Service difficulty report · Pump · Piper PA23150

Difficulty date
March 1, 2003
Submitted
March 4, 2003
Operation
General aviation
Aircraft
N211CR
Make and model
Piper PA23150
Aircraft serial
23358
Engine
Lyc O320*
Part
Pump
Part number
67B025
Condition
Failed
Location
Hyd System
Part time
4,456 hours
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

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

What was found

ONE PRESSURE LINE FAILED IN THE WING BETWEEN PUMP AND THE POWER PACK. AFTER REPLACEMENT OF ALUMINUM LINE THE SYSTEM WAS SERVICED AND TESTED. ON THE TEST HOP THE ENGINE DRIVEN PUMP FAILED AND THE PUMP CASE RUPTURED. THE PUMP WAS REPLACED, THE SYSTEM RESERVICED AND GROUND CHECKS COMPLETED. ON TEST HOP WITH THE SECOND PUMP, THE SAME FAILURE OCCURRED. THE PUMP RUPTURED, THE CASE SPLIT AND AFTER LOSS OF PRESSURE THE GEAR WAS EXTENDED BY HAND PUMP SUCCESSFULLY. THE TWO PUMPS AND THE POWER PACK HAVE BEEN SENT TO REPAIR STATION FOR IRAN. THIS IS ON A 1954 APACHE WITH 4456 HOURS TT. NORMAL CONFIGURATION IS WITH ONE ENGINE DRIVEN HYDRAULIC PUMP ON THE LEFT ENGINE. (EMERGENCY EXTEND BY HAND PUMP OR CO2 BLO DOWN.)

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