Service difficulty report · Floorbeam · Boeing 7377H4

Difficulty date
June 3, 2021
Submitted
July 19, 2021
Operation
Air carrier
Aircraft
N489WN
Make and model
Boeing 7377H4
Aircraft serial
33855
Aircraft time
54,253 hours, 32,244 cycles
Part
Floorbeam
Condition
Corroded
Location
Bs 270
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

CORROSION BS 270 FLOOR BEAM UPPER FLANGE APPROX. BS 270; LBL 9; WL 207.5 ; / [01] UPDATED MEASUREMENT TABLE; [02] REMOVED DAMAGE ON BS270 FLOOR BEAM UPPER FLANGE FROM LBL4-LBL9 WL207.5;5'X1' AREA I.A.W SRM 51-10-02-0G-0 AND SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 FIG.104 GROUP 3 PAR 4.C(2) FIG105 DETAIL C;E; [03] CORROSION ON BS270 FLOOR BEAM UPPER FLANGE FROM LBL4-LBL9 WL207.5;5'X1' ORIGINAL MATERIAL THICKNESS IS 0.050' REMAINING MATERIAL THICKNESS IS 0.030'AREA FOUND TO BE OUT LIMITS I.A.W SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 FIG.104 GROUP 3 PAR 4.C(2) FIG105 DETAIL C;E; [04] VERIFIED OUT OF LIMITS DUE TO DEPTH OF DAMAGE REMOVAL PER SRM 53-10-51-1A-1; [05] UPDATED TTG8Q005FP4A.; [06] UT THICKNESS TESTED BLENDED AREA ON LATERAL INTERCOSTAL PER 737NDT PART 4 51-00-00 PROCEDURE 2. LOWEST REMAINING THICKNESS IS .044' CAL ID ATS2341 S/N 190848104.; [07] COMPLETED STEPS 7; 8 AND 9 OF TTG8Q005FP4A; [08] COMPLETED STEP 6 OF TTG8Q005FP4A; [09] ADDED TSR MEASUREMENT; [10] VERIFIED; [11] REPAIRED DAMAGE ON BS 270 FLOOR BEAM UPPER FLANGE APPROX. BS 270; LBL 9; WL 207.5 PER EA M-21-153-00277.; [12] VERIFIED REPAIRED DAMAGE ON BS 270 FLOOR BEAM UPPER FLANGE APPROX. BS 270; LBL 9; WL 207.5 PER EA M-21-153-00277.; [13] COMPLETED

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