N258WN

Service difficulty reports · 285

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N258WN' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWAA2024061498230Frame · worn#2 ENGINE STRUT FORWARD FAIRING FRAME HAS WORN AREA (COMMON TO THUMBNAIL UPPER AFT LATCH)<[01] VERIFIED STEP 5 COMPLETE.;[02] VERIFIED STEPS 6 COMPLETE; STEP 7 IN PARTIAL.;[03] VERIFIED STEP 7 COMPLETE AND MEASUREMENT FIELD.;[04] VERIFIED RII STEP COMPLETE.;[0May 19, 2024 · N258WN · Boeing 7377H4 · Nacelle/Pylon, Frame/Spar/RibSDR SWAA2024061487783Rub Strip · debonded#1 ENGINE PYLON UPPER WEB PANEL CUT OUT RUB STRIP DISBONDED (COMMON TO PANEL 433AT)<[01] UPDATED MEASUREMENTS.;[02] REMOVED AND REINSTALLED #1 ENGINE PANEL 433AT CUT OUT RUB STRIP PER AMM 51-51-00-340-803.;[03] VERIFIED CORRECTIVE ACTION ITEMS 1-2; CARD COMPLEMay 19, 2024 · N258WN · Boeing 7377H4 · Nacelle/Pylon, Main FrameSDR SWAA2024061487788Rub Strip · debonded#1 ENGINE PYLON UPPER WEB PANEL CUT OUT RUB STRIP DISBONDED (COMMON TO PANEL 433BT)<[01] UPDATED MEASUREMENTS.;[02] REMOVED AND REINSTALLED #1 ENGINE PANEL 433BT CUT OUT RUB STRIP PER AMM 51-51-00-340-803.;[03] VERIFIED CORRECTIVE ACTION ITEMS 1-2; CARD COMPLEMay 19, 2024 · N258WN · Boeing 7377H4 · Nacelle/Pylon, Main FrameSDR SWAA2024061486971Angle · crackedCRACKED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS918 RBL10 WL172.<[01] REMOVED AND REPLACED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS918 RBL10 WL172.IAW SRM 51-40-05 AND DWG 147A7221.;[02] VERIFIED CORRECTIVE ACTION 1.May 17, 2024 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061486976Shield · corrodedCORROSION ON FWD SHIELD AT ACB BS767 - BS787 RBL21 WL157.<[01] REMOVED AND REPLACED ACB R/H FLOOR TO SIDEWALL SUPPORT ANGLE BS 727 TO BS 767; RBL21; WL 157; IAW SRM 51-40-02-0G-0 AND <BR>DWG#146A7500 REV-A;[02] REMOVED AND REPLACED ACB FWD SHIELD IAW SRM 51-40May 17, 2024 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061486978Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727D+14; BS727E+14 - BS767 RBL21 WL156. MARKED<[01] REMOVED AND REPLACED ACB FWD SHIELD IAW SRM 51-40-02-0G-0 AND DWG#146A0081;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS.;[03] REMOVED AND REPLACED ACB R/May 17, 2024 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061486982Cargo Track · corrodedCORROSION ON TRACK AT ACB BS767+6 RBL13 WL157. MARKED<[01] FAULT WAS RESOLVED ON ANOTHER FAULT<BR>ASSY REPLACED IN TTG8Q00TE3PT;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.May 17, 2024 · N258WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024061486983Attach Angle · corrodedCORROSION ON ATTACH CLIP AT ACB BS727D+4 RBL7 WL151.<[01] REMOVED AND INSTALLED ATTACH CLIP AT ACB BS727D+4 RBL7 WL151.IAW SRM 51-40-02 AND DWG 146A7730May 17, 2024 · N258WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024061486984Attach Angle · corrodedCORROSION ON ATTACH CLIP AT ACB BS727D RBL7 WL151.<[01] REMOVED AND REPLACED ATTACH CLIP LOCATED AT ACB BS 727D; RBL 7 WL 151 IAW B-737-700 SRM 51-40-02 & DWG# 146A7810 REV: AMay 17, 2024 · N258WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024061486974Rub Strip · debonded#2 ENGINE PYLON UPPER WEB RUBSTRIP DISBONDED COMMON TO PANEL 443CT CUT OUT<[01] INSTALLED SERVICEABLE RUB STRIP ON #2 ENGINE PYLON PANEL 443CT CUT OUT PER AMM 51-51-00-340-803 STEPS 3. D. (2)(A). ADHESIVE APPLIED AT 15:05 UTC.;[02] INSTALLED SERVICEABLE RUB STMay 17, 2024 · N258WN · Boeing 7377H4 · Nacelle/Pylon, Main FrameSDR SWAA2024061386973Cargo Track · crackedCRACKED TRACK AT ACB BS727E RBL13 WL156.<[01] REMOVED AND REPLACED ACB TRACK ASSY<BR>BS727+4 TO BS887 RBL13 WL156<BR>IAW SRM 51-40-02 & DWG 146A7501;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.May 17, 2024 · N258WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024061485411Bracket · crackedLT WING T/E PANEL FWD MOUNTING BRACKET IS CRACKED (MARKED) PANEL 551FB<[01] REMOVED AND REPLACED LT WING T/E PANEL FWD MOUNTING BRACKET IAW SRM 51-40-02 AND AIPC 57-50-00-38.<BR>BRACKET PART NUMBER: 287A9152-23;[02] VERIFIED CORRECTIVE ACTION 1.May 14, 2024 · N258WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2024061385553Floor Panel · crackedAFT FLOOR PANEL 241ABF FWD O/B CORNER IS CRACKED.<[01] CRACKED FWD O/B CORNER ON AFT FLOOR PANEL 241ABF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1May 14, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061485223Vapor Barrier · crackedCRACK FOUND BETWEEN FASTENERS ON LH FWD VAPOR BARRIOR PICTURE ATTACHED LBL 40; BS 663; WL 160<[01] CRACK FOUND BETWEEN FASTENERS ON LH FWD VAPOR BARRIOR WERE REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED JOB COMPLETEMay 13, 2024 · N258WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2024061485387Stringer Clip · crackedCRACKED STR CLIP AT MID CABIN BS727E S-5L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT MID CABIN BS 727E S-5L IAW SRM 51-40-02 AND DWG 146A1112;[02] JOB COMPLETE.May 13, 2024 · N258WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024061485385Stringer Clip · crackedCRACKED STR CLIP AT MID CABIN BS727E S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT MID CABIN BS 727E S-6L IAW SRM 51-40-02 AND DWG 146A1112;[02] JOB COMPLETE.May 13, 2024 · N258WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024061485386Stringer Clip · crackedCRACKED STR CLIP AT MID CABIN BS727B S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT MID CABIN BS 727E S-6L IAW SRM 51-40-02 AND DWG 146A1102;[02] REMOVED AND REPLACED STRINGER CLIP AT MID CABIN BS 727B S-6L IAW SRM 51-40-02 AND DWG 146A1102;[03] JOB CMay 13, 2024 · N258WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024061485219Floor Support · corrodedCORROSION FOUND ON INTERCOASTAL FLOOR BEAM BETWEEN BS 294-312; BL 0; WL 208 UPDATE-CORROSION FOUND ON INTERCOASTAL FLOOR BEAM BETWEEN 294-312 LBL 11 WL 208.<[01] REMOVED AND REPLACED NEW INTERCOSTAL FROM BS294-BS312; LBL11 PER SRM 51-40-02 AND PER DWG#141A5600May 13, 2024 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061485004Vapor Barrier · crackedR/H VAPOR BARRIER COMPOSITE CRACKING AT FASTER ON THE FWD WALL AREA NEAR FASTENERS<[01] REPAIRED CRACK DAMAGE ON R/H COMPOSITE VAPOR BARRIER IAW SRM 51-70-04-2R-10.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] JOB COMPLETE.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2024061485005Angle · corrodedMULTIPLE CORROSION FOUND ON FWD ENTRY DOOR MOPSILL BS 312-344; LBL 64; WL 208<[01] REMOVED AND REPLACE ON FWD ENTRY DOOR MOPSILL ANGLE BETWEEN BS 312 - BS 346 LBL 64 WL 208 IAW B-737-700; IAW B-737-700 SRM 51-40-02 & DWG# 141A8110.;[02] VERIFIED COMPLETE;[03] May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061485006Bracket · corrodedCORRROSION FOUND ON ANGELED BRACKETS NEAR MOPSIL BS 344; LBL 65; WL 208<[01] REMOVED AND REPLACE TIEDOWN ASSY P/N 141A5220-4; LOT:1540667-1 LOCATED AT BS. 344.65 LBL.65 WL. 208 IAW SRM 51-40-02 AND DWG# 141A5220.;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CAMay 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061485008Attach Bracket · corrodedCORRROSION FOUND ON ANGELED BRACKET NEAR FED MOPSIL BS 312; LBL 65; WL 208<[01] REMOVED AND REPLACED TIEDOWN ASSY P/N 141A5220-2; LOT:1559507-1. LOCATED AT BS. 312.67 LBL.65 WL. 208 IAW SRM 51-40-02 AND DWG# 141A5220.;[02] VERIFIED CORRECTIVE ACTION STEP 1. TAMay 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024061384588Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS AN AREA OF PULLED STARNDS. (MARKED)<[01] 04 - REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEETS.;[02] VERIFIED CORRECTIVMay 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384593Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS AN AREA OF PULLED STARNDS. (MARKED)<[01] FLOOR PANEL 241ZF UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384589Floor Panel · pulledAFT FLOOR PANEL 241YF UPPER SKIN HAS AN AREA OF PULLED STARNDS. (MARKED)<[01] AFT FLOOR PANEL 241YF WITH UPPER SKIN HAS AN AREA OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB CO;MPLETE.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384594Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW FLOOR PANEL 241AAF HAS BEEN COMPLETED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384590Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] ARES OF PULLED STRANDS ON UPPER SKIN OF AFT FLOOR PANEL 241ABF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384595Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF AFT FLOOR PANEL 241ACF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384597Floor Panel · pulledAFT FLOOR PANEL 241AEF UPPER SKIN HAS AN AREA OF PULLED STRANDS.<[01] UPPER SKIN ON AFT FLOOR PANEL 241AEF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384596Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ADF AREAS OF PULLED STRANDS ON UPPER SURFACE WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384598Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242UF UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384591Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384601Floor Panel · pulledFWD FLOOR PANEL 221AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221AF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384602Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384603Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 221CF WERE REPAIRED IAW SRM 53-00-50-2R-6.;[02] VERIFIED CORRECTIVE ACTION #1May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384604Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384605Floor Panel · pulledFWD FLOOR PANEL 221GF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FLOOR PANEL 221GF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384606Floor Panel · pulledFWD FLOOR PANEL 221AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FAULT TTG8Q00T9SAV WILL BE RESOLVED ON FAULT TTG8Q00T9RB9.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384607Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384608Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384611Floor Panel · pulledFWD FLOOR PANEL 231BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 231BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.May 11, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384291Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] ATTACHED CURE SHEET.;[02] FLOOR PANEL 241AF WAS REPLACED BY FABRICATION IAW SRM 53-00-50-2R-0 AND BOEING DRAWING 144A5810 SHEET 126.;[03] VERIFIED CORRECTIVE ACTION #2May 10, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384284Floor Panel · pulledFLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231YF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1May 10, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384285Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] ATTHACED CURE SHEET;[02] FLOOR PANEL 241AF WAS REPLACED BY FABRICATION IAW SRM 53-00-50-2R-0 AND BOEING DRAWING 144A5810 SHEET 126.;[03] VERIFIED CORRECTIVE ACTION #2May 10, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384286Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1May 10, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384292Floor Panel · pulledFLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 241CF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-42A ITEM 55.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.May 10, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061384293Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241ADF WAS REPLACED BY FABRICATION USING BMS4-23 TYPE II LOT 1553922-1 AND ADHESIVE: BMS5-107 CLASS 1 TYPE 1 LOT AK3BA2380A/A; CURED ADHESIVE UNDER A HEAT LAMP; USING THERMOMETER CAL IDMay 10, 2024 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024061484281Strap · corrodedCORROSION ON TENSION STRAP AT AFT WET AREA BS1016+9 LBL3 WL208.<[01] REMOVED AND REPLACED THE TENSION STRAP P/N 147A5620U3 AT AFT WET AREA BS1016 LBL3 WL208 IAW SRM 51-40-02 AND DWG # 147A5600 REV B;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.May 9, 2024 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061484288Web · corrodedCORROSION ON 1016 WEB AT AFT WET AREA BS1016 LBL5 WL208.<[01] CORROSION REPAIR ON 1016 WEB AT AFT WET AREA BS 1016 LBL5 WL208 COMPLETED IAW EA 24-153-01371.;[02] VERIFIED CORRECTIVE ACTION #1May 9, 2024 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024061484289Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT WET AREA BS986 LBL43 WL208. MARKED<[01] ACCOMPLISHED REPAIR PER SRM 53-70-51-2R-6 REPAIR 6;[02] VERIFIED CORRECTIVE ACTION 1.May 9, 2024 · N258WN · Boeing 7377H4 · Fuselage Main, Floor Beam
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