Service difficulty report · Stiffener · Boeing 767238

Difficulty date
June 10, 2009
Submitted
June 16, 2009
Operation
Air carrier
Aircraft
N673BF
Make and model
Boeing 767238
Aircraft serial
23402
Aircraft time
61,332 hours, 27,015 cycles
Part
Stiffener
Part number
100T144034
Condition
Corroded
Location
Zone 100
Part time
61,332 hours, 27,015 cycles
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 THE PROCESS OF GAINING ACCESS TO THE FAIL-SAFE STRAP TRIM OUT AREA, IT WAS DETERMINED THAT THE INSTRUCTION IAW REV 1 OF THE SB WAS INSUFFICIENT TO REMOVE THE T-FITTINGS. MFG WAS CONTACTED VIA FIRST RESPONSE ON 6/9/09 AND THE SB ENGINEERING GROUP RESPONDED WITH THE INSTRUCTION REQUIRED VIA E-MAIL ON 6/10/09. THE SKIN STIFFENERS (T-FITTINGS) WERE REMOVED AND CORROSION WAS FOUND ON BOTH THE LT AND RT SKIN STIFFENERS (T-FITTINGS). IAW THE SENT INSTRUCTION, REV 2 OF THE SB, WHICH IS DUE OUT Q3 OF THIS YEAR, WILL INCLUDE THE DATA FOR T-FITTING REMOVAL AND INSTRUCTION TO CHANGE ANY CORRODED T-FITTINGS. CURRENTLY WE HAVE ORDERED AND RECEIVED BOTH OF THE T-FITTINGS FOR REPLACEMENT (PN 100T1440U3(LT) & 100T1440U4(RT). THE TRIM OUT PROCEDURE WAS COMPLIED WITH IAW THE SB 767-53A0100 FIGURE 15 ON 6/12/09. THE FINAL NDT TESTING WAS COMPLIED WITH ON 6/13/09 AND IT WAS VERIFIED THAT ALL CRACKS WERE REMOVED. CURRENTLY THE ACFT IS BEING RESTORED BACK TO THE USUAL CONDITION AND TERMINATING ACTION WILL BE COMPLETE IAW SB 767-53A0100. MFG DID INFORM AA767,LLC. THAT ALL TERMINATING ACTION IAW REV 1 OF THE SB WILL BE ACCEPTABLE AND THE UPCOMING REV 2 WILL HAVE NO FURTHER REQUIREMENTS.