Service difficulty report · Upper Drag Link · Piper PA28RT201T

Difficulty date
October 27, 1995
Submitted
March 26, 2000
Operation
General aviation
Make and model
Piper PA28RT201T
Engine
Cont
Part
Upper Drag Link
Part number
7642603
Condition
Broken
Location
Fwd Of Actuator
Part time
2,235 hours
Component
Piper · 7642603
Stage of operation
CL
Nature of condition
O
Precautionary procedure
A

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

What was found

(CAN)A LOUD BANG WAS HEARD DURING GEAR RETRACTION. TWO GREEN LIGHTS WERE NOTED ON EXTENSION. THE ACFT LANDED WITHOUT FURTHER INCIDENT AND THE UPPER DRAG BRACE WAS FOUND BROKEN IN HALF FWD OF THE HY D ACTUATOR. FURTHER EXAMINATION REVEALED EVIDENCE OF CORROSION INITIATED STRESS CRACK. THE SUBMITTER STATES THAT AD 94-14-14 HAD BEEN C W 160 HRS PREVIOUSLY WITH NO EVIDENCE OF CRACK BEING FOUND. NEW PART IS 50 PERCENT THICKER THAN THE OLD PART IN THE AREA OF THE CRACK. SUBMITTER HAS PERSONAL KNOWLEDGE OF TWO ADDITIONAL FAILURES OF THE SAME KIND.

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