Service difficulty report · Shaft · Braero BAE125800A

Difficulty date
November 4, 2004
Submitted
March 3, 2005
Operation
General aviation
Make and model
Braero BAE125800A
Aircraft time
5,419 hours
Engine
Garrtt TFE7315R
Part
Shaft
Part number
25CF263321A
Condition
Worn
Location
Flap Vane
Component
Flap Vane · Bac
Component part number
25WF101A
Stage of operation
IN
How discovered
O
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) UPON PERIODIC INSPECTION IT WAS NOTED THAT THERE WAS APPARENT CONTACT BETWEEN THE IB FLAP VANES ON BOTH LT AND RT ASSEMBLIES ONTO THE TORQUE SHAFT AND BEVEL HOUSING ASSY. THIS UNUSUAL CONTACT WAS DEDUCED TO OCCUR DURING FLIGHT LOADS AS THE CLEARANCE BETWEEN THESE ASSEMBLIES AT ITS CLOSEST LOCATION (ABOUT 15 DEGREES OF FLAP DEFLECTION) HAS APPROXIMATELY 0.600' CLEARANCE. EVEN WITH ANY ABNORMAL PLAY CAUSED BY WORN BUSHINGS ON THE ATTACHING HARDWARE OF THE FLAP MECHANISM COULD NOT PRODUCE THIS KIND OF CONTACT. INVESTIGATION IS ONGOING.