N912WN
Service difficulty reports · 270
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 = 'N912WN' 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 = 'N912WN' 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 SWAA2023091189433Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AAF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATE FLOOR PANEL PER SRM 53-00-50-2R-0. ATTACHED CURE SHEET TO THIS FAULT RECORD.;[02] VERIFIED COSDR SWAA2023091189423Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ADF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION #1;[03] VERIFIED MSDR SWAA2023091189436Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] REPAIRED AREAS OF PULLED STRANDS ON UPPER SKIN OF AFT FLOOR PANEL 242TF IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.;[03] VERIFIED MEASUREMENTS TABLE.SDR SWAA2023091189437Floor 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. ATTACHED CURE RECORDS TO THIS FAULT.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED MEASUREMENTSDR SWAA2023091388412Panel · crackedWING CENTER SECTION BREAK PANEL IS CRACKED AT FASTENER; BS 540; LBL 1; WL 207<[01] VERIFIED APPLICABILITY OF SRM 51-10-02-0G-0; NO DAMAGE LIMITS GIVEN IN SRM PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARA 9. REMOVED WING CENTER SECTION CRACK DAMASDR SWAA2023091388413Panel · crackedWING CENTER SECTION BREAK PANEL IS CRACKED AT FASTENER; BS 540; RBL 1; WL 207<[01] REMOVED AND REPLACED WING CENTER SECTION BREAK PANEL; BS 540; RBL 1- RBL 25; WL 207 IAW SRM 51-40-02-0G-0 AND DWG 143A0060;[02] VERIFIED MEASUREMENTS TABLE.<BR>VERIFIED CORRECTISDR SWAA2023091388414Attach Angle · crackedWING CENTER SECTION CABLE INTERCOSTAL ATTACH ANGLE IS CRACKED AT BS 685+11; RBL 24; WL 203<[01] NO DAMAGE LIMITS GIVEN IN SRM; PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9; FABRICATED NEW BRACKET FROM BAC1490-2782 7075-T0 CLAD .050 LOT# 148227SDR SWAA2023091388409Attach Angle · crackedWING CENTER SECTION CABLE INTERCOSTAL ATTACH ANGLE IS CRACKED AT BS 685+11; LBL 24; WL 203<[01] REMOVED CRACK DAMAGED BRACKET FROM BS 685+11 LBL 24 WL 203 IAW SRM 51-40-02-0G-0. NO DAMAGE LIMITS GIVEN IN SRM PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0SDR SWAA2023091188411Beam · corrodedWING CENTER SECTION INNER CHORD CREASE BEAM HAS CORROSION AT BS 616+22; LBL 63; WL 207<[01] UPDATE MEASUREMENTS AND STEPS 1-3;[02] REMOVED AND REPLACED WING CENTER SECTIN INNER CHORD CREASE BEAM AT 616+22; LBL 63; WL 207. IAW SRM 51-40-02-0G-0 AND BOEING DWG 1SDR SWAA2023091288122Seat Track · corrodedR/H CABIN SEAT TRACK HAS CORROSION ON TOP OF CROWN AND WELL; BS 380+6; 380+14; 400+12; 440+4; RBL 45; WL 208<[01] PARTIALLY COMPLETED STEP 1;[02] PARTIALLY COMPLETED STEPS 1 AND 2;[03] PARTIALLY COMPLETED STEPS STEP 5.<BR>UPDATES MEASUREMENTS TABLE;[04] UPDATESDR SWAA2023091288134Seat Track · corrodedR/H CABIN SEAT TRACK HAS CORROSION ON TOP OF CROWN AND WELL; BS 480+7; 597+13; 706+6; 727+14; RBL 25; WL 208 FAULT GENERATED IN ERROR. CORROSION BS ON SEPERATE TRACKS.<[01] FAULT RAISED IN ERROR. DAMAGE CORRECTED ON CCN: TTG8Q00MRHVJ AND TTG8Q00MRJS1;[02] VERISDR SWAA2023091288116Seat Track · corrodedR/H CABIN SEAT TRACK HAS CORROSION IN WELL; BS 500A+16; 706+6; 706+17; RBL 45; WL 208 FAULT GENERATED IN ERROR. CORROSION BS ON SEPERATE TRACKS.<[01] FAULT RAISED IN ERROR. DAMAGE CORRECTED ON CCN: TTG8Q00MRJAP AND TTG8Q00MRHJFE.;[02] VERIFIED CORRECTIVE ACTIOSDR SWAA2023091288117Seat Track · corrodedR/H CABIN SEAT TRACK HAS CORROSION IN WELL; BS 500+7; 500+16; 500A+18; 639+8; RBL 25; WL 208 FAULT GENERATED IN ERROR. CORROSION BS ON SEPERATE TRACKS.<[01] FAULT RAISED IN ERROR. DAMAGE CORRECTED ON CCN: TTG8Q00MRJJ5 AND TTG8Q00MRHVC.;[02] VERIFIED CORRECTIVESDR SWAA2023091188142Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-25R WL155. MARKED<[01] REPAIRED AS PER EA-23-153-02485.;[02] TASK CARD COMPLETE.;[03] VERIFIED MEASUREMENT TABLE.SDR SWAA2023091188143Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-26R WL153. MARKED<[01] VERIFIED COMPLETION TASK CARD AND MEASUREMENT TABLE.SDR SWAA2023091387635Rib · crackedLEFTT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 2ND VERTICAL STIFFENER IS CRACKED.<[01] OK TO INSTALL T- SECTION; ANGLE AND SHIM GIVEN;[02] VERIFIED MEASUREMENT TABLE.<BR>TASK COMPLETESDR SWAA2023091387636Stiffener · crackedLEFTT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED.<[01] OK TO INSTALL T- SECTION; ANGLE AND SHIM GIVEN;[02] REMOVED CRACK DAMAGE ON LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 129.SDR SWAA2023091186742Panel · debondedPANEL 194FR OUTER SKIN IS DISBONDED. (MARKED)<[01] PANEL 194FR DIS BOND REPAIRED IAW 51-70-05-2R-2;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023080786067Unknown · unknownBLEW #3 RH MLG TIRE ON TAKEOFF ROLL<[01] PERFORMED TIRE BURST CONDITIONAL INSPECTION PER AMM 05-51-54. DAMAGE DOCUMENTED ON LP# 2026258; 2026259; 2026260; 2026261 AND 2026262.SDR SWAA2023072080444Power Supply · failedEMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK @ 17ABC<[01] REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-06SDR SWAA2023061257325Battery Pack · inoperativeEMERGENCY LIGHTS AT 3DEF AND 6DEF INOP<[01] R&R FWD RH BATTERY PACK IAW AMM 33-51-06SDR SWAA2023051548022Floor Panel · crackedRAMP REPORTS AFT CARGO FLOOR PANEL 140 BF HAS A CRACK.<[01] INSPECTED AND FOUND CRACK TO BE MORE THAN 2 INCHES FROM EDGE. REPAIRED CRACK ON FLOOR PANEL IN REFERENCE TO AMM 25-52-01. OK FOR CONTINUED SERVICE.SDR SWAA2022110267132Assist Assy · brokenFWD DOOR ASSIST HANDLE BROKEN. / [01] R&R FWD ENTRY DOOR HANDLE REF AMM 52-11-32.SDR SWAA2022031182114Lens · inoperativeRH OVERWING LOWER EXIT SIGN LIGHTS INOP AND LENS DAMAGED / [01] RELAMPED AND REPLACED LENS IAW AMM 33-51-01SDR SWAA2022013164118Panel · elongated193D PANEL HAS ELONGATED FASTENER HOLES ; 193D PANEL HAS ELONGATED HOLES. / [01] ACCOMPLISH EA 22-153-00260 ASSIGNED AS A SUBTASK.; [02] COMPLIED WITH TSR 202200634SDR SWAA2022013164119Panel · elongated194E PANEL HAS ELONGATED HOLES ; 194E PANEL HAS ELONGATED HOLES. / [01] REMOVED AND REPLACED 194E PANEL PER SRM 51-40-02. REF TSR 202200632.SDR SWAA2021121350989Bracket · brokenSUPPLEMENTAL INFORMATION: GIRT BAR BRACKET ON FWD PASSENGER ENTRY ; GIRT AR RACKET ON FWD PASSENGER ENTRY DOOR ROKE OFF REF TTG8Q009NK81 / [01] INSTALLED FASTENERS IAW SRM 51-40-02.SDR SWAA2021120950628None · brokenSUPPLEMENTAL INFORMATION: GIRT BAR BRACKET ON FWD PASSENGER ENTRY DOOR BROKE OFF ; / [01] C/W EA 21-125-03628 ; MUST BE REPAIRED WITHIN 10 CYCLES.SDR SWAA2021091416474Slide · out of adjustCUSTOMER WALK- R2 DOOR GIRT CURTAIN GRABS THE BOTTOM WHEN CLOSING WHEN CLOSING. NEEDS ADJUSTMENT/REPOSITIONING ; / [01] READJUSTED Z FOLD ON R-2 DOOR ESCAPE SLIDE GIRT BAR AS PER B737-700 AMM 25-66-01-400-804; [02] VERIFIED STEP 1SDR SWAA2021091416131Retainer · brokenFWD CARGO DOOR ASSIST LANYARD HAS BROKEN CLIP ; / [01] REMOVED AND REPLACED FWD CARGO DOOR ASSIST LANYARD CLIP REF B 737-700 AMM 52-31-00-400-801; [02] VERIFIED STEP 1SDR SWAA2021091414617Intercostal · corroded***CORROSION*** FOUND CORROSION UNDER LT WING L/E PANEL 521DB ; / [01] REMOVED ACCESS PANELS FOR REPAIR #521CB;521EB;521FB AND 521GB AS PER B-737-700-AMM-57-41-02-000; [08] FABRICATED REPAIR Z ANGLE (-1) MATERIAL 0.100 THICK BARE ALUMINUM 2024-0 AS PER EA-21-1SDR SWAA2021091410885Angle · elongatedRIGHT VAPOR BARRIER WEB UPPER ANGLE HAS 12 HOLES THAT ARE ELONGATED ; / [01] PERFORMED HFEC ROTO INSP ON ELONGATED EXISTING FASTENER HOLES IAW B737 NDT PART 6; 51-00-00; PROCEDURE 16. NO CRACKS NOTED<BR>TOOL: NORTEC 600 B/C: 166317 DUE:10/12/2021<BR>TOOL: OLYMSDR SWAA2021091549683Gusset · crackedFWD. CARGO COMPT. AFT BLKH. STA 500D;STR. 18L;FOUND GUSSET CRACKED. ; / [01] REMOVED DAMAGE GUSSET AT FWD. CARGO COMPT. AFT. BLKH. STA. 500D; S-18L. PER B737-7 SRM 51-40-02-0G-0.; [02] VERIFIED STEP 1; [03] OK TO INSTALL GUSSET; [04] INSTALLED NEW GUSSET P/N 1SDR SWAA2021091409670Scuff Plate · crackedFWD CARGO DOOR AFT SCUFF PLATE CRACKED ; / [01] RECEIVED NEW SERVICEABLE AFT SCUFF PLATE CORNER; P/N:143A8331-4; PO # 1684224. ISSUE TAG : WN4833. THIS PLATE WILL BE INSTALLED 0N CARD TTG8Q0067XQY.; [02] VERIFIED STEP 1SDR SWAA2021091409645Bracket · crackedFWD CARGO COMPT L/H STA 500C STR 25 UNDER ZEE ANGLE BRACKET APPEARED CRACKED ; / [01] CRACK VERIFIED AT 'Z'-ANGLE BRACKET LOWER AREA AT FWD CARGO COMPARTMENT L/H STA 500C STR 25;IAW NDTM PART 6;51-00-00 PROCEDURE 23. LENGTH OF CRACK-0.197'; [02] REMOVED & REPLSDR SWAA2021091409642Angle · corrodedEVIDENCE OF CORROSION AT FWD CARGO COMPT R/H ZEE ANGLE UPPER SURFACE BETWEEN STA 500 AND STA 500A ; / [01] REMOVED THE CORROSION AT FWD CARGO COMPT R/H Z ANGLE UPPER SURFACE BETWEEN STA. 500 & 500A;REF.B737-700 SRM 51-10-02-0G-0.; [02] ORIG. [08] COMPLETED FABSDR SWAA2021091409643Angle · corrodedCORROSION AT FWD CARGO COMPT R/H ZEE ANGLE UPPER SURFACE BETWEEN STA 500A AND STA 500D ; / [01] REMOVED THE CORROSION AT FWD. CARGO COMPT. R/H Z ANGLE UPPER SURFACE BETWEEN STA. 500A & 500D. REF. B737-700 SRM 51-10-02-0G-0.; [02] ORIG. MAT. OF Z ANGLE: 0.040';SDR SWAA2021091409667Pressure Deck · damagedFLIGHT DECK FLOOR AREA AROUND PANEL 211AF;FOUND DAMAGE AT PREVIOUS REPAIR WEB STA. 259.5 - 1.5;LBL 15.0'. ; / [01] INSTALL EWIS PROTECTION AT REPAIR AREA; AS PER B737-7 AMM 20-60-07-913-801.; [02] REPAIRED COCKPIT FLOOR PER EA M-21-153-00734/ 1503096; [03] REMSDR SWAA2021091549669Pressure Deck · crackedHORIZONTAL PRESSURE DECK WEB CRACKED AT STA 671 AND RBL 43 ; / [01] PERFORMED HFEC AND CONFIRMED CRACK ON HORIZONTAL PRESSURE DECK WEB STA 671 RBL 43 IAW NDTM PART 6;51-00-00 PROCEDURE 23. CRACK LENGTH-1.181'.<BR>[NORTEC 600;B/C 166316;CALIB.DUE-10/21]; [02] ISDR SWAA2021091409640Skin · crackedLEFT HORIZONTAL STABILIZER LOWER SURFACE SKIN HAS A CRACK AT STA 184.70 ;4.00' FROM TRAILING EDGE. CRACK LENGTH ;1.181' ( AREA MARKED). ; / [04] REMOVED PANEL 331BZ FOR ACCESS AT L/H HORIZT STAB FRONT SPAR REF B737-700 SRM 51-40-02-0G-0; 2 PER EA NO:21-155-024SDR SWAA2021091408430Floor Panel · deterioratedFLOOR PANEL 140BF DETERIORATED AND SHOWING BURRS ; / [01] FABRICATED AFT CARGO COMPARTMENT FLOOR PANEL 140BF REF B 737-700 AMM 25-52-01-201-801.SDR SWAA2021091408436Floor Panel · warpedAFT CARGO FLOOR PANEL 120AF WARPED AND DEFORMED ; / [01] FABRICATED NEW FLOOR PANEL 120AF; MAT. USED: A90RG1W-48144; PO # 1724657; REF. B737-7 AMM 25-52-01-201-801.; [02] VERIFIED STEP 1SDR SWAA2021091408438Floor Panel · deterioratedFLOOR PANEL 141AF DETERIORATED AND SHOWING BURRS ; FLOOR PANEL 140AF DETERIORATED AND SHOWING BURRS / [01] FABRICATED AFT CARGO COMPARTMENT SIDEWALL PANEL 140AF REF B 737-700 AMM 25-52-01-201-801. CORRECTION TO THIS STEP: ACCESS PANEL 140AF IS NOT A SIDEWALL PSDR SWAA2021091548858Bulkhead Web · crackedR/H WHEEL WELL VAPOR BARRIER CRACKED AT RBL 43' 5' FROM LOWER SECTION APPROX. 7' IN LENGTH ; / [01] MEASUREMENTS; [02] REMOVED DAMAGE PLIES; PREPARED DAMAGE AREA FOR REPAIR; STOP DRILL CRACKS; PERFORMED DRY OUT AS PER B737 SRM 51-70-04-2R-10 SECTION A;B;C AND SDR SWAA2021082308861Support Bracket · crackedRIGHT WING T/E FLAP DEFLECTION CONTOL RIB UPPER PANEL SUPPORT BRACKET HAS SMALL CRACK AT CONTROL RIB ATTACH POINT. REMOVED AND REPLACED R/W T/E FLAP DEFLECTION CONTROL RIG UPPER PANEL SUPPORT BRACKET IN REF SRM 51-40-02-0G-0.SDR SWAA2021060178405Computer · inoperativeDURING INITIAL CLIMB OUT; ELECTRIC TRIM BECAME INOP; BOTH SIDES. MANUAL TRIM NORMAL. ; / REMOVED AND REPLACED FCC B AND STAB TRIM RELAY; AMM 22-11-33 AND SWPM 20-81.SDR SWAA2021060178767Relay · inoperativeDURING INITIAL CLIMB OUT; ELECTRIC TRIM BECAME INOP; BOTH SIDES. MANUAL TRIM NORMAL. ; / REMOVED AND REPLACED FCC B AND STAB TRIM RELAY; AMM 22-11-33 AND SWPM 20-81.SDR SWAA2021012143502Battery Pack · failedEMERGENCY LIGHT BATTERY PACKS AT FOLLOWING LOCATIONS FAILED CAPACITY CHECK M1675; M1673; M1672. R & R EMERGENCY LIGHT BATTERY PACKS AT M1675; M1673; M1672, PER AMM 33-51-06.SDR SWAA2021050646120Seal · crackedRIGHT HAND HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED. / R&R RIGHT HAND HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL REF AMM 53-31-31.SDR SWAA2021050646119Seal · crackedLEFT HAND HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED. / R&R LEFT HAND HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL REF AMM 53-31-31.
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