Service difficulty report · Compressor · Bolkms BO105S

Difficulty date
October 29, 2005
Submitted
June 6, 2006
Operation
General aviation
Make and model
Bolkms BO105S
Aircraft time
6,280 hours
Engine
Allsn 250C20B
Part
Compressor
Condition
Damaged
Location
Engine
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

FOLLOWING A REPORT OF HIGHER THAN NORMAL TOT ON NR 2 ENGINE A POWER CHECK WAS CONDUCTED AND TROUBLESHOOTING LED TO SPLITTING THE COMPRESSOR FOR INSPECTION. SUBSTANTIAL DAMAGE WAS FOUND ON THE 5TH AND 6TH ROW STATOR VANES AND 6TH STAGE ROTOR BLADES. NO DAMAGE WAS EVIDENT FORWARD OF THE FIFTH COMPRESSOR STAGE. TWO STATOR BLADES WERE MISSING LEADING THE OPERATOR TO BELIEVE THAT A BLADE SEPARATION HAD CAUSED THE DAMAGE.