Service difficulty report · Frame · Piper PA28140

Difficulty date
April 25, 2003
Submitted
November 3, 2003
Operation
General aviation
Make and model
Piper PA28140
Aircraft time
5,835 hours
Engine
Lyc O320E3D
Part
Frame
Condition
Cracked
Location
Cabin Seat
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

(CAN) THIS FORWARD CABIN SEAT AND SOME SEATS IN OTHER SAME MODEL. DUE TO THEIR AGE, HAVE WEAKENED AND CRACKED AT WELDED JOINTS. THE MOST COMMON LOCATON HAS BEEN THE WELDED JOINT BETWEEN THE SEAT CUSHION FRAME AND THE 'S' BEND SUPPORT TUBE. THE OPPOSITE END OF THIS SUPPORT TUBE IS ALSO WELDED TO THE SEATLOWER TUBULAR FRAMEWORK WHICH IS STRONG ENOUGH NOT TO CRACK. ALTHOUGH THE SEATISSTILL STYRONG ENOUGH TO BEAR THE WEIGHT OF THE PILOT/PASSENGER EVEN WITH BOTHTHE LEFT AND RIGHT SUPPORT TUBE FAILURE, THE DANGER IS AS FOLLOWS:WITH BOTH SUPPORT TUBES FAILED, IF THE PILOT WOULD LEANBACK WITH ENOUGH REARWARD FORCE ON THE SEAT BACK, THE SEAT WILL DISENGAGE FROM THE SEAT TRACKS INADVERTENTLY AND SLIDE BACK.

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