Service difficulty report · Fitting · Cndair CL6002B19

Difficulty date
May 3, 2011
Submitted
September 14, 2015
Operation
General aviation
Make and model
Cndair CL6002B19
Aircraft time
34,170 hours
Engine
Ge CF343A1
Part
Fitting
Part number
600210582
Condition
Corroded
Location
Vertical Stab
Part time
37,361 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

(CAN) WHILE CARRYING OUT A DETAILED INSPECTION OF THE HORIZONTAL STABILIZER PIVOT FITTINGS IAW TASK NR RJ2-55-320-502, THE AME OBSERVED IRON OXIDE COLORED SUBSTANCE ON AND AROUND THE STABILIZER PIVOT PINS. UPON FURTHER CLEAN UP OF THE AREA AND CLOSER INSPECTION, THE RT SIDE PIVOT FITTING BUSHING IN THE VERTICAL STABILIZER PIVOT FITTING WAS FOUND MIGRATED 0.028". THE HORZONTAL STABILIZER WAS REMOVED FOR ACCESS TO REMOVE THE BUSHING IN THE RT SIDE VERTICAL STABILIZER LUG. FURTHER CORROSION WAS FOUND IN AND AROUND THE LUGS. CORROSION REMOVED AND THE LUG WAS REAMED TO FIRST OVERSIZE HOLE. THE BORE MEASUREMENTS WERE FOUND WITHIN LIMITS OF SB601R-55-007, REV D. FITTING REPAIRED IAW REO601R-55-31-210. CAD PLATING CARRIED OUT ON BOTH THE REWORKED BORE AND PORTION OF THE HAT BUSHING WITH REF TO THE REO.