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 SWAA2017101016979Pump · low pressureDIVERSION, DURING CLIMB ENGINE 1 A HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. COMPLIED WITH QRH A QUANTITY DROPPED TO 35%. R&R NR 1 EDMP PER MM.SDR SWAA2017092116494Battery Pack · dischargedLT EMERGENCY EXIT LIGHT INOP BETWEEN ROW 9 TO ROW 12. R&R BATTERY PACK IAW AMM.SDR SWAA2017092016492Battery Pack · dischargedEMERGENCY LIGHTS BATTERY PACK M1670 INOP. R&R BATTERY PACK IAW MM.SDR SWAA2022013108539Scuff Plate · crackedFWD CARGO COMP FWD CORNER SCUFF PLATE CRACKED / SCUFF PLATE FWD OF FWD CARGO WAS REPAIRED IN THE BACK SHOP W/O 36297-8100-0001 P/N 143A8333-1 E.A 1-A53-2076 REV: 11SDR SWAA2017091916424Light · brokenFORWARD LAV EMERGENCY LIGHT BROKEN. R&R LIGHT IAW AMM.SDR SWAA2017091216283Housing · damagedPASSENGER CABIN SIDEWALL 232YHW EMERGENCY EXIT SIGN HOUSING DAMAGED. R&R SIGN HOUSING IAW AMM.SDR SWAA2017091416333Rib · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT HSS 95.96. R & R THE RIB IAW SRM AND DWG.SDR SWAA2017091216282Stiffener · crackedRT HORIZONTAL STABILIZER AFT VERTICAL STIFFENER CRACKED AT STAB STATION 129.50, FORWARD OF AFT SPAR. REPAIRED STIFFENER IAW SRM.SDR SWAA2017091216281Stiffener · crackedRT HORIZONTAL STABILIZER 3RD VERTICAL STIFFENER CRACKED AT STAB STATION 92.70, AFT OF FRONT SPAR. REPAIRED STIFFENER IAW SRM.SDR SWAA2017091216280Stiffener · crackedRT HORIZONTAL STABILIZER 2ND VERTICAL STIFFENER CRACKED AT STAB STATION 92.70, AFT OF FRONT SPAR. REPAIRED STIFFENER IAW SRM.SDR SWAA2017091216279Stiffener · crackedRT HORIZONTAL STABILIZER 1ST VERTICAL STIFFENER CRACKED AT STAB STATION 92.70 AFT OF FRONT SPAR. REPAIRED STIFFENER IAW SRM.SDR SWAA2017091216227Rib · crackedLEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.70, 38 INCHES AFT OF THE FRONT SPAR. REPAIRED THE RIB IAW SRM.SDR SWAA2017091216225Rib · crackedLEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.70, 26 INCHES AFT OF FRONT SPAR. REPAIRED THE RIB IAW SRM.SDR SWAA2017091216223Rib · crackedLEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.70, 20 INCHES AFT OF FRONT SPAR. REPAIRED RIB IAW SRM.SDR SWAA2017091216222Rib · crackedLEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.70, 10 INCHES AFT OF FRONT SPAR. REPAIRED THE RIB IAW SRM.SDR SWAA2017082915959Support Bracket · crackedLT SIDE OUTER FUSELAGE SUPPORT STRUCTURE FOR WING TO BODY ACCESS PANEL FAIRINGS 191AL AND 195AL SUPPORT BRACKET CRACKED AT BS 500D, BETWEEN STR 18L TO STR 19L. R&R BRACKET IAW SRM & DWG.SDR SWAA2017091216278Floorbeam · corrodedFLOORBEAM CORRODED AT BS 328, BETWEEN BL 0 TO RBL 64. REPAIRED T-CHORD PER SRM.SDR SWAA2022020108494Intercostal · crackedSUPPLEMENTAL INFORMATION: PASS CABIN FLOOR; 3 CRACKS AT FASTENER HOLES ON UPPE R FLANGE OF INTERCOSTAL BETWEEN BS 5OOD AND BS 520. AT BL0. / REMOVED; LOCATED AND CRILLED AND INSTALLED NEW ANLGE AT PASS CABIN FLOOR STA: 500D AND 520 BL-O; AND APP LIED CIC AREA SDR SWAA2022020108468Balance Weight · corrodedSUPPLEMENTAL INFORMATION: RUDDER BALANCE ARM WEIGHT IS CORRODED. / REMOVED AND INSTALLED NEW RUDDER BALANCE ARM WEIGHT IAW BOEING CMM CHAPTER 55-40-09 STEP (3) WEIGHT WN49 06SDR SWAA2022020108456Floor Panel · delaminatedCABIN FLOORBOARD 221 DF HAS TOP PLY DE-LAM (MISSING FIBER STRANDS) / REPAIRED FRAYED FIBERS IAW SRM 53-00-50-2R-11SDR SWAA2022020108457Intercostal · crackedPASSENGER CABIN INTERCOSTAL CRACKED AT STA 328-12' RBL 31. / REMOVED CRACKED INTERCOSTAL AT STA 328-12'; DRILLED AND INSTALLED NEW NACHINED INTERCOSTAL I/A/W BOEING DRAWING 141A5410; REVA AND B737 SRM 51-40-02; PARA 7.D. INSTALLED 2 EA NUTPLATES FOR FLOORBOARDSDR SWAA2022020108458Floor Panel · delaminatedPASSENGER CABIN FLOOR BOARD 221BF TOP LAYER DELAMED / REPAIR CABIN FLOORBOARD 221BF TOP LAYER IAWSRM53-00-50 REPAIR 11; PG 1.SDR SWAA2022020108459Floor Panel · delaminatedPASSENGER CABIN FLOOR BOARD 221CF TOP LAYER DELAMED / REPAIRED TOP LAYER ON FLOOR PANEL 221CF IAW SRM 53-00-50-2R-11 REPAIRIIISDR SWAA2022020108462Floor Panel · delaminatedPASSENGER CABIN FLOOR BOARD 221EF TOP LAYER DELAMED / REPAIRED UPPER FACE SHEET ON FLOORBOARD 221EF IAW SRM 53-00-50SDR SWAA2022020108464Floor Panel · delaminatedPASSENGER CABIN FLOOR BOARD 221FF TOP LAYER DELAMED / REPAIRED FRAYED TOP LAYER ON PANEL 221FF IAW SRM 53-00-50-2R-11 REPAIR 11 A83844SDR SWAA2022020108465Floor Panel · delaminatedPASSENGER CABIN FLOOR BOARD 221GF TOP LAYER DELAMED / REPAIRED TOP LAYERS ON FLOORPANEL 221GF IAW SRM 53- 00-50-2R-11 REPAIR 11SDR SWAA2017091816365Floorbeam · corrodedFLOORBEAM CORRODED AT BS 986, BETWEEN RBL 38 TO RBL 48. REPAIRED FLOOR BEAM IAW SRM AND EA.SDR SWAA2017090516102Crease Beam · corrodedLT AFT CREASE BEAM CORRODED BETWEEN BS 947 TO BS 987. R&R CREASE BEAM IAW SRM AND DWG.SDR SWAA2022020108425Balance Weight · corrodedRUDDER BALANCE ARM WEIGHT IS CORRODED. / REMOVED AND INSTALLED NEW RUDDER BALANCE ARM WEIGHT IAW BOEING CMM CHAPTER 55-40-09 STEP (3) WEIGHT WN49 06SDR SWAA2017091816364Crease Beam · corrodedAFT GALLEY DOOR CREASE BEAM CORRODED ON UPPER AND LOWER SURFACE. R&R CREASE BEAM IAW DWG AND SRM.SDR SWAA2017082915962Support Bracket · crackedFUSELAGE LOWER LOBE KEEL BEAM SUPPORT BRACKET CRACKED AT BS 546, LBL 5. R&R BRACKET IAW SRM.SDR SWAA2022020108404Cargo Track · corrodedSUPPLEMENTAL INFORMATION: AFT PIT TIE DOWN TRACK/FLOOR SUPPORT ANGLE; FROM STA 786 TO 867 RH SIDE; HAS MULTIPLE AREAS OF CORROSION. / EVALUATED CORROSION DEEPEST BLEND .022' FROM ORIGINAL .070' WITH .098' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-0SDR SWAA2022020108396Angle · corrodedAFT PIT RH Z ANGLE BETWEEN STA 727E AND 767 HAS CORROSION. / BLENDED OUT DAMAGE-ORIG MAT'L: .040'; MAT'L REMOVED: .012'; MAT'L REMAINING: .028'. BLENDOUT IS OUT OF LIMITS I/A/W B737 ARM 53-00-53-1A-2. REMOVED DAMAGED Z-ANGLE IN AFT PIT; R/H STA 727 TO STA 737;SDR SWAA2022020108400Strap · corrodedAFT PIT STA 772; LATERAL FLOOR PANEL SUPPORT STRAP/STRIP; HAS CORROSION ON UPPER AND LOWER SURFACES. / EVALUATED CORROSION PER B737-700 SRM 53-00-53. ORIGINAL THICKNESS= .070'. 100% MATERIAL LOSS NOTED.PART OUT OF LIMITS PER B737-700 SRM 53-00-53-1A-2 PARA 4A SDR SWAA2022020108410Strap · corrodedAFT CARGO PIT STA 887; LATERAL FLOOR SUPPORT STRAP H AS CORROSION. / REMOVED AND REPLACED THE AFT PIT STA 887 FLOOR SUPPO RT STRAP IAW B737-700 SRM 51-40-02-0G-0; STEP 7 AND DWG# 146A7500; REV.A.SDR SWAA2022020108412Baffle · crackedFWD CARGO COMPARTMENT BETWEEN STA 500B AND 500C HAS A CRACKED BAFFLE / REMOVED; LOVACTED; DRILLED AND INSTALLED NEW BAFFLE IN FORWARD CARGO PIT BETWEEN STA 500B AND 500C ON L/H SIDE UNDER '2' MEMBER;IAW BOEING 737 SRM 51-40-02-0G-0 STEP 4B; 51-40-05-0G-0 FIG 3SDR SWAA2022020108418Panel · delaminatedA/C RAM INLET PANEL 191BR DELAMINATED / REPAIRED 191BR DELAM IAW B737 SRM 51-20-04-2R-1 REV 62SDR SWAA2017090716174Floorbeam · corrodedAFT CARGO FLOORBEAM ANGLE CORRODED AT BS 772, RBL 7. REPAIRED THE FLOORBEAM IAW EA & SRM.SDR SWAA2017090516111Floor Support · corrodedAFT PIT FLOOR SUPPORT CORRODED ANGLE AT BS 772, RBL 13. REPAIRED ANGLE IAW SRM AND EA.SDR SWAA2017090516110Floor Support · corrodedAFT PIT FLOOR SUPPORT ANGLE CORRODED AT BS 772, LBL 12. R&R CHANNEL PER SRM AND EA.SDR SWAA2017090516109Floor Support · corrodedAFT PIT FLOOR SUPPORT ANGLE CORRODED AT BS 772, LBL 8. R&R CHANNEL PER EA.SDR SWAA2017083015999Angle · crackedFORWARD CARGO BAY BAFFLE ANGLE CRACKED AT BS 500C, LBL 25. R & R THE ANGLE IAW SRM AND DWG.SDR SWAA2017082915961Support Angle · corrodedAFT PIT FLOOR SUPPORT ANGLE CORRODED AT BS 772, RBL 2. REPAIRED ANGLE IAW SRM.SDR SWAA2017082915960Support Angle · corrodedAFT PIT STA 772 AT FLOOR SUPPORT ANGLE CORRODED AT BS 772, LBL 3. R&R ANGLE IAW SRM.SDR SWAA2022020108374Bracket · crackedLH WING FIXED TRAILING EDGE PANEL HAS CRACKED SEAL RETAINER BRACKET 11' INBD OF DEFLECTOR RIB. MARKED. / REMOVED CRACKED SEAL RETAINER BRACKET ON L/H WING FIXED TRAILING EDGE PANEL; 11' INBD OF DEFECTER RIB I/A/W SRM 51-40-02. LOCATED AND DRILLED FASTNER HOLESSDR SWAA2022020108375Frame · crackedR/H SIDE OUTER FUSELAGE SUPPORT STRUCTURE FOR WING TO BODY ACCESS PNL FAIRINGS 191AR AND 195AR STA 500D BETWEEN STR 18R AND 19R SUPPORT BRACKET IS CRACKED AS MARKED / REMOVED RH OUTER FUSELAGE SUPPORT STRUCTURE (FROME) IAW B737-700 SRM 51-40-02; VERIFIED FRAMESDR SWAA2022020108376Bracket · crackedFUSELAGE LOWER LOBE KEEL BEAM STA 546 RBL 5 SUPPORT BRACKET FOR LOWER LOBE ACCESS PNL# 192 E IS BROKEN AS MARKED / REMOVED AND REPLACED SUPPORT BRACKET AT STA 546 5 IAW SRM 51-40-05; SRM 51-40-02-0G-0; AND SRM 51-40-0G-0SDR SWAA2017090516065Plate · crackedLT WING WIGGLE PLATE CRACKED AT SHEARED FASTENER UNDER 551 GB. R&R PLATE ASSEMBLY PER SRM.SDR SWAA2022013108350Retainer · corrodedAFT CARGO COMPARTMENT DOOR FWD SURROUND CORNER RETAINER IS CORRODED. / REMOVED AND REPLACED AFT CARGO DOOR FWD SURROUND PLATE IAW B737 DRAWING 453A2611 REV C AND IPC 25-52-10-02 P/N 453A2611-1 ATAG A02753SDR SWAA2022013108351Retainer · corrodedAFT CARGO COMPARTMENT DOOR AFT SURROUND CORNER RETAINER IS CORRODED. / EVALUATED CORROSION ON AFT CARGO; AFT SURROUND CORNER. FOUND 100% MATERIAL LOSS. REMOVED AND REPLACED REVEAL RETAINER ON SHELF I/A/W S/W 53-00-53-1A-1
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