Service difficulty report · Nozzle · Bell 206BELL

Difficulty date
April 10, 2000
Submitted
June 23, 2000
Operation
General aviation
Make and model
Bell 206BELL
Engine
Allsn 250C20
Part
Nozzle
Part number
6878426
Condition
Cracked
Location
1 Blade Path Cir
Component
Turbine Assy · Allsn
Stage of operation
IN
How discovered
V
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) A GROUP OF 2ND STAGE NOZZLES ARE IN THE PROCESS OF RECALL. IT WAS FOUND THAT REPAIRS MADE TO SOME NOZZLES; WHICH WAS AN APPROVED REPAIR , HAVE FAILED TO REACH O/H AND ARE CRACKING WHERE THE FIRST STAGE BLADE PATH WAS JOINED TO THE 2ND STAGE NOZZLE. TRANSPORT CAW CORRECTIVE ACTION GROUP IS ADRESSSING THIS ISSUE.