Service difficulty report · Floorbeam · Boeing 7377H4

Difficulty date
June 22, 2021
Submitted
August 4, 2021
Operation
Air carrier
Aircraft
N940WN
Make and model
Boeing 7377H4
Aircraft serial
36900
Aircraft time
39,596 hours, 24,067 cycles
Part
Floorbeam
Condition
Corroded
Location
Bs 270
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

CORROSION FOUND ON LATERAL BEAM UPPER FLANGE AT BS 270; LBL 11 - RBL 11; WL 208 ; / REMOVED FASTENER ON DAMAGED AREA FOR ACCESS I.A.W SRM 51-40-02-0G-0; VERIFIED APPLICABILITY PER SRM 53-10-51-1A-1 PAR 4.C(2)(A) FIGURE 105/ALLOWABLE DAMAGE 1 DETAIL E; [03] REMOVED CORROSION ON LATERAL BEAM UPPER FWD FLANGE BS270 LBL11-RBL11 WL207.5;22'X1' AREA I.A.W SRM 51-10-02-0G-0 AND SRM 53-10-51-1A-1 PAR 4.C(2)(A) FIGURE 105/ALLOWABLE DAMAGE 1 DETAIL E; VERIFIED CORROSION REMOVED; ET INSPECTED BLEND AND HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23 AND 16; NO CRACKS NOTED.<BR>UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.092'<BR><BR>CAL ID ATS1465 N600<BR>CAL ID ATS2031 E650; [06] EDIT ACTION 5:<BR><BR>LOWEST THICKNESS IS ACTUALLY = 0.040'; CORROSION ON LATERAL BEAM UPPER FWD FLANGE BS270 LBL11-RBL11 WL207.5;22'X1' AREA FOUND TO BE OUT LIMITS ORIG. MAT. THICKNESS IS 0.050';REMAINING MAT. THICKNESS IS 0.040' I.A.W SRM 53-10-51-1A-1 PAR 4.C(2)(A) FIGURE 105/ALLOWABLE DAMAGE 1 DETAIL E AND SRM 53-10-51-0I-2 TABLE 2 ITEM 4 CONTACTED ENGINEERING FOR REPAIR INSTRUCTION; VERIFIED CORROSION OUT OF LIMITS; REFER TO EA 21-153-01911 SUMMARY REQUIREMENT; BARCODE: TTG8Q005V48S AND MULTI EFFECTIVITY EA M-21-153-00277; BARCODE: TTG8Q005PK28.; ACCOMPLISHED REPAIR PER EA 21-153-01911/TTG8Q005V48S<BR>AND EA 21-153-01911-WIP1/TTG8Q005QZ1F

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