Service difficulty report · Bracket · Piper PA44180

Difficulty date
April 5, 2017
Submitted
April 5, 2017
Operation
General aviation
Aircraft
N433PA
Make and model
Piper PA44180
Aircraft serial
4496063
Aircraft time
9,405 hours
Engine
Lyc O360A1H6
Part
Bracket
Part number
67031003
Condition
Broken
Location
Downlock
Stage of operation
IN
How discovered
9
Nature of condition
O
Precautionary procedure
K

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

What was found

DURING A ROUTINE INSPECTION, THE GEAR RETRACTION FITTING OF THE RIGHT MAIN LANDING GEAR WAS FOUND TO BE BROKEN. THE THINNER OF THE TWO EARS THAT BOLTS TO THE ACTUATOR ROD-END HAD SEPARATED. THE FITTING IN QUESTION IS MOUNTED AT THE TOP OF THE GEAR TRUSS ASSY AND CONNECTS THE TRUSS, ACTUATOR, AND DOWNLOCK. HAD THE SECOND EAR FAILED, THERE WOULD NO LONGER BE ANY CONNECTION BETWEEN THE ACTUATOR, THE SPRING, AND THE DOWNLOCK. THIS WOULD HAVE PRECLUDED THE GEAR FROM LOCKING IF DOWN, AND WOULD HAVE ALLOWED IT TO FALL INTO THE EXTENDED POSITION ON ITS OWN. VISUAL EXAMINATION OF THE FAILED PART REVEALED A .25 INCH AREA OF THE FRACTURE SURFACES THAT ARE CONSISTENT WITH THE EXISTANCE OF A CRACK BEFORE THE REMAINDER OF THE MATERIAL FRACTURED (APPROX 1".) SUBMITTER SPECULATES THAT WEAR TO THE PART, CAUSED BY THE SIDES OF THE ACUTATOR ROD END BEDDING INTO THE MATERIAL, PRODUCED STRESS TO THE PART THAT CONTRIBUTED TO ITS FAILURE.

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