N264LV
Service difficulty reports · 274
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 = 'N264LV' 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 = 'N264LV' 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 SWAA2026081146248Lens · looseEMERGENCY LIGHT LENS AT COCKPIT LOOSE. R & R FWD CENTERLINE EMERGENCY EXIT SIGN HOUSING IAW MM 33-51-01SDR SWAA2026071696568Floor Panel · crackedCRACKED FLOOR OF AFT CARGO BAY FLOOR PANEL.. REMOVED AFT CARGO PANEL 140 BF INSTALLED AFT CARGO FLOOR PANEL 140BF IAW AMM 25-52-10.SDR SWAA2026051296699Cover · detachedCABIN EMERGENCY LIGHT COVER FELL OFF UNDER 1ABC OVHD BIN. OK TO CONTINUE PER MEL 25-10-01 SP# 1B; AUTH # 318563. INSTALLED NEW EMERGENCY LIGHT COVER PER SIP.SDR SWAA2025110630515Doubler · corrodedFOUND CORROSION ON BS 887 BUTT SPLICE INTERNAL STRAP DOUBLER UNDER FUSELAGE SKIN AFTER ACCOMPLISHING EA 25-153-02998. CORROSION MEASURES 2.50 BY 1.0 . REPAIRED IAW EA 25-153-02998-WIP3 & REF TTG8Q016Q10M.SDR SWAA2025110630856Stringer · corrodedPAINT BUBBLING ON FUSELAGE AT BS 887, STRINGER L25 +3'. REPAIRED PER EA 25-153-02998.SDR SWAA2025110329964Pan · buckledFUSELAGE TOILET SERVICE DOOR PAN, AFT LOWER CORNER IS BUCKLED. REMOVED FUSELAGE TOILET SERVICE DOOR PAN IAW SRM 51-40-02. AFTER REMOVAL OF FUSELAGE TOILET SERVICE DOOR PAN FOUND CORROSION ON THE MATING SKIN OF SERVICE DOOR PAN. REMOVED CORROSION IAW SRM 53-SDR SWAA2025090309800Bulb · inoperativeRH OVER WING EMERGENCY LIGHT OUT. REPLACED BULB PER AMM 33-51-04.SDR SWAA2025070186835Tailpipe · fire#2 ENGINE TAILPIPE FIRE REPORTED. EXTINGUISHED AFTER SHUTDOWN. NO ABNORMAL ENGINE INDICATIONS<[01] INSPECTED #2 ENGINE IN REF TO AMM 71-00-00-800-803-F00. NO OIL PUDDLING. FLAME ARRESTOR HONEYCOMB NOT DAMAGED. A/C OK FOR SERVICESDR SWAA2025062383013Door · crackedR/H MLG CTR DOOR HAS CRACK AT LWR FWD CUTOUT AT MOUNT ATTACH POINT. <[01] REMOVED R/H CTR & INNER MLG DOOR ASSEMBLY I.A.W AMM 32-13-11 OK TO CONTINUE SERVICE PER CDL 32-10-3XD.SDR SWAA2025041422673Pump · failed#1 ENG. STUCK ON 86.0 ON CLIMB OUT AND WOULD NOT ADVANCE WITH MANUAL ADVANCE OF THRUST LEVER; POWER SETTINGS WORKED NORMAL ON RETURN TO FIELD <[01]. REPLACED #1 ENGINE FUEL PUMP IAW MT 773-11-00. SEE LP# 2929450 FOR HIGH POWER ENGINE RUN.; [02] LABOR ADDED TSDR SWAA2024120573909Light · inoperativeR1 DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT PER AMM 33-51-04SDR SWAA2024090532667Light · inoperativeAED EXTERIOR EMERGENCY EXIT LIGHT IS INOPERABLE AED EXTERIOR EMERGENCY EXIT LIGHT IS INOPERABLE<[01] RELAMPED EXTERIOR EMERGENCY EXIT LIGHT AND PERFORMED A GOOD FUNCTIONAL TEST PER AMM 33-51-04-960-801;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION STEP 1. TASKSDR SWAA2024090532661Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1673 ARE INOP<[01] REMOVED; REPLACED; AND PERFORMED GOOD TEST OF M1673 PER AMM33-51-06-960-805SDR SWAA2024090528299Floorbeam · crackedREJECT - FLOOR BEAM REPAIR STRAP HAS 1EA OPEN COUNTERSUNK FASTENER HOLE @ BS294; RBL-37;WL-208. REPAIR ANGLE HAS 1EA HILOK W/O COLLAR; 1EA UNDERSIZED HILOK @ BS294; RBL-53; WL-207. (MARKED) (PICS)<[01] INSTALLED FASTENERS ON UPPER CHORD FLOOR BEAM 3EA PER SRM SDR SWAA2024090526529Support · elongatedFWD CARGO BAY AFT CENTER BULKHEAD RH SUPPORT HAS 2EA ELONGATED FASTENER HOLES AT BS 500D; RBL 25; WL 157<[01] REMOVED AND REPLACED FWD CARGO BAY AFT CENTER BULKHEAD RH IAW SRM 51-40-02 AND DWG 143A9481 ID: 0014 REV: -;[02] REJECTED CORRECTIVE ACTION 1; SEE NRCSDR SWAA2024090625975Scuff Plate · crackedFCB FWD CORNER SCUFF CRACKED<[01] REPAIRED THE CORNER SCUFF PLATE WITH ACCOMPLISHED STEPS 1 - 6 IAW SRM 53-30-15-2R-1. REPAIR 1.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024090625576Intercostal · crackedINTERCOSTAL HAS CRACK BTW STA 294.5 & 303.9; STR 16L.<[01] REMOVED AND INSTALLED NEW INTERCOSTAL STA 294.5 & 303.9; STR 16L.IAW SRM 51-40-02 AND DWG 141A8180 REV:C;[02] VERIFIED TASK COMPLETEDSDR SWAA2024090624707Angle · corrodedCORROSION ON THRESHOLD ATTATCHMENT ANGLE ATTACHED TO THE R1 DOOR MOPSILL FROM BS 294 - 328 RBL 57 WL208<[01] REMOVED AND REPLACED THRESHOLD ATTACH ANGLE; ANGLE CAME WHIT SERVICEABLE MOPSILL ASSY P/N 654A0004-106 INSTALLATION ACCOMPLESHED ON COSTUMER CARD TTG8QSDR SWAA2024090523306Bear Strap · crackedCRACKED BEAR STRAP AT R1 DOOR JUST ABOVE SEAL DEPRESSOR; 3' BELOW FWD UPPER STOP FITTING. MARKED CORRECTION: CRACK FOUND ON FSD STUB FRAME.<[01] REMOVED AND REPLACED FWD SERVICE DOOR FWD UPPER STUB FRAME IAW SRM 51-40-02-0G-0 AND DWG#141A8370 REV-C;[02] VERIFISDR SWAA2024090523304Slide · misinstalledAFT ENTRY DOOR SLIDE PACK NOT INSTALLED CORRECTLY.<[01] INSTALLED CORRECTLY AFT ENTRY DOOR SLIDE PACK IAW AMM 25-66-01-400-801 AND MT 725-61-06 AE ON FAULT TTG8Q00VDBM0.;[02] REJECTED: SEE TTG8Q00VE73Z;[03] UPDATE REJECTION TTG8Q00VE73Z WAS CREATED FOR ASD;[04SDR SWAA2024090622032Seat Track · damagedMAIN CABIN SEAT TRACK MISSING A PIECE OF THE CROWN AT WL208 RBL45 BS500+7. MARKED<[01] REMOVED AND REPLACED NEW ON MAIN CABIN OF SEAT TRACK BS 480 TO BS520 RBL 45. IAW SRM 51-40-02 AND DWG 143A5300. ID: 0042 REV: ASDR SWAA2024090622033Seat Track · corrodedMAIN CABIN SEAT TRACK HAS CORROSION AT WL208 RBL45 BS500C+8<[01] THIS FAULT WILL BE ACCOMPLISHED ON CARD TTG8Q00UZBY9 (REPLACEMENT OF PART);[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2024090621613Panel · debondedPANEL 195BR OUTER SKIN IS DISBONDED NEAR AFT END. (MARKED)<[01] 195BR OUTER SKIN DISBOND DAMAGE HAS BEEN REPAIRED IAW SRM 51-70-05-2R-2.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR SWAA2024090621009Support Bracket · crackedWATER SERVICE PAN SUPPORT AFT BRACKET CRACKED AT BS BETWEEN 907-927 (MARKED) BRACKET IS INSIDE AFT CARGO BAY<[01] REMOVED AND REPLACED WATER SERVICE PAN SUPPORT AFT BRACKET IAW SRM 51-40-02 AND DWG: 147A7221 ID:0001 REV: F.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024090621039Shear Web · corrodedCORROSION ON SHEAR WEB AT STA 1003+4 LBL 38; WL 208.2<[01] REFER TO FAULT TTG8Q00UYAWJ FOR REPAIR RESOLUTION;[02] REFER TO FAULT TTG8Q00UYAWJ FOR REPAIR RESOLUTION PER EA 24-153-02257-WIP1;[03] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024090621593Angle · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS387 LBL13 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL (ANGLE) BETWEEN BS.380 - BS400 LBL.13 WL.208.IAW B-737-700 SRM 51-40-02 DWG# 143A5400 REV: A.;[02] VERIFIED RII STEP 5 COMPLETE.;[03] VERIFIED STEP 2 COMPLETE; ALL STESDR SWAA2024090621604Shield · corrodedCORROSION ON AFT SHIELD AT FCB BS500 - BS500A RBL24 WL156. MARKED<[01] REMOVED AND REINSTALLED SHIELD IAW SRM 51-40-02<BR>AND DWG# 143A8126 REV:-<BR>CARD COMPLETED;[02] CC COMPLETESDR SWAA2024090621606Support Angle · corrodedCORROSION ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FCB BS500D RBL25 WL157. MARKED<[01] VERIFIED STEP 3 IN PARTIAL.;[02] REMOVED AND REPLACED SIDEWALL SUPPORT P/N 143A7501U186AT BS500-BS500D FCB RBL25 WL157 I.A.W SRM 51-40-02-0G-0 AND DWG 143A7500.;[03] VERSDR SWAA2024090621340Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT FWD WET AREA BS297; BS302 LBL11 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL AT BS294.5-BS312 LBL11 IAW SRM 51-40-02 AND DWG 141A5600 ID:0002 REV: N.;[02] CC COMPLETE;[03] VERIFIED RII ITEMS COMPLETESDR SWAA2024090621041Strap · corrodedCORROSION ON TENESION STRAP AT STA 1016 RBL 3 AND STA 1016+6 TO 1016+14 RBL 3.<[01] REMOVE AND REPLACED AFT WET AREA TENSION STRAP P/N 147A5744-1 AT BS 1006 TO BS 1026 RBL 3 IAW SRM 51-40-02-0G-0 AND DWG#147A5730 REV-C;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024090621342Floor Support · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS321 LBL45 WL208.<[01] 01 - REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA BS321 LBL45 WL208 PER SRM 51-40-02.;[02] 01 - REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA BS321 LBL45 WL208 PER SRM 51-40-02 AND DWG 141A5400SDR SWAA2024090621040Strap · corrodedCORROSION ON TENSION STRAP AT STA 1006+1 LBL 7.7; 1006+7 LNL 4.5 STA 1016+7 LBL 2.5.<[01] REMOVED AND INSTALLED TENSION STRAP BS 1006 TO BS 1026 LBL3 IAW SRM 51-40-02-0G-0 AND DWG 147A5600 REV H.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024090520991Floor Panel · pulledFLOOR PANEL 231FF HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231FF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ASDR SWAA2024090520993Floor Panel · pulledFLOOR PANEL 231JF HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231JF WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0; AND BOEING DWG 143A5810 ID: 0118.;[02] VERIFIED JOB COMPLETESDR SWAA2024090520996Floor Panel · pulledFLOOR PANEL 231WF HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231WF WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0; AND BAC DWG 143A5810 ID:0107.;[02] VERIFIED JOB COMPLETESDR SWAA2024090520995Floor Panel · pulledFWD FLOOR PANEL 221EF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIEDSDR SWAA2024090520985Floor Panel · pulledFWD FLOOR PANEL 221FF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221FF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VESDR SWAA2024090520999Floor Panel · pulledFLOOR PANEL 232DF HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232DF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024090520998Floor Panel · pulledFWD FLOOR PANEL 231CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 231CF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VESDR SWAA2024090520987Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222CF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED.SDR SWAA2024090521002Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222DF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED.SDR SWAA2024090521010Floor Panel · pulledAFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241UF FLOOR PANEL FABRICATION HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 146A5810 ID: 0054.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED JOB COMPLETESDR SWAA2024090521016Floor Panel · pulledAFT FLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241VF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIEDSDR SWAA2024090521017Floor Panel · pulledAFT FLOOR PANEL 241WF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 41WF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241WF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[03] VESDR SWAA2024090521018Floor Panel · pulledAFT FLOOR PANEL 242QF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242QF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIEDSDR SWAA2024090521019Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024090521014Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ZF AREAS OF PULLED STRANDS ON UPPER SKIN WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024090521023Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF AFT FLOOR PANEL 241ABF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED.SDR SWAA2024090521028Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241ADF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024090521025Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242TF UPPER SKIN; WITH AREAS OF PULLED STRANDS; WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACITON 1.
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