N244WN

Service difficulty reports · 297

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 = 'N244WN' 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 SWAA2024082729357Mount · brokenAFT ENTRY DOOR; AFT SLIDE MOUNT POINT BRACKET BROKEN- PIC ATTACHED<[01] R&R AFT ENTRY DOOR; AFT SLIDE MOUNT POINT BRACKET/ISOLATOR IAW SRM 51-40-02.;[02] MICHAEL THOMPSON (TECHNICIAN); 23-AUG-2024 04:26 UTC<BR>R&R AFT ENTRY DOOR; AFT SLIDE MOUNT POINT BRACKET/Aug 23, 2024 · N244WN · Boeing 7377H4 · Escape SlideSDR SWAA2024082729356Isolator · crackedPASSENGER CABIN FWD GALLEY SERVICE DOO ESCAPE SLIDE BONNET AFT ATTACH POINT ISOLATOR CRACKED<[01] R&R PASSENGER CABIN FWD GALLEY SERVICE DOOR ESCAPE SLIDE BONNET AFT ATTACH POINT ISOLATOR IAW SRM 51-40-02.;[02] INSPECTION C/W R&R PASSENGER CABIN FWD GALLEY SERAug 23, 2024 · N244WN · Boeing 7377H4 · Escape SlideSDR SWAA2024061300818Slide · misinstalledFWD SERVICE DOOR SLIDE NOT PROPERLY SECURED<[01] R/R FWD SVC ESCAPE SLIDE IAW MT 725-61-06-FS AND AMM 25-66-01.Jun 12, 2024 · N244WN · Boeing 7377H4 · Escape SlideSDR SWAA2024061300473Slide · unpackedFWD SERVICE DOOR SLIDE CAME APART<[01] REPACKED & RESECURED FWD SERVICE DOOR SLIDE REF MT1725-61-06 AND AMM 25-66-01.Jun 11, 2024 · N244WN · Boeing 7377H4 · Escape SlideSDR SWAA2024061300804Slide · dislodgedFWD SERVICE DOOR EMER EXIT SLIDE FELL OUT OF CONTAINER AFTER DOOR WAS CLOSED FOR PUSHBACK<[01] RESECURED FWD SERV DOOR SLIDE IAW MT 725-61-06 AND IAW AMM 25-66-01. A/C OK FOR SERVICE.Jun 11, 2024 · N244WN · Boeing 7377H4 · Escape SlideSDR SWAA2024052185596Light · inoperativeEMERGENCY EXIT SLIDE LIGHT OUTSIDE AFT ENTRY DOOR INOP<[01] REPLACED LAMP FOR AFT ENTRY DOOR SLIDE LIGHT AND PERFORMED GOOD TEST PER AMM 33-51-04-960-802.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.May 15, 2024 · N244WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024052185197Battery Pack · inoperativeMULTIPLE EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK 1669 INOP<[01] CORRECTED IMPROPERLY CONNECTED LIGHT ASSEMBLIES; REPLACED INOP FUSES IN M1669 BATTERY CHARGER AND PERFORMED GOOD INSTALLATION TEST OF ALL INOP EMERGENCY EXIT LIGHTS AS DOCUMENTED ON ATTACHEDMay 13, 2024 · N244WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024052181098Sidewall Support · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AROUND FASTENER HOLES BS 727 - 767 RBL 25 WL 156<[01] REMOVED AND REPLACED AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 767 RBL 25 IAW SRM 51-40-02 AND DWG 146A7500May 1, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052179654Baffle · crackedFWD CARGO BAY BAFFLE CRACKED AT BS 500+10 LBL 24; WL 156 LOCATION CORRECTION: BAFFLE IS LOCATED AT BS 500B+10 LBL 24 WL 156<[01] REMOVED AND REPLACED FCB BAFFLE FROM BS500 B TO BS 500 C;LBL24;WL156.IAW SRM 51-40-02 AND DWG#143A7505.;[02] VERIFIED CORRECTIVE ACApr 26, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052179408Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS500+5; BS500+15 LBL24 WL156. MARKED<[01] REMOVED AND REPLACED LH SIDEWALL SUPPORT FROM BS 396 TO BS 500D; LBL 24; WL 156; IAW DWG#143A7500 AND SRM 51-40-02.;[02] VERIFIED CORRECTIVE ACTION 1; DWG 143A7500 IS REV.Apr 25, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052179409Shield · canningCORROSION ON AFT SHIELD AT FCB BS500 - BS500A RBL24 WL156. MARKED<[01] REMOVED AND REPLACED AFT SHIELD AT FCB LOCATED BETWEEN BS 492.4 - BS 500A RBL 24 WL 156 IAW SRM 51-40-02 AND DWG# 143A0080.;[02] VERIFIED CORRECTIVE ACTION 1.Apr 25, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052179410Cargo Track · corrodedCORROSION ON TRACK TIEDOWNS AT FCB BS400; BS436; BS496; BS500 LBL18 WL156.<[01] REMOVED AND REPLACED TRACK-TIEDOWN LBL 18 BS 396 TO BS 500D I.A.W SRM 53-00-53-1A-2 PARA 4B (2) FIG 103 DETAIL G; SRM 51-10-02-0G PAR 9C; SRM 51-40-02-0G-0 AND DWG 143A7500.;[02] VApr 25, 2024 · N244WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024052178146Intercostal · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS284 BL0 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL BS277-BS294 BL0<BR>IAW SRM 51-40-02 & DWG 141A5400;[02] VERIFIED CORRECTIVE ACTION 1Apr 22, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052178140Intercostal · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS350 BL0 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL P/N:141A5410-23 IAW SRM 51-10-02-0G. STEP 9; SRM 51-40-02-0G-0 AND DWG 141A5400.;[02] VERIFIED CORRECTIVE ACTION #1Apr 22, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052178147Intercostal · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS353 LBL11 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL P/N:141A5410-148 LOT:1561882-1 I.A.W SRM 51-10-02-0G. STEP 9; SRM 51-40-02-0G-0 AND DWG 141A5400.;[02] VERIFIED CORRECTIVE ACTION #1Apr 22, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052178148Intercostal · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS353 RBL11 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL BS344-B360 RBL11<BR>IAW SRM 51-40-02 & DWG 141A5400;[02] VERIFIED CORRECTIVE ACTION 1Apr 22, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052178141Attach Angle · crackedCRACKED ATTACH ANGLE JUST FWD OF FSD BS294 RBL54 WL208.<[01] REMOVED AND REPLACED ATTACH ANGLE JUST FWD OF FSD BS294 RBL54 WL208 IAW SRM 51-40-02 AND DWG # 141A8312 REV B;[02] VERIFIED CORRECTIVE ACTION 1.Apr 22, 2024 · N244WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024052178145Support Angle · corrodedCORROSION ON FED THRESHOLD SUPPORT ANGLE BS318 LBL62 WL208.<[01] REMOVED AND REPLACED SUPPORT ANGLE BS318 LBL62 WL208 I.A.W SRM 51-40-02. AND DWG 141A8112;[02] REMOVED AND REPLACED SUPPORT ANGLE BS318 LBL62 WL208 I.A.W SRM 51-40-02. AND DWG 141A8110;[03] UPDATApr 22, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052178144Support Angle · corrodedCORROSION ON FED THRESHOLD SUPPORT ANGLE BS318 - BS342 LBL60 WL208.<[01] REMOVED AND REPLACED FED THRESHOLD SUPPORT ANGLE LBL 60 WL 208 IAW SRM 51-40-02 AND DWG 141A8110.;[02] UPDATED CORRECTIVE ACTION #1<BR>REMOVED AND REPLACED FED THRESHOLD SUPPORT ANGLE LBLApr 22, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052186629Skin · misrepairedREPAIR NEEDS TO BE REMOVED AND REPLACED BETWEEN STA 480-500; AT S-5R REF: 23-153-01145-TLD.<[01] REPAIR AT STA 480-500; S-5R WAS REMOVED AND REPLACED PER EA 24-143-01103;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.;[03] REPAIR AT STA 480-500; S-5R WAS REMOVED AND Apr 22, 2024 · N244WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2024052177481Sidewall Support · corrodedCORROSION ON AFT CARGO LH SECTION 1 FLOOR TO SIDEWALL SUPPORT BS 727-752; LBL 21; WL 160.<[01] THIS TASK CARD WILL BE ACCOMPLISHED WITH CUSTOMER CARD # TTG8Q00SVYRA; REQUEST FINAL BUY OFF.;[02] VERIFIED CORRECTIVE ACTION 1;[03] COMPLETEApr 20, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052177484Sidewall Support · corrodedCORROSION ON AFT CARGO LH SECTION 2 FLOOR TO SIDEWALL SUPPORT BS 752-847; LBL 21; WL 160.<[01] REMOVED AND REPLACED AT ACB; FLOOR TO SIDEWALL SUPPORT P/N 146A7502-27 LOCATED BETWEEN BS 727 TO BS 847 LBL 21 WL 160 IAW B-737-700 SRM 51-40-02 DWG# 146A7500 REV: AApr 20, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052177556Floor Panel · corrodedFLOOR PANEL 241ABF HAS MULTIPLES INSERTS CORRODED AND THE HONEYCOMB AT THE AFT EDGE DAMAGED. (MARKED)<[01] FAULT TTG8Q00SW3WT WILL BE RESOLVED ON FAULT TTG8Q00SUQQW.;[02] REJECTED AMT UPDATE FOR DOCUMENTATION ONLY; HONEYCOMB DAMAGE WILL NOT BE RESOLVED ON INSEApr 20, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052177557Stiffener · corrodedAFT WET AREA; STIFFENER LOCATED AT LBL 45; WL 208 BETWEEN STA967 AND 947.5 HAS 3 EA DRILLS WITH CORROSION. (MARKED)<[01] REMOVED AND REPLACED AFT WET AREA STIFFENER P/N 140A9872-7; LOT#1561985-1 IAW SRM 51-40-02-0G-0 AND DWG#140A9870 REV-A;[02] VERIFIED CORRECApr 20, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052177558Channel · corrodedASD MOPSILL HAS MULTIPLES SPOTS OF CORROSION BETWEEN THE BS947.5 AND BS986.5+10'. (MARKED)<[01] REMOVED AND REPLACED ASD MOPSILL IAW SRM 51-40-02 AND DWG 147A0000 ID: 0045 REV: AApr 20, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052177560Stiffener · corrodedAFT WET AREA ; STIFFENER LOCATED BTWN BS986.5 AND BS967; RBL17' WL 208 HAS CORROSION AROUND DRILL UNDER THE UPPER LEFT FLANGE. (MARKED)<[01] REMOVED AND REPLACED AFT WET AREA STIFFENER P/N 140A9872-10; LOT#1562050-1; AT BS-967 -BS-986; RBL-17; WL 208 IAW SRM 5Apr 20, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052177561Strap · corrodedAFT WET AREA; STRAP LOCATED AT RBL3 HAS 2 EA SPOTS OF CORROSION BETWEEN BS1016 AND BS1040; WL208. (MARKED)<[01] REMOVED AND REPLACED STRAP LOCATED AT RBL3 BETWEEN BS1016 AND BS1040; WL208. I.A.W SRM 51-40-02-0G-0; SRM 51-10-02 PARG. 9.C. AND DWG 147A5730.;[02]Apr 20, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052177562Strap · corrodedAFT WET AREA; STRAP LOCATED AT LBL3 HAS ONE SPOT OF CORROSION BETWEEN BS1016 AND BS1040; WL208. (MARKED)<[01] REMOVED AND REPLACED STRAP LOCATED AT LBL3 BETWEEN BS1016 AND BS1040; WL208 I.A.W SRM 51-40-02-0G-0; SRM 51-10-02 PARG. 9.C. AND DWG 147A5600.;[02] VEApr 20, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052176860Floor Panel · delaminatedFLOORBOARD 242UF IS DELAMED AT AFT EDGE NEXT TO AFT DRAIN.<[01] FLOORBOARD 242UF IS DELAMINATED AT AFT EDGE NEXT TO AFT DRAIN WAS REPAIRED IAW SRM 53-00-50-2R-6.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 19, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052176861Floor Panel · delaminatedFLOORBOARD 241ABF; IS DELAMINATED AT AFT EDGE; AFT OF AFT DRAIN.<[01] FLOORBOARD 241ABF DELAMINATED AT AFT EDGE; AFT OF AFT DRAIN WILL BE REPAIRED ON FAULT TTG8Q00SW3WT.;[02] COMPLETE.Apr 19, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052177040Floor Panel · delaminatedFWD FLOOR PANEL 221DF HAS TOP SURFACE DELAMINATION<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 221DF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 19, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052177041Floor Panel · delaminatedFWD FLOOR PANEL 222BF HAS TOP SURFACE DELAMINATION<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 222BF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 19, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052177042Floor Panel · delaminatedFLOOR PANEL 222DF HAS TOP SURFACE DELAMINATION<[01] FLOOR PANEL 222DF HAS TOP SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 19, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052177050Floor Panel · delaminatedFWD FLOOR PANEL 222CF HAS TOP SURFACE DELAMINATION<[01] FWD FLOOR PANEL 222CF HAS TOP SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] RII REQUIREMENTS COMPLETED.;[03] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.Apr 19, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052177051Floor Panel · delaminatedFWD FLOOR PANEL 221EF HAS TOP SURFACE DELAMINATION<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 221EF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 19, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052177044Floor Panel · delaminatedFLOOR PANEL 232BF HAS TOP SURFACE DELAMINATION<[01] FLOOR PANEL 232BF HAS TOP SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 19, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052177308Floorbeam · damagedOBLONG HOLE TOP OF FLOOR BEAM STA. 278 RBL. 7 WL 208.1<[01] ALL REPAIRS COMPLETED IAW EA 24-153-01182.;[02] VERIFIED CORRECTIVE ACTION #1Apr 19, 2024 · N244WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024052177046Floorbeam · corrodedCORROSION ON BS 986 FLOOR BEAM FWD FASTENER HOLE AT RBL 43 WL 208<[01] REPAIRED FLOOR BEAM FWD FASTENER HOLE AT BS986 RBL43 WL208; IAW SRM 53-70-51-2R-6 REPAIR 6Apr 19, 2024 · N244WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024052177047Floorbeam · corrodedCORROSION ON BS 986 FLOOR BEAM FWD FASTENER HOLE AT LBL 43 WL 208<[01] REMOVED AND REPLACED BS 986 FLOOR BEAM LBL 1- LBL 51; WL-208 I.A.W SRM 51-40-02-0G-0 AND SRM 53-70-51-2R-4 REPAIR-4;[02] JOB COMPLETE.Apr 19, 2024 · N244WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024052177311Channel · corrodedCORROSION ON MOP SEAL STA 312- 305 LBL 63 WL 208.1<[01] REMOVED AND REPLACED FED MOP SILL IAW SRM 51-40-02 AND DWG 141A8110.;[02] VERIFIED CORRECTIVE ACTION 1.Apr 19, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052176858Stiffener · crackedLEFT HORIZONTAL STAB RIB 5; #3 STIFFENER IS CRACKED AT LOWER RADIUS.<[01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 129.50 RIB 3RD VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4.;[02] VERIFIED CORRECTIVE ACTION 1Apr 19, 2024 · N244WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024052177310Channel · corrodedCORROSION BELOW FED THRESHOLD ON MOP SILL STA 312 - 328 LBL 63 WL 208.1<[01] THIS CARD WILL BE ACCOMPLISHED ON CUSTOMER CARD NBR: TTG8Q00SVNZX;[02] VERIFIED CORRECTIVE ACTION 1Apr 19, 2024 · N244WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052176849Floor Panel · delaminatedFLOOR PANEL 241UF HAS TOP SURFACE DELAMINATION<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 241UF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-22 ITEM 168.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 18, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052176850Floor Panel · delaminatedFLOOR PANEL 241EF HAS TOP SURFACE DELAMINATION<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241EF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTIONS. CARD COMPLETEApr 18, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052176851Floor Panel · delaminatedFLOOR PANEL 241AF HAS TOP SURFACE DELAMINATION<[01] FLOOR PANEL 241AF WITH TOP SURFACE DELAMINATION 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 #1Apr 18, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052176845Floor Panel · delaminatedFLOOR PANEL 232FF HAS TOP SURFACE DELAMINATION<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 232FF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 18, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052176839Floor Panel · delaminatedAFT FLOOR PANEL 241ACF HAS TOP SURFACE DELAMINATION<[01] AFT PANEL 241ACF TOP SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1Apr 18, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052176834Floor Panel · delaminatedAFT FLOOR PANEL 242UF HAS TOP SURFACE DELAMINATION<[01] AFT FLOOR PANEL 242UF HAS TOP SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 18, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052176841Floor Panel · delaminatedAFT FLOOR PANEL 242TF HAS TOP SURFACE DELAMINATION<[01] TOP SURFACE DELAMINATION ON AFT FLOOR PANEL 242TF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1Apr 18, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052176837Floor Panel · delaminatedAFT FLOOR PANEL 242SF HAS TOP SURFACE DELAMINATION<[01] AFT FLOOR PANEL 242SF TOP SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1Apr 18, 2024 · N244WN · Boeing 7377H4 · Fuselage Floor Panel
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