Service difficulty report · Hinge Pin · Cndair CL6002D24

Difficulty date
December 18, 2011
Submitted
December 21, 2011
Operation
Air carrier
Aircraft
N200PQ
Make and model
Cndair CL6002D24
Aircraft serial
15200
Aircraft time
7,467 hours, 5,209 cycles
Part
Hinge Pin
Condition
Corroded
Location
Horiz Stab
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

DURING A 3FH8 INSPECTION DAMAGE WAS FOUND TO THE HORIZONTAL STAB HINGE FITTING (RT O/B). HEAVY CORROSION (RUST) WAS FOUND ON THE HINGE PIN BUSHING AND HINGE PIN. IT APPEARS AS IF THE HINGE PIN AND BUSHING HAVE SEIZED TOGETHER AND AS THE STABILIZER WAS ACTUATED IN FLIGHT THE ANTI-ROTATION TAB OF THE PIN AND BUSHING HAVE GOUGED THE ANTI-ROTATION TANG OF THE HINGE FITTING. THE ANTI-ROTATION TANG IS 1 & 3/16" LONG AND 7/32" DEEP, THE GOUGED AREA IS 7/8" LONG AND IS 7/32" DEEP AT ITS MAXIMUM POINT. REPAIRED RT HORIZONTAL STAB ANTI ROTATION TAB IAW REO 690-55-11-005. GOOD FOR 5000FH FROM TIME OF REPAIR. SEE REO 690-55-11-005 FOR EXTENSIONS AS NEEDED. REINSPECT TABS AT EVERY SUBSEQUENT 2000FH.