Service difficulty report · Skin · Cndair CL6002B19

Difficulty date
August 9, 2010
Submitted
August 25, 2010
Operation
Air carrier
Aircraft
N926EV
Make and model
Cndair CL6002B19
Aircraft serial
7843
Aircraft time
16,776 hours, 14,636 cycles
Engine
Ge CF343B1
Part
Skin
Condition
Corroded
Location
Bs 319.17 S26l/R
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

BELLY CORROSION JUST FWD OF FRAME 319.17 BETWEEN 26L AND 26R. REMOVED 6 EA FASTENERS FROM 319 FRAME BETWEEN 26L & 26R IAW SRM 51-42-06. REMOVED CORROSION IAW SRM 51-21-06. AREA REQUIRES NDT TO DETERMINE MATERIAL REMOVED. PERFORMED UT THICKNESS INSP OF BLEND AREA ON FRAME AT FS 319.70 BETWEEN STR 26L AND 26R IAW MAC NDT INSP PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS .048". REFER TO SRM FOR ALLOWABLE DAMAGE OR NOT. FOUND BLENDED AREA TO BE WITHIN LIMITS IAW SRM 53-00-00, BLOCK 101-199. BLENDED AREA NEEDS TO BE NDT FOR CRACKS AND REINSTALL REMOVED FASTENERS AND RESTORE FINISH. PERFORMED LPI, TYPE 1 METHOD C ON BLENDED AREA IAW SRM 51-12-00 IAW MAC NDT INSP PROCEDURE PT-1 NO INDICATIONS NOTED AT THIS TIME.