Service difficulty report · Flow Divider

Difficulty date
August 11, 1996
Submitted
March 26, 2000
Operation
General aviation
Engine
Pwa PW125B
Part
Flow Divider
Condition
Faulty
Location
#1 Engine
Stage of operation
AP
Nature of condition
X, R
Precautionary procedure
O

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

What was found

(CAN) ON APPROACH #1 ENGINE SUFFERED TORQUE FLUCTUATIONS BEFORE FLAMING OUT. THE FUEL FLOW DIVIDER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.