N242WN
Service difficulty reports · 327
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 = 'N242WN' 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 = 'N242WN' 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 SWAA2024031252836Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PULLED STRANDS ON AFT FLOOR PANEL 241XF UPPER SKIN HAVE BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2024031252837Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ZF UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED REPAIR OF FLOOR PANEL 241ZF UPPER SKIN IAW SRM 53-00-50SDR SWAA2024031252821Floor Panel · pulledAFT FLOOR PANEL 241ABFF UPPER SKIN HAS AREAS OF PULLED STRANDS. PANEL SHOULD BE 241ABF<[01] AREAS OF PULLED STRANDS ON FLOOR PANEL 241ABF WERE REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>DOWNLOADED CURE SHEETS AND TAPE.;[02] VERIFIED FLOOR PANEL 241ABF WAS REPAIREDSDR SWAA2024031252839Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ACF UPPER AND LOWER SKIN DAMAGED AREAS HAVE BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED REPAIR OF FLOOR PANEL 241ACF PER SRSDR SWAA2024031252822Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON AFT FLOOR PANEL 241ADF UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2024031252823Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242TF UPPER SKIN AREAS OF PULLED STRANDS WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED REPAIR OF FLOOR PANEL 242TF UPPER SKIN IAW SRM 53-00-50-2R-1.;[03] WORKSCOPE IS COMPLSDR SWAA2024031252825Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024031252842Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] REPAIRED AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 221CF IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024031252843Floor Panel · pulledFWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 221EF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024031252830Floor Panel · pulledFWD FLOOR PANEL 222AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222AF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2024031252832Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BAC DWG 141A5810 ID: 245.;[02] INFORMATION ENTERED ON ITEM 1 WAS ENTERED IN ERROR. THIS IS AN INSPECTOR BLOCK.;[03] FWD FSDR SWAA2024031252833Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222DF WITH UPPER SKIN PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BAC DWG 141A5810 ID:185.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024031253146Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS460 - BS500C LBL23 WL156.<[01] VERIFIED STEP 15 IN PARTIAL.;[02] VERIFIED STEP 16 COMPLETE.;[03] REJECT - INSTALLATION OF SIDEWALL SUPPORT; FOUND CRACK AT INTERCOSTAL FASTENER ATTACHMENT POINT; BS460; WL156; LBL2SDR SWAA2024031452452Skin · debondedPANEL 194CL OUTER SKIN HAS 2 TIGHTLY GROUPED DISBONDS NEAR CENTER OF PANEL. (MARKED)<[01] PANEL 194CL OUTER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 51-70-05-2R-2.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED PANEL 194CL OUTER SKIN HAS BEEN REPAIRED IASDR SWAA2024031452669Web · corrodedCORROSION ON 1016 WEB AT AFT WET AREA BS1016+13 LBL7 WL208. MARKED<[01] REMOVED CORROSION ON 1016 WEB AT AFT WET AREA BS 1016+13 LBL 7; WL 208 AND REWORKED PER EA 24-153-00486.;[02] TASK CARD COMPLETESDR SWAA2024031452670Strap · corrodedCORROSION ON TENSION STRAP AT AFT WET AREA BS1016; BS1016+11; RBL3 WL208. MARKED<[01] CORROSION ON TENSION STRAP AT AFT WET AREA BS 1016+11 RBL 3 WL 208 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED AFT WET AREA TENSION STRAP IAW SRM 51-40-02-0G-0 AND DWG 14SDR SWAA2024031452815Angle · crackedRIGHT WING FIXED T/E PANEL JUST AFT OF THE PYLON ATTACH ANGLE CRACKED JUST IB OF DEFLECTION RIB. MARKED<[01] REMOVED AND REPLACED RIGHT WING FIXED T/E ATTACH ANGLE JUST AFT OF PYLON AND I/B OF DEFLECTION RIB IAW SRM 51 -40-02-0G-0 PARA. 4.;[02] VERIFIED COMPLESDR SWAA2024031252665Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT WET AREA BS986 RBL43 WL208. MARKED<[01] CORROSION ON BS 986 FLOOR BEAM AT RBL 43; WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-6.;[02] CORRECTED MEASUREMENT;[03] CUSTOMER CARD COSDR SWAA2024031252666Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT WET AREA BS986 LBL43 WL208. MARKED<[01] COMPLETED STEP 8; PARTIAL STEP 9.;[02] COMPLETED STEP 9.;[03] VERIFIED STEPS 11;13 COMPLETE.;[04] REMOVED CORROSION FROM AFT WET AREA FLOOR BEAM BS 986 LBL 43 WL 208 FOUND TO BE OUT OF LIMISDR SWAA2024031252671Skin · crackedDURING HFEC INSPECTION OF LH HORIZONTAL STABILIZER LOWER SKIN (TTG8Q00BDWA5); CRACK FOUND AT STA:193.90; 18' FROM FWD EDGE; MEASURED L: 1.0' MARKED<[01] REPAIRED LH HORIZONTAL STABILIZER LOWER INSPAR SKIN AT STA 193.90 18' FROM FWD EDGE IAW SRM 55-10-01-2R-11;SDR SWAA2024031352136Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0.;[02] ADDITION TO ITEM 1: IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 SHEET:8.;[03] VERIFIED CORRECTIVE ACTION ITEMSDR SWAA2024031352137Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241DF IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024031352135Floor Panel · pulledFLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241EF IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024031352138Floor Panel · pulledFLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241FF WITH PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0013;[02] VERIFIED FLOOR PANEL 241FF WAS REPLACED BY FABRICATING A NEW PANEL SDR SWAA2024031352139Floor Panel · pulledFLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242CF WITH PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0006;[02] JOB COMPLETE.SDR SWAA2024031451950Inlet · cracked#2 ENGINE INLET COWL OUTER LIP SKIN HAS A CRACKED RIVET HEAD AT THE 10:00 POSITION SPLICE SECOND ONE IN FROM THE AFT SIDE OF LIP SKIN.<[01] UPDATED PARTS;[02] REMOVED AND REPLACED #2 ENGINE INLET COWL IAW 71-11-01-000-802-F00 AND 71-11-01-400-802-F00 STEP 5.H.SDR SWAA2024031352128Pressure Deck · crackedWHEEL WELL PRESSURE DECK CRACKED; BS665; RBL40; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024031352130Pressure Deck · crackedWHEEL WELL PRESSURE DECK CRACKED; BS672; RBL41; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024031352131Pressure Deck · crackedWHEEL WELL PRESSURE DECK CRACKED; BS666; RBL41; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024031352129Pressure Deck · crackedWHEEL WELL PRESSURE DECK CRACKED; BS666; RBL42; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024031251943Pressure Deck · crackedCRACK FOUND DURING HFEC INSPECTION OF HORIZONTAL PRESSURE DECK WEB (TTG8Q00BCA3K) AT RBL 41 BS663+2. L:0.4IN MARKED<[01] REPAIRED BEADED PRESSURE DECK BETWEEN BS 663.5 TO BS 675; RBL 30 TO RBL 60 WL 202 IAW SRM 53-40-51-2R-2 REPAIR 2. FIGURE 202.;[02] VERIFIEDSDR SWAA2024031251942Pressure Deck · crackedCRACK FOUND DURING HFEC INSPECTION OF HORIZONTAL PRESSURE DECK WEB (TTG8Q00BCA3K) AT LBL 34.5 BS663+1.5. L:0.5IN MARKED<[01] REPAIRED HORIZONTAL PRESSURE DECK AT LBL 34.5 BS663+1.5 PER SRM 53-40-51-2R-2 REPAIR 2. FAULT COMPLETE.;[02] VERIFIED ALL RII STEPS ARESDR SWAA2024031252132Pressure Deck · crackedWHEEL WELL PRESSURE DECK CRACKED; BS665; LBL35; WL200<[01] PRESSURE DECK AT BS 665 LBL 35 WL 200 REPAIRED ON FAULT TTG8Q00RJ619. FAULT COMPLETE.;[02] VERIFIED RII ITEMS WERE COMPLETED ON FAULT TTG8Q00RJ619.;[03] VERIFIED COMPLETION ON FAULT TTG8Q00RJ619. CARD SDR SWAA2024011139649Floor Panel · crackedFWD CARGO FLOOR AFT OF DOOR HAS CRACK IN IT. REPLACED FWD CARGO FLOOR PANEL REF AMM 25-52-10.SDR SWAA2023112021649Battery Pack · failedEMERGENCY LIGHT BATTERY PACKS POS M1675 AND M1674 FAILED CAPACITANCE CHECK<[01] R/R EMERGENCY LIGHT BATTERY PACKS AT POSITIONS M1675 AND M1674 REF AMM 33-51-06.SDR SWAA2023112021657Tail Cone · delaminatedTAIL-CONE RH SIDE HAS A DENT MEASURING 10 LONG 2 WIDE AND .106 DEEP. DENT HAS AREAS THAT ARE DELAMINATED.<[01] APPLIED SPEED TAPE TO TAIL CONE RH SIDE AND COMPLIED WITH EA - 23-153-03378.SDR SWAA2023111721856Tail Cone · delaminatedTAIL CONE RH SIDE HAS A DENT 12 FWD OF ELEVATOR INDEX PLATE MEASURING 3 LONG 3 WIDE AND .087 DEEP. DENT IS DELAMINATED. DAMAGE IS WITHIN 4 OF PREVIOUS DENT.<[01] C/W EA: 23-153-03381;[02] EDIT STEP 3 TO INDICATE 'YES'SDR SWAA2023071176370Handle · looseALL FOUR DOOR LINER ASSIST HANDLES ARE LOOSE.<[01] RESECURED ALL FOUR DOOR LINER ASSIST HANDLE IAW AMM-25-99-99-SWA-001 PAGE 6 STEP B ITEM (C);[02] VERIFIED ITEM 1.<BR>AUDITED.SDR SWAA2023071775840Web · crackedDURING DVI INSPECTION FOUND L/H VAPOR BARRIER WEB CRACKED AT STA 663 WL 167 LBL47<[01] EVALUATED DAMAGE; CRACKS ARE REPAIRABLE IAW B737 SRM 57-10-10-2R-2. TAP TEST GOOD; NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 51-70-04-2R-10SDR SWAA2023071875272Bracket · crackedDOT A24-07 RH WING I/B L/E WING TO BODY FAIRING / L/E SUPPORT STRUCTURE ANGLE CRACKED AT FASTENER HOLE. MARKED<[01] REMOVED CRACKED ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05-0G-0 AND BOEING DWG# 116A3110 ID:0005 REV:B. WORK PESDR SWAA2023071275275Floor Panel · delaminatedDOT A160-46; FLOOR PANEL 241BF HAS DELAMINATION<[01] WORK ACCOMPLISHED ON NON-ROUTINE TTG8Q00M1DKDSDR SWAA2023071275283Floor Panel · delaminatedDOT A160-44; FLOOR PANEL 231ZF HAS DELAMINATION OF TOP PLYS<[01] WORK ACCOMPLISHED ON NON-ROUTINE TTG8Q00M1D0ESDR SWAA2023071874510Angle · crackedL/H VAPOR BARRIER UPPER ANGLE IS CRACKED AT STA663 WL 167 AT LBL 10 I/B<[01] ACCOMPLISHED HFEC SURFACE AND OPEN HOLE IAW B737 NDT P6 51-00-00 P16 AND P23 TOOL 44291 DUE 03NOV23 NO CRACKS NOTED;[02] AUDIT C/WSDR SWAA2023071775271Angle · crackedR/H VAPOR BARRIER UPPER ANGLE HAS CRACK AT STA663 WL 167 AT RBL 45<[01] RECEIVED REPAIR ANGLES FROM BACK SHOP 2024-0 .071 W/O 44942-1000-0004 AND 2024-0 .063 W/O 44942-1000-0001;[02] VERIFIED ITEM 1;[03] ACCOMPLISHED HFEC SURFACE AND OPEN HOLE IAW B737 NDT P6 SDR SWAA2023071773765Bulkhead Web · crackedR/H VAPOR BARRIER WEB AT STA 663 HAVE CRACK AT RBL 45 AND RBL 37<[01] EVALUATED DAMAGE; CRACK IS REPAIRABLE IAW B737 SRM 57-10-10-2R-2 REPAIR 2. NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 51-70-04-2R-10 PAR 4 STEPS A; B; AND C.SDR SWAA2023052250514Slide · out of adjustR1 DOOR SLIDE UNSEATED FROM HOLDER<[01] INSPECTED R1 DOOR SLIDE; RE-SECURED GIRT BAR INTO RETAINING CLIPS NO DEFECTS NOTED PER AMM 25-66-01.SDR SWAA2023041024008Panel · elongatedPANEL 193B HAS SEVERAL ELONGATED HOLES.<[01] REMOVED AND REPLACED WITH NEW PANEL PER AMM 53-51-01.;[02] INSPECTION VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2022090148406Slide · out of adjustFWD ENTRY SLIDE MORE THAN ONE NEEDLE WIDTH INTO THE RED / [01] R&R FWD ENTRY SLIDE PER AMM 25-66-01SDR SWAA2022082947453Slide · lowFORWARD ENTRY DOOR SLIDE PRESSURE IN THE RED / [01] INSPECTED SLIDE PRESSURE IAW AMM 25-66-01; FOUND WITHIN LIMITS AT THIS TIMESDR SWAA2022040690568Girt Bar · out of positionL2 DOOR SLIDE GIRT BAR NEEDS TO BE REPOSITIONED 2022-129940 / [01] INSTALLED CORRECTLY L2 DOOR SLIDE GIRT BAR IAW B737-700 AMM 25-66-01-000-804;[02] CORRECTED ACTION<BR>INSTALLED CORRECTLY L2 DOOR SLIDE GIRT BAR IAW B737-700 AMM 25-66-01-400-803;[03] INSTALLED
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