Service difficulty report · Blade · Bolkms BO105S

Difficulty date
February 17, 2004
Submitted
March 1, 2004
Operation
General aviation
Make and model
Bolkms BO105S
Aircraft time
8,431 hours
Engine
Allsn 250C20
Part
Blade
Part number
10531980
Condition
Peeling
Location
Tail Rotor
Component
Tail Rotor · Urocop
Component part number
10531702
Stage of operation
IN
How discovered
V
Nature of condition
W
Precautionary procedure
K

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

What was found

(CAN) TAIL ROTOR BLADES RECEIVED FROM MFG WITH THE PAINT REFINISHED AFTER REPAIR OR INSPECTION ARE PEELING OR SHREDDING TO THE BLADE BODY SURFACE BELOW. THIS IS OCCURRING USUALLY WITHIN THE FIRST 100 HOURS OF OPERATION. THE NEW REFINISHED PAINT SURFACE IS THICK ENOUGH TO PROTRUDE CONSIDERABLY ABOVE THE LEADING EDGE ABRASION STRIP CAUSING THE PAINT TO PEEL BACK ON THE SURFACE OF THE BLADE, CAUSING IMBALANCE, AND BLADE SURFACE TO BE SUSCEPTIBLE TO MOISTURE. THE PAINT REFINISHING PROCESS APPEARS TO BE TOO THICK WITH NO TRANSITION POINT TO THE LEADING EDGE ABRASION STRIP. THIS IS AN ON GOING PROBLEM INVOLVING NUMEROUS TAIL ROTOR BLADE SETS FOR THE PAST 18 MONTHS.