Service difficulty report · Bolt · Boeing 1072

Difficulty date
October 16, 2010
Submitted
March 15, 2011
Operation
Air carrier
Make and model
Boeing 1072
Aircraft time
38,910 hours
Engine
Ge CT581402
Part
Bolt
Part number
107CK27332
Condition
Broken
Location
Cyclic
Stage of operation
AP
How discovered
O
Nature of condition
F
Precautionary procedure
A

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

What was found

DURING NORMAL OPERATIONS A "SNAP" IN THE CYCLIC WAS NOTICED BY THE PIC. AS POWER WAS APPLIED THE PIC NOTED ABNORMAL BEHAVIOR IN THE ACFT THAT REQUIRED A FULL RT AND FWD CYCLIC INPUT TO MAINTAIN STRAIGHT AND LEVEL ATTITUDE. ACFT WAS STABILIZED AND LANDED IMMEDIATELY. NO INJURIES OR DAMAGE TO ACFT UPON LANDING. ACFT WAS SHUTDOWN NORMALLY. BOLT, PN 107CK2733-2 WAS FOUND WITH THE HEAD BROKEN OFF. THE BOLT HAD WORKED ITS WAY OUT OF THE CONTROLS UNTIL IT CONTACTED THE LT COWLING. WITH THE BOLT BROKEN THE LT RETENSION PIN BECAME PARTIALLY DISENGAGED FROM THE FWD UPPER CONTROLS YOKE CAUSING THE UNUSUAL CONTROL INPUTS. COMPLETE SET OF FWD UPPER CONTROLS HAS BEEN REPLACED ON THIS ACFT. ALL OTHER ACFT WERE INSPECTED WITH NO DEFECTS NOTED. AS A PRECAUTIONARY MX ACTION ALL BOLTS FROM THE SAME PRODUCTION BATCH HAVE BEEN REMOVED FROM SERVICE. THE FAILED BOLT HAS BEEN RETURNED TO THE TYPE CERTIFICATE HOLDER FOR METALLURGY ANALYSIS.