Service difficulty report · None · Boeing 767323

Difficulty date
October 11, 2021
Submitted
October 12, 2021
Operation
General aviation
Filed by
MK1Y325K
Bedek Aviation Group
Aircraft
N398AN
Make and model
Boeing 767323
Aircraft serial
29605
Aircraft time
79,217 hours, 13,165 cycles
Part
None
Condition
None
Stage of operation
IN
How discovered
V
Nature of condition
Z
Precautionary procedure
K

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

What was found

EXTERNAL FUSELAGE SKIN – STA 1349.5, BETWEEN S-23R AND S-24R, AND STA 1363.5, S-26R: DURING CONVERSUON AT IAI, MAINTENANCE HAVE FOUND TWO (2) EXISTING BLEND OUT ZONES IN EXTERNAL FUSELAGE SKIN AMONG FASTENER AREAS. M0383: STA 1349.5, BETWEEN S-23R AND S-24R. NDT INSPECTIONS WERE PERFORMED AND FOUND NO EVIDENCE FOR CORROSION OR CRACKS. INITIAL SKIN THICKNESS: 0.210”. MIN THICKNESS: 0.206”. BLEND OUT DIMENSION 1: L=9.29” X W=0.73”. BLEND OUT DIMENSION 2: L=10.09” X W=0.59”. SHOP REMOVED FASTENERS IN ACCORDANCE WITH SRM 51-40-02. (THREE SOLID RIVETS 1/4”, ONE HI-LOK ¼” AND ONE HI-LOK 5/16”). REMOVED MATERIAL IN BLEND OUTS IS LESS THAN 5%. M0384: STA 1363.5 STR 26R. NDT INSPECTIONS WERE PERFORMED AND FOUND NO EVIDENCE FOR CORROSION OR CRACKS. INITIAL SKIN THICKNESS: 0.162”. MIN THICKNESS: 0.157”. BLEND OUT DIMENSION: L=3.74” X W=0.47”. SHOP REMOVED A FASTENER IN ACCORDANCE WITH SRM 51-40-02 (ONE HI-LOK ¼”).