Service difficulty report · Fitting · Bell 212

Difficulty date
August 2, 2011
Submitted
September 9, 2011
Operation
Air carrier
Make and model
Bell 212
Engine
Pwa PT6T3B
Part
Fitting
Part number
212030154101
Condition
Cracked
Location
M/R Gearbox
Part time
292 hours
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

LIFT LINK FITTING AFT LUG FOUND CRACKED BY MECHANIC DURING DAILY INSP. CAUSE WAS FOUND TO BE WRONG P/N BOLT INSTALLED. TB 212-91-132 HAD BEEN COMPLETED WHICH INCORPORATES IMPROVED LIFT LINK FITTING P/N 212-030-154-101 THAT REQUIRES LARGER DIAMETER BOLT P/N 412-030-224-101. P/N 212-030-155-001 BOLT WAS FOUND INSTALLED. THIS BOLT IS .050" SMALLER DIAMETER THAN THE IMPROVED BOLT AND WOULD HAVE PERMITTED MOVEMENT WITHIN THE INSTALLED BUSHING. THIS SMALLER BOLT IS ALSO NORMALLY INSTALLED WITH THE HEAD FACING AFT WHILE THE NEW INSTALLATION IS WITH THE HEAD FORWARD. ANOTHER VISIBLE DIFFERENCE IS THE ORIGINAL BOLTS HAVE A FLAT SURFACE HEAD WHILE THE IMPROVED BOLTS HAVE A DIMPLED HEAD SURFACE. WE WILL BE ISSUING A FIELD COMPLIANCE FORM TO INSPECT ALL COMPANY ACFT FOR THE CORRECT LIFT LINK FITTING AND BOLT INSTALLATION.

More about the Bell 212