Service difficulty report · Fitting · Boeing 7378H4

Difficulty date
April 9, 2024
Submitted
May 2, 2024
Operation
Air carrier
Aircraft
N8685B
Make and model
Boeing 7378H4
Aircraft serial
36723
Aircraft time
26,629 hours, 13,050 cycles
Part
Fitting
Part number
UNKNOWN
Condition
Corroded
Location
Aft Galley
Stage of operation
IN
How discovered
9
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

AFT GALLEY LAV E O/B AND AFT TIE DOWN FITTING POSSIBLE CORROSION UNDER FITTING. (MARKED)<BLENDED CORROSION PER SRM 51-10-02. MAX MATERIAL REMOVED 0.075?. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1;REMOVED DAMAGED SECTION OF FLOOR BEAM UPPER FLANGE PER SRM 53-70-51-2R-5; ALTERNATIVE 2 FLAP PEENED THE CUT EDGE OF 947 FLOOR BEAM PER SRM 53-70-51-2R-5 AND SOPM 20-10-03.;[05] INSPECTED AS REQUIRED. CORRECTIVE ACTION #4;[06] TRIMMED; LOCATED; AND FLAP PEENED 947 FLOOR BEAM T CHORD REPAIR SECTION PER SRM 53-70-51-2R-5 AND SOPM 20-10-03 FABRICATED (-2) SPLICE REPAIR ANGLES; (-3) SPLICE REPAIR STRAPS; AND (-4) FILLERS PER SRM 53-70-51-2R-5.;[0914-APR-2024 20:57 UTC FABRICATED (-2) SPLICE REPAIR ANGLES; (-3) SPLICE REPAIR STRAPS; AND (-4) FILLERS PER SRM 53-70-51-2R-5.TREATED AND PRIMED T CHORD REPAIR SECTION AND (-2) SPLICE REPAIR ANGLES; (-3) SPLICE REPAIR STRAPS; AND (-4) FILLERS ALL PER SRM 53-70-51-2R-5.;[12] DEBURRED ALL FASTENER HOLES; TREATED AND PRIMED ON REPAIR AREA OF AIR CRAFT ALL PER SRM 53-70-51-2R-5.RII-INSTALLED REPAIR ANGLES; STRAPS; AND T-CHORD BETWEEN BL 0? TO RBL 43? AND BETWEEN RBL 56? TO RBL 60? PER SRM 53-70-51-2R; ALTERNATIVE 2.;[16] RII: VERIFIED CORRECTIVE ACTION #15; INSTALLED REMAINING FASTENERS IN T-CHORD BETWEEN RBL 43 AND RBL 56. VERIFIED T-CHORD AND REPAIR PARTS ARE INSTALLED COMPLETE PER SRM 53-70-51-2R; ALTERNATIVE 2;[18] RII: C/W INSPECTION OF C/A #17;CLOSED PARTS SECTION;[20] C/W INSPECTION;[21] C/W INSPECTION

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