Service difficulty report · Torque Shaft · Bombdr DHC8400

Difficulty date
February 16, 2005
Submitted
April 1, 2005
Operation
General aviation
Make and model
Bombdr DHC8400
Engine
Pwc PW150A
Propeller
Rotol CR4086123F17
Part
Torque Shaft
Condition
Cracked
Location
Nr 1 Engine
Stage of operation
CL
How discovered
O
Nature of condition
E
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) DURING CLIMB, NR1 PEC CAUTION LIGHT ILLUMINATED FOLLOWED BY A DROP IN NP AND TQ. A FEW SECONDS LATER THE NR1 ENG FADEC FAIL WARNING LIGHT ILLUMINATED AND ALL PARAMETERS BECAME (DASHES). THE PILOTS ELECTED TO SHUTDOWN NR1 ENGINE AND RETURN TO BASE. SINGLE ENGINE LANDING COMPLETED. ENG FAULTS BOTH CHANNELS 162, 470, 719, 734, 735, 938. AND CHANNEL-A HAD FAULT: 718-MECHANICS FOUND THE TORQUE SHAFT REFERENCE TUBE SEPARATED FROM THE TORQUE TUBE. THE CRACK/SEPARATION OCCURRED JUST AFT OF THE WELD THAT JOINS THE TWO PIECES TOGETHER (VERIFIED BY REMOVING LAY SHAFT COVER). ENGINE ASSEMBLY REPLACED. FOLLOW-UP INVESTIGATION TO BE CARRIED OUT.