# N786SW: 2000 Boeing 737-7H4, registration cancelled 2025-10-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 1, 2025
- 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: 29811
- Year built: 2000
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 31, 2000
- Certificate issued: December 5, 2000
- Last registry action: July 22, 2023
- Mode S code: AAA875
- 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/N786SW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=786SW
- Page: https://openairdocs.org/deregistered/N786SW-2025-10-01

From the FAA registry file of October 28, 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 (257, newest 50)

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

- [SDR SWAA2024080723039](https://openairdocs.org/sdr/SWAA2024080723039), Aug 6, 2024: MEGAPHONE. FAILED. FWD MEGAPHONE DOES NOT TEST<[01] REMOVED AND REPLACED MEGAPHONE IAW AMM 25-64-00
- [SDR SWAA2024070105857](https://openairdocs.org/sdr/SWAA2024070105857), Jun 26, 2024: INDICATION SYS. FALSE INDICATION. IN CRUISE 'A' SYSTEM HYDRAULICS DROPPED TO 56% SUSPECTED LEAK NO 30 HIST<[01] OK TO CONTINUE PER MEL 29-11-01; C/W SP-1; AUTHORIZATION # 200538;[02] AFTER FURTH
- [SDR SWAA2024050983522](https://openairdocs.org/sdr/SWAA2024050983522), May 8, 2024: BALANCE WEIGHT. CORRODED. RUDDER WEIGHT MISSING MATERIAL AND CORRODED<[01] R&R RUDDER WEIGH PER CMM 55-40-09;[02] INSPECTION C/W R&R RUDDER WEIGH PER CMM 55-40-09
- [SDR SWAA2024041173528](https://openairdocs.org/sdr/SWAA2024041173528), Apr 10, 2024: SLIDE. LOOSE. EMERGENCY SLIDE, AFT FO SIDE, HAS EXCESS MATERIAL EXPOSED. ONLY VISIBLE WHEN DOOR IS ARMED. INSPECTED AFT SERVICE DOOR EMERGENCY SLIDE IAW AMM 25-66-01. FOUND S
- [SDR SWAA2024031362199](https://openairdocs.org/sdr/SWAA2024031362199), Mar 12, 2024: FLOOR PANEL. CRACKED. FWD CARGO PIT AFT FLOOR HAS CRACKS.<[01] OK TO CONTINUE AS PER MEL 25-16-01 SP1B AUTH#183645;[02] REMOVED AND REPLACED FWD CARGO AFT FLOOR PANEL PER AMM 25-52-1
- [SDR SWAA2024012242897](https://openairdocs.org/sdr/SWAA2024012242897), Jan 20, 2024: FAIRING. DELAMINATED. WING-TO-BODY FAIRING PANEL 194CL HAS PUNCTURE DAMAGE WITH DELAM IN OUTER SKIN. -MARKED-<[01] REMOVED AND REPLACED PANEL 194CL IN REF WITH AMM 20-50-11.
- [SDR SWAA2024012242899](https://openairdocs.org/sdr/SWAA2024012242899), Jan 20, 2024: PANEL. DELAMINATED. WING-TO-BODY FAIRING PANEL 194CR HAS TWO PUNCTURE DAMAGED AREAS WITH DELAM. -MARKED-<[01] REMOVED AND REPLACED 194CR PANEL IN REF WITH AMM 20-51-11 AND TASK CAR
- [SDR SWAA2024012242898](https://openairdocs.org/sdr/SWAA2024012242898), Jan 20, 2024: FAIRING. PULLED. WING-TO-BODY FAIRING PANEL 193AR SEVERAL SCREWS PULLED THROUGH AT THE IB END OF PANEL.<[01] REMOVED AND REPLACED 193AR PANEL IN REF WITH AMM 20-51-11 AND TASK C
- [SDR SWAA2024012242900](https://openairdocs.org/sdr/SWAA2024012242900), Jan 20, 2024: FAIRING. PULLED. WING-TO-BODY FAIRING PANEL 194CR HAS A SCREW PULLED THROUGH AT THE FWD IB MOST CORNER.<[01] REMOVED AND REPLACED 194CR PANEL IN REF WITH AMM 20-51-11 AND TASK C
- [SDR SWAA2024012242901](https://openairdocs.org/sdr/SWAA2024012242901), Jan 20, 2024: FAIRING. BULGED. WING-TO-BODY FAIRING PANEL 193AR HAS TWO BULGED AREAS IN EXTERIOR SKIN WITH TAP TEST SOUND OF DELAM. -MARKED-<[01] REMOVED AND REPLACED 193AR PANEL IN REF WITH 
- [SDR SWAA2023122735208](https://openairdocs.org/sdr/SWAA2023122735208), Dec 24, 2023: DOOR. DELAMINATED. RT AC BAY DOOR; RT FWD O/B CORNER DELAM; MEASURES 4.25' X 4.25'<[01] REFERENCE EA 23-153-03744
- [SDR SWAA2023100908178](https://openairdocs.org/sdr/SWAA2023100908178), Oct 6, 2023: TAIL CONE. DELAMINATED. LEFT WING #3 FLAP FAIRING TAIL CONE DELAMINATED.<[01] REMOVED AND REPLACED LH WING #3 FLAP FAIRING TAIL CONE PER SRM 51-40-02
- [SDR SWAA2023091499492](https://openairdocs.org/sdr/SWAA2023091499492), Sep 12, 2023: SLIDE. OUT OF ADJUST. AFT SVC DOOR SLIDE HAS EXCESS MATERIAL OUT OF SLIDE COVER<[01] REPOSITIONED SLIDE ASSY REF AMM 25-66-01 / MT 725-61-06
- [SDR SWAA2023062972746](https://openairdocs.org/sdr/SWAA2023062972746), Jun 29, 2023: STUD. MISSING. AFT CARGO DOOR HANDLE TEFLON STUD MISSING<[01] INSTALLED AFT CARGO DOOR HANDLE TEFLON STUD PER AMM 52-31-14.
- [SDR SWAA2023052552297](https://openairdocs.org/sdr/SWAA2023052552297), May 25, 2023: LIGHT. INOPERATIVE. R1 DOOR ESCAPE SLIDE EMERGENCY LIGHT INOP.<[01] RELAMPED R1 EXTERNAL SLIDE EMERGENCY LIGHT.<BR>IAW B737 MM 33-51-04
- [SDR SWAA2023050131173](https://openairdocs.org/sdr/SWAA2023050131173), Apr 25, 2023: COVER. BROKEN. RH LOWER EMERGENCY EXIT LIGHT COVER BROKEN<[01] REPLACED RH LOWER EMERGENCY EXIT LIGHT COVER PER AMM 33-51-01
- [SDR SWAA2022101860517](https://openairdocs.org/sdr/SWAA2022101860517), Oct 17, 2022: SIGN. INOPERATIVE. CUSTOMER WALK. L-1 DOOR EMERGENCY LIGHT TWO BULBS OUT NEED SIX WORKING. / [01] RELAMPED L-1 DOOR EMERGENCY EXIT SIGN 2EA AS PER REF B737 AMM 33-51-01-960-801. T
- [SDR SWAA2022101858000](https://openairdocs.org/sdr/SWAA2022101858000), Oct 9, 2022: SIGN. BROKEN. R-1 DOOR LOWER EXIT SIGN LENS BROKEN / [01] REMOVED AND REPLACED R-1 DOOR LOWER EXIT SIGN. REF. BOEING 737-700 AMM 33-51-01-960-802.;[02] VERIFIED 1
- [SDR SWAA2022101858004](https://openairdocs.org/sdr/SWAA2022101858004), Oct 9, 2022: SIGN. BROKEN. R-2 DOOR LOWER EXIT SIGN BROKEN / [01] REMOVED AND REPLACED R2 LOWER EXIT SIGN AS PER AMM 33-51-01-960-802-NG.;[02] VERIFIED STEP 1
- [SDR SWAA2022101852289](https://openairdocs.org/sdr/SWAA2022101852289), Oct 3, 2022: SIGN. BROKEN. L-1 DOOR LOWER EXIT SIGN LENS BROKEN. / [01] REMOVED AND REPLACED L-1 DOOR LOWER EXIT SIGN. REF. BOEING 737-700 AMM 33-51-01-960-802.;[02] VERIFIED 1
- [SDR SWAA2022101851666](https://openairdocs.org/sdr/SWAA2022101851666), Oct 1, 2022: PANEL. DETERIORATED. PANEL 231XF (PANEL 231XF FLOOR PANEL) UPPER SURFACE RESIN DETERIORATED / [01] MEASUREMENTS;[02] PREPARED AND REPAIRED FLOOR PANEL #231XF AT DAMAGED AREA PER B73
- [SDR SWAA2022101951668](https://openairdocs.org/sdr/SWAA2022101951668), Oct 1, 2022: SKIN PANEL. CRACKED. RT WING LOWER MID SPAN T/E PANEL 661BB - INNER SKIN HAS CRACKS AND BULGING AROUND NUMEROUS FASTENER HOLES AS MARKED. 124-023 / [01] CLEANED AND PREPARED DAMAGE 
- [SDR SWAA2022101851221](https://openairdocs.org/sdr/SWAA2022101851221), Sep 30, 2022: SCUFF PLATE. CRACKED. AFT CARGO AFT CORNER SCUFF PLATE CRACKED / [01] RECEIVED SCUFF PLATE PART # 146A8341-9 FROM JL WELDING TAG #011178 LOCATED AND DRILLED AS PER B 737-700 SRM 51-4
- [SDR SWAA2022101949319](https://openairdocs.org/sdr/SWAA2022101949319), Sep 29, 2022: RIB. CRACKED. LEFT HORIZONTAL STABILIZER LEADING EDGE; INTERNAL #3 RIB CRACK NOTED (DOT-223 LHLE3). / [01] REMOVED #3 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0
- [SDR SWAA2022101949318](https://openairdocs.org/sdr/SWAA2022101949318), Sep 29, 2022: RIB. CRACKED. LEFT HORIZONTAL STABILIZER LEADING EDGE; INTERNAL #5 RIB CRACK NOTED AT RIVET EDGE HOLE (DOT-223 LHLE5). / [01] REMOVED L/H HORIZONTAL STAB #5 RIB AS PER B737-7
- [SDR SWAA2022101949317](https://openairdocs.org/sdr/SWAA2022101949317), Sep 29, 2022: RIB. CRACKED. LEFT HORIZONTAL STABILIZER LEADING EDGE; INTERNAL #4 RIB CRACK NOTED AT RIVET EDGE HOLE (DOT-223 LHLE4). / [01] REMOVED #4 RIB AT L/H HORIZONTAL STAB L/E AS PER
- [SDR SWAA2022101949316](https://openairdocs.org/sdr/SWAA2022101949316), Sep 29, 2022: RIB. CRACKED. LEFT HORIZONTAL STABILIZER LEADING EDGE; INTERNAL #2 RIB CRACK NOTED (DOT-223 LHLE2). / [01] REMOVED #2 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0
- [SDR SWAA2022101852288](https://openairdocs.org/sdr/SWAA2022101852288), Sep 28, 2022: FLOOR PANEL. DELAMINATED. PANEL 241AF HAS SURFACE DELAMINATION / [01] MEASUREMENTS;[02] CLEANED AND PREPARED DAMAGE AREAS AS MARKED FOR REPAIR ON TOP SURFACE OF MAIN CABIN FLOOR PANEL 24
- [SDR SWAA2022092082832](https://openairdocs.org/sdr/SWAA2022092082832), Sep 17, 2022: NONE. MISSING. EXIT SALINA SIGN MISSING FROM RH OVERWING EXIT / [01] INSTALL EXIT SALIDA COVER ON RH OVER WING EXIT DOOR PER SIP
- [SDR SWAA2022091252175](https://openairdocs.org/sdr/SWAA2022091252175), Sep 11, 2022: PANEL. SMOKE. AFT #1 COFFEE POT SMELLS OF ELECTRICAL SMOKE WHEN ON / [01] REMOVED AND REPLACED #1 COFFEE MAKER IAW AMM 25-30-01 OPS CK GOOD
- [SDR SWAA2022071126631](https://openairdocs.org/sdr/SWAA2022071126631), Jul 7, 2022: FLAP. DELAMINATED. LEFT WING OUTBOARD AFT FLAP HAS SEVERAL SPOTS OF DELAMINATION ON THE UNDER AND UPPER SIDE OF THE INBOARD 15 INCHES. (MARKED) / [01] REPAIRED AFT FLAP PER SRM 51
- [SDR SWAA2022071126003](https://openairdocs.org/sdr/SWAA2022071126003), Jul 5, 2022: LENS. BROKEN. CREW REPORTS FWD ENTRY EMERGENCY EXIT SIGN LENS IS BROKEN / [01] C/W EA M-21-133-00720
- [SDR SWAA2022031181441](https://openairdocs.org/sdr/SWAA2022031181441), Mar 9, 2022: LENS. MISSING. RIGHT OVERWING EMERGENCY EXIT LIGHT LENS ( AFT SIDE) MISSING DIRECTIONAL ARROW / [01] R & R LENS IAW AMM 33-51-01;[02] INSPECTED
- [SDR SWAA2021120249457](https://openairdocs.org/sdr/SWAA2021120249457), Dec 2, 2021: LIGHT. INOPERATIVE. LH OUTER OVERWING EMERGENCY EXIT LIGHT INOP ; / [01] RELAMPED LH OUTER OVERWING EMER LIGHT IAW 33-51-04. OPS CHECKS GOOD.
- [SDR SWAA2021112446451](https://openairdocs.org/sdr/SWAA2021112446451), Nov 20, 2021: FITTING. CORRODED. SUPPLEMENTAL INFORMATION: LFT MLG FWD TRUNNION SUPPORT FITTING UPPER O/B (#1) BORE HAS EVIDENCE OF CORROSION ; LFT MLG FWD TRNNION SPPORT FITTING PPER O (#1) OR
- [SDR SWAA2021112446450](https://openairdocs.org/sdr/SWAA2021112446450), Nov 20, 2021: FITTING. CORRODED. SUPPLEMENTAL INFORMATION: LFT MLG FWD TRUNNION SUPPORT FITTING; LOWER O/B LUG (#3) BORE HAS EVIDENCE OF CORROSION ; LFT MLG FWD TRNNION SPPORT FITTING; LOWER O 
- [SDR SWAA2021111842925](https://openairdocs.org/sdr/SWAA2021111842925), Nov 11, 2021: NONE. BROKEN. RT WING I/B FIXED T/E DEFLECTOR RIB LOWER SIDE ROD ATTACH LUG BROKEN. ; / [01] TRIMMED OUT AND REMOVED DMG TURNBUCKLE LUG AS PER B737-700 SRM 57-51-02-2R-2 REPA
- [SDR SWAA2021111742225](https://openairdocs.org/sdr/SWAA2021111742225), Nov 10, 2021: BATTERY PACK. INOPERATIVE. INTERNAL EMERGENCY EXIT SIGN INOP; AT LEFT OVERWING DOOR. DURING T/S FOUND BATTERY PACK INOPERATIVE. REMOVED AND REPLACED BATTERY AND PERFORMED TEST; TEST PASSE
- [SDR SWAA2021111742223](https://openairdocs.org/sdr/SWAA2021111742223), Nov 10, 2021: BATTERY PACK. OUT OF POSITION. INTERNAL EMERGENCY EXIT SIGN INOP AT R/H OVERWING DOOR. REPOSITIONED BATTERY PACK ; PERFORMED OPERATIONAL TEST; TEST PASS IAW AMM 33-51-06=960-805.
- [SDR SWAA2021111838750](https://openairdocs.org/sdr/SWAA2021111838750), Oct 29, 2021: CAP. CORRODED. AFT CARGO FLOOR L/H CAP STRIPS WITH CORROSION ; / [01] AFT CARGO FLOOR L/H CAP STRIPS WITH EXFOLIATION CORROSION PASSING THROUGH MATERIAL; [02] RECEIVED CAP STR
- [SDR SWAA2021111838751](https://openairdocs.org/sdr/SWAA2021111838751), Oct 29, 2021: CAP. CORRODED. AFT CARGO FLOOR R/H CAP STRIPS WITH CORROSION ; / [01] AFT CARGO FLOOR R/H CAP STRIPS WITH EXFOLIATION CORROSION PASSING THROUGH MATERIAL; [02] RECEIVED CAP STR
- [SDR SWAA2021111838752](https://openairdocs.org/sdr/SWAA2021111838752), Oct 29, 2021: CAP. CORRODED. AFT CARGO COMPARTMENT CAP STRIPS FWD AND AFT SIDE OF CARDO DOOR CUTOUT WITH CORROSION ; / [01] AFT CARGO COMPARTMENT CAP STRIPS FWD AND AFT SIDE OF CARGO DOOR C
- [SDR SWAA2021111833916](https://openairdocs.org/sdr/SWAA2021111833916), Oct 26, 2021: INTERCOSTAL. CRACKED. FWD CARGO COMPARTMENT FLOOR STRUCTURE INTERCOSTAL S25L BETWEEN STA 500B-500C CRACKED ; / [01] REMOVED DAMAGE INTERCOSTAL FROM FWD CARGO PER 737-700 SRM 51-40-02
- [SDR SWAA2021111833917](https://openairdocs.org/sdr/SWAA2021111833917), Oct 26, 2021: INTERCOSTAL. CRACKED. FWD CARGO COMPARTMENT FLOOR STRUCTURE INTERCOSTAL S25L BETWEEN STA 500-500A CRACKED ; / [01] REMOVED DAMAGE INTERCOSTAL FROM FWD CARGO PER 737-700 SRM 51-40-02-
- [SDR SWAA2021111832175](https://openairdocs.org/sdr/SWAA2021111832175), Oct 20, 2021: RIB. CRACKED. RT HORIZONTAL STAB NR 4 INSPAR RIB HSS 120 FWD LOWER OTBD CORNER CRACKED. REMOVED CRACK IAW SRM 51-10-02-0G-0 & 55-10-09-2R-5 REPAIR 5. PERFORMED HFEC INSP OF C
- [SDR SWAA2021111831843](https://openairdocs.org/sdr/SWAA2021111831843), Oct 19, 2021: RETAINER. CRACKED. RT WING T/E AT FLEX CONTROL RIB; TOP PANEL SEAL RETAINER CRACKED. REMOVED AND REPLACED R/H WING AT FLEX CONTROL RIB TOP PANEL SEAL RETAINER AS PER B737-700 SOPM
- [SDR SWAA2021101830289](https://openairdocs.org/sdr/SWAA2021101830289), Oct 14, 2021: RUB STRIP. MISSING. AT FRAME BS 235.8 MISSING SECTION WHERE INITIAL RUBBING STRIP ATTACH. TRIMMED DAMAGE AREA AT FRAME STA 235.8 PER SRM 51-10-02-0G-0 VERIFIED STEP 1. PERFORMED HF
- [SDR SWAA2021111829855](https://openairdocs.org/sdr/SWAA2021111829855), Oct 13, 2021: SHIELD. CORRODED. AFT CARGO COMPARTMENT FLOOR STRUCTURE SHIELD PANEL AT S-25R BETWEEN STA 847-867 WITH EXFOLIATION CORROSION ; / [01] REMOVED CORROSION FROM AFT CARGO SHIELF STA 
- [SDR SWAA2021111829276](https://openairdocs.org/sdr/SWAA2021111829276), Oct 11, 2021: PANEL. CRACKED. FLAP SUPPORT NO.8 PANEL 644EB LOWER SECTION CRACKED/DELAMINATED ; / [01] REMOVED DAMAGED PLIES AND PREPARED DAMAGED AREA FOR REPAIR AT PANEL 644EB AS PER B737-7
- [SDR SWAA2021111828877](https://openairdocs.org/sdr/SWAA2021111828877), Oct 8, 2021: NONE. CRACKED. LOWER FUSELAGE CENTER WING L/H AIR CONDITIONING EXHAUST AIR EXIT SEAL RETAINER CRACKED @ INB. SIDE ;STA 663.75 MKD DOT ; / [01] REMOVED PREVIOUS REPAIR FOR ACCE

All 257: https://openairdocs.org/deregistered/N786SW-2025-10-01/reports.md

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