Service difficulty report · Skin · Boeing 757232

Difficulty date
May 17, 1996
Submitted
March 26, 2000
Operation
Air carrier
Aircraft
N628DL
Make and model
Boeing 757232
Aircraft serial
22918
Part
Skin
Condition
Fatigue
Location
Nr 1 Eng Strut
Stage of operation
IN
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 NR 1 ENGINE NACELLE STRUT SKIN WAS FOUND CRACKED IN THE UPPER FWD CORNER OF 442 AT ACCESS PANEL. THE CRACK LENGTH MEASURED 1 INCH LONG. THE STRUT SKIN IN THIS LOCATION IS THREE LAYERS OF 0.080 CLAD 2024-T3 WHICH ARE STRUCTURALLY BONDED. AT LETTER CHECK, MTC REPORTS CRACK HAS PROGRESSED PAST THE SECOND STOP DRILL AND IS OUTSIDE THE ALLOWABLE CRACK REGION OF FIG 2. ALSO, MTC REPORTS AN ADDITIONAL CRACK EMANATING FROM THE ACCESS HOLE IMMEDIATELY AFT THE 443 AT ACCESS PANEL, SEE FIG 3 FOR LOCATION AND LENGTHS OF THE 2 CRACKS.