Service difficulty report · Skin · Boeing 767323

Difficulty date
February 21, 2021
Submitted
February 22, 2021
Operation
General aviation
Filed by
MK1Y325K
Bedek Aviation Group
Aircraft
N385AM
Make and model
Boeing 767323
Aircraft serial
27059
Aircraft time
102,560 hours, 16,713 cycles
Part
Skin
Condition
Dented
Location
Rt Wing Te Flap
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

DURING MAINTENANCE INSPECTIONS AT IAI, 2 EXISTING DENTS WERE FOUND ON UNDERSIDE OF THE RT WING OUTBOARD TRAILING FLAP. THE DENTS WERE MEASURED AS HAVING WIDTHS OF 1.8" AND 1.7" AS DEPTHS OF 0.027" AND 0.029" RESPECTIVELY. THE DAMAGES WERE FOUND ABOVE LIMITS PER B767-300SRM 57-53-01, ALLOWABLE DAMAGE 1, FIGURE 101. THESE DIMENSIONS ARE WITHIN ALLOWABLE DAMAGE LIMITS AS PER SRM B767-300 SRM 57-53-01 ALLOWABLE DAMAGE 1, DETAIL IV. HOWEVER, DUE TO THE DISTANCE BETWEEN THE 2 DENTS BEING 0.85", WHICH IS LESS THAN THE MINIMUM OF 3" REQUIRED, THIS DAMAGE DOES NOT MEET ALLOWABLE DAMAGE LIMIT AS PER SRM B767-300 SRM 57-53-01 ALLOWABLE DAMAGE 1, DETAIL IV. THE LOWER PANEL OUTER SKIN IS MADE FROM 0.100, 2024-T3 CLAD ALUMINUM CHEM-MILLED TO 0.013 MIN PER 767-300 SRM 57-53-01. THE DENTS ARE COMMON TO 0.090" THICKNESS. THE STRUCTURE IS CLASSIFIED A SECONDARY STRUCTURE PER B767-300 SRM 51-00-04.