# Service difficulty reports: N264LV

A list on [N264LV](https://openairdocs.org/aircraft/N264LV.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 6 · 274 reports

- [SDR SWAA2026081146248](https://openairdocs.org/sdr/SWAA2026081146248.md): Lens · loose · Aug 7, 2026 · N264LV · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT LENS AT COCKPIT LOOSE. R & R FWD CENTERLINE EMERGENCY EXIT SIGN HOUSING IAW MM 33-51-01
- [SDR SWAA2026071696568](https://openairdocs.org/sdr/SWAA2026071696568.md): Floor Panel · cracked · Jul 14, 2026 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > CRACKED 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 SWAA2026051296699](https://openairdocs.org/sdr/SWAA2026051296699.md): Cover · detached · May 8, 2026 · N264LV · Boeing 7377H4 · Emergency Lighting
  > CABIN 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 SWAA2025110630515](https://openairdocs.org/sdr/SWAA2025110630515.md): Doubler · corroded · Oct 31, 2025 · N264LV · Boeing 7377H4 · Fuselage Main, Structure
  > FOUND 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 SWAA2025110630856](https://openairdocs.org/sdr/SWAA2025110630856.md): Stringer · corroded · Oct 30, 2025 · N264LV · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > PAINT BUBBLING ON FUSELAGE AT BS 887, STRINGER L25 +3'. REPAIRED PER EA 25-153-02998.
- [SDR SWAA2025110329964](https://openairdocs.org/sdr/SWAA2025110329964.md): Pan · buckled · Oct 30, 2025 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FUSELAGE 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 SWAA2025090309800](https://openairdocs.org/sdr/SWAA2025090309800.md): Bulb · inoperative · Aug 30, 2025 · N264LV · Boeing 7377H4 · Emergency Lighting
  > RH OVER WING EMERGENCY LIGHT OUT. REPLACED BULB PER AMM 33-51-04.
- [SDR SWAA2025070186835](https://openairdocs.org/sdr/SWAA2025070186835.md): Tailpipe · fire · Jun 30, 2025 · N264LV · Boeing 7377H4 · Engine Collector/Tailpipe/Nozzle
  > #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 SERVICE
- [SDR SWAA2025062383013](https://openairdocs.org/sdr/SWAA2025062383013.md): Door · cracked · Jun 19, 2025 · N264LV · Boeing 7377H4 · Main Landing Gear
  > R/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 SWAA2025041422673](https://openairdocs.org/sdr/SWAA2025041422673.md): Pump · failed · Apr 8, 2025 · N264LV · Boeing 7377H4 · Engine Fuel Pump
  > #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 T
- [SDR SWAA2024120573909](https://openairdocs.org/sdr/SWAA2024120573909.md): Light · inoperative · Dec 4, 2024 · N264LV · Boeing 7377H4 · Emergency Lighting
  > R1 DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT PER AMM 33-51-04
- [SDR SWAA2024090532667](https://openairdocs.org/sdr/SWAA2024090532667.md): Light · inoperative · Sep 1, 2024 · N264LV · Boeing 7377H4 · Emergency Lighting
  > AED 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. TASK
- [SDR SWAA2024090532661](https://openairdocs.org/sdr/SWAA2024090532661.md): Battery Pack · inoperative · Aug 31, 2024 · N264LV · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1673 ARE INOP<[01] REMOVED; REPLACED; AND PERFORMED GOOD TEST OF M1673 PER AMM33-51-06-960-805
- [SDR SWAA2024090528299](https://openairdocs.org/sdr/SWAA2024090528299.md): Floorbeam · cracked · Aug 20, 2024 · N264LV · Boeing 7377H4 · Fuselage Main, Floor Beam
  > REJECT - 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 SWAA2024090526529](https://openairdocs.org/sdr/SWAA2024090526529.md): Support · elongated · Aug 16, 2024 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD 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 NRC
- [SDR SWAA2024090625975](https://openairdocs.org/sdr/SWAA2024090625975.md): Scuff Plate · cracked · Aug 14, 2024 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB 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 SWAA2024090625576](https://openairdocs.org/sdr/SWAA2024090625576.md): Intercostal · cracked · Aug 13, 2024 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 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 COMPLETED
- [SDR SWAA2024090624707](https://openairdocs.org/sdr/SWAA2024090624707.md): Angle · corroded · Aug 10, 2024 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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 TTG8Q
- [SDR SWAA2024090523306](https://openairdocs.org/sdr/SWAA2024090523306.md): Bear Strap · cracked · Aug 6, 2024 · N264LV · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED 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] VERIFI
- [SDR SWAA2024090523304](https://openairdocs.org/sdr/SWAA2024090523304.md): Slide · misinstalled · Aug 6, 2024 · N264LV · Boeing 7377H4 · Escape Slide
  > AFT 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;[04
- [SDR SWAA2024090622032](https://openairdocs.org/sdr/SWAA2024090622032.md): Seat Track · damaged · Aug 2, 2024 · N264LV · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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: A
- [SDR SWAA2024090622033](https://openairdocs.org/sdr/SWAA2024090622033.md): Seat Track · corroded · Aug 2, 2024 · N264LV · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 ACTION
- [SDR SWAA2024090621613](https://openairdocs.org/sdr/SWAA2024090621613.md): Panel · debonded · Aug 2, 2024 · N264LV · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > PANEL 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 SWAA2024090621009](https://openairdocs.org/sdr/SWAA2024090621009.md): Support Bracket · cracked · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > WATER 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 #1
- [SDR SWAA2024090621039](https://openairdocs.org/sdr/SWAA2024090621039.md): Shear Web · corroded · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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 #1
- [SDR SWAA2024090621593](https://openairdocs.org/sdr/SWAA2024090621593.md): Angle · cracked · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED 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 STE
- [SDR SWAA2024090621604](https://openairdocs.org/sdr/SWAA2024090621604.md): Shield · corroded · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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 COMPLETE
- [SDR SWAA2024090621606](https://openairdocs.org/sdr/SWAA2024090621606.md): Support Angle · corroded · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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] VER
- [SDR SWAA2024090621340](https://openairdocs.org/sdr/SWAA2024090621340.md): Floor Support · corroded · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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 COMPLETE
- [SDR SWAA2024090621041](https://openairdocs.org/sdr/SWAA2024090621041.md): Strap · corroded · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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 SWAA2024090621342](https://openairdocs.org/sdr/SWAA2024090621342.md): Floor Support · cracked · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED 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 141A5400
- [SDR SWAA2024090621040](https://openairdocs.org/sdr/SWAA2024090621040.md): Strap · corroded · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION 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 SWAA2024090520991](https://openairdocs.org/sdr/SWAA2024090520991.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR 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 A
- [SDR SWAA2024090520993](https://openairdocs.org/sdr/SWAA2024090520993.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR 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 COMPLETE
- [SDR SWAA2024090520996](https://openairdocs.org/sdr/SWAA2024090520996.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR 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 COMPLETE
- [SDR SWAA2024090520995](https://openairdocs.org/sdr/SWAA2024090520995.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > FWD 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] VERIFIED
- [SDR SWAA2024090520985](https://openairdocs.org/sdr/SWAA2024090520985.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > FWD 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] VE
- [SDR SWAA2024090520999](https://openairdocs.org/sdr/SWAA2024090520999.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR 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 SWAA2024090520998](https://openairdocs.org/sdr/SWAA2024090520998.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > FWD 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] VE
- [SDR SWAA2024090520987](https://openairdocs.org/sdr/SWAA2024090520987.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > FWD 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 SWAA2024090521002](https://openairdocs.org/sdr/SWAA2024090521002.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > FWD 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 SWAA2024090521010](https://openairdocs.org/sdr/SWAA2024090521010.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > AFT 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 COMPLETE
- [SDR SWAA2024090521016](https://openairdocs.org/sdr/SWAA2024090521016.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > AFT 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] VERIFIED
- [SDR SWAA2024090521017](https://openairdocs.org/sdr/SWAA2024090521017.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > AFT 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] VE
- [SDR SWAA2024090521018](https://openairdocs.org/sdr/SWAA2024090521018.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > AFT 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] VERIFIED
- [SDR SWAA2024090521019](https://openairdocs.org/sdr/SWAA2024090521019.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > AFT 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 SWAA2024090521014](https://openairdocs.org/sdr/SWAA2024090521014.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > AFT 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 SWAA2024090521023](https://openairdocs.org/sdr/SWAA2024090521023.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > AFT 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 SWAA2024090521028](https://openairdocs.org/sdr/SWAA2024090521028.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > AFT 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 SWAA2024090521025](https://openairdocs.org/sdr/SWAA2024090521025.md): Floor Panel · pulled · Aug 1, 2024 · N264LV · Boeing 7377H4 · Fuselage Floor Panel
  > AFT 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.

Next page: https://openairdocs.org/aircraft/N264LV/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N264LV/reports

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