Service difficulty report · Shaft · Dhav DHC8301

Difficulty date
February 7, 2011
Submitted
September 14, 2015
Operation
General aviation
Make and model
Dhav DHC8301
Engine
Pwa PW123
Propeller
Hamstd 14SF23
System (JASC)
7603 · Power Lever
Part
Shaft
Part number
87620130101
Condition
Broken
Location
Engine Control
Part time
9,180 hours
Stage of operation
NR
How discovered
O
Nature of condition
J
Precautionary procedure
E

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

What was found

(CAN) DURING POST C-CHECK ENGINE GROUND RUN AT 85 PERCENT TORQUE, THE LT ENGINE TORQUE INCREASED RAPIDLY TO AN OVERTORQUE SITUATION AND ENGINE CONTROL VIA THE POWER AND CONDITION LEVERS WAS LOST. THE ENGINE WAS SHUTDOWN USING THE FUEL SHUTOFF T-HANDLE. ON INSPECTION THE ENGINE CONTROL SPRING STRUT SHAFT WAS FOUND TO HAVE BROKEN. THE STRUT WAS PRE MS8Q101678 WHICH INTRODUCES AN IMPROVED MATERIAL FOR THE STRUT SHAFT AND A REDUCED DIAMETER RIVET. FDR DATA REVEALED A VERY BRIEF OVERTORQUE EVENT. THE ENGINE WILL REMAIN "ON WING" BUT THE PROP HAS BEEN REMOVED FOR A LOCALLY PERFORMED INSPECTION. OPERATOR INTENDS TO CARRY OUT A FLEET CHECK OF THEIR SPRING STRUTS TO DETERMINE HOW MANY PRE-MOD STRUTS THEY HAVE, AND TO PERFORM A CAMPAIGN TO REPLACE THEM WITH POST MOD UNITS.