Service difficulty report · Propeller · Dhav DHC8103

Difficulty date
August 24, 2013
Submitted
September 14, 2015
Operation
General aviation
Make and model
Dhav DHC8103
Aircraft time
9,466 hours
Engine
Pwc PW150A
Propeller
Rotol CR4086123F17
Part
Propeller
Condition
Malfunctioned
Stage of operation
CL
How discovered
O
Nature of condition
J
Precautionary procedure
E, A

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

What was found

(CAN) ON 24-AUG-2013, DURING THE ENROUTE CLIMB PORTION OF THE FLIGHT, THE NR 1 PROPELLER WENT INTO AN OVERSPEED CONDITION. THE CREW CONDUCTED THE QRH MEMORY AND CHECKLIST DRILLS IAW THE PORTER SOP, INCLUDING AN IN-FLIGHT SHUTDOWN OF THE AFFECTED ENGINE. THE SINGLE ENGINE APPROACH WAS SAFELY FLOWN AND THE ACFT ARRIVED AT THE GATE WITHOUT FURTHER INCIDENT. 24-AUG-2013 ROUTINE DEPARTURE FOR FIRST FLIGHT OF THE DAY. NO ISSUES, NO MEL`S, FLIGHT WAS CLEARED TO FL240, THROUGH 17000 FT. CAPTAIN AND F/O HEARD AN INCREASE ENGINE NOISE SIMILAR TO AN ENGINE SURGE. THEY NOTICED A SMALL FLUCTUATION OF TORQUE. SECONDS LATER A PROPELLER INDICATION OF 1060 TO 1080 AND ASSOCIATED PEC NR 1 CAUTION LIGHT WITH THE MASTER CAUTION. F/O ADVISED OF A PROP OVERSPEED ON NR 1 ENGINE WITH ASSOCIATED PEC. ATC WAS CONTACTED AND A REQUEST TO RETURN TO POINT OF DEPARTURE WAS MADE AND EMERGENCY WAS DECLARED. SUCCESSFUL SINGLE ENGINE LANDING WAS ACHIEVED. THE NR 1 PEC, PROPELLER ELECTRONIC CONTROL, INFORMATION WAS DOWNLOADED. 3 FAULTS WERE LOGGED: 260, 236, AND 122. IAW THE FAULT ISOLATION MANUAL TASK 61-20-06-810-818, THE PEC WAS REPLACED. A RETURN TO SERVICE ENGINE RUN CHECK WAS COMPLETED ON THE EVENING OF AUGUST 24. THE ACFT IS RELEASED AND WILL BE READY TO RETURN TO SERVICE.