Service difficulty report · Skin · Boeing 767323

Difficulty date
March 24, 2021
Submitted
March 24, 2021
Operation
General aviation
Filed by
MK1Y325K
Bedek Aviation Group
Aircraft
N29430
Make and model
Boeing 767323
Aircraft serial
29430
Aircraft time
83,191 hours, 13,654 cycles
Part
Skin
Condition
Damaged
Location
Bs 474-1373
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

PROBLEM DESCRIPTION: REPAIR – FUSELAGE SKIN STA 474.5, STA 476, STA 615.5, STA 1346 AND STA 1373, STR 26R/36R (SECTION 43 & 46), SKIN PANEL P/N 143T3521-5, P/N 146T3531-3. DURING MAINTENANCE INSPECTIONS AT IAI, EXISTING BLEND OUTS WERE FOUND ON THE R/H SIDE OF THE FUSELAGE. THE DAMAGE AREAS ARE CALLED AS M0239, M0240, M0241, M0247, M0248, M0249 AND M0250, AT (SECTION 43 & 46), FUSELAGE SKIN STA 474.5, STA 476, STA 615.5, STA 1346 AND STA 1373, STR 26R/36R. THE BLEND OUTS FALL ON RIVENTED AREAS AND THEY HAVE LESS THAN 2D AND/OR THE BLEND OUTS FALL WITHIN THE NO REPAIR ZONE BY A FUSELAGE SKIN CUTOUT AND THERFORE DO NOT MEET SRM ALLOWABLE DAMAGE REQUIREMENTS. THE DAMAGED AREAS WERE BEYOND LIMITS PER SRM 53-00-01, ALLOWABLE DAMAGE 1, FIGURE 101, DETAIL II AND/OR SRM 53-00-01, ALLOWABLE DAMAGE 1, FIGURE 202, SHEET 3. AN ULTRASONIC THICKNESS (UT) INSPECTION WAS ACCOMPLISHED, AND LESS THAN 10% OF MATERIAL WAS REMOVED AT ALL BLEND OUT LOCATIONS. THE SKINS ARE MADE FROM 0.160, 2024-T3 CLAD ALUMINUM MACHINED TO 0.056 MIN AND 0.210, 2024-T3 CLAD ALUMINUM CHEM-MILLED TO 0.056 MIN, THE EXISTING BLEND OUTS ARE COMMON TO DIFFERENT THICKNESS AREAS.