Service difficulty report · Fire Detector · Skrsky S92A

Difficulty date
July 22, 2013
Submitted
September 14, 2015
Operation
General aviation
Make and model
Skrsky S92A
Aircraft time
4,398 hours
Engine
Ge CT78A
Part
Fire Detector
Part number
9231004802
Condition
Inoperative
Stage of operation
CR
How discovered
O
Nature of condition
P, B
Precautionary procedure
O

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

What was found

(CAN) CREW REPORTED INTERMITTENT "FIRE WARNING" ON NR 2 ENGINE. AN "S" TURN WAS CONDUCTED TO TRY AND VERIFY IF SMOKE WAS VISIBLE, NONE WAS SEEN. WARNING WOULD ILLUMINATE FOR 1 OR 2 SECONDS THEN EXTINGUISH. THIS OCCURRED SEVERAL TIMES. ACFT RETURNED WITHOUT FURTHER INCIDENT. THIS IS THE THIRD FALSE FIRE WARNING ON THIS ENGINE IN A SPAN OF 5 DAYS. 1 DETECTOR WAS REPLACED ORIGINALLY, THE SECOND TIME BOTH DETECTORS WERE REMOVED THE CONNECTIONS BETWEEN THE HARNESSES AND DETECTORS WERE CLEANED, RECONNECTED AND RESEALED. THIS TIME BOTH DETECTORS AND THE OTBD HARNESS WERE REPLACED. THERE HAVE BEEN NO FURTHER OCCURRENCES SINCE. THE NR 2 OTBD FLAME DETECTOR APPEARS TO BE THE ONE CAUSING THE VAST MAJORITY OF FALSE WARNINGS, DUE TO ITS LOCATION. ALTHOUGH A HEAT SHRINK TYPE MATERIAL HAS BEEN ADDED OVER TOP OF THE CONNECTION BETWEEN THE HARNESS AND DETECTOR, WE STILL SEE THIS ISSUE OCCASIONALLY. IT IS THOUGHT THAT THE VIBRATION, EXHAUST, AND DOWN WASH FROM THE ROTOR IN THE AREA OF THE OTBD DETECTOR IS HARSHER AT THIS LOCATION THEN ANY OF THE OTHER DETECTOR LOCATIONS. THIS CAUSES THE PINS IN THE CONNECTORS TO FRET WITH TIME AND CARBON TO ACCUMULATE, EVENTUALLY PROVIDING THE GROUND THAT THE SYSTEM NEEDS TO TRIGGER THE WARNING. MFG IS NOW WORKING ON A BETTER CONNECTION/HARNESS WITH THE GOAL OF ELIMINATING THIS ISSUE ENTIRELY.