Service difficulty report · Stiffener · Boeing 7377H4

Difficulty date
July 28, 2021
Submitted
September 14, 2021
Operation
Air carrier
Aircraft
N491WN
Make and model
Boeing 7377H4
Aircraft serial
33867
Aircraft time
53,758 hours, 31,898 cycles
Part
Stiffener
Condition
Cracked
Location
Horizontal Stab
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

RT HORIZ. STAB RIB ASSY 5 (STAB STA 129.50) 2ND VERT STIFFENER IS CRACKED. ; / [01] CUT AND REMOVED CRACK DAMAGE FROM VERTICAL STIFFENER AND WEB IAW SRM 55-10-09-2R-4 ITEM 4.B.; [02] VERIFIED DAMAGE WAS REMOVED FROM R/H HORIZ. STAB. RIB ASSY. 5 (2ND VERTICAL STIFFENER) AND INSPECTED PER SRM 55-10-09-2R-4 PARA. 4.E. NO FURTHER DAMAGE FOUND.; [03] REQUEST HFEC INSPECTION OF CUT EDGES OF STIFFENER AND WEB. REQUEST HFEC INSPECTION OF ALL EXISTING FASTENER HOLES WITHIN REPAIR AREA IAW SRM 55-10-09-2R-4 ITEM 4.C & D.; [04] HFEC INSPECTED OPEN HOLES AND CUTOUT IN REPAIR AREA PER 737 NDT PT 6; 51-00-00 PROC 16 AND 23. NO DEFECTS NOTED; [05] FABRICATED REPAIR PARTS; T-SECTION 60-5872#7075T76511 0.063' THICK LOT # 1430775-2; ANGLE BAC1490-2793#7075T62 0.063' THICK LOT # 1461745-1 AND 2.E.A SHIMS 7075T6#0.016' THICK IAW SRM 55-10-09-2R-4 STEP 4.F-J.; [08] APPLIED BMS 10-11 PRIMER TO REPAIR PARTS; BARE SURFACES AND EDGES OF THE RIB IAW SRM 55-10-09-2R-4 ITEM 4.L.OK TO INSTALL.; [09] VERIFIED APPLICATION OF PRIMER PER SRM 55-10-09-2R-4 STEP 4.L. OK TO INSTALL REPAIR PARTS; [10] CALIBRATED EQUIPMENT USED ID# ATS729; S/N N500X106291205. ID# ATS1411; S/N MM12030Z012384; [11] INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4 STEP 4.M-P.; [15] REMOVED CRACK DAMAGE RIGHT HORIZONTAL STABILIZER RIB AT STA 129.50 2ND VERTICAL STIFFENER AND INSTALLED REPAIR IAW SRM 55-10-09-2R-4.

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