Service difficulty report · Engine · Dhav DHC8*

Difficulty date
August 25, 2015
Submitted
April 22, 2016
Operation
General aviation
Make and model
Dhav DHC8*
Engine
Pwa PW121
Part
Engine
Condition
Power Loss
Location
Nr 2
Stage of operation
AP
How discovered
O
Nature of condition
R
Precautionary procedure
A

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

What was found

(CAN) LOSS OF NR 2 ENGINE POWER OCCURRED DURING APPROACH AND THE TORQUE INDICATION SHOWS 3 %. THE AIRCRAFT PERFORMED AND UNEVENTFUL LANDING. IT WAS FOUND THAT A TUBE WAS BROKEN AT CONNECTION TO HMU. THE TUBE WILL BE REPLACED.