Service difficulty report · Skin · Cndair CL6002C10

Difficulty date
September 23, 2010
Submitted
September 23, 2010
Operation
Air carrier
Aircraft
N611QX
Make and model
Cndair CL6002C10
Aircraft serial
10041
Aircraft time
22,103 hours, 16,230 cycles
Engine
Ge CF348C1
Part
Skin
Condition
Chafed
Location
Bs 977
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

C-CHECK - FUSELAGE SKIN CHAFED FROM BELLY FAIRING CHANNEL 195DL, 2 AREAS ON FWD AND AFT SKIN AT FS: 977.0. BLENDED 2 CHAFED AREAS ON 2 BELLY SKINS AT FS 974.0 IAW SRM 51-12-00-001-001-A01. FWD BLEND MEASURES 0.82" X 0.8"W X .008D, ORIGINAL THICKNESS IS .180" REMAINING MATERIAL IN BLEND IS .172" WITHIN LIMITS OF REO 670-53-00-014. AFT BLEND MEASURES 1.1"L X 1.3"W X .027"D, ORIGINAL THICKNESS OF SKIN IS 0.125", REMAINING MATERIAL IN BLEND AREA IS .098, WITHIN LIMITS OF REO 670-53-00-014. PERFORMED LPI ON BLENDED AREAS NO CRACKS FOUND AT THIS TIME IAW NDTM LPI 51-20-0080230-A01, REO 670-53-00-014. TREATED AND PRIMED AREAS WORKED IAW SRM 51-21-11 AND 51-25-06. APPLIED TOP COAT IAW SRM 51-25-16-001.