Service difficulty report · Rib · Boeing 7377CT

Difficulty date
January 10, 2022
Submitted
January 31, 2022
Operation
Air carrier
Aircraft
N7881A
Make and model
Boeing 7377CT
Aircraft serial
35084
Aircraft time
44,806 hours, 23,070 cycles
Part
Rib
Condition
Cracked
Location
Horizontal Stab
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; STATION 120.30.; 4TH VERTICAL STIFFENER IS CRACKED. ; / REMOVED DAMAGE FROM RH HORIZONTAL STABILIZER INSPAR RIB STA. 120.30 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4 REPAIR-4; [04] VERIFIED CORRECTIVE ACTION 1-3;<BR><BR>APPLICABILITY AND DAMAGE REMOVAL.; [05] HFEC INSPECTED CUTOUT IN STIFFENER PER 737NDT PART 6 51-00-00 PROCEDURE 23. FOUND CRACK IN WEB AND MARKED IN RED INK. TOOL N600 ATS1465.;FABRICATED [1] T-SECTION MADE FROM 60-5872#7075-T76511 EXTRUSION ; AMS-QQ-A-200/15 ; LOT# 1476286-1 ; FABRICATED [2] ANGLE MADE FROM BAC1490-2793 # 7075T62 EXTRUSION LOT# 1474027-1 AND FABRICATED (2EA) [4] SHIMS MADE FROM 7075T6#0.020' LOT# 1472548-1 ; LOCATED AND DRILLED ALL REPAIR PARTS IAW SRM 55-10-09-2R-5 REPAIR-5; OK TO TREAT AND PRIME ALL REPAIR PARTS AND CUTOUT; [11] FABRICATED (3)FILLER 7075 T6 0.050' CLAD LOT# 1407842-2 APPLIED CHEMICAL CONVERSION COATING IAW SRM 55-10-09-2R-5 ] APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO REPAIR PARTS AND COMMON AREA IAW SRM 55-10-09-2R-5 OK TO INSTALL.; [15] VERIFIED SRM APPLICABILITY STEP 8 FOR FLANGE REPAIR AND STEP 14. OK TO INSTALL REPAIR PARTS; [16] INSTALLED REPAIR PARTS PER SRM 55-10-09-2R-5; [17] RII- VERIFIED REPAIR OF THE R/H HORZ. INSPAR RIB ON 4TH STIFFENER PER SRM 55-10-09-2R-5.; [18] VERIFIED RIB REPAIR IS COMPLETE PER SRM 55-10-09-2R-5. RIB WILL BE REINSTALLED ON TTG8Q00A83QY

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