Service difficulty report · Rib · Beech C90A

Difficulty date
February 15, 2016
Submitted
April 22, 2016
Operation
General aviation
Make and model
Beech C90A
Aircraft time
8,209 hours
Engine
Pwa PT6A21
Part
Rib
Part number
5061000090
Condition
Cracked
Location
Lt Elevator
Part time
10,295 hours
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

(CAN) DURING A SCHEDULED INSPECTION OF THE LT ELEVATOR, THE INBOARD RIB WAS FOUND TO BE CRACKED. IT IS BELIEVED THAT THE REASON THE RIB WAS CRACKED WAS DUE TO THE FACT THAT NO WASHERS WERE FOUND UNDER THE NUTS SECURING THE RIB TO THE ELEVATOR TORQUE TUBE. ONCE THE ELEVATOR TORQUE TUBE WAS DISASSEMBLED FROM THE END CLOSE OUT RIB AND THE REMOVAL OF THE END RIB SUPPORT BRACKET, THE FULL EXTENT OF THE CRACK BECAME APPARENT. THE TOTAL CRACK LENGTH IN THE RIB IS APPROX. 1.75" IN LENGTH. THE CRACK IS LOCATED AT THE UPPER TORQUE TUBE ATTACHMENT BOLT HOLE AND EMANATING AFT.

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