# N233LV: 2006 Boeing 737-7H4, registration cancelled 2026-06-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 5, 2026
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (registry code 1384404)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 32501
- Year built: 2006
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 11, 2006
- Certificate issued: April 19, 2006
- Last registry action: October 13, 2023
- Mode S code: A214B3
- Owner when cancelled: [Southwest Airlines Co](https://openairdocs.org/faa-owner/SOUTHWEST%20AIRLINES%20CO)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: Corporation
- Owner's area on the map: 32.8326° N, 96.8491° W: Placed by OpenAirDocs at the center of ZIP code 75235, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N233LV
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=233LV
- Page: https://openairdocs.org/deregistered/N233LV-2026-06-05

From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 737-7H4: https://openairdocs.org/model/boeing-737-7h4.md

## Service difficulty reports (286, newest 50)

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

- [SDR SWAA2025102125098](https://openairdocs.org/sdr/SWAA2025102125098), Oct 17, 2025: SEAL. CRACKED. 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 PE
- [SDR SWAA2025052273985](https://openairdocs.org/sdr/SWAA2025052273985), May 22, 2025: SLIDE. OUT OF POSITION. 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), Mar 13, 2025: LIGHT. INOPERATIVE. L1 EMERGENCY EXIT LIGHT INOP <[01]. 01 - REMOVED AND REPLACED PER [AMM 33-51-00-501-NG.
- [SDR SWAA2025010382175](https://openairdocs.org/sdr/SWAA2025010382175), Dec 31, 2024: SEAT BACK. OUT OF ADJUST. 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 SEAT
- [SDR SWAA2024111258119](https://openairdocs.org/sdr/SWAA2024111258119), Nov 9, 2024: ATTACH BRACKET. CRACKED. 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
- [SDR SWAA2024082628540](https://openairdocs.org/sdr/SWAA2024082628540), Aug 21, 2024: GIRT BAR. OUT OF ADJUST. 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), Apr 4, 2024: LAMP. INOPERATIVE. 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), Feb 11, 2024: SLIDE. PARTIAL DEPLOY. 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
- [SDR SWAA2023121329974](https://openairdocs.org/sdr/SWAA2023121329974), Dec 10, 2023: HANDLE. LOOSE. 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), Dec 8, 2023: LIGHT. INOPERATIVE. 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), Dec 8, 2023: BATTERY PACK. INOPERATIVE. 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 33-5
- [SDR SWAA2023121324421](https://openairdocs.org/sdr/SWAA2023121324421), Nov 23, 2023: SEAL. CRACKED. 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 FAUL
- [SDR SWAA2023121323694](https://openairdocs.org/sdr/SWAA2023121323694), Nov 21, 2023: SCUFF PLATE. CRACKED. 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 C
- [SDR SWAA2023121323695](https://openairdocs.org/sdr/SWAA2023121323695), Nov 21, 2023: SCUFF PLATE. CRACKED. 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 CORR
- [SDR SWAA2023121322014](https://openairdocs.org/sdr/SWAA2023121322014), Nov 16, 2023: FRAME. ELONGATED. AFT CARGO COMPARTMENT DOOR CUTOUT; AFT FRAME UPPER CORNER; PANEL PLATE HAS ELONGATED FASTENER HOLE.<[01] ACCOMPLISHED EA 23-153-03457 INSTRUCTIONS FOR ELONGATED
- [SDR SWAA2023121322226](https://openairdocs.org/sdr/SWAA2023121322226), Nov 16, 2023: RIB. CRACKED. 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
- [SDR SWAA2023121322013](https://openairdocs.org/sdr/SWAA2023121322013), Nov 16, 2023: STRIP. CRACKED. AFT CARGO COMPARTMENT CAPSTRIP PN 453A2611-5 CRACKED<[01] RECEIVED PART ; WORK WITH BE ACCOMPLISHED ON SEPARATE WORK ORDER PLEASE REFER TO WORK CARD [TTG8Q00PUY
- [SDR SWAA2023121321609](https://openairdocs.org/sdr/SWAA2023121321609), Nov 14, 2023: FRAME. DAMAGED. 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 
- [SDR SWAA2023121320119](https://openairdocs.org/sdr/SWAA2023121320119), Nov 10, 2023: DOOR FRAME. CRACKED. 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;[
- [SDR SWAA2023121320120](https://openairdocs.org/sdr/SWAA2023121320120), Nov 10, 2023: DOOR FRAME. CRACKED. 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] 
- [SDR SWAA2023121319522](https://openairdocs.org/sdr/SWAA2023121319522), Nov 8, 2023: FLOOR PANEL. DELAMINATED. LH PASSENGER CABIN PANEL#221AF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL #141A5810-53 (221AF) INSTALLATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HKSE.;[02] 
- [SDR SWAA2023121319675](https://openairdocs.org/sdr/SWAA2023121319675), Nov 8, 2023: FLOOR PANEL. DELAMINATED. LH PASSENGER CABIN PANEL#221BF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL #141A5810-56 (221BF) INSTALLATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HKSE.;[02] 
- [SDR SWAA2023121319676](https://openairdocs.org/sdr/SWAA2023121319676), Nov 8, 2023: FLOOR PANEL. DELAMINATED. LH PASSENGER CABIN PANEL#221DF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL #141A5810-59 (221DF) INSTALLATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HKSE.;[02] 
- [SDR SWAA2023121319677](https://openairdocs.org/sdr/SWAA2023121319677), Nov 8, 2023: FLOOR PANEL. DELAMINATED. LH PASSENGER CABIN PANEL#221CF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL #141A5810-9 (221CF) INSTALLATION WILL BE ACCOMPLISHED IN N/R: TTG8Q003HKSE.;[02] V
- [SDR SWAA2023121319678](https://openairdocs.org/sdr/SWAA2023121319678), Nov 8, 2023: FLOOR PANEL. DELAMINATED. 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: TTG8Q
- [SDR SWAA2023121319679](https://openairdocs.org/sdr/SWAA2023121319679), Nov 8, 2023: FLOOR PANEL. DELAMINATED. LH PASSENGER CABIN PANEL#241ZF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL 147A5810-98 (241ZF) INSTALLATION WILL BE ACCOMPLISHED IN N/R: TTG8Q00NCL70.;[02] V
- [SDR SWAA2023121319683](https://openairdocs.org/sdr/SWAA2023121319683), Nov 8, 2023: FLOOR PANEL. DELAMINATED. 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
- [SDR SWAA2023121319684](https://openairdocs.org/sdr/SWAA2023121319684), Nov 8, 2023: FLOOR PANEL. DELAMINATED. 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: TTG8Q
- [SDR SWAA2023121319685](https://openairdocs.org/sdr/SWAA2023121319685), Nov 8, 2023: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR ACCESS PANEL#241AAF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL PN #147A5810-8 (241AAF) INSTALATION WILL BE ACCOMPLISHED IN N/R: TTG8Q0
- [SDR SWAA2023121319681](https://openairdocs.org/sdr/SWAA2023121319681), Nov 8, 2023: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR ACCESS PANEL#241ABF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL PN #147A5810-88 (241ABF) INSTALATION WILL BE ACCOMPLISHED IN N/R: TTG8Q
- [SDR SWAA2023121319693](https://openairdocs.org/sdr/SWAA2023121319693), Nov 8, 2023: INTERCOSTAL. CRACKED. 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
- [SDR SWAA2023121319694](https://openairdocs.org/sdr/SWAA2023121319694), Nov 8, 2023: FLOOR PANEL. DELAMINATED. 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: T
- [SDR SWAA2023121319695](https://openairdocs.org/sdr/SWAA2023121319695), Nov 8, 2023: FLOOR PANEL. DELAMINATED. 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: TTG8
- [SDR SWAA2023121319691](https://openairdocs.org/sdr/SWAA2023121319691), Nov 8, 2023: FLOOR PANEL. DELAMINATED. LH PASSENGER CABIN FLOOR ACCESS PANEL#222DF HAS DELAMINATION<[01] RECEIVED NEW FLOOR PANEL #141A5810-185(222DF) INSTALLATION WILL BE ACCOMPLISHED IN N/R: TTG8Q0
- [SDR SWAA2023121319698](https://openairdocs.org/sdr/SWAA2023121319698), Nov 8, 2023: FLOOR PANEL. DELAMINATED. 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: TTG
- [SDR SWAA2023121319700](https://openairdocs.org/sdr/SWAA2023121319700), Nov 8, 2023: PLATE. CRACKED. 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 R
- [SDR SWAA2023121318899](https://openairdocs.org/sdr/SWAA2023121318899), Nov 7, 2023: SKIN. CRACKED. 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 STABILIZ
- [SDR SWAA2023121319117](https://openairdocs.org/sdr/SWAA2023121319117), Nov 7, 2023: RIB. CRACKED. 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 SR
- [SDR SWAA2023121319348](https://openairdocs.org/sdr/SWAA2023121319348), Nov 7, 2023: PLATE. CRACKED. 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 P
- [SDR SWAA2023121318436](https://openairdocs.org/sdr/SWAA2023121318436), Nov 5, 2023: ATTACH BRACKET. CRACKED. 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 
- [SDR SWAA2023121318432](https://openairdocs.org/sdr/SWAA2023121318432), Nov 5, 2023: SKIN. CRACKED. 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 
- [SDR SWAA2023121318437](https://openairdocs.org/sdr/SWAA2023121318437), Nov 5, 2023: PANEL. CRACKED. FWD CARGO PANEL #120YAC CRACKED<[01] RECIEVED NEW PANEL; INSTALLATION COMPLETED ON TASK [TTG8Q00NCLSK].;[02] VERIFIED PANEL RECIEVED AND INSTALLATION TO BE ACCO
- [SDR SWAA2023121318422](https://openairdocs.org/sdr/SWAA2023121318422), Nov 5, 2023: DOOR. CRACKED. 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 ADJ
- [SDR SWAA2023102715125](https://openairdocs.org/sdr/SWAA2023102715125), Oct 26, 2023: LENS. LOOSE. 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), Oct 21, 2023: SLIDE. OUT OF ADJUST. 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] RE
- [SDR SWAA2023072881938](https://openairdocs.org/sdr/SWAA2023072881938), Jul 25, 2023: SEAL. CRACKED. 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), Jul 6, 2023: BATTERY PACK. INOPERATIVE. 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), Mar 3, 2023: FITTING. CRACKED. 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;[0
- [SDR SWAA2023031312455](https://openairdocs.org/sdr/SWAA2023031312455), Mar 1, 2023: STIFFENER. CRACKED. 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 S
- [SDR SWAA2023031311572](https://openairdocs.org/sdr/SWAA2023031311572), Mar 1, 2023: DOUBLER. DEBONDED. 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 

All 286: https://openairdocs.org/deregistered/N233LV-2026-06-05/reports.md

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