Service difficulty report · Fire Loop · Dhav DHC3

Difficulty date
November 20, 2000
Submitted
January 19, 2001
Operation
Air carrier
Make and model
Dhav DHC3
Aircraft time
25,169 hours
Engine
Pwa R134059
Part
Fire Loop
Condition
Broken
Location
Engine Mount
Part time
1 hours
Stage of operation
NR
How discovered
O
Nature of condition
E
Precautionary procedure
O

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

What was found

(CAN) AIRCRAFT HAD ENGINE FAILURE CAUSED BY RBOKEN EXHAUST ROCKER ARM. THIS HAPPENED DURING CRUISE. ENGINE RAN VERY ROUGH AND CAUSED ENGINE TO ROCK EXCESSIVELY. THIS CAUSED THE FIRE DETECTION RING TO BREAK. WITH THIS BROKEN YOU WOULD NOT GET A WARNING LIGHT IF YOU HAD AN ENGINE FIRE. NOTE: RING IS MOUNTED TO ENGINE MOUNT AND ISOLATOR RUBBERS. THIS MAKES RING REGENT ON ENGINE MOUNT AND ALLOWS RING TO ROCK WITH ENGINEMOVEMENT. NOTE ATTACHED DRAWAING. THIS INSTALLATION WAS APPROVED UNDER STC NO.SA00-48 ISSUED BY VIKING AIR LTD. VIKING WAS NOTIFIED OF PROBLEM. THIS INSTALLATION IS TO C/W AD CF-99-06.2000-12-18TC: PACIFIC REGIONAL ENGINEERING TO REVIEW STC INFORMATION AND ARE THE OPI FOR POSSIBLE CORRECTIVE ACTION