Service difficulty report · Line

Difficulty date
October 5, 2006
Submitted
December 4, 2006
Operation
General aviation
Engine
Pwa JT15D4
Part
Line
Condition
Damaged
Location
Anti Ice Sys
Part time
7,161 hours
Stage of operation
NR
How discovered
9
Nature of condition
K
Precautionary procedure
O

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

What was found

(CAN) SEE REPORT ATTACHED GAS GENERATOR DISPLAYED VISIBLE SIGNS OF COKED OIL ON THE EXTERNAL CASING. ENGINE OIL LEAK WAS CAUSED BY ANTI-ICING STEEL TUBE DEBONDING FROM THE INTERMEDIATE CASE CASTING AT THE STEEL TAB USED TO LOCATE THE TUBE DURING THE CASTING PROCESS. THE TAB PROTRUDES INTO THE OIL TANK AND IF DEBONDED CAN CAUSE OIL LEAKAGE. ENGINEERING REPORT ATTACHED TO THIS SDR. (TC NR 20061005001)