Service difficulty report · Floorbeam · Cndair CL6002C10

Difficulty date
November 4, 2010
Submitted
November 5, 2010
Operation
Air carrier
Aircraft
N619QX
Make and model
Cndair CL6002C10
Aircraft serial
10246
Aircraft time
13,772 hours, 10,159 cycles
Engine
Ge CF348C5B1
Part
Floorbeam
Condition
Cracked
Location
Bs 280
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

C3 CHECK - 280 BEAM IS CRACKED ON LT AND RT SIDE. PERFORMED CUTLINE ON NEW BEAM IAW REO 670-53-11-047. REMOVED LT AND RT 280 DRIP PANS AND INTERCOSTALS IAW SRM 51-42-21-001-001-A01. FOUND COCKPIT FLOOR ANGLE OF FS 280 CRACKED. PERFORMED LPI ON CUTLINE NO CRACKS FOUND AT THIS TIME IAW NDTM LPI 51-20-008-230-A01 AND REO 670-53-11-047. REMOVED LT AND RT CRACKED 280 BEAM AND FLOOR ANGLE IAW SRM 51-42-06-001-001-A01 AND REO 670-53-11-047. LOCATED HOLES IN NEW BEAMS IAW 51-40-11-001-001-A01, 670-53-11-047. INSTALLED LT AND RT 280 BEAM IAW REO 670-53-11-047. INSTALLED PREVIOUSLY REMOVED DRIP PANS AND INTERCOSTALS IAW SRM 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. LOCATED HOLES IN NEW ANGLE AND INSTALLED ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01, 51-42-15-001-001-A01 AND REO 670-53-11-047. APPLIED CORROSION INHIBITING COMPOUND AND TOPCOATED IAW SRM 51-25-16-001-001-A01 AND 51-21-11-001-001-A01.