N257WN

Service difficulty reports · 305

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 = 'N257WN' 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 SWAA2024081309936Shield · corrodedCORROSION ON FWD CARGO DOOR FWD SHIELD BS 440-3; RBL 21; WL 156<[01] REMOVED AND REPLACED SHIED AT BS 420 TO BS 440 RBL 21 IAW SRM 51-40-02 AND DWG 143A0080 REV:;[02] REMOVED AND REPLACED SHIED AT BS 420 TO BS 440 RBL 21 IAW SRM 51-40-02 AND DWG 143A0080 REV:-Jul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309768Bracket · crackedRH 663 VAPOR BARRIER BRACKET (P:N 276A9183-2) CRACKED.<[01] REMOVED AND REPLACED BRACKET AT BS 663 FWD SIDE RB 45 TO RBL 54 PER SRM 51-40-02-0G-0 AND DWG 111A1001;[02] REMOVED AND REPLACED BRACKET AT BS 663 FWD SIDE RB 45 TO RBL 54 PER SRM 51-40-02-0G-0 AND DWJul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024080909924Support · corrodedMULTIPLE CORROSION ON AFT CARGO BAY LH FLOOR TO SIDEWALL SUPPORT SECTION 5;787+10 TO 847+13; RBL 21; WL 156 . MULTIPLE CORROSION ON AFT CARGO BAY LH FLOOR TO SIDEWALL SUPPORT SECTION 5787+10 TO 847 RBL 21 WL 156<[01] REMOVED CORROSION DAMAGE IAW SRM 51-10-02<BJul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024080909932Support · corrodedMULTIPLE CORROSION ON LH FWD CARGO FLOOR TO SIDEWALL SUPPORT SEC 1; BS 473-469; LBL 21; WL 156.<[01] REMOVED AND REPLACED SIDEWALL SUPPORT AT FCB BETWEEN BS 396 TO BS 500D ;LBL 21 ;WL 156 PER SRM 51-40-02 ; SRM 53-00-53-2R-6 AND DWG:143A7500 ID:0058 REV:-;[02]Jul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024080909760Stiffener · crackedRIGHT HORIZONTAL STAB RIB #4 STIFFENER 3 ARE CRACKED IN THE LOWER RADIUS.<[01] REPAIRED R/ HOR. STAB. RIB #4; STIFFENER 3 IAW SRM 55-10-09-2R-4 REPAIR 4; FIG. 202; DETAIL A AND SRM 51-40-05-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION ITEMS AND STEPS; CARD COMPLETJul 6, 2024 · N257WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024080909757Shield · corrodedCORROSION AFT CARGO BAY AFT DOOR SHIELD BS 847+3; RBL 21; WL 156.<[01] UPON FURTHER INVESTIGATION; FOUND TO BE NO ALLOWABLE DAMAGE PER SRM. REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION 1;[03] INSTALLED ACB AFT NEW SHIELD BETWEEN Jul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024080909761Shield · corrodedCORROSION AFT CARGO BAY FWD DOOR SHIELD BS 777; RBL 21; WL 156 CORROSION AFT CARGO BAY FWD DOOR SHIELD BS 777 TO 781 RBL 21 WL 156<[01] UPON FURTHER INVESTIGATION; FOUND TO BE NO ALLOWABLE DAMAGE PER SRM. REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIJul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024080909763Support · corrodedMULTIPLE CORROSION ON AFT CARGO BAY RH FLOOR TO SIDEWALL SUPPORT SECTION 1; BS 727-727C; RBL 21; WL 156<[01] THIS TASK ACCOMPLISHED ON TTG8Q00UDXAG;[02] VERIFIED CORRECTIVE ACTION ITEMS AND STEPS; CARD COMPLETE.Jul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024080909923Support · corrodedMULTIPLE CORROSION ON AFT CARGO BAY LH FLOOR TO SIDEWALL SUPPORT SECTION A BS 727D-727E+7; RBL 21; WL 156 MULTIPLE CORROSION ON AFT CARGO BAY LH FLOOR TO SIDEWALL SUPPORT SECTION 2 BS 727D-727E+7 RBL 21 WL 156 [TTG8Q00UDXBP]<[01] THIS TASK ACCOMPLISHED ON TTG8Jul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024080909766Support · corrodedMULTIPLE CORROSION ON AFT CARGO BAY LH FLOOR TO SIDEWALL SUPPORT SECTION 3;727E+7 TO 747+13; RBL 21; WL 156<[01] THIS TASK ACCOMPLISHED ON TTG8Q00UDXCA;[02] VERIFIED CORRECTIVE ACTION ITEMS AND STEPS; CARD COMPLETE.Jul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309590Shield · corrodedAFT CARGO DOOR AFT SHIELD HAS 2 CORRODED NUTPLATE HOLES AT STA 847 +2 RBL 28 WL 150 MARKED<[01] UPON FURTHER INVESTIGATION; FOUND TO BE NO ALLOWABLE DAMAGE PER SRM. REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0<BR><BR>ACB AFT SHIELD WILL BE REPLACED ON CUSTOMER Jul 5, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309591Web · corrodedAFT CARGO DOOR SCUFF PLATE HAS NUMEROUS AREAS OF CORROSION FROM STA 787 + 7 - 847 RBL 33 WL 150<[01] CORRECTION FAULT TITLE S/B AFT CARGO DOOR SUB THRESHOLD WEB;[02] EVALUATED CORROSION AT AFT CARGO BAY THRESHOLD BS 787+7 TO 847; RBL 33; WL 150. L=1.5' W=0.5' Jul 5, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309592Doubler · crackedBS663 RH VAPOR BARRIER DOUBLER CRACKED BS663 RH VAPOR BARRIER DOUBLER RBL6-RBL31 CRACKED<[01] FABRICATED DOUBLER IAW DWG 111A1511 AND SRM 51-30-01-0G-0 PARA. 8.<BR>DOUBLER GOING TO BE INSTALL ON W/C TTG8Q00UBG4C ITEM 5;[02] VERIFIED CORRECTIVE ACTION ITEMS; CAJul 5, 2024 · N257WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2024081309146Strap · corrodedCORROSION ON TENSION STRAP AT AFT PAX CABIN BS1025 RBL3 WL208.<[01] COMPLETE;[02] REMOVED AND REPLACED TENSION STRAP AT AFT PAX CABIN FROM BS 1006 -1029 RBL 3 PER SRM 51-40-02-0G-0 AND BOEING DWG 147A5730.;[03] REMOVED AND REPLACED TENSION STRAP AT AFT PAX CABJul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309150Sill Drain · corrodedCORROSION ON FWD SERVICE DOOR MOPSILL STA 298-330 ON VERTICAL FLANGE; RBL 54-RBL 58; WL 208.<[01] VERIFIED;[02] VERIFIED;[03] REPLACED FWD SERVICE DOOR MOPSILL STA 250-BS 360 RBL54-RBL58 WL208 IAW SRM 51-10-02-0G-0; SRM 51-40-02-0G-0; 51-40-05-0G-0; SRM 51-40-Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309149Attach Angle · crackedCRACKED ATTACH ANGLE AT FWD CABIN BS294 RBL54 WL208. MARKED<[01] REMOVED AND REPLACED CRACKED ANGLE AT FSD CUTOUT BS294 RBL54 WL208 IAW SRM 51-40-02 AND DWG#141A8310 REV B;[02] VERIFIED CORRECTIVE ACTION 1.;[03] EDITED TABLE;[04] VERIFIEDJul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024081309156Intercostal · crackedCRACKED INTERCOSTAL STA 277-294; RBL 1; WL 208.<[01] REMOVED AND REPLACED CRACKED INTERCOSTAL AT BS 277-294; RBL 1; WL 208 IAW SRM 51-40-02; SRM 51-40-05; SRM 51-40-08; AND DWG 141A5400 REV-.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309162Bracket · corrodedCORROSION ON FWD ENTRY GIRT BAR FITTING SUPPORT BRACKETS AT STA 312; STA 328; LBL 55; WL 208.5<[01] REPLACED CORRODED FWD ENTRY GIRT BAR FITTING SUPPORT BRACKETS AT STA 312; STA 328; LBL 55; WL 208.5 PER SRM 51-40-02-0G-0. TORQUED PER SRM 51-40-04. TOOLING USEJul 4, 2024 · N257WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2024081309144Web · corrodedCORROSION ON WEB AT AFT PAX CABIN BS1025 RBL1 WL208.<[01] REMOVED CORROSION FROM WEB AT AFT PASSENGER CABIN BETWEEN BS 1016 TO 1030 RBL 0 TO RBL 3 WL 208; BLEND OUT MEASURE L: 14' W: 2.3 D: .002' FROM ORIGINAL THICKNESS OF .040' IAW SRM 51-10-02-0G-0. NO ALLOWJul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309141Strap · corrodedCORROSION ON TENSION STRAP AT AFT PAX CABIN BS1023 LBL3 WL208.<[01] COMPLETE;[02] REMOVED AND REPLACED TENSION STRAP AT AFT PAX CABIN FROM BS 1006 -1029 LBL 3 PER SRM 51-40-02-0G-0 AND BOEING DWG 147A5730.;[03] REMOVED AND REPLACED TENSION STRAP AT AFT PAX CABJul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309147Strap · corrodedCORROSION ON TENSION STRAP AT AFT PAX CABIN BS1028 RBL18 WL208.<[01] COMPLETE;[02] ALL WORK COMPLETE;[03] REMOVED TENSION STRAP BS1028 RBL18 WL208 IAW SRM 51-40-02-0G-0 AND INSTALLED NEW TENSION STRAP BS1028 RBL18 WL208 IAW SRM 51-40-02-0G-0 AND DWG #147A5730 Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309151Attach Angle · corrodedCORROSION ON FWD SERVICE DOOR MOPSILL ATTACH ANGLE STA 304-324; RBL 55-RBL 59; WL 209.<[01] FWD SERVICE DOOR MOPSILL ATTACH ANGLE REPLACED AS PART OF MOPSILL ASSY P/N 654A0004-106 (CHORD ASSY) FAULT #TTG8Q00UD1ET;[02] VERIFIED CORRECTIVE ACTION;[03] VERFIED COJul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024081309153Frame · corrodedCORROSION ON 303 FRAME; LBL 58; WL 209-211.<[01] REMOVED CORROSION ON FRAME BS 303.9 LBL 55 WL 209-211 IN A 3.1' X 1.4' X .037' FROM ORIGINAL THICKNESS OF .330'. FOUND TO BE OUT OF LIMITS. ACCOMPLISHED REPAIR TO BS 303.9 FRAME IAW EA 24-153-01913;[02] VERIFIEDJul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024081309154Intercostal · crackedCRACKED INTERCOSTAL STA 344-360; RBL 33; WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5400.;[02] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 REV-;[03] VERIFIED CORRECTIVE ACTION 2Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309159Attach Angle · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; RBL 40; WL 208.<[01] REMOVED AND REPLACED ATTACH ANGLE STA 380-400; RBL 40; WL 208. PER SRM 51-40-02-0G-0 AND BOEING DWG 143A5400.;[02] VERIFIED CORRECTIVE ACTION 1.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024081309160Attach Angle · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; BL0; WL 208.<[01] REMOVE AND REPLACE INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; BL 0; WL 208.;[02] REMOVED AND REPLACED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; BL 0; WL 208. PER SRM 51-40-02-0G-0 AND BOEJul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024081309163Attach Angle · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 13; WL 208.<[01] REMOVE AND REMPLACE INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; RBL 40; WL 208.;[02] REMOVED AND REPLACED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; RBL13; WL 208. PER SRM 51-40-02-0G-0 Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024081309164Attach Angle · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; RBL 9; WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; RBL 9 WL 208 PER SRM 51-10-02-0G-0 PAR 9 AND BOEING DWG 143A5400;[02] REMOVED AND REPLACED INTERCOSTAL UPPER ATTACH ANGLE SJul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024081309161Support Angle · corrodedCORROSION ON FWD ENTRY MOPSILL SUPPORT ANGLE 314-326; LBL 57-58; WL 209.<[01] UPDATED STEPS AND TABLE.;[02] PARTIAL UPDATE STEP 3;[03] UPDATED STEP 4; DWG REVISION #; 141A8112 REV:-;[04] CERTIFY UPDATE.;[05] REMOVED AND REPLACED FED MOPSILL SUPPORT ANGE PER SRJul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309152Sill Drain · crackedFWD MOPSILL IS CRACKED AT STA 303; LBL 58; WL 209.<[01] UPDATED MEASUREMENT TABLE AND STEPS.;[02] STEP 4 UPDATE;[03] UPDATED STEP 4 DWG REVISION#; DWG 141A8110 REV:E;[04] CERTIFY;[05] REMOVED AND REPLACED FED MOP SILL BETWEEN BS 270 TO BS 360 ; LBL 58 ;WL 209 Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309155Intercostal · crackedCRACKED INTERCOSTAL STA 344-360; RBL 12; WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL FROM BS 344 TO BS 360; RBL 12 AND BOEING DWG 141A5400 ID: 13.;[02] VERIFIED CORRECTIVE ACTION 1Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309157Intercostal · crackedCRACKED INTERCOSTAL STA 312-328; LBL 44; WL 208.<[01] REMOVED AND REPLACE INTERCOSTAL STA 312-328; LBL 44; WL 208. AND BOEING DWG 141A5400 PER SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION 1.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309158Intercostal · crackedCRACKED INTERCOSTAL STA 328-344; LBL 44; WL 208.<[01] REMOVE AND REMPLACE INTERCOSTAL STA 328-344; LBL 44; WL 208 AND BOEING DWG 141A5400 PER SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION 1.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081309138Panel · debondedPANEL 195CL PREVIOUS REPAIR AT AFT EDGE CORNER RADIUS IS DISBONDED.<[01] PANEL 195CL DISBONDED PREVIOUS REPAIR AT AFT EDGE CORNER RADIUS WAS REPAIRED IAW SRM 51-70-05-2R-6;[02] VERIFIED CORRECTIVE ACTION 1Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024080909114Floor Panel · pulledFWD FLOOR PANEL 221AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SURFACE OF FWD FLOOR PANEL 221AF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024080909115Floor 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-1.;[02] JOB COMPLETE.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024080909123Floor Panel · pulledFWD FLOOR PANEL 222AF UPPER SKIN HAS AREAS OF PULLED STRANDS ALONG THE O/B EDGE.<[01] FWD FLOOR PANEL 222AF HAD PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED COMPLETEJul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024080909125Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FORWARD FLOOR PANEL 222CF UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024080909126Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FORWARD FLOOR PANEL 222DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED COMPLETEJul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024080909129Floor Panel · pulledFWD FLOOR PANEL 232BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 232BF UPPER SKIN HAD AREAS OF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024080909122Floor Panel · pulledFWD FLOOR PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221FF 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.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024080909117Floor Panel · pulledFWD FLOOR PANEL 221GF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221GF 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.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024080909124Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED FWD FLOOR PANEL 222BF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-50D ITEM 96.;[02] VERIFIEDJul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024080909120Floor 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.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024080909116Floor Panel · pulledFWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221EF 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.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024080909118Floor Panel · pulledFWD FLOOR PANEL 231CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 231CF 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.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024080909128Floor Panel · pulledFWD FLOOR PANEL 232AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 232AF 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.Jul 4, 2024 · N257WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024081309096Floorbeam · corrodedCORROSION ON TOP FLANGE OF BS 986.5 FLOOR BEAM RBL 45-RBL 28 AND LBL 44 WL 208<[01] COMPLETED STEP 1; UPDATED TABLE;[02] EDITED STATEMENT;[03] EVALUATED CORROSION ON TOP FLANGE OF BS 986.5 FLOOR BEAM RBL 45-RBL 28 AND LBL 44 WL 208. FOUND TO BE OUT OF LIMITS DJul 3, 2024 · N257WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024081309093Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK IN THE WELL; RBL45 BS727E+10; BS800; BS831; BS840 WL208.<[01] COMPLETED STEP 1 AND STEP 2.;[02] COMPLETED STEP 4.;[03] EDIT TO STEP #5; DWG REVISION.;[04] ADDITIONAL FABRICATION EDIT TO STEP #5;[05] CERTIFY;[06] SUMMERY Jul 3, 2024 · N257WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024081309100Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK IN THE WELL LBL45 BS500D+10 WL208.<[01] SEAT TRACK TO BE RELACED ON TTG8Q00UCL0H.;[02] CORRECTED MEASUREMENT TABLE STEPS 1;2; AND 3.;[03] VERIFIED. CARD COMPLETE.Jul 3, 2024 · N257WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
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