Service difficulty report · Spar · Cessna A185F

Difficulty date
November 16, 2009
Submitted
November 17, 2009
Operation
General aviation
Aircraft
N585CM
Make and model
Cessna A185F
Aircraft serial
18504099
Aircraft time
1,480 hours, 100 cycles
Engine
Cont IO550D
Engine time
211 hours, 100 cycles
Propeller
Mcauly D3A34C401
Part
Spar
Part number
0731026207310281
Condition
Cracked
Location
Zone 300
Part time
1,480 hours, 100 cycles
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

CRACKS WERE DETECTED BY VISUAL INSP ON THE VERT STAB AFT SPAR WHERE THE SPAR ATTACHES TO THE AFT TAIL CONE BULKHEAD AT STA FS230.187. CRACKS PENETRATED THE VERT SPAR PN 0731026-2 AND DOUBLER 0731028-1, AT THE WEAK POINT AT THE BOTTOM WHERE THE SPAR IS REDUCED IN DIMENSION AND CUT OUT TO ALLOW CLEARANCE FOR THE ELEVATOR TORQUE TUBE AND PUSH ROD. DAMAGED PARTS WERE DRILLED OUT, NEW SPAR PN 0731026-1,DOUBLER 0731027-1,DOUBLER 0731028-1 WERE ASSEMBLED AND INSTALLED. MFG SERVICE KIT SK180-43 WAS INSTALLED TO STRENGTHEN THE ATTACH POINTS OF VERTICAL SPAR TO BULKHEAD BY ADDITION OF A DOUBLER ON THE BULKHEAD FWD SIDE AND ALSO THE ADDITION OF 4 STRUCTURAL SCREWS THROUGH BULKHEAD AND SPAR. THE CRACKS WERE DISCOVERED BY AN FAA INSPECTOR DURING A VISUAL INSP. AFTER DISASSEMBLY IT WAS DETERMINED THE CRACKS WERE VERY RECENT. ACFT WAS ON FLOATS.

More about the Cessna A185F