Service difficulty report · Skin · Boeing 777268

Difficulty date
June 15, 2010
Submitted
June 15, 2010
Operation
General aviation
Make and model
Boeing 777268
Part
Skin
Part number
315W117625
Part serial
NONE
Condition
Damaged
Location
Thrust Reverser
Component
Thrust Reverser · Boeing
Component part number
315W1295219
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

THE 315W1176-25 AFT COWL SKIN HAS AN AREA OF DISCOLORATION, POSSIBLE OVERHEAT CENTERED 5.0 INCHES FROM THE AFT EDGE OF THE SKIN AND 4.25 INCHES FROM THE LOWER EDGE OF THE SKIN. THE DISCOLORATION MEASURES 2.5" X 1.5". HEAT DAMAGE ANALYSIS PER SRM 51-20-03 REVEALED THE FOLLOWING, DEFECT: CONDUCTIVITY AND HARDNESS OUT OF RANGE. MATERIAL: 2024-T62 ALUMINUM. ACTUAL CONDUCTIVITY (MAX OF 35 READINGS): 42.3 % IACS (17" FROM AFT EOP; 19" FROM UPPER EOP). IDEAL CONDUCTIVITY: 36.0--40.0 % IACS. ACTUAL HARDNESS (MAX OF 5 READINGS): 66.0 HRB (2 INCHES FROM THE AFT EOP; 18.5 INCHES FROM UPPER EOP). IDEAL HARDNESS: 72.0--86.0 HRB. LOCATION: ENTIRE AFT COWL SKIN. TOTAL MEASUREMENTS: 35 CONDUCTIVITY READINGS; MAX, 42.3 % IACS; MIN, 40.3 % IACS; MEDIAN, 41.00 % IACS; MODE, 40.90 % IACS; MEAN, 41.28 % IACS; STD DEV, 0.86 % IACS.