE WALL. THIS HOLE WAS NOT INSULATED WITH RUBBER OR NYLON GROMMET MATERIAL AND WIRE HARNESS HAD RUBBED THROUGH THE INSTALLATION AT APPROXIMATELY 10 WIRES AGAINST SHARP METAL EDGES OF THE HOLE.