N282WN
Service difficulty reports · 298
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 = 'N282WN' 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 = 'N282WN' 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 SWAA2021050468780Battery Pack · inoperativeLH OVER WING EMERGENCY EXIT LIGHTS INOP. / R&R'D LH OVER WING EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06.OPS CHECK GOOD IAW AMM 33-51-06SDR SWAA2021050468755Skin · crackedLT HORIZONTAL STAB LOWER SKIN FASTENER HOLE HAS A CRACK INDICATION 18TH HOLE AFT ON I/B ROW AT RIB STA 120.30. / REPAIRED LT HORIZONTAL STAB LOWER SKIN FASTENER HOLE ; 8TH HOLE AFT ON I/B ROW AT RIB STA 120.30 PER EA 21-155-01138SDR SWAA2021050468753Stiffener · crackedLT HORIZ STAB #4 RIB STA 120.30 #2 VERTICAL STIFFENER CRACKED. / ACQUIRED NEW RIB FROM STOCK FOR REPLACEMENT. NEW RIB WILL BE INSTALLED ON NON ROUTINE # G776065.SDR SWAA2021050468696Seat Track · wornCABIN #2 SEAT TRACK HAS DEEP WEAR ON UPPER CROWN AT STA 520. / REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1. REMOVED AND REPLACED SEAT TRACK FROM STA 500C+10 TO STA 520 PER SRM 53-0052-2R-4 AND EA 1-A53-11779; CORRECTED NRC TO MAJOR REPAISDR SWAA2021050468695Seat Track · wornCABIN #1 SEAT TRACK HAS DEEP WEAR ON UPPER CROWN AT STA 520. / REMOVED DAMAGE PER SRM 53-00-52-1A-1 AND FOUND TO BE OUT-OF-LIMITS PER SRM 53-00-52-1A-1. REMOVED AND REPLACED SEAT TRACK STA 500C+10 TO STA 520 PER SRM 53-00-52-2R-4 AND EA 1-A53-11779.SDR SWAA2021050468694Seat Track · corrodedCABIN #2 SEAT TRACK HAS CORROSION ON UPPER AND LOWER SURFACE OF CROWN AT STA 685+12. / REMOVED AND REPLACED SEAT TRACK #2 STA 538-727B IAW SRM 51-40-02. P/N 144A5350-1 TRACK CROWN INSTALLED.SDR SWAA2021050468678Stiffener · crackedHFEC VERIFIED LT HORIZ STAB #4 RIB STA 120.30 #4 VERTICAL STIFFENER CRACKED. / ACQUIRED NEW RIB FROM STOCK FOR REPLACEMENT. NEW RIB WILL BE INSTALLED ON NON ROUTINE # G776065.SDR SWAA2021050468677Stiffener · crackedHFEC VERIFIED LT HORIZ STAB #4 RIB STA 120.30 #3 VERTICAL STIFFENER CRACKED. / REMOVED AND REPLACED #4 RIB ON LEFT HAND ELEVATOR PER SRM 55-10-09 REF TASKS AND WHIPS FOR ALL RELATED STEPSSDR SWAA2021050468676Rib · crackedRIGHT HORIZONTAL INTERNAL RIB IS CRACKED AT STAB STA 120.30 VERTICAL RIB #3. THE CRACK WAS VERIFIED HFEC. / REPAIRED RIGHT HORIZONTAL STAB. INTERNAL RIB AT STAB STA 120.30 VERTICAL RIB #3 PER SRM 55-10-09-2R-4SDR SWAA2021050468668Floor Panel · deterioratedFLOOR PANEL 242AF HAS PUNCTURE AND FOAM ON BOTTOM IS DETERIORATED / REMOVED AND REPLACED FLOORBOARD 242AF IAW AMM 53-21-00SDR SWAA2021050468669Floor Panel · deterioratedFLOOR PANEL 242BF FOAM ON BOTTOM OF PANEL IS DETERIORATED / REMOVED AND REPLACED FLOORBOARD 242BF IAW AMM 53-21-00SDR SWAA2021050468670Floor Panel · deterioratedFLOOR PANEL 241BF FOAM ON BOTTOM OF PANEL IS DETERIORATED / REMOVED AND REPLACED FLOORBOARD 241BF IAW AMM 53-21-00SDR SWAA2021020144954Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE @ ROWS 9 & 11 ABC & EXTERIOR WING GND ILLUMINATION LT & RT. R & R EMERGENCY LT BATTERY PACK M1670 PER AMM 33-51-06.SDR SWAA2020121737081Lamp · inoperativeRT FUSELAGE EMERGENCY EXIT LIGHT INOPERABLE. RE-LAMPED RT AFT LOWER FUSEAGE EMERGENCY EXIT LIGHT, PER AMM 33-51-04. OPERATIONS CHECKS GOOD.SDR SWAA2020121737080Lamp · inoperativeLT FUSELAGE EMERGENCY EXIT LIGHT INOPERABLE. RE-LAMPED LT AFT LOWER FUSELAGE EMERGENCY EXIT LIGH LIGHT, PER AMM 33-51-04. OPERATIONS CHECKS GOOD.SDR SWAA2020102324536Lens · dislodgedAFT SERVICE DOOR EMERGENCY LIGHT COVER WILL NOT STAY SECURE, OVER THE DOOR. REMOVED & REPLACED AFT SERVICE DOOR EMERGENCY LIGHT ASSEMBLY, PER AMM 33-51-01 CL 56810 (CLOSING DMA 0264419).SDR SWAA2020100720064Light · inoperativeLT AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERABLE. RELAMPED LIGHT AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT, PER AMM 73-51-00. OPERATIONS CHECK GOOD.SDR SWAA2020091015112Bulkhead Web · crackedLEFT WHEEL WELL FORWARD WALL VAPOR BARRIER CRACKED. LEFT WHEEL WELL FORWARD WALL VAPOR BARRIER CRACKED. PERFORMED INTERIM REPAIR, PER EA NR 1-A57-13410R1. THIS IS A TIME LIMITED REPAIR TO REINSPECT THE EFFECTED AREA EVERY 100 CYCLES AND TO PERFORM A PERMANESDR SWAA2021070712837Panel · bentEXTERNAL POWER RECEPLACLE PANEL BENT. WILL NOT CLOSE MOD / C/W DVI OF GRD POWER RECEPTACLE DOOR PER E.A. NO 20-153-01597 REPLACED LATCHES AND SECURED GRD POWER RECEPTACLE DOOR. PERMANENT REPAIR LIMIT ACTION REQUIRED: ACCOMPLISH A PERMANENT REPAIR (REF 737-700 SDR SWAA2020062393529Handle · looseAFT SERVICE DOOR INTERIOR HANDLE IS LOOSE. TIGHTENED AFT SERVICE DOOR HANDLE PER MM. 52-13-00SDR SWAA2020032634444Module · faultyAT CRUISE FLIGHT LEVEL 400 WE HAD A CABIN ALTITUDE LIGHT AS WELL AS A CABIN ALTITUDE WARNING HORN. WE STARTED AN EMERGENCY DESCENT AND COMPLIED WITH THE CABIN ALTITUDE WARNING EMERGENCY DESCENT CHECKLIST PER THE QRH. / DUE TO RESCENT PRESSURIZATION ISSUES PERFSDR SWAA2020032634129Outflow Valve · faultyAT CRUISE FLIGHT LEVEL 400 WE HAD A CABIN ALTITUDE LIGHT AS WELL AS A CABIN ALTITUDE WARNING HORN. WE STARTED AN EMERGENCY DESCENT AND COMPLIED WITH THE CABIN ALTITUDE WARNING EMERGENCY DESCENT CHECKLIST PER THE QRH. / DUE TO RESCENT PRESSURIZATION ISSUES PERFSDR SWAA2020032634445Control Valve · faultyAT CRUISE FLIGHT LEVEL 400 WE HAD A CABIN ALTITUDE LIGHT AS WELL AS A CABIN ALTITUDE WARNING HORN. WE STARTED AN EMERGENCY DESCENT AND COMPLIED WITH THE CABIN ALTITUDE WARNING EMERGENCY DESCENT CHECKLIST PER THE QRH. / DUE TO RESCENT PRESSURIZATION ISSUES PERFSDR SWAA2020032634446Control Valve · faultyAT CRUISE FLIGHT LEVEL 400 WE HAD A CABIN ALTITUDE LIGHT AS WELL AS A CABIN ALTITUDE WARNING HORN. WE STARTED AN EMERGENCY DESCENT AND COMPLIED WITH THE CABIN ALTITUDE WARNING EMERGENCY DESCENT CHECKLIST PER THE QRH. / DUE TO RESCENT PRESSURIZATION ISSUES PERFSDR SWAA2020031942569Controller · malfunctionedPRESSURIZATION EVENT, CABIN ALT WARN HORN AT FL 410. / R&R #2 CPC AND RESECURED LOOSE OFV CONNECTORSDR SWAA2020010840259Control Module · faultyDECLARED EMERGENCY------------------------------------------------CABIN ALTITUDE WARNING HORN AND LIGHT ILLUMINATED AT CRUISE AT FL400. CABIN ALTITUDE MAX 11,000. SELECTED MANUAL AND PRESSURE RETURNED TO NORMAL. / R&R CABIN PRESSURE CONTROL MODULE IAW AMM.SDR SWAA2019120239227Outflow Valve · faultyCABIN ALT WARNING HORN CAME ON AT 37,000. / R&R NET OUTFLOW VALVE ASSEMBLY PER AMM.SDR SWAA0144050132614Attach Angle · crackedRT VAPOR BARRIER ATTACH ANGLE CRACKED AT BS. 663, RBL 9.5, 2ND FASTENER HOLE FROM INBOARD SIDE. REPAIRED ATTACH ANGLE IAW EA.SDR SWAA2019050932503Web · corrodedAFT CARGO BAY WEB CORRODED AT FASTENER HOLES BETWEEN BS. 747 TO BS. 767, STR. 25R. R&R WEB IAW SRM & DWG.SDR SWAA2022030727473Intercostal · crackedPASSENGER CABIN FLOOR SUPPORT INTERCOSTAL AT STA 500D TO STA 520 BL0; UPPER FLANGE IS CRACKED / REMOVED PASSENGER CABIN FLOOR SUPPORT INTERCOSTAL AT STA 500D TO STA 520 BL0 UPPER FLANGE IAW SRM 51-40-02-0G-0 FABRICATED PN # 143A5410-11 ON SHOP TRAVELER WO#3926SDR SWAA2019052032832Support Angle · corrodedWING BOX CENTER SECTION UPPER WEB SUPPORT ANGLE CORRODED AT BS. 663, RBL 47. REPAIRED ANGLE IAW EA.SDR SWAA2022030727467Floor Panel · delaminatedCABIN FLOOR PANEL 242NF DELAM TOP SIDE (MARKED) / REPAIRED CABIN FLOOR PANEL 242NF OF DELAM ON TOP SIDE (AS MARKED) IAW B737-700 SRM 53-00-50-2R-0 REV 67 AND B737-700 SRM 53-00-50-2R-1 REV 67 A44553; A02940 A11445SDR SWAA2022030727466Floor Panel · damagedCABIN FLOOR PANEL 242MF EDGE CRUSHED TOP SIDE (MARKED) / REPAIRED CABIN FLOOR PANEL 242 MF EDGE CRUSHED TOP SIDE (MARKED) IAW B737 SRM 53-00-50-2R-9. A02941; A36551; A09245; A09940.SDR SWAA2022030727465Floor Panel · delaminatedCABIN FLOOR PANEL 242LF DELAM TOP SIDE (MARKED) / REPAIRED CABIN FLOOR PANEL 242LF IAW B737-700 SRM 53-00-50-2R-1 REV 67 PARA 1-A; 53-00-50-2R-1 REV 67 PARA 3A;C-F; 53-00-50-2R-1 REV 67 TABLE 201; 53-00-50-2R-1 REVF 67 TABLE 201; 53-00-50-2R-1 REV 67 REPAIR 1 SDR SWAA2022030727463Floor Panel · puncturedCABIN FLOOR PANEL 241UF 3EA PUNCTURES TOP SIDE (MARKED) / EVALUATED; PREPPED; CLEANED AND REPAIRED 3 PUNCTURE DAMAGES TO UPPER FACESHEET ON FLOORBOARD 241 UF IAW B737 SRM 53-00-0-2R-2; PAR (3) REV 67.SDR SWAA2022030727461Floor Panel · delaminatedCABIN FLOOR PANEL 241SF DELAM TOP SIDE (MARKED) / REPAIRED CABIN FLOOR PANEL 241 SF DELAM TOP SIDE (MARKED) IAW B737 SRM 53-00-50-2R-1. CURED IN OVEN FOR 5 HRS. IN AT 9AM - 08T AT 2PM. A02940; A11445; A44583.SDR SWAA2022030727458Floor Panel · puncturedCABIN FLOOR PANEL 241RF PUNCTURED TOP SIDE (MARKED) / REPAIRED PUNCTURE ON CABIN FLOOR PANEL 241RF IAW B737 SRM 53-00-50-2R-2 REV 67SDR SWAA2022030727455Floor Panel · puncturedCABIN FLOOR PANEL 241NF PUNCTURED (MARKED) / EVALUATED; PREPPED; CLEANED AND REPAIRED PUNCTURE DAMAGE ON UPPER FACESHEET ON FLOORBOARD 241NF IAW B737 SRM 53-00-50-2R-2; PAR (3) REV 67SDR SWAA2019050732377Floorboard · delaminatedSUPPLEMENTAL INFORMATION, CABIN FLOOR PANEL 241MF DELAMINATED, (BETWEEN BS. 727B TO BS. 887). R&R FLOOR BOARD IAW SRM.SDR SWAA2019050232187Rib · crackedRT HORIZONTAL STABILIZER LEADING EDGE PANEL 341B 4TH RIB FROM INBOARD EDGE CRACKED AT FASTENER. R&R RIB IAW DWG AND SRM.SDR SWAA2019050232186Rib · crackedRT HORIZONTAL STABILIZER LEADING EDGE PANEL 341B 3RD RIB FROM INBOARD EDGE CRACKED AT FASTENER. R&R RIB IAW DWG AND SRM.SDR SWAA2022030727435Door · corrodedLAV SERVICE DOOR 145AL CORROSION AROUND GROUDING STUD FOR BONDING JUMPER. / REMOVED CORROSION ON LAV SERVICE DOOR; CORROSION OUT OF LIMITS; RECEIVED NEW PANEL P/N: 146A7410-6 TAG # XD0638; TREATED; PRIMED; TOP COATED; AND INSTALLED REF B737 SRM 51-40-02-0G-0.SDR SWAA2022030727449Floor Panel · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140CF HAS SEVERAL AREAS OF CORROSION AROUND PERIMETER OF PANEL. MARKED AREAS / REMOVED CORROSION AND FOUND AFT CARGO FLOOR PANEL 140CF TO BE OUT OF LIMITS WITH ORIG. 080 LOSS .017 AND REMAINING .063 USING AAR TOOL #32209 DUE 4SDR SWAA2022030727411Strap · corrodedAFT CARGO COMPARTMENT; STA 887; STR 27L-25R; FLOOR BOARD SPLICE STRAP SEVERELY CORRODED / AFT CARGO STA 887 FLOOR BOARD STRAP DOES NOT HAVE ENTRIES IN SRM PART REPAIRABLE BY REPLACEMENT. REMOVED AND REPLACED-39 SPLICE STRAP PER SRM 51-40-02-0G-0 AND DWG 147A75SDR SWAA2022030727418Strap · corrodedFWD CARGO COMP.PANEL STRAP FOR 120AF/122AW CORRODED ON BACK SIDE (MARKED) / REPLACED ON BENCH CARGO STRAP 453A1611-5 FOR 120AF/122AW IAW DWG. 453A1600SDR SWAA2022030727410Strap · corrodedAFT CARGO COMPARTMENT; STA 847+2; STR 25R; STRAP I/B OF SHIELD HAS CORROSION ON UNDERSIDE / REMOVED CORROSION ON AFT CARGO STR 25R STA 847+2 NUT PLATE STRIP IAW B737-700 SRM 51-00-02-0G-0. FOUND TO BE OUT OF LIMITS. 'NO LIMITS FOUND' IAW SRM 53-00-53-1A-2. ORISDR SWAA2019051332576Cargo Track · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT STRINGER CORRODED ON UPPER LOWER SURFACES AROUND AT BS. 927+18, STR. 26R. R&R CARGO TRACK PER SRM AND DWG.SDR SWAA2019050932502Shield · corrodedAFT CARGO COMPARTMENT SHIELD ABOVE STRINGER CORRODED ON UNDERSIDE AT BS. 847+2, STR. 25R. R&R SHIELD IAW SRM & DWG.SDR SWAA2022030727392Frame · corrodedPASSENGER CABIN; STA 706 RH MAIN FRAME HAS CORROSION AT EDGE OF INNER FLANGE 5' ABOVE FLOOR; MARKED. / REMOVED CORROSION AT STA 706 R/H AFT FITTING 144A1561-2 AT EDGE OF FLANGE 5' ABOVE FLOOR; IAW B737-700 SRM 51-10-0G-00 PAR 15. .080' MATERIAL LOSS ON EDGE DASDR SWAA2022030727395Skin · corrodedAFT CARGO DOOR SURROUND STRUCTURE EXTERNAL SKIN BELOW CUTOUT HAS CORROSION AROUND FASTENER HOLES STA 797-842 RBL 27 / BLENDED AND REMOVED CORROSION AT AFT CARGO DOOR SURROUND EXTERNAL SKIN BELOW CUTOUT AROUND FASTENER HOLES ORG T .080' MAX MATERIAL LOSS OF .00
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