Service difficulty report · Shutoff Valve · Boeing 767338

Difficulty date
December 12, 2005
Submitted
June 6, 2006
Operation
General aviation
Make and model
Boeing 767338
Engine
Ge CF680C2*
Part
Shutoff Valve
Part number
7321870018
Condition
Failed
Location
Flight Control
Stage of operation
IN
How discovered
O
Nature of condition
K
Precautionary procedure
K

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

What was found

FLAP/SLAT SHUTOFF VLV LOCATED IN RT W/W LEAKING. INSPECTION FOUND CAP P/N 732-18718 HAD AN OPEN CRACK AT LAST/OUTERMOST THREAD RUNNING 270 DEGREES AROUND ITS CIRCUMFERENCE (CRACKED THROUGH). HEX-NUT END OF ALUMINUM CAP HAD LIFTED BY 0.1 INCHES UNDER HYD PRESS. CRACK WAS LOCATED ON PRESSURE SIDE OF `O` RING SEAL. CLOSE EXAM OF FRACTURE SURFACE SHOWED THAT CRACK STARTED AT ROOT OF LAST THREAD, PROPAGATED 0.050` AXIALLY (TOWARD THE SHUT-OFF VALVE MODULE), TRAVELED 75% OF WAY AROUND CAP’S OUTSIDE DIAMETER BEFORE FAILING RADIALLY WITH ONE FRACTURE PLANE. NO BEACH MARKS WERE EVIDENT ON FINAL FRACTURE PLANE, INDICATING SUDDEN FAILURE. CRACK COULD HAVE INITIALIZED DUE TO OVER-TORQUING DURING ASSY, OR FROM SUBSTAND