# Service difficulty reports: N233LV, cancelled Jun 5, 2026

A list on [N233LV, cancelled Jun 5, 2026](https://openairdocs.org/deregistered/N233LV-2026-06-05.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 · 286 reports

- [SDR SWAA2025102125098](https://openairdocs.org/sdr/SWAA2025102125098.md): Seal · cracked · Oct 17, 2025 · N233LV · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED. R & R LEFT HORIZONTAL UPPER SLIDER IAW AMM CH.53-31-31. INSPECTED LEFT HORIZONTAL UPPER SLIDER PER AMM 53-31-31.
- [SDR SWAA2025052273985](https://openairdocs.org/sdr/SWAA2025052273985.md): Slide · out of position · May 22, 2025 · N233LV · Boeing 7377H4 · Escape Slide
  > CREW REPORTED L1 DOOR SLIDE DRAGS ON FLOOR WHEN OPENING <[01]. REPOSITIONED FWD ENTRY DOOR SLIDE REF MT 725-61-06.
- [SDR SWAA2025031404815](https://openairdocs.org/sdr/SWAA2025031404815.md): Light · inoperative · Mar 13, 2025 · N233LV · Boeing 7377H4 · Emergency Lighting
  > L1 EMERGENCY EXIT LIGHT INOP <[01]. 01 - REMOVED AND REPLACED PER [AMM 33-51-00-501-NG.
- [SDR SWAA2025010382175](https://openairdocs.org/sdr/SWAA2025010382175.md): Seat Back · out of adjust · Dec 31, 2024 · N233LV · Boeing 7377H4 · Passenger Compartment Equipment
  > 11D SEATBACK WONT STAY UP AND IMPEDESACCESS TO EMERGENCY EXIT<[01] SECURED SEAT 11D IN FWD POSITION. SEATS 11E AND 11F INOP. OK TO CONTINUE PER MEL 25-6-01 SEATS 11DEF INOP.;[02] REMOVED AND REPLACED PASSENGER ROW SEATS 11 FED IAW AMM 25-22-00.
- [SDR SWAA2024111258119](https://openairdocs.org/sdr/SWAA2024111258119.md): Attach Bracket · cracked · Nov 9, 2024 · N233LV · Boeing 7377H4 · Wing, Attach Fittings
  > RIGHT WING UPR I/B PANEL SUPPORT FWD ATTACH BRACKET CRACKED. (Z BRACKET)<[01] REMOVED AND REPLACED RH WING UP I/B PANE SUPPORT FWD ATTACH BRACKET IAW. SRM 51-40-02
- [SDR SWAA2024082628540](https://openairdocs.org/sdr/SWAA2024082628540.md): Girt Bar · out of adjust · Aug 21, 2024 · N233LV · Boeing 7377H4 · Emergency Equipment
  > LEFT CLIP THAT HOLDS GIRT BAR ON FWD SERVICE DOOR IS NOT HOLDING TIGHT<[01] ADJUSTED LEFT CLIP ON FWD SERVICE DOOR GIRT BAR PER SIP
- [SDR SWAA2024040470235](https://openairdocs.org/sdr/SWAA2024040470235.md): Lamp · inoperative · Apr 4, 2024 · N233LV · Boeing 7377H4 · Emergency Lighting
  > AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED AFT ENTRY DOOR EXTERIOR EMERGENCY LAMP PER AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2024021251215](https://openairdocs.org/sdr/SWAA2024021251215.md): Slide · partial deploy · Feb 11, 2024 · N233LV · Boeing 7377H4 · Escape Slide
  > INADVERTENT PARTIAL SLIDE DEPLOYMENT; FORWARD SERVICE DOOR.<[01] REMOVED AND REPLACED FORWARD SERVICE DOOR SLIDE PER MT 725-61-06-FS AND TSR# 2024001015.;[02] C/W
- [SDR SWAA2023121329974](https://openairdocs.org/sdr/SWAA2023121329974.md): Handle · loose · Dec 10, 2023 · N233LV · Boeing 7377H4 · Passenger/Crew Doors
  > ASSIST HANDLE JUST AFT OF L-1 DOOR IS LOOSE<[01] SECURED ASSIST HANDLE JUST AFT OF L-1 DOOR AS PER AMM 25-21-31-420-802;[02] VERIFIED STEP 1.
- [SDR SWAA2023121329138](https://openairdocs.org/sdr/SWAA2023121329138.md): Light · inoperative · Dec 8, 2023 · N233LV · Boeing 7377H4 · Emergency Lighting
  > R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.
- [SDR SWAA2023121329584](https://openairdocs.org/sdr/SWAA2023121329584.md): Battery Pack · inoperative · Dec 8, 2023 · N233LV · Boeing 7377H4 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHT INOP EMERGENCY LIGTHS STA 603 LH & RH; STA 727 L/H; STA 952 LH & RH INOPS<[01] PERFORMED EMERGENCY LIGHTING PROBLEM AS PER REF FIM 33-50 TASK 801 FINDING THE FOLLOWING POWER SUPPLY BATTERY PACKS DEFECTIVE IN POSITION: <BR>M1668 BATTERY
- [SDR SWAA2023121324421](https://openairdocs.org/sdr/SWAA2023121324421.md): Seal · cracked · Nov 23, 2023 · N233LV · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STABILIZER GAP COVER ACCESS PANEL 343AT METAL BLADE SEAL 'CORD' CRACKED PN: 186A3104-10<[01] RECEIVED NEW PART PN: 186A3104U10 <BR><BR>SEE FAULT: TTG8Q00PJPBW FOR INSTALLATION OF PART AS PER SRM 51-40-02-0G-0;[02] VERIFIED STEP #1.
- [SDR SWAA2023121323694](https://openairdocs.org/sdr/SWAA2023121323694.md): Scuff Plate · cracked · Nov 21, 2023 · N233LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO AFT SCUFF PLATE CRACKED<[01] RECEIVED AFT CARGO AFT SCUFF PLATE P.N#146A8341-9 INSTALLATION WILL BE ACCOMPLISHED IN N.R# TTG8Q00PHG82.;[02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2023121323695](https://openairdocs.org/sdr/SWAA2023121323695.md): Scuff Plate · cracked · Nov 21, 2023 · N233LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FWD SCUFF PLATE CRACKED<[01] RECEIVED AFT CARGO SCUFF PLATE P.N# 146A8341-7 INSTALLATION WILL BE ACCOMPLISHED IN N.R# TTG8Q00PHG82.;[02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2023121322014](https://openairdocs.org/sdr/SWAA2023121322014.md): Frame · elongated · Nov 16, 2023 · N233LV · Boeing 7377H4 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT DOOR CUTOUT; AFT FRAME UPPER CORNER; PANEL PLATE HAS ELONGATED FASTENER HOLE.<[01] ACCOMPLISHED EA 23-153-03457 INSTRUCTIONS FOR ELONGATED HOLES AT AFT CARGO COMPARTMENT DOOR CUTOUT;[02] VERIFIED EA 23-153-03457 ACCOMPLISHED
- [SDR SWAA2023121322226](https://openairdocs.org/sdr/SWAA2023121322226.md): Rib · cracked · Nov 16, 2023 · N233LV · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > R/H STAB RIB #4 AT STA. 120.30 CRACKED AT AFT LWR END<[01] ACCOMPLISHED REPAIR AT R/H STAB RIB #4 AT STA. 120.30 AFT LOWER END PER EA 23-155-03443;[02] VERIFIED REPAIR ACCOMPLISHED.
- [SDR SWAA2023121322013](https://openairdocs.org/sdr/SWAA2023121322013.md): Strip · cracked · Nov 16, 2023 · N233LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT CAPSTRIP PN 453A2611-5 CRACKED<[01] RECEIVED PART; WORK WITH BE ACCOMPLISHED ON SEPARATE WORK ORDER PLEASE REFER TO WORK CARD [TTG8Q00PUY0H];[02] VERIFIED STEP #1.
- [SDR SWAA2023121321609](https://openairdocs.org/sdr/SWAA2023121321609.md): Frame · damaged · Nov 14, 2023 · N233LV · Boeing 7377H4 · Fuselage Main, Frame
  > REF: NRC: G086480: AFT CARGO COMPARTMENT DOOR CUTOUT; FWD FRAME UPPER CORNER; PANEL PLATE HAS ELONGATED FASTENER HOLE. MARKED<[01] ACCOMPLISHED EA 23-153-03457 INSTRUCTIONS FOR ELONGATED HOLES AT AFT CARGO COMPARTMENT DOOR CUTOUT;[02] VERIFIED EA 23-153-03457
- [SDR SWAA2023121320119](https://openairdocs.org/sdr/SWAA2023121320119.md): Door Frame · cracked · Nov 10, 2023 · N233LV · Boeing 7377H4 · Fuselage Main, Structure
  > L-1 DOOR CUTOUT STA 312 BETWEEN STR 5L-6L FRAME END CRACK<[01] ACCOMPLISHED TRIM REPAIR AT L-1 DOOR CUTOUT STA 312 BETWEEN STR 5L-6L FRAME PER EA 22-153-01244;[02] VERIFIED STEP 1.
- [SDR SWAA2023121320120](https://openairdocs.org/sdr/SWAA2023121320120.md): Door Frame · cracked · Nov 10, 2023 · N233LV · Boeing 7377H4 · Fuselage Main, Structure
  > L-1 DOOR CUTOUT INNER CHORD STA 303.9 CRACK<[01] REMOVED AND INSTALLED NEW INNER CHORD AT L-1 DOOR CUTOUT STA 303.9 PER SRM 51-40-02-0G-0 AND DWG 141A8110;[02] VERIFIED INNER CHORD REPLACED
- [SDR SWAA2023121319522](https://openairdocs.org/sdr/SWAA2023121319522.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > LH PASSENGER CABIN PANEL#221AF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL #141A5810-53 (221AF) INSTALLATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HKSE.;[02] VERIFIED PANEL RECIEVED NEW AND WILL BE INSTALLED ON TTG8Q003HKSE
- [SDR SWAA2023121319675](https://openairdocs.org/sdr/SWAA2023121319675.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > LH PASSENGER CABIN PANEL#221BF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL #141A5810-56 (221BF) INSTALLATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HKSE.;[02] VERIFIED PANEL RECIEVED NEW AND INSTALLATION TO BE ACCOMPLISHED ON TTG8Q003HKSE
- [SDR SWAA2023121319676](https://openairdocs.org/sdr/SWAA2023121319676.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > LH PASSENGER CABIN PANEL#221DF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL #141A5810-59 (221DF) INSTALLATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HKSE.;[02] VERIFIED PANEL RECIEVED NEW AND WILL BE INSTALLED ON TTG8Q003HKSE
- [SDR SWAA2023121319677](https://openairdocs.org/sdr/SWAA2023121319677.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > LH PASSENGER CABIN PANEL#221CF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL #141A5810-9 (221CF) INSTALLATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HKSE.;[02] VERIFIED PANEL RECIEVED NEW AND WILL BE INSTALLED ON TTG8Q003HKSE
- [SDR SWAA2023121319678](https://openairdocs.org/sdr/SWAA2023121319678.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR STA 890 PANEL#241XF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL PN #147A5810-100 (241XF) INSTALATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HRAS.;[02] VERIFIED PANEL RECEIVED NEW AND INSTALLATION TO BE ACCOMPLISHED ON TTG8Q003HRAS
- [SDR SWAA2023121319679](https://openairdocs.org/sdr/SWAA2023121319679.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > LH PASSENGER CABIN PANEL#241ZF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL 147A5810-98 (241ZF) INSTALLATION WILL BE ACCOMPLISHED IN N/R: TTG8Q00NCL70.;[02] VERIFIED STEP # 1
- [SDR SWAA2023121319683](https://openairdocs.org/sdr/SWAA2023121319683.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > RH PASSENGER CABIN PANEL#242XF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL PN #147A5810-11 (242XF) INSTALATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HRAS.;[02] VERIFIED PANEL RECEIVED NEW AND INSTALLATION TO BE ACCOMPLISHED ON TTG8Q003HRAS
- [SDR SWAA2023121319684](https://openairdocs.org/sdr/SWAA2023121319684.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > RH PASSENGER CABIN FLOOR ACCESS PANEL#242RF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL PN #147A5810-2 (242RF) INSTALATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HRAS.;[02] VERIFIED PANEL RECEIVED NEW AND INSTALLATION TO BE ACCOMPLISHED ON TTG8Q003HRAS
- [SDR SWAA2023121319685](https://openairdocs.org/sdr/SWAA2023121319685.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR ACCESS PANEL#241AAF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL PN #147A5810-8 (241AAF) INSTALATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HRAS.;[02] VERIFIED PANEL RECEIVED NEW AND INSTALLATION TO BE ACCOMPLISHED ON TTG8Q003HRAS
- [SDR SWAA2023121319681](https://openairdocs.org/sdr/SWAA2023121319681.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR ACCESS PANEL#241ABF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL PN #147A5810-88 (241ABF) INSTALATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HRAS.;[02] VERIFIED PANEL RECEIVED NEW AND INSTALLATION TO BE ACCOMPLISHED ON TTG8Q003HRAS
- [SDR SWAA2023121319693](https://openairdocs.org/sdr/SWAA2023121319693.md): Intercostal · cracked · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD WET AREA STA 312 TO STA 328;LBL 46 INTERCOSTAL HAS HOLE SCREW CRACKED.<[01] REMOVED AND INSTSLLED NEW INTERCOSTAL P/N: 141A5410U140; PO# 2043476 AT FWD WET AREA STA 312 TO STA 328; LBL 46 PER SRM 51-40-02-0G-0 AND DWG# 141A5410;[02] VERIFIED STEP 1; INTER
- [SDR SWAA2023121319694](https://openairdocs.org/sdr/SWAA2023121319694.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > RH PASSENGER CABIN FLOOR ACCESS PANEL#222BF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL P.N# 141A5810-464 (222BF) INSTALLATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HKSE.;[02] CORRECTING STEP 1: RECEIVED NEW FLOOR PANEL P.N# 141A5810-464 (222BF) INSTALLATION
- [SDR SWAA2023121319695](https://openairdocs.org/sdr/SWAA2023121319695.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > RH PASSENGER CABIN FLOOR ACCESS PANEL#242UF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL PN #147A5810-95 (242UF) INSTALATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HRAS.;[02] VERIFIED NEW PANEL RECIEVED AND INSTALLATION TO BE ACCOMPLISHED ON TTG8Q003HRAS
- [SDR SWAA2023121319691](https://openairdocs.org/sdr/SWAA2023121319691.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > LH PASSENGER CABIN FLOOR ACCESS PANEL#222DF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL #141A5810-185(222DF) INSTALLATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HKSE.;[02] VERIFIED PANEL RECIEVED NEW AND WILL BE INSTALLED ON TTG8Q003HKSE
- [SDR SWAA2023121319698](https://openairdocs.org/sdr/SWAA2023121319698.md): Floor Panel · delaminated · Nov 8, 2023 · N233LV · Boeing 7377H4 · Fuselage Floor Panel
  > RH PASSENGER CABIN FLOOR ACCESS PANEL#242VF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL PN #147A5810-350 (242VF) INSTALATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HRAS.;[02] VERIFIED PANEL RECEIVED NEW AND INSTALLATION TO BE ACCOMPLISHED ON TTG8Q003HRAS
- [SDR SWAA2023121319700](https://openairdocs.org/sdr/SWAA2023121319700.md): Plate · cracked · Nov 8, 2023 · N233LV · Boeing 7377H4 · Wing Miscellaneous Structure
  > LT WING REAR SPAR LOWER CHORD AT APPROX. ORSS 264 WIGGLE PLATE IS CRACKED. 124-005<[01] REMOVED LT WING REAR SPAR LOWER CHORD AT APPROX. ORSS 264 WIGGLE PLATE REF: SRM 51-40-O2-OG-0;[02] STEP 1 ENTERED IN ERROR;[03] REMOVED AND REPLACED WIGGLE PLATE AT LT WING
- [SDR SWAA2023121318899](https://openairdocs.org/sdr/SWAA2023121318899.md): Skin · cracked · Nov 7, 2023 · N233LV · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON LH HORIZONTAL STABILIZER LWR SKIN AT STAB STA 193.90;16.5' FROM FRONT SPAR; I/B ROW. CRACK LENGTH: 0.718' CRACK FOUND ON LH HORIZONTAL STABILIZER LWR SKIN AT STAB STA 193.9016.5' FROM FRONT SPAR I/B ROW. CRACK LENGTH: 0.718'<[01] ACCOMPLISHED
- [SDR SWAA2023121319117](https://openairdocs.org/sdr/SWAA2023121319117.md): Rib · cracked · Nov 7, 2023 · N233LV · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > R/H HORIZONTAL STAB RIB #4 STA. 120.30 STIFFENER #3 CRACKED AT LWR RADIUS<[01] ACCOMPLISHED REPAIR AT R/H HORIZONTAL STAB RIB #4 STA. 120.30 STIFFENER #3 PER SRM 55-10-09-2R-5 REPAIR 5;[02] VERIFIED REPAIR ACCOMPLISHED
- [SDR SWAA2023121319348](https://openairdocs.org/sdr/SWAA2023121319348.md): Plate · cracked · Nov 7, 2023 · N233LV · Boeing 7377H4 · Wing Miscellaneous Structure
  > RT WING FIXED T/E AT REAR SPAR LOWER CHORD APPROX ORSS 322 WIGGLE PLATE IS BENT AND PHENOLIC SUPPORT IS CRACKED. 124-002<[01] REMOVED AND INSTALLED NEW WIGGLE PLATE AT R/W FIXED T/E REAR SPAR LWR CHORD APPROX ORSS 322 AS-PER SRM 51-40-02-0G-0;[02] VERIFIED PLA
- [SDR SWAA2023121318436](https://openairdocs.org/sdr/SWAA2023121318436.md): Attach Bracket · cracked · Nov 5, 2023 · N233LV · Boeing 7377H4 · Trailing Edge Flaps
  > L/H WING T/E @ WS 278.50 DEFLECTION RIB I/B SIDE ATTACHMENT BRACKET CRACKED.<[01] REMOVED AND INSTALLED NEW BRACKET AT L/W DEFFLECTION RIB I/B SIDE @ WS 278.50 ASPER SRM 51-40-02-0G-0;[02] VERIFIED BRACKET REPLACED
- [SDR SWAA2023121318432](https://openairdocs.org/sdr/SWAA2023121318432.md): Skin · cracked · Nov 5, 2023 · N233LV · Boeing 7377H4 · Leading Edge Devices
  > R/H WING L/E #8 SLAT NOSE SKIN AT ACTUATOR RIB HAS CRACKS AROUND FASTENER HEAD. (18-002)<[01] ACCOMPLISHED REPAIR AT R/H WING L/E #8 SLAT NOSE SKIN AT ACTUATOR RIB AS PER SRM 57-42-01-2R-8.;[02] VERIFIED REPAIR ACCOMPLISHED
- [SDR SWAA2023121318437](https://openairdocs.org/sdr/SWAA2023121318437.md): Panel · cracked · Nov 5, 2023 · N233LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO PANEL #120YAC CRACKED<[01] RECIEVED NEW PANEL; INSTALLATION COMPLETED ON TASK [TTG8Q00NCLSK].;[02] VERIFIED PANEL RECIEVED AND INSTALLATION TO BE ACCOMPLISHED ON TTG8Q00NCLSK
- [SDR SWAA2023121318422](https://openairdocs.org/sdr/SWAA2023121318422.md): Door · cracked · Nov 5, 2023 · N233LV · Boeing 7377H4 · Landing Gear Doors
  > LH GEAR DOOR CRACKED<[01] REMOVED AND REPLACED LH GEAR DOORS REFERENCE AMM 32-13-11-000-803 & AMM 32-13-11-420-803;[02] RII---VERIFIED AND INSPECTED STEP #1 ADJUSTED L/H MAIN GEAR DOOR.
- [SDR SWAA2023102715125](https://openairdocs.org/sdr/SWAA2023102715125.md): Lens · loose · Oct 26, 2023 · N233LV · Boeing 7377H4 · Emergency Lighting
  > L1 EXTERIOR EMERGENCY EXIT LIGHT LENS APPEARS LOOSE<[01] RESECURED EMERGENCY EXIT LENS BY L1 DOOR PER AMM 33-51-00.
- [SDR SWAA2023102412996](https://openairdocs.org/sdr/SWAA2023102412996.md): Slide · out of adjust · Oct 21, 2023 · N233LV · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR ESCAPE SLIDE GIRT BAR GOT CAUGHT A LITTLE BIT WHILE OPENING THE DOOOR<[01] REMOVED FWD SERVICE DOOR ESCAPE SLIDE IAW AMM CHPT. 25-66-01;[02] REMOVED AND REPLACED FWD SERVICE DOOR ESCAPE SLIDE IAW MT 725-61-06 AND AMM CHPT. 25-66-01
- [SDR SWAA2023072881938](https://openairdocs.org/sdr/SWAA2023072881938.md): Seal · cracked · Jul 25, 2023 · N233LV · Boeing 7377H4 · Empennage Structure
  > THE RIGHT UPPER HORIZONTAL STAB TO BODY FRONT SLIDING SEAL IS CRACKED.<[01] REMOVED AND REPLACED SEAL PER AMM 53-31-31
- [SDR SWAA2023070675707](https://openairdocs.org/sdr/SWAA2023070675707.md): Battery Pack · inoperative · Jul 6, 2023 · N233LV · Boeing 7377H4 · Emergency Lighting
  > R1 DOOR EMERGENCY LIGHT AND SECONDARY LIGHT INOP<[01] REMOVED AND REPLACED M1675 BATTERY PACK IAW AMM 33-51-06. OPERATIONAL TESTED SATISFACTORY AT THIS TIME
- [SDR SWAA2023031312104](https://openairdocs.org/sdr/SWAA2023031312104.md): Fitting · cracked · Mar 3, 2023 · N233LV · Boeing 7377H4 · Wing Miscellaneous Structure
  > DOT A24-55 #1 STRUT HYDRAULIC LINE CLAMP SUPPORT FITTING CRACKED JUST O/B OF AFT DIAGONAL BRACE FITTING.<[01] REMOVED SUPPORT FITTING I.A.W SRM 51-40-02-0G-0;[02] TRANSFERRED HOLES FROM OLD PART TO NEW P/N 272A9125-11 FITTING IAW SRM 51-40-05-0G-0 AND BOEING D
- [SDR SWAA2023031312455](https://openairdocs.org/sdr/SWAA2023031312455.md): Stiffener · cracked · Mar 1, 2023 · N233LV · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > A225-008 #1 I/B FAN COWLI OIL ACCESS DOOR AFT INTERIOR STIFFNER CRACKED.<[01] REMOVED CRACKED STIFFENER IAW SRM 51-40-02-0G-0.;[02] DRILLED NEW P/N 314-2259-4 SHIELD IAW SRM 51-40-05-0G-0 AND CMM 71-13-30.;[03] VERIFIED STEPS AND OK TO INSTALL;[04] STARTED INS
- [SDR SWAA2023031311572](https://openairdocs.org/sdr/SWAA2023031311572.md): Doubler · debonded · Mar 1, 2023 · N233LV · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > A225-011 ANTENNA DOUBLER IS DISBONDING AT 0 BL BS 663 - 27'.<[01] REPAIRED ANTENNA DOUBLER FILLET AT 0 BL; BS 663-27' I.A.W. AMM 51-31-00-390-812;[02] VERIFIED TASK COMPLETE

Next page: https://openairdocs.org/deregistered/N233LV-2026-06-05/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 = 'N233LV' AND deregistration_id = 'N233LV-2026-06-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N233LV-2026-06-05/reports

---
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