N284WN

Service difficulty reports · 308

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 = 'N284WN' 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 SWAA2025042955261Shield · corrodedAFT CARGO 767+7 RBL 20 SILL PLATE IS CORRODED MARKED<[01] REMOVED AND REPLACED AFT CARGO FWD SHIELD IAW SRM 51-40-02-0G-0 AND DWG#146A0081;[02] COMPLETEApr 5, 2025 · N284WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025042955256Strap · corrodedAFT CARGO BS 787+4 RBL 19 ANCHOR NUT AT UNDERSIDE OF STRUCTURE HAS CORRSION<[01] REMOVED AND REPLACED STRAP AT BS 787 TO BS 794 RBL 19 IAW SRM 51-40-02 AND DWG 146A0081 ID:0031 REV: -;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.Apr 5, 2025 · N284WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025050621755Tie Down · corrodedFWD CARGO TIE DOWN HAS PITTING CORRSION AT BS 420+15 LBL 12 WL 140. MARKED FWD CARGO TIE DOWN HAS PITTING CORRSION AT BS 420+15 LBL 18 WL 156.<[01] REMOVED CORROSION FROM FWD CARGO BAY TIE DOWN BS 420+15; LBL-18; WL-156 FOUND TO BE WITH IN THE LIMIT IAW SRM 53Apr 4, 2025 · N284WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025050621758Scuff Plate · corrodedFWD CARGO R/H SILL PLATE HAS SURFACE CORROSION AT 500A+14 AND 500C+12 WL 140 RBL24 MARKED<[01] REMOVED AND REPLACED NEW FLOOR TO SIDEWAL SUPPORT FROM BS500A TO BS500D RBL24 IAW SRM 51-40-02 AND DWG 143A7500 ID: 0071 REV: -;[02] VERIFIED COMPLETION CORRECTIVE AApr 4, 2025 · N284WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025050621757Scuff Plate · corrodedFWD CARGO R/H SILL PLATE HAS SURFACE CORROSION 480+16 AND 500+8 WL140 RBL 24<[01] REMOVED AND REPLACED FWD CARGO AFT SHIELD FROM BS492.4 TO BS500A WL140 RBL 24 IAW SRM 51-40-02 AND DWG#143A0080.;[02] JOB COMPLETEApr 4, 2025 · N284WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025043039468Support · corrodedFWD CARGO R/H SILL PLATE HAS SURFACE CORROSION AT 500A+14 AND 500C+12 WL 140 RBL24 MARKED<[01] REMOVED AND REPLACED NEW FLOOR TO SIDEWAL SUPPORT FROM BS500A TO BS500D RBL24 IAW SRM 51-40-02 AND DWG 143A7500 ID: 0071 REV: -;[02] VERIFIED COMPLETION CORRECTIVE AApr 4, 2025 · N284WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025043039467Shield · corrodedFWD CARGO R/H SILL PLATE HAS SURFACE CORROSION 480+16 AND 500+8 WL140 RBL 24<[01] REMOVED AND REPLACED FWD CARGO AFT SHIELD FROM BS492.4 TO BS500A WL140 RBL 24 IAW SRM 51-40-02 AND DWG#143A0080.;[02] JOB COMPLETEApr 4, 2025 · N284WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025042955246Shield · corrodedFWD CARGO R/H SILL PLATE HAS SURFACE CORROSION 480+16 AND 500+8 WL140 RBL 24<[01] REMOVED AND REPLACED FWD CARGO AFT SHIELD FROM BS492.4 TO BS500A WL140 RBL 24 IAW SRM 51-40-02 AND DWG#143A0080.;[02] JOB COMPLETEApr 4, 2025 · N284WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025042955247Support · corrodedFWD CARGO R/H SILL PLATE HAS SURFACE CORROSION AT 500A+14 AND 500C+12 WL 140 RBL24 MARKED<[01] REMOVED AND REPLACED NEW FLOOR TO SIDEWAL SUPPORT FROM BS500A TO BS500D RBL24 IAW SRM 51-40-02 AND DWG 143A7500 ID: 0071 REV: -;[02] VERIFIED COMPLETION CORRECTIVE AApr 4, 2025 · N284WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025042955224Connector · missingSIDEWALL PANEL 231YHW EXIT LIGHT ON PANEL HAS WIRE CONNECTOR MISSING.<[01] REMOVED; REPLACED AND PERFORMED GOOD OPS CHECK OF THE CONNECTOR D3670 OF EMERGENCY EXIT LIGHT AT SIDEWALL PANEL 231YHW IAW AMM 33-51-00 AND SWPM 20-30-12.<BR><BR>COMPLETED TASK CARD;[02Apr 3, 2025 · N284WN · Boeing 7377H4 · Light System WiringSDR SWAA2025042955213Fairing · damagedPANEL 642BB; #6 FLAP TRACK FAIRING; HAS SEVERAL ELONGATED HOLES (AFT END).<[01] REMOVED PANEL 642BB FAIRING DRIVE LINKAGE AND INSTALLED ON NEW PANEL 642BB IAW AMM 27-51-18-400-802.<BR>TORQUE WRENCH 2321 S/N 0119121014 DUE: 06/2025;[02] VERIFIED CORRECTIVE ACTIApr 3, 2025 · N284WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2025042955217Fairing · crackedPANEL 642BB; #6 FLAP TRACK FAIRING; HAS POSSIBLE CRACK 16 INCHES FWD FROM AFT BULKHEAD ASSY BOTTOM OF FAIRING (MARKED).<[01] #6 FLAP TRACK FAIRING 642BB IS BEING REPLACED ON FAULT: TTG8Q00ZN8EZ.;[02] #6 FLAP TRACK FAIRING 642BB IS BEING REPLACED ON FAULT: TTG8Apr 3, 2025 · N284WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2025042955215Fairing · damagedPANEL 642EB; #6 FLAP TRACK FAIRING TAILCONE; HAS SEVERAL ELONGATED HOLES.<[01] REMOVED AND REPLACED PANEL 642EB; #6 FLAP TRACK FAIRING TAILCONE; P/N 113A9352-1 LOT 1601033-1<BR>RECEIVED NEW TAIL CONE WITH FULL SIZE HOLES; COUNTERSANK HOLES IAW SRM 51-40-08 & IApr 3, 2025 · N284WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2025050620938Seat Track · corrodedCORROSION ON THE SEAT TRACK AT BS540; BS578+4; BS706; AND BS727+6 RBL25 WL208<[01] FAULT RAISED IN ERROR (FAULT WAS RAISED IN ERROR AND IS BEING CLOSED);[02] VERIFIED CORRECTIVE ACTION 1Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025050620703Floor 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.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025050620705Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025050620708Stub Frame · crackedCRACK 2.5' ON INNER STUB FRAME OF FWD GALLEY DOOR (R1); BETWEEN S-8R AND S-9R (BS STA 299; RBL 52; WL 265.5 APPROX; MARKED)<[01] REPLACED STUBFRAME IAW B737-7SRM 53-10-01-2R-6 SRM 51-40-02-0G-0 AND DWG 141A8370;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2025043039339Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025043039337Floor 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.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025043039343Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231XF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025043039342Stub Frame · crackedCRACK 2.5' ON INNER STUB FRAME OF FWD GALLEY DOOR (R1); BETWEEN S-8R AND S-9R (BS STA 299; RBL 52; WL 265.5 APPROX; MARKED)<[01] REPLACED STUBFRAME IAW B737-7SRM 53-10-01-2R-6 SRM 51-40-02-0G-0 AND DWG 141A8370;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2025042955197Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-5R. MARKED<[01] REMOVED AND REPLACED STR CLIP AT BS 727E S-5R IAW SRM 51-40-02 AND DWG 146A1112 ID:0009 REV:-;[02] VERIFIED CORRECTIVE ACTION #1Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025042955196Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS685 S-2L. MARKED<[01] REMOVED AND REPLACE CLIP AT B727D S-6L IAW SRM 51-40-02 AND DWG 146A1106 ID:0019 REV: A;[02] REMOVED AND REPLACED CLIP AT BS 685 S-2L IAW SRM 51-40-02 AND DWG 146A1106 ID:0019 REV: A;[03] VERIFIED CORRECTIVApr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025042955193Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS706 S-4L. MARKED<[01] REMOVED AND REPLACED CLIP AT B727D S-6L IAW SRM 51-40-02 AND DWG 146A1107 ID:0015 REV: -;[02] REMOVED AND REPLACED CLIP AT B706 S-4L IAW SRM 51-40-02 AND DWG 146A1107 ID:0015 REV: -;[03] VERIFIED CORRECTIVEApr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2025042955195Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS706 S-3L. MARKED<[01] REMOVED AND REPLACE CLIP AT BS 706 S-3L IAW SRM 51-40-02 AND DWG 146A1107 ID:0015 REV: -;[02] VERIFIED CORRECTIVE ACTION #1Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025042955192Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727D S-6L. MARKED<[01] REMOVED AND REPLACED CLIP AT B727D S-6L IAW SRM 51-40-02 AND DWG 146A1111 ID:0011 REV: -;[02] VERIFIED CORRECTIVE ACTION #1Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025042955194Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727D S-7L. MARKED<[01] REMOVED AND REPLACED CLIP AT B727D S-7L IAW SRM 51-40-02 AND DWG 146A1111 ID:0011 REV: -;[02] VERIFIED CORRECTIVE ACTION #1Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2025042955191Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-7L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT BS 727E S-7L IAW SRM 51-40-02 AND DWG 146A1112 ID:0009 REV:-;[02] VERIFIED CORRECTIVE ACTION #1Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025042955190Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS747 S-7L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT BS 747 S-7L IAW SRM 51-40-02 AND DWG 146A1131 ID:0013 REV: -;[02] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.;[03] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025042955189Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS767 S-6L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT BS 767 S-6L IAW SRM 51-40-02 AND DWG 146A1132 ID:0007 REV:-;[02] VERIFIED CORRECTIVE ACTION #1Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2025042955184Strap · corrodedCORROSION ON TENSION STRAP @ BS1016+13; LBL3 WL 208<[01] THE CORROSION ON TENSION STRAP @ BS1016+13; LBL3 WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM FOR THIS ITEM AND IT IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02; REMOVED AND REPApr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025042955171Bear Strap · crackedCRACK 1.5' ON INNER BEAR STRAP OF FWD GALLEY DOOR (R1); BETWEEN S-8R AND S-9R (BS STA 294.5; RBL 52; WL 265.5 APPROX; MARKED)<[01] DAMGE REMOVED AND AREA WAS REPAIRED IAW B737-7 SRM 53-10-01-2R-6;[02] CORRECTION TO ACCTION 1 DAMAGE REMOVED AND AREA WAS REPAIREApr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2025042955148Scuff Plate · crackedFCB AFT CORNER SCUFF PLATE IS CRACKED.<[01] EDITED STEP 5; WRITTEN IN ERROR;[02] CRACKED FCB AFT CORNER SCUFF PLATE IS REPAIRED BY WELDING IAW SRM 53-30-15-2R-1.;[03] OK TO INSTALL;[04] REPAIRED THE CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1.;[05] VERIFIED ACTIOApr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025042955147Scuff Plate · crackedFCB FWD CORNER SCUFF PLATE IS CRACKED.<[01] CRACKED FCB FWD CORNER SCUFF PLATE IS REPAIRED BY WELDING IAW SRM 53-30-15-2R-1.;[02] REPAIR THE CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1.;[03] VERIFIED ACTION 2.<BR>JOB COMPLETE.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2025042955144Floor Panel · crackedAFT FLOOR PANEL 242XF LOWER SKIN IS CRACKED. (MARKED)<[01] AFT FLOOR PANEL 242XF LOWER SKIN WITH CRACK AS MARKED WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF DAMAGE.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955145Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955140Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ABF; WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955139Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW AFT FLOOR PANEL 241AAF IAW SRM 53-00-50-2R-0 AND BOEING DWG 147A5810 ID:0008.;[02] VERIFIED CORRECTIVE ACTION 1Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955135Floor Panel · pulledAFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241YF STRAND DAMAGE WAS REPAIRED IAW<BR>SRM 53-00-50-2R-1;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955134Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955137Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241UF 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.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955124Floor Panel · pulledFLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATE FLOOR PANEL PER SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955133Floor Panel · pulledFLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 242AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955132Floor Panel · pulledFLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241EF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATE FLOOR PANEL PER SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955131Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955130Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241BF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955129Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF 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.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955128Floor Panel · pulledFLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232SF 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.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955123Floor Panel · pulledFLOOR PANEL 232RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 232RF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025042955122Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231XF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION ITEM 1.Apr 2, 2025 · N284WN · Boeing 7377H4 · Fuselage Floor Panel
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