N224WN
Service difficulty reports · 281
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 = 'N224WN' 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.
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 = 'N224WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2026062415073Fuse · inoperativeRIGHT OVERWING EMERGENCY LIGHT COVER MISSING ON BOTTOM RIGHT DOOR AND LIGHT INOPERATIVE. CENTER TOP EMERGENCY LIGHT INOP AS WELL. REMOVED AND REPLACED M1669 POWER SUPPLY FUSES IAW AMM 33-51-06. OPS CHECKED GOOD. INSTALLED NEW EMERGENCY LIGHT COVER ON BOTTOM SDR SWAA2025103130480Sign · out of adjustFORWARD EXIT SIGN BY L1 DOOR FELL OFF. SECURED FWD EMERGENCY EXIT SIGN COVER BY L1 DOOR PER AMM 33-51-01.SDR SWAA2025102928779Strap · brokenR2 SAFETY STRAP BROKEN. REPLACED R 2 DOOR SAFETY STRAP PER SIP AND AMM 52-41-31SDR SWAA2025102726133Charger · inoperativeRIGHT FWD OVER DOOR EMERGENCY SIGN INOP<[01] R&R CHARGER ASSEMBLY FOR RIGHT FWD OVER DOOR EMERGENCY SIGN PER AMM 33-51-06. OPS CHECK GOODSDR SWAA2025091212848Fuse · inoperativeFED EMERGENCY EXIT LIGHT ON AFT FACE OF LAV-A INOP<[01] OK TO CLOSE STEP 1. REPLACED FUSE OF M1675 BATTERY POWER SUPPLY AND PERFORMED GOOD OPERATIONAL TEST OF FED EMERGENCY EXIT LIGHT ON AFT OF LAV-A IAW B737 AMM 33-51-06-960-804 AND AMM 33-51-00-710-801.SDR SWAA2025091208093Bulkhead · crackedB.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 15; WL 167. BS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 15; WL 167; WAS REPAIRED IAW SRM 51-70-04-2R-10.SDR SWAA2025091104028Support Plate · corrodedCORROSION FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500A+1' TO BS500C+10' LBL22 WL156. EVALUATED; LOCATED AND DRILLED; REMOVED AND REPLACED FWD CARGO BAY L/H NEW SECTION FLOOR SIDEWALL SUPPORT PLATE BS480+10 TOSDR SWAA2025091104029Support Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156. CORROSION EVALUATION ON ACB L/H FLOOR TO SIDEWALL SUPPORT BS727B TO BS767 LBL22 WL156 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-5SDR SWAA2025091104351Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727D+6' RBL11.5 WL156. EVALUATED CORROSION ON AFT CARGO BAY FLOOR STRAP BS 727D+6 RBL 11.5 WL 156; FOUND TO BE OUT OF LIMITS; RECEIVED NEW STRAP AND APPLIED ENAMEL; ALL PER SRM 51-10-02-0G-0;SDR SWAA2025091503810Skin · delaminatedLEFT WING OTBD AFT FLAP INBD UPPER SURFACE DELAMINATED. REMOVED AND REPLACED THE LT WING OTBD AFT FLAP IAW AMM 27-51-22-000-801, AND AMM 27-51-22-400-801.SDR SWAA2025091203774Floorbeam · crackedCRACKED PANEL BREAK AT PASSENGER COMPARTMENT BS 540; RBL 2; WL 208. REMOVED PANEL BREAK ASSY AT STA 520; RBL 1-24 PER SRM 51-40-02-0G-0. REMOVED AND REPLACED PANEL BREAK AT PASSENGER COMPARTMENT BS 540; RBL 2; WL 208 IAW SRM 51-40-02-0G-0.SDR SWAA2025091203119Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 45; W.L. 167.<[01] REMOVED AND INSTALLED NEW UPPER ATTACH ANGLE AT BS 663 L.B.L. 45; W.L. 167 PER SRM 51-40-02-0G-0; DWG 111A1000 REV. B AND DWG 111A700 REV.A.SDR SWAA2025091103388Handle · damagedFED AFT SURROUND SIDEWALL LINING PANEL ASSIST HANDLE ASSY AND YELLOW SAFETY STRAP DAMAGED. REMOVED AND REPLACED ASSIST HANDLE ASSY AND YELLOW SAFETY ON THE FED AFT SURROUND SIDEWALL LINING PANEL IAW IPC 25-21-25-22 ITEM 20;25-66-10-02 ITEM 30;25-21-25-22 ITESDR SWAA2025091200092Panel · debondedPANEL 193CL HAS LARGE DISBONDS ON BOTH SKINS. DUE TO THE EXTENT OF DAMAGE; REPLACED PANEL 193CL WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-14-00-03A ITEM 290.;SDR SWAA2025091200093Panel · debondedPANEL 193CR INNER SKIN IS DISBONDED. REPAIRED IAW SRM 51-70-05-2R-2-A00733, REPAIR 2. REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE.SDR SWAA2025091100083Cradle · broken1EA AFT EMERGENCY FLASHLIGHT HOLDER ASSY BROKEN. REMOVED AND REPLACED 1EA AFT EMERGENCY FLASHLIGHT HOLDER PER SOPM 20-50-01.SDR SWAA2025091299693Scuff Plate · crackedFWD SERVICE DOOR SCUFF PLATE IS CRACKED AT AFT EDGE. REMOVED ALL THE COATINGS AND OTHER UNWANTED FROM THE SCUFF PLATE BEFORE WELDING PER SRM 53-10-15-2R-1 STEP 4.B.(3). WELDED THE DAMAGED AREA ON SCUFF PLATE IAW SRM 53-10-15-2R-1 STEP 4.B.(4). INSPECTED SDR SWAA2025072192774Slide · dislodgedFWD SERVICE DOOR SLIDE FELL OUT OF HOLDER. REINSTALLED FWD SERVICE DOOR SLIDE.SDR SWAA2025050165462Handle · looseFWD ENTRY DOOR ASSIST HANDLE LOOSE<[01] RESECURED FWD ENTRY DOOR ASSIST HANDLE PER AMM 52-11-31.SDR SWAA2025042864023Wedge · debondedLH IB MAIN FLAP TE WEDGE ASSY ADDITIONAL DISBOND UPPER AND LOWER SKINS WHILE PERFORMING TAP TEST FOUND ADDITIONAL AREAS OF DISBOND TO UPPER AND LOWER SKINS OF TE WEDGE. FOUND LOWER SKIN DISBOND 30 IN. L X 12 IN. W. FOUND UPPER SKIN DISBOND OF 27.5 IN. L X 6 INSDR SWAA2024051384116Light · failedSIDEWALL LIGHT OUT AT L/H OVERWING EXIT DOOR.<[01] R/R SIDEWALL LIGHT AT L/H OVERWING LIGHT PER AMM 33-51-04SDR SWAA2024042377338Circuit Breaker · trippedINFO ONLY FOUND EMERGENCY PANEL LIGHT BREAKER POPPED CONTACTED DAVE IN MOC -NO 10 DAY HISTORY - PERFORMED ONE TIME RESET BREAKER REMAINED CLOSED <BR>P6-3 BREAKER D8<[01] 02 - INSPECTED PER [GENERAL MPM 52.06.05 (INFO ONLY ITEM; NOTED BY MX)]<BR>NOTED BY MX REFSDR SWAA2024041774900Cover · out of adjustLOWER EMER EXIT LIGHT @ 11BC EMER EXIT ROW COVER BROKEN<[01] C/W EA M-21-133-00720; LENS COVER SECURED W/ CLEAR TAPE.SDR SWAA2024010937896Battery Pack · failedEMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATIONS M1673;M1675;M1669;M1668;M1670 EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATIONS M1673M1675M1669M1668M1670<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS M1673;MSDR SWAA2023091499348Girt Bar · out of adjustAFT ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED AFT ENTRY DOOR SLIDE GIRT PER AMM 25-66-01SDR SWAA2023091499340Light · inoperativePASSENGER CABIN OWE SIDEWALL LIGHT IS INOP<[01] RE LAMPED OWE EMERGENCY LIGHT REF AMM 33-51-01.SDR SWAA2023091198597Battery · inoperativeAFT MEGAPHONE INOPERATIVE<[01] R/R BATTERIES IAWMM 25-64-00SDR SWAA2023082890342Door · crackedR1 SERVICE DOOR SLIDE AFT SHOCK MOUNT CRACKED. (51-011)<[01] FWD GALLEY DOOR WAS REPLACED ON TASK CARD TTG8Q00MWSPU;[02] CORRECTION TO STEP 1 SHOULD READ FWD GALLEY DOOR WAS REPLACED ON TASK CARD TTG8Q00MS4S4;[03] VERIFIED 2.SDR SWAA2023082890341Door · crackedR1 SERVICE DOOR HANDLE TORQUE BOX UPPER BEAM CRACKED NEAR TORQUE BOX FORWARD ATTACH BOLT. (51-012)<[01] REPLACED FWD GALLEY SERVICE DOOR PER B737 AMM 52-41-00-400-801-NG INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00MS4S4;[02] VERIFIED 1.SDR SWAA2023082389891Battery Pack · inoperativeLH SIDE OVER WING EXIT EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY POWER SUPPLY; PERFORMED OPERATIONAL TEST; TEST PASSED;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2023082389892Battery Pack · inoperativeRH SIDE OVERHEAD BIN ROW 8 AREA EMERGENCY LIGHT INOP.<[01] PERFORMED T/S AND REMOVED BATTERY PACK FOUND FUSE LOOSE; REPOSITIONED FUSE; REINSTALLED BATTERY PACK AND PERFORMED TEST; TEST PASSED.;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2023082888399Door · out of adjustR-1 DOOR VERTICAL ADJUSTMENT OUT OF LIMITS AT .020-.024 IN; MIN .060 IN; R-1 DOOR MECHANICAL ADJUSTMENT AT DOOR TORQUE TUBE IS AT MAX VERTICAL ADJUSTMENT.<[01] FWD GALLEY SERVICE DOOR ADJUSTMENT WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00MS4S4;[02] VERIFIED CORRSDR SWAA2023082491380Plate · corrodedCUSTOMER REQUEST AAI INSPECTION; - FUSELAGE LOWER LOBE- AFT ANTENNA AT STA 450; STR 27L APPROX. HAS EVIDENCE OF CORROSION FUSELAGE LOWER LOBE- AFT COVER PLATE AT STA 450 STR 27L APPROX. HAS EVIDENCE OF CORROSION<[01] REMOVED AND INSTALLED NEW AFT ALTIMETER FAISDR SWAA2023082490333Plate · corrodedCUSTOMER REQUEST AAI INSPECTION; - FUSELAGE LOWER LOBE - FWD ANTENNA AT STA 410; STR 27L APPROX. HAS EVIDENCE OF CORROSION FUSELAGE LOWER LOBE - FWD COVER PLATE AT STA 410 STR 27L APPROX. HAS EVIDENCE OF CORROSION<[01] REMOVED AND INSTALLED NEW AFT ALTIMETER FSDR SWAA2023082383807Floor Panel · damagedFWD CABIN FLOOR PANEL 231CF UPPER SKIN SURFACE CHIPPING AT EDGE.<[01] REMOVED AND REPLACED FWD CABIN FLOOR PANEL 231CF UPPER SKIN ASPER AMM 53-21-000-801 AND 53-21-00-400-801;[02] VERIFIED REMOVED AND REPLACED FWD CABIN FLOOR PANEL 231CF.SDR SWAA2023082383806Floor Panel · peelingR/H FWD CABIN FLOOR 232AF UPPER SKIN SURFACE PEELING.<[01] RECEIVED R/H FWD CABIN FLOOR 232AF UPPER SKIN SURFACE WILL BE CLOSED ON TTG8Q00LYLAQ ASPER DWG#141A5810;[02] VERIFIED 1.SDR SWAA2023082483507Skin · corrodedL/H AFT STRUT FAIRING I/B SIDE AFT LOWER SKIN SURFACE HAS CORROSION.<[01] REMOVED AND REPLACED #1 PYLON STRUT AFT LOWER EDGE SKIN IN REF B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING #313A2750.;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2023082483506Skin · corrodedR/H AFT STRUT FAIRING I/B SIDE AFT LOWER SKIN SURFACE HAS CORROSION.<[01] REMOVED AND REPLACED R/H LOWER STRUT FAIRING EDGE IN REF B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING # 313A2750.;[02] VERIFIED STEP 1 COMPLETE.SDR SWAA2023082883505Access Panel · crackedL/H WING T/E ACCESS PANEL 561AB LOWER SKIN SURFACE AROUND FASTENER HOLES CRACKS.<[01] APPLIED TOPCOAT ON L/H WING T/E ACCESS PANEL 561AB LOWER SKIN SURFACE REF B 737 AMM 51-21-73-370-803;[02] APPLIED REPAIR IN DAMAGE AREA AROUND FASTENER HOLES ON PANEL #561AB SDR SWAA2023082888996Access Panel · crackedAFT CENTER WHEEL WELL ACCESS PANEL # 193D HAS BULGING/CRACKED FASTENER HOLES<[01] APPLIED A PERMANENT REPAIR ON DAMAGED FASTENER HOLES AS MARKED ON PANEL #193D AS PER B737 SRM 51-70-04-2R-9 PARA 4.L-M-N ; MATERIAL USED PO#2011230; PO#1775890 AND PO#1690463;[02SDR SWAA2023082483246Shield · corrodedAFT CARGO R/H FWD SHIELD FROM ST 767 TO 787 ; RBL 20 AROUND THE 4 FASTENER HOLE HAVE COROCION. (228-008) AFT CARGO R/H FWD SHIELD FROM ST 767 TO 787 RBL 21 AROUND THE 4 FASTENER HOLE HAVE CORROSION. (228-008) [TTG8Q00MGCG3]<[01] REMOVED CORROSION AT R/H FWD SHSDR SWAA2023082483245Channel · corrodedAFT CARGO R/H Z CHANNE AT ST 747 + 18.5' ; RBL 20 HAS CORROCION ATROUND THE HOLE FASTENER (228-007) AFT CARGO R/H CHANNE AT ST 747 + 18.5' RBL 21 HAS CORROCION ATROUND THE HOLE FASTENER (228-007) [TTG8Q00MGCEU]<[01] AFT CARGO R/H Z CHANNE AT ST 747 + 18.5' ; RSDR SWAA2023082483243Channel · corrodedAFT CARGO R/H Z CHANNE AT ST 747 + 10' ; RBL 21 HAS CORROCION ATROUND THE HOLE FASTENER (228-005)<[01] AFT CARGO R/H Z CHANNE AT ST 747 + 10' ; RBL 21; TO BE REPLACED ON CUSTOMER BAR CODE TTG8Q00MGCKT.;[02] VERIFIED STEP # 1.SDR SWAA2023082483242Channel · corrodedAFT CARGO R/H Z CHANNE AT ST 747 + 6' ; RBL 21 HAS CORROCION ATROUND THE HOLE FASTENER (228-004)<[01] AFT CARGO R/H Z CHANNE AT ST 747 + 6' ; RBL 21 ; TO BE REPLACED ON CUSTOMER BAR CODE TTG8Q00MGCKT;[02] VERIFIED STEP # 1.SDR SWAA2023082483244Channel · corrodedAFT CARGO R/H Z CHANNE AT ST 747 + 15' ; RBL 20 HAS CORROCION ATROUND THE HOLE FASTENER (228-006) AFT CARGO R/H CHANNE AT ST 747 + 15' RBL 21 HAS CORROCION ATROUND THE HOLE FASTENER (228-006) [TTG8Q00MGCED]<[01] AFT CARGO R/H Z CHANNE AT ST 747 + 15' ; RBL 21;SDR SWAA2023082483241Channel · corrodedAFT CARGO R/H Z CHANNE AT ST 727E + 8.5' ; RBL 20 HAS CORROCION ATROUND THE HOLE FASTENER (228-003) AFT CARGO R/H CHANNEL AT ST 727E + 8.5' RBL 21 HAS CORROSION AT ROUND THE HOLE FASTENER (228-003) [TTG8Q00MGCCH]<[01] AFT CARGO R/H Z CHANNE AT ST 727E + 8.5' ;SDR SWAA2023082483247Channel · corrodedAFT CARGO R/H Z CHANNE AT ST 727D + 8' ; RBL 20 HAS CORROCION ATROUND THE HOLE FASTENER (228-002) AFT CARGO R/H Z CHANNEL AT ST 727D + 8' RBL 21 HAS CORROSION AT ROUND THE HOLE FASTENER (228-00<[01] INSTALLED NEW FABRICATED Z CHANNEL R/H AFT CARGO; FROM STA. 7SDR SWAA2023082483240Channel · corrodedAFT CARGO R/H Z CHANNE AT ST 727D + 3' ; RBL 20 HAS CORROCION ATROUND THE HOLE FASTENER (228-001) AFT CARGO R/H CHANNE AT ST 727D + 3' RBL 21 HAS CORROSION AT ROUND THE HOLE FASTENER (228-001) [TTG8Q00MGCBY]<[01] FT CARGO R/H Z CHANNE AT ST 727D + 3' ; RBL 21;SDR SWAA2023082383417Door · crackedL/H LANDING GEAR DOOR CRACKED<[01] REMOVED AND REPLACED L/H LANDING GEAR DOOR AS PER B737 AMM 32-13-11-000-803;32-13-11-420-802; 32-13-11-420-803; AND PERFORMED ADJUSTMENTS/OPS CHECK AS PER B737 AMM 32-13-11-820-801. ADJUSTMENTS WITHIN LIMITS AND OPS CHECK GOOSDR SWAA2023082882998Panel · crackedR/H WING I/B FLAP TRACK ACCESS PANEL # 194CR HAS BULGING/CRACKED FASTENER HOLES<[01] REPAIRED DAMAGE TO PANEL 194CR PER SRM 51-70-04-2R-9 PARA 4.E; SRM 51-70-04-2R-9 PRIMED AND TOP COAT PER AMM 51-21-72-370-51-21-73-370-803804. REPAIR COMPLETE.;[02] VERIFIED C
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