N225WN
Service difficulty reports · 289
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 = 'N225WN' 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 = 'N225WN' 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 SWAA2023012695205Charger · inoperativeAFT RIGHT EMERGENCY LIGHTING CHARGER INOP. REMOVED AND REPLACED CHARGER PER AMM 33-51-06. RESEALED GALLEY CEILING ACCESS PANEL.SDR SWAA2023011087188Vapor Barrier · crackedUPPER VAPOR BARRIER ANGLE IN ECS BAY IS CRACKED AT STA 663; WL 167; LBL 41.<[01] REMOVED VERTICAL STIFFENER AT LBL 39 AND HORIZONTAL U-CHANNEL IAW SRM 51-40-02-0G-0.;[02] VERIFIED ITEM 1 OF STEPS 3; 4; 6 AND 7;[03] VERIFIED ITEM 5 OF STEP 7 AND ITEM 1 OF STEP SDR SWAA2023011087182Vapor Barrier · crackedUPPER VAPOR BARRIER ANGLE IN ECS BAY IS CRACKED AT STA 663; WL 167; RBL 41.<[01] VERIFIED ACTION STEP 1 OF STEPS 1; 2 AND 3;[02] VERIFIED ITEM 1 OF STEPS 4; 6; AND 7;[03] VERIFIED ITEM 5 OF STEP 7 AND ITEM 1 OF STEP 8;[04] VERIFIED ITEM 3 OF STEP 8;[05] VERIFISDR SWAA2023011086809Floor Panel · pulledCABIN FLOOR PANEL 231YF UPPER SURFACE HAS PULLED FIBERS. FOUND WITHIN REPAIRABLE LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1. BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 231YF IAW SRM 53-00-50-2R-1, REPAIR 1 STEPS 3, (K-O).SDR SWAA2023011086812Floor Panel · damagedCABIN FLOOR PANEL 231ZF UPPER SURFACE HAS PULLED FIBERS. FOUND WITHIN REPAIRABLE LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1. BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 231ZF IAW SRM 53-00-50-2R-1, REPAIR 1, STEPS 3, (K-O).SDR SWAA2023011086811Floor Panel · damagedCABIN FLOOR PANEL 231XF UPPER SURFACE HAS PULLED FIBERS. FOUND WITHIN REPAIRABLE LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1. BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 231XF IAW SRM 53-00-50-2R-1, REPAIR 1 STEPS 3, (K-O).SDR SWAA2023011086813Floor Panel · damagedCABIN FLOOR PANEL 241AF UPPER SURFACE HAS PULLED FIBERS. FOUND OUT OF LIMITS OF SRM 53-00-50-2R-0. FABRICATED A NEW FLOOR PANEL 241AF IAW DWG 1445810 AND SRM 53-00-50-2R-0, REPAIR GENERAL.SDR SWAA2023011086810Floor Panel · pulledCABIN FLOOR PANEL 232SF UPPER SURFACE HAS PULLED FIBERS. FOUND WITHIN REPAIRABLE LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1. PREPPED FLOOR PANEL 232SF FOR WET LAY-UP REPAIR IAW SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (A-J). BONDED REPAIR PLIES TO UPPER SURFACE OF SDR SWAA2022100451617Seat · wrong partPASSENGER SEAT 11D RECLINES INTO EMERGENCY ROW / [01] ADJUSTED HYDROLOCK COLLAR ON SEAT 11D PER CMM 25-21-42;[02] C/WSDR SWAA2022042697229Handle · looseFWD GIRT BAR HANDLE DOES NOT SECURE IN PLACE WHEN STOWED CREW VERBALLY STATED IT WAS FWD SERVICE DOOR. / [01] SECURED FWD SERVICE DOOR GIRT BAR HANDLE PER SIP.SDR SWAA2022021070609Water Heater · inoperativeAFT LAV SMOKE ALARM AT 8K ON APPROACH FA NOTICED ELECTRICAL SMELL. WATER HEATER AFT LAV FLASHING YELLOW. NO EVIDENCE OF FIRE. / [01] PERFORMED CONDITIONAL INSPECTION AMM 05-51-56. SEE LOG PAGE 1883562 FOR INOP WATER HEATER. AC OK FOR SERVICESDR SWAA2022021070610Smoke Detector · faultedAFT LAV ALARM ALERTED;FAINT ELECTRIC SMELL AFTER AHUTDOWN / [01] REMOVED AND REPLACED AFT LAV SMOKE DETECTOR IAW M.M 26-14-01 ;AND PREFORMED CONDITIONAL INSP IAW M.M 05-51-56. NO DEFECTS NOTEDSDR SWAA2022012763110Light · inoperativeAREA LIGHT NEAR RH OVER WING EXIT IS INOP. ; / [01] RELAMPED AREA LIGHT NEAR RH OVER WING EXIT PER AMM 33-51-03SDR SWAA2021100422831Battery Pack · inoperativeASSOCIATED EMERGENCY LIGHTS WITH BATTERY PACK M1674 ARE INOP. ; ASSOCIATED EMERGENCY LIGHTS WITH ATTERY PACK M1674 ARE INOP. / [01] REMOVED AND REPLACED BATTERY PACK M1674 PER AMM 33-51-06-960-805. GND TEST NORMAL<BR>AAR TAG WN8585; [02] REMOVED AND REPLACED BSDR SWAA2021100422215Fairing · delaminatedFUSELAGE FAIRING PANEL 193AR HAS A DENT AND AREA DELAMINATED ; / [01] REMOVED DAMAGED PLIES AT PANEL 193AR AS PER B737-700 SRM 51-70-04 GENERAL ; PARAGRAPH 4.B. NO WATER FOUND; [02] PREPARED DAMAGED AREA FOR REPAIRAS PER B737-700 SRM 51-70-04-2R-1; [03] LATE ESDR SWAA2021100422214Panel · delaminatedPANEL 191AR DELAMINATED AT 4 SCREWS ATTACHMENTS POINT AREA ; / [01] REMOVED PANEL#191AR FOR ACCESS TO REPAIR AT R/H FORWARD WING TO BODY FAIRING PANEL PER B737-700 AMM 53-51-21-000-803.; [02] MEASUREMENTS; [03] CLEANED AREA AND PREPARED AREA FOR REPAIR ON DAMASDR SWAA2021100416652Shield · corrodedAFT CARGO FLOOR STRUCTURE R/H SIDE REVEAL AT S-25R BETWEEN STA 767-787 WITH CORROSION ; / [01] REMOVED CORROSION ON AFT CARGO FLOOR STRUCTURE R/H SIDE REVEAL STA 767-787 AS PER B737-700 SRM 51-10-02-0G-0; [02] VERIFIED STEP 1; [03] PERFORMED UT THICKNESS INSP SDR SWAA2021100415308None · crackedSTA 663 VAPOR BARRIER UPPER FWD SIDE ATTACH ANGLE CRACKED AT RBL 10 ; / REMOVED FASTENERS FOR REPAIR IAW B737-700 RM 51-40-02-0G-0 AND 57-10-10-2R-5<BR> REPAIR 5;TRIM DAMABED AREA IAW B737-700 SRM 57-10-10-2R-5; [07] VERIFIED STEP 4 AND 6.ACCOMPLISHED DVI ; NOSDR SWAA2021100415307None · crackedSTA 663 VAPOR BARRIER UPPER FWD SIDE ATTACH ANGLE CRACKED AT LBL 10 ; / REMOVED FASTENERS LOWER SIDE ANGLE VAPOR STA. 663 LBL 10 AS PER SRM 51-40-02-0G-0; [04] VERIFIED 2 & 3; [05] REMOVED FASTENERS FOR REPAIR IAWB737-700 SRM 51-40-02-0G-0 AND 57-10-10-2R-5 RESDR SWAA2021100414722Channel · corrodedAFT CARGO COMPARTMENT STA 727 TO STA 747 LBL 24 STR 25R Z-CHANNEL SPOTS OF CORROSION ; / [01] REMOVED CORROSION ON AFT CARGO ZEE CHANNEL AT STA 727 THROUGH STA 747 LBL 24 AS PER B737-700 SRM 51-10-02-0G-0.; [02] VERIFIED STEP 1; [03] PERFORMED UT THICKNESS INSSDR SWAA2021100414715Light · crackedEXIT SIGN AT FWD GALLEY G1 BASE IS CRACKED ; / [01] REMOVED AND REPLACED EXIT SIGN AT FWD GALLEY G1 AS PER B737-700 AMM 33-51-01-960-802; [02] VERIFIEDSDR SWAA2021100414711Light · crackedEXIT SIGN AT AFT GALLEY 4 BASE IS CRACKED ; / [01] REMOVED AND REPLACED EXIT SIGN AT AFT GALLEY 4 AS PER B737-700 AMM 33-51-01-960-802.; [02] VERIFIEDSDR SWAA2021100414710Light · crackedEXIT SIGN AT FWD L1 BASE IS CRACKED ; / [01] REMOVED AND REPLACED EXIT SIGN AT FWD L1 AS PER B737-700 AMM 33-51-01-960-802.; [02] PARTS VERIFIED; [03] VERIFIED 1 & 2SDR SWAA2021100414706Baffle · crackedFWD CARGO COMPARTMENT CLIP CRACKED AT STA 400 AND S-25L (UNDER ZEE ANGLE) ; / [01] REMOVED CLIP AND INTERCOSTAL CRACKER AT FWD. CARGO COMPARTMENT STA. 400 TO STA. 420 AND S-25L IAW B-737-700 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW BAFFLE AND CLIP PER SDR SWAA2021100426165None · crackedFWD CARGO COMPARTMENT CLIP CRACKED AT STA 400 AND S-25L (UNDER ZEE ANGLE) ; / [01] REMOVED CLIP AND INTERCOSTAL CRACKER AT FWD. CARGO COMPARTMENT STA. 400 TO STA. 420 AND S-25L IAW B-737-700 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW BAFFLE AND CLIP PER SDR SWAA2021100414707Gusset · crackedFWD CARGO GUSSET AT STA 500D AND S-19L INNER CURVATURE CRACKED ; / [01] REMOVED GUSSET AT STA. 500D AND S-19L FWD CARGO AS PER SRM 51-40-02-0G-0; [02] LOCATED AND DRILL NEW GUSSET AS PER SRM 51-40-05-0G-0; [03] OK TO INSTALL NEW GUSSET; [04] INSTALLED FWD CARGSDR SWAA2021100414708Gusset · crackedFWD CARGO GUSSET AT STA 500D AND S-19R INNER CURVATURE CRACKED ; / [01] REMIOVED GUSSET FROM FWD CARGO AS PER SRM 51-40-02; [02] LOCATED AND DRILLED NEW GUSSET PER SRM 51-40-05-OG-0; [03] VERIFIED 1 & 2; [04] OK TO INSTALL NEW GUSSET; [05] INSTALLED GUSSET PERSDR SWAA2021100413963None · crackedINSPAR RIB ASSY 4 (STAB STA 120.30); STIFFENER 3 CRACKED ; / [01] PERFORMED HFEC INSP. ON INSPAR RIB ASSY 4 (STAB. STA 120.30) STIFFENER 3 IAW B737 NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED. EQUIP: NORTEC 600 CAL DUE: 10/21 B/C 166317; [02] PERFORMED LAYOUSDR SWAA2021100413962None · crackedINSPAR RIB ASSY 4 (STAB STA 120.30); STIFFENER 2 CRACKED ; / [01] PERFORMED HFEC INSP. ON INSPAR RIB ASSY 4 (STAB STA 120.30) STIFFENER 2 IAW B737 NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED. EQUIP: NORTEC 600 B/C 166317 CAL DUE: 10/21; [02] PERFORMED LAYOUTSDR SWAA2021031756114Battery · failedEMERGENCY LIGHT BATTERY'S FAILED CAPACITY CHECK AT LOCATIONS M1669; M1672; M1673; M1675; M1668 / REMOVED AND REPLACED EMERGENCY LIGHT BATTERY'S AT LOCATIONS M1669; M1672; M1673; M1675; M1668 PER AMM. 33-51-06 REFERENCING DWG-33500005SDR SWAA2020112432098Ballast · inoperativeCABIN RT OVER WING EXIT LIGHT INOPERABLE UNDER SIGN. R & R CABIN RT OVER WING EXIT LIGHT BALLAST, PER MM 33-21-00.SDR SWAA2020040235190Rivet · looseFWD CABIN FWD SERVICE DOOR ESCAPE SLIDE COVER FWD GIRT BAR HANGER LOOSE (SHEARED RIVET) / REMOVED AND REPLACED RIVET IAW SRM 51-40-02SDR SWAA2019100877640Bulb · unsecureDURING DESCENT FLIGHT ATTENDANTS AND PASSENGERS REPORTED BURNING SMELL IN AFT CABIN/GALLEY AREA. LASTED APPROXIMATELY 5 MINUTES, THEN WENT AWAY. FOUND BULB NOT SECURED IN LIGHT ASSEMBLY. CORRECTLY SECURED BULB PER AMM.SDR SWAA2022032308304Strip · corrodedAFT CARGO FWD R/H FLOOR TO SIDEWALL CAP STRIP SHOWS SIGNS OF CORROSION. / R&R'D R/H FLOOR TO SIDEWALL CAP STRIP PER AMM 25-52-06.SDR SWAA2022032308305Strip · corrodedAFT CARGO COMPARTMENT R/H MIDDLE FLOOR TO SIDEWALL CAP STRIP SHOWS SIGNS OF CORROSION. / R&R'D R/H MIDDLE FLOOR SIDEWALL CAP STRIP PER AMM 25-52-06.SDR SWAA2022032308306Strip · corrodedAFT CARGO COMPARTMENT FWD L/H FLOOR TO SIDEWALL CAP STRIP SHOWS SIGNS OF CORROSION. / R&R'D L/H FWD FLOOR SIDEWALL CAP STRIP PER AMM 25-52-06.SDR SWAA2022032308307Strip · corrodedAFT CARGO COMPARTMENT L/H MIDDLE FLOOR TO SIDEWALL CAP STRIP SHOWS SIGNS OF CORROSION. / R&R'D L/H MIDDLE FLOOR SIDEWALL CAP STRIP PER AMM 25-52-06.SDR SWAA2022032308308Strip · corrodedAFT CARGO COMPARTMENT L/H AFT FLOOR TO SIDEWALL CAP STRIP SHOWS SIGNS OF CORROSION. / R&R'D L/H AFT FLOOR SIDEWALL CAP STRIP PER AMM 25-52-06.SDR SWAA2022032308310Strip · corrodedAFT RIGHT CAP STRIP IN AFT CARGO PIT IS CORRODED BEYOND LIMITS. / REMOVED AND REPLACED RIGHT AFT CAP STRIP IAW SRM 51-10-02.SDR SWAA2019091636894Stringer · crackedLT WING #7 HOLE ON VERTICAL ROW FROM TOP INBOARD OF PYLON CRACKED IN THE HORIZONTAL STIFFENER. REPAIRED STRINGER PER SRM.SDR SWAA2022031608292Floor Support · corrodedSUPPORT CHANNEL (1)141A5211 UNDER FLIGHT DECK FLOORBOARD 211AF HAS SEVERAL SURFACE CORRODED AREAS. / REMOVED AND REPLACED SUPPORT CHANNEL 141A5211-1 IAW SRM 51-40-02 AND EA#1-753-35563.SDR SWAA2019092437113Floor Support · corrodedFLOOR SUPPORT CORRODED AT BS 270, BL 0 SEVERAL AREAS. (ENTRY TO THE FLIGHT DECK) REPAIRED FLOOR SUPPORT PER EA.SDR SWAA2022031608285Fairing · cracked#1 ENG. I/B T/R SLEEVE; KRUGER FLAP AFT DEFLECTOR FAIRING CRACKED. / REMOVED AND REPLACED FAIRING PER REF SRM51-40-02. SEE TASKS FOR ADDITIONAL SIGN OFFS.SDR SWAA2022030108276Wedge · delaminatedL/H WING OUTBOARD TRAILING EDGE FLAP HAS SMALL AREA OF DELAM ON INBOARD AFT CORNER. / REMOVED DAMAGE AND ACCOMPLISHED REPAIR TO FLAP REF SRM 57-53-01-2R-4. RESTORED FINISH TO AREA REF AMM 51-21-99.SDR SWAA2019091236825Seat Track · corroded#1 SEAT TRACK CORRODED IN CHANNEL AT BS 727A+11. R&R SEAT TRACK PER SRM.SDR SWAA2022031808230Panel · delaminatedRIGHT WING PANEL 621LB HAS CORNER DELAMINATION. / REPAIRED PER SRM 51-70-04.SDR SWAA2019091236823Plate · crackedLT WING WIGGLE PLATE CRACKED AT RSS 273. R&R WIGGLE PLATE PER SRM.SDR SWAA2018122727916Window · arcedAIR RETURN/EMERGENCY DECLARED, L1 COCKPIT WINDOW PANE ARCED AND CRACKED. R&R L1 WINDOW ASSY PER MM.SDR SWAA2018061822790Slide · out of positionR2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.SDR SWAA2018022620018Fitting · looseL1 DOOR EMERGENCY EVAC SLIDE LT RETENTION CLIP LOOSE. R&R GIRT BAR CLIP ASSEMBLY IAW SRM.
Back to N225WN