Service difficulty report · Flow Divider · Piper PA28R180

Difficulty date
January 12, 2004
Submitted
January 12, 2004
Operation
General aviation
Aircraft
N4658J
Make and model
Piper PA28R180
Aircraft serial
28R30553
Aircraft time
4,947 hours
Engine
Lyc IO360B1E
Engine time
4,947 hours
Propeller
Hartzl HCC2YK1
Part
Flow Divider
Part number
2524321
Part serial
725
Condition
Bypassing
Location
Fuel System
Part time
4,947 hours
Component
Diaphragm · Bendix
Component part number
25253611
Stage of operation
TO
How discovered
C
Nature of condition
G, R, J
Precautionary procedure
O

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

What was found

FUEL FLOW DIVIDER, TEARDOWN AND TEST OF DIVIDER SHOWED UNIT WAS BY-PASSING FUEL , WHICH INTERRUPTED FLOW OF FUEL TO ENG UNDER HIGH POWER SETTINGS, LEADING TO INTERRUPTION OF ENG POWER AND/OR TOTAL LOSS OF ENG POWER. FURTHER TEAR DOWN, REVEALED DIAPHRAGM WAS STIFF, AN INDICATION OF LONG TIME IN SERVICE. CONNECTING SCREW WHICH ATTACHES DIAPHRAGM TO SHAFT WAS LOSE, NOT TORQUED. ESTIMATED DIAPHRAM WAS MANUFACTURED IN 1967. AFTER TIGHTENING ATTACHMENT SCREW TO ITS PROPER TORQUE, DIVIDER WAS TESTED AGAIN. AT 2.5 POUNDS OF FUEL PRESSURE APPLIED, NO INDICATION OF FUEL DIVIDER FLOWING UNTIL 3.7500 POUNDS OF FUEL PRESS WAS APPLIED. 1 POUND OF PRESSURE DIFFERENCE FOR FUEL FLOW WAS DUE TO STIFFNESS OF DIAPHRAGM.

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