Service difficulty report · Angle · Boeing 7377H4

Difficulty date
December 28, 2021
Submitted
April 26, 2022
Operation
Air carrier
Aircraft
N233LV
Make and model
Boeing 7377H4
Aircraft serial
32501
Aircraft time
53,746 hours, 31,891 cycles
Part
Angle
Condition
Cracked
Location
Center Wing
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

B.S. 663 LOWER COMPOSITE UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8; W.L. 164. ; / [01] REMOVED BS 663 LOWER COMPOSITE UPPER ATTACH ANGLE RBL8-RBL65 WL164 IAW SRM 51-40-02.; [02] VERIFIED CORRECTIVE ACTION 4.; [03] UPDATED MEASUREMENT TABLE; [04] RECIEVED;LOCATED;DRILLED AND APPLIED CHEMICAL CONVERSION COATING TO BS 663 LOWER COMPOSITE UPPER ATTACH ANGLE RBL6-RBL65 WL164 IAW SRM 51-40-05; DWG 111A1000 AND 111A1322; VERIFICATION OF FABRICATION AND HEAT TREATMENT IAW DWG 111A1322 AND BAC5602 MATERIAL USED 2024T42#0.063 CLAD LOT# 1419330-1.; [05] VERIFIED BS 663 LOWER COMPOSITE UPPER ATTACH ANGLE RBL6-RBL65 WL164 FABRICATED AND DRILLED IAW SRM 51-40-05; DWG 111A1000 AND DWG 111A1322. OKAY TO PRIME ANGLE.; [06] APPLIED PRIMER AND PAINT TO NEW UPPER ATTACH ANGLE PER DRAWING 111A1322; [07] VERIFIED CORRECTIVE ACTION STEP 6.; [08] OK TO INSTALL; [09] OK TO INSTALL; [10] INSTALLED FASTENERS ON HORIZONTAL FLANGE OF UPPER ATTACH ANGLE THRU FUEL CELL BS663 RBL 6-65 WL 164 IAW SRM 51-40-02; DWG 111A1000 AND 111A1322.; [11] CAP SEAL OF FASTENERS INSIDE OF FUEL CELL WILL BE DOCUMENTED ON CARD TTG8Q00A0UW9.; [12] VERIFIED CORRECTIVE ACTION STEP 10.; [13] FASTENERS COMMON TO VERTICAL FLANGE ON UPPER ATTACH ANGLE FROM RBL6 TO RBL65 WL 164 BS 663 WILL BE INSTALLED ON FAULT # TTG8Q00A130H; [14] VERIFIED CORRECTIVE ACTION 13.

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