# N754SW: 1999 Boeing 737-7H4, registration cancelled 2024-10-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 4, 2024
- 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: 29849
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 9, 1999
- Certificate issued: December 15, 1999
- Last registry action: July 21, 2023
- Mode S code: AA2A8A
- 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/N754SW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=754SW
- Page: https://openairdocs.org/deregistered/N754SW-2024-10-04

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 (298, newest 50)

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

- [SDR SWAA2023071176799](https://openairdocs.org/sdr/SWAA2023071176799), Jul 10, 2023: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS AT ROWS 9ABC; 12ABC; AND 14ABC INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT POSITION M1670 PER AMM 33-51-06
- [SDR SWAA2023070674450](https://openairdocs.org/sdr/SWAA2023070674450), Jul 2, 2023: PRESSURE SYSTEM. FAULTED. LOSS OF CABIN PRESSURE AT 36K FEET EMERGENCY DESCENT PERFORMED CABIN ALT WARNING HORN SOUNDED PAX OXY MASKS DEPLOYED. EMERGENCY DECLARED LANDING UNEVENTFUL. ACC
- [SDR SWAA2023062370585](https://openairdocs.org/sdr/SWAA2023062370585), Jun 22, 2023: COVER. OUT OF ADJUST. FWD ENTRY DOOR EXIT LIGHT COVER CAME OFF<[01] INSTALLED COVER AS PER SIP.
- [SDR SWAA2023061959880](https://openairdocs.org/sdr/SWAA2023061959880), Jun 16, 2023: FLAP. DELAMINATED. LH OUTBOARD AFT FLAP IS DELAMINATED ON INBOARD AFT CORNER DELAMINATION MEASURES APRROX 1.25IN BY 4.5IN ON LOWER SKIN<[01] VERIFIED THE DAMAGE RECORD ENTERED; AN
- [SDR SWAA2023061959881](https://openairdocs.org/sdr/SWAA2023061959881), Jun 16, 2023: FLAP. DELAMINATED. RH OUTBOARD AFT FLAP IS DELAMINATED ON INBOARD AFT CORNER DELAMINATION MEASURES APRROX 2IN BY 3.5IN ON UPPER SKIN<[01] VERIFIED THE DAMAGE RECORD ENTERED; AND C
- [SDR SWAA2023013196494](https://openairdocs.org/sdr/SWAA2023013196494), Jan 28, 2023: GIRT BAR. DAMAGED. FWD ENTRY DOOR SLIDE GIRT BAR MISSING STOP RING<[01] INSTALLED MISSING FWD ENTRY DOOR SLIDE GIRT BAR STOP RING IAW AMM 25-66-01.
- [SDR SWAA2023013196493](https://openairdocs.org/sdr/SWAA2023013196493), Jan 28, 2023: SIGN. DAMAGED. EMERGENCY EXIT SIGN FELL OFF AT L1 DOOR<[01] RE-INSTALLED EXIT SIGN PER SIP
- [SDR SWAA2022120176659](https://openairdocs.org/sdr/SWAA2022120176659), Nov 30, 2022: FAIRING. DAMAGED. FOUND 2 LOCK FASTENER HOLES ON THE LT STRUT FAIRING ELONGATED ON THE LT SIDE. REPAIRED THE DAMAGEIAW EA 22-154-03528.
- [SDR SWAA2022092830341](https://openairdocs.org/sdr/SWAA2022092830341), Sep 26, 2022: PANEL. DAMAGED. 193B FASTENER HOLES AT POSITIONS 7; 8; 18; 20; 25; 26 AND 33 HAVE BEEN ELONGATED. 193B FASTENER HOLES AT POSITIONS 7 8 18 20 25 26 AND 33 HAVE BEEN ELONGATED. /
- [SDR SWAA2022092283045](https://openairdocs.org/sdr/SWAA2022092283045), Sep 18, 2022: SLIDE. OUT OF POSITION. L1 DOOR SLIDE NEEDS REPOSITIONED / [01] REPOSITIONED L1 DOOR SLIDE PER S.I.P.
- [SDR SWAA2022081240386](https://openairdocs.org/sdr/SWAA2022081240386), Aug 10, 2022: COVER. LOOSE. RIGHT AFT ESCAPE SLIDE PULL STRAP IS NOT SECURED. / [01] RESECURED AFT RH ESCAPE SLIDE PULL STRAP COVER AS REQUIRED PER SIP.
- [SDR SWAA2022052309686](https://openairdocs.org/sdr/SWAA2022052309686), May 19, 2022: MEGAPHONE. FAILED. FWD GALLEY MEGAPHONE BATTERY IS DEPLETED / [01] R&R FWD MEGAPHONE AS NEEDED AMM 25-64-00. OPS CHK GOOD.
- [SDR SWAA2022052310324](https://openairdocs.org/sdr/SWAA2022052310324), May 19, 2022: MEGAPHONE. FAILED. FWD GALLEY MEGAPHONE BATTERY IS DEPLETED / [01] R&R FWD MEGAPHONE AS NEEDED AMM 25-64-00. OPS CHK GOOD.
- [SDR SWAA2021091010655](https://openairdocs.org/sdr/SWAA2021091010655), Aug 24, 2021: RIB. CRACKED. CRACK LEADING EDGE SKIN ACCESS PANEL 341B AT STA 95.96 AT RT HORIZONTAL STABILIZER (1 EA) ; 2021-368797 / [01] TOOK MEASURES OF CRACK RIB LEADING EDGE SKIN ACCE
- [SDR SWAA2021091010656](https://openairdocs.org/sdr/SWAA2021091010656), Aug 24, 2021: RIB. CRACKED. CRACK LEADING EDGE SKIN ACCESS PANEL 341B AT STA 105.26 AT RT HORIZONTAL STABILIZER (1 EA) ; 2021-368798 / [01] TOOK MEASURES OF CRACK RIB LEADING EDGE SKIN ACC
- [SDR SWAA2021091007193](https://openairdocs.org/sdr/SWAA2021091007193), Aug 13, 2021: RIB. CRACKED. CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER ; 2021-368760 / [01] TOOK MEASURE OF CRACK INSPAR RIB LOCATED ST
- [SDR SWAA2021091007194](https://openairdocs.org/sdr/SWAA2021091007194), Aug 13, 2021: ANGLE. CRACKED. CRACK ON ANGLE AT PLENUM RT APU AIR INLET ; 2021-368759 / [01] REMOVED ANGLE AND FASTENERS AT PLENUM RT APU AIR INLET IAW B737-700 SRM 51-40-02 AND PERFORMED VI
- [SDR SWAA2021091005853](https://openairdocs.org/sdr/SWAA2021091005853), Aug 11, 2021: SUPPORT ANGLE. CRACKED. CRACK FRONT SPAR SUPPORT ANGLE LOCATED AT IFSS 120 AT LT WING ; 2021-368744 / [01] REMOVED SUPPORT ANGLE LOCATED FRONT SPAR WEB AT IFSS 120 AT LT WING IAW B737-
- [SDR SWAA2021091005852](https://openairdocs.org/sdr/SWAA2021091005852), Aug 11, 2021: SPAR. CORRODED. CORROSION FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APPROX; LOWER AREA AT LT WING ; 2021-368745 / [01] TOOL USED/ EDDY CURRENT PN/ NORTEC 600D; SN/ 200005
- [SDR SWAA2021091005851](https://openairdocs.org/sdr/SWAA2021091005851), Aug 10, 2021: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARMENT ; 2021-368743 / [01] WELDED CRACKS LOCATED AT FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I.A.W BOEING 
- [SDR SWAA2021091005435](https://openairdocs.org/sdr/SWAA2021091005435), Aug 9, 2021: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT ON ACCESS PANEL 834DZ AFT ENTRY DOOR AT AFT GALLEY AREA ; 2021-368699 / [01] REMOVED ANGLE LOC. ON ACCESS PANEL 834DZ AFT ENTRY DOOR AT AF
- [SDR SWAA2021091005436](https://openairdocs.org/sdr/SWAA2021091005436), Aug 9, 2021: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT ON ACCESS PANEL 844DZ AFT SERVICE DOOR AT AFT GALLEY AREA ; 2021-368698 / [01] REMOVED ANGLE LOC. ON ACCESS PANEL 844DZ AFT SERVICE DOOR A
- [SDR SWAA2021091004683](https://openairdocs.org/sdr/SWAA2021091004683), Aug 8, 2021: STUB FRAME. CRACKED. CRACK ON STUB FRAME LOCATED AT BS 294.5 AT LEVEL STR 9R FWD GALLEY DOOR AREA ; 2021-368691 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 14281
- [SDR SWAA2021091004682](https://openairdocs.org/sdr/SWAA2021091004682), Aug 7, 2021: ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS 827 STR 25R AT AFT CARGO COMPARTMENT ; 2021-368685 / [01] REMOVED ANGLE - SUPPORT LOCATED BS 827 STR 25R AT AFT CARGO COMPARTME
- [SDR SWAA2021091004676](https://openairdocs.org/sdr/SWAA2021091004676), Aug 7, 2021: SCUFF PLATE. CRACKED. CUSTOMER REQUEST CRACK SCUFF PLATE FWD CORNER FWD ENTRY DOOR AT FWD GALLEY AREA ; 2021-368687 / [01] EVALUATED SCUFF PLATE FWD CORNER FWD ENTRY DOOR AT FWD GALL
- [SDR SWAA2021091004679](https://openairdocs.org/sdr/SWAA2021091004679), Aug 7, 2021: SCUFF PLATE. CRACKED. CUSTOMER REQUEST CRACK SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA ; 2021-368684 / [01] EVALUATED SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA FOUND CRAC
- [SDR SWAA2021091004678](https://openairdocs.org/sdr/SWAA2021091004678), Aug 7, 2021: ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BETWEEN BS 907 TO BS 927 AND STR 27R TO STR 25R FWD POSITION AFT CARGO COMPARTMENT ; 2021-368686 / [01] TOOK MEASURE OF CRACK ON S
- [SDR SWAA2021091004681](https://openairdocs.org/sdr/SWAA2021091004681), Aug 7, 2021: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BETWEEN BS 907 TO BS 927 AND STR 25R TO STR 27R AFT POSITION AFT CARGO COMPARTMENT ; 2021-368689 / [01] TOOK MEASURE OF CRACK ON S
- [SDR SWAA2021091004680](https://openairdocs.org/sdr/SWAA2021091004680), Aug 7, 2021: SCUFF PLATE. CRACKED. CUSTOMER REQUEST CRACK SCUFF PLATE AFT CORNER FWD ENTRY DOOR AT FWD GALLEY AREA ; 2021-368688 / [01] EVALUATED AFT CORNER SCUFF PLATE AT FWD ENTRY DOOR GALLEY A
- [SDR SWAA2021091003820](https://openairdocs.org/sdr/SWAA2021091003820), Aug 5, 2021: PRESSURE DECK. CRACKED. CRACK WEB PRESSURE DECK HORIZONTAL AT MAIN WHEEL WELL COMPARTME (2 EA) (CRACK 1 LOC. AT RBL 41 AND BS 663; L= 1.125 INCH APPROX; AND CRACK 2 LOC. AT RBL 42 AND 
- [SDR SWAA2021091003792](https://openairdocs.org/sdr/SWAA2021091003792), Aug 5, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS 695 AND BL0 LH SIDE AT PASSENGER CABIN ; 2021-368563 / [01] REMOVED SUPPORT ANGLE LOC. BS 695 AND BL0 LH SIDE AT PASSENGER CABIN 
- [SDR SWAA2021091004665](https://openairdocs.org/sdr/SWAA2021091004665), Aug 5, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED ON BS540 AND BL0 TO LBL24.5 AT PASSENGER CABIN ; 2021-368610 / [01] REPLACED SUPPORT ANGLE LOCATED ON BS540 AND BL0 TO LBL24.5 AT PA
- [SDR SWAA2021091003819](https://openairdocs.org/sdr/SWAA2021091003819), Aug 5, 2021: RIB. CRACKED. CRACK DORSAL FIN RIB FWD POSITION AT VERTICAL STABILIZER ; 2021-368570 / [01] REMOVED RIB LOC. DORSAL FIN FWD POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 5
- [SDR SWAA2021091011165](https://openairdocs.org/sdr/SWAA2021091011165), Aug 5, 2021: BRACKET. CRACKED. CRACK OUTBOARD FAN COWL SUPPORT BRACKET LOC. INTERNAL AREA ACCESS DOOR 424AR ON ENGINE 2 ; 2021-368631 / [01] MEASURED OF CRACK OUTBOARD FAN COWL SUPPORT BRACKE
- [SDR SWAA2021091003811](https://openairdocs.org/sdr/SWAA2021091003811), Aug 5, 2021: BEAR STRAP. CRACKED. CRACK INDICATION FOUND AROUND FASTENERS ON BEAR STRAP (2EA) LOCATED BETWEEN BS 293 TO BS 293.5 AND BETWEEN STR 8 AND STR 9 RH SIDE IN FWD GALLEY AREA LENGTH (1)
- [SDR SWAA2021091003789](https://openairdocs.org/sdr/SWAA2021091003789), Aug 4, 2021: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET TRAILING EDGE DEFLECTION CONTROL RIB ORSS 271 AT LT WING ; 2021-368553 / [01] REMOVED SUPPORT BRACKET TRAILING EDGE DEFLECTION CONTROL RIB
- [SDR SWAA2021091003784](https://openairdocs.org/sdr/SWAA2021091003784), Aug 4, 2021: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 RT WING ; 2021-368530 / [01] REMOVED ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 RT WING
- [SDR SWAA2021091003801](https://openairdocs.org/sdr/SWAA2021091003801), Aug 4, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS 695 AND BL0 RH SIDE AT PASSENGER CABIN ; 2021-368562 / [01] REMOVED SUPPORT ANGLE LOC. BS 695 AND BL0 RH SIDE AT PASSENGER CABIN 
- [SDR SWAA2021091003382](https://openairdocs.org/sdr/SWAA2021091003382), Aug 3, 2021: LIGHT. BROKEN. BROKEN GALLEY 1 EMERGENCY LIGHT ASSY AND LENS AT FWD GALLEY AREA ; 2021-368307 / [01] REPLACED GALLEY 1 EMERGENCY LIGHT ASSY AND LENS AT FWD GALLEY AREA IAW B73
- [SDR SWAA2021091003380](https://openairdocs.org/sdr/SWAA2021091003380), Aug 3, 2021: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT ; 2021-368319 / [01] TOOL USED; DIGITAL CALIPER P/N:500-197-30 S/N: B20189526 DUE DATE 22-NOV-21; [02] REP
- [SDR SWAA2021091003393](https://openairdocs.org/sdr/SWAA2021091003393), Aug 3, 2021: RIB. CRACKED. CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER ; 2021-368396 / [01] TOOK MEASURE OF CRACK INSPAR RIB LOCATED ST
- [SDR SWAA2021091003381](https://openairdocs.org/sdr/SWAA2021091003381), Aug 3, 2021: SPAR. CORRODED. CORROSION FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APPROX AT LT WING ; 2021-368354 / [01] TOOL USED/ EDDY CURRENT PN/ NORTEC 600D; SN/ 2000053402; DUE DA
- [SDR SWAA2021091003396](https://openairdocs.org/sdr/SWAA2021091003396), Aug 3, 2021: BULKHEAD WEB. CRACKED. CUSTOMER REQUEST CRACK BODY STATION 663.75 VAPOR BARRIER APPROX LBL 14 AT MAIN WHEEL WELL COMPARTMENT ; 2021-368398 / [01] TOOL USED CALIPER: P/N:500-197-20 S/N
- [SDR SWAA2021091003394](https://openairdocs.org/sdr/SWAA2021091003394), Aug 3, 2021: RIB. CRACKED. CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER ; 2021-368397 / [01] TOOK MEASURE OF CRACK INSPAR RIB LOCATED ST
- [SDR SWAA2021091002930](https://openairdocs.org/sdr/SWAA2021091002930), Aug 2, 2021: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 194E BODY FAIRING FASTENER HOLES AT LOWER FUSELAGE ; 2021-368288 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: B17030925; DUE DATE: 06-AUG-21.
- [SDR SWAA2021091002931](https://openairdocs.org/sdr/SWAA2021091002931), Aug 2, 2021: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 193D BODY FAIRING HOLES AT LOWER FUSELAGE ; 2021-368286 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: B17030925; DUE DATE: 06-AUG-21.; [02] TO
- [SDR SWAA2021091000852](https://openairdocs.org/sdr/SWAA2021091000852), Aug 2, 2021: ACCESS PANEL. BROKEN. BROKEN ACCESS PANEL 192BR WING TO BODY FAIRING STUDS AT LOWER FUSELAGE (8 EA) ; 2021-368265 / [01] REPLACED STUDS ACCESS PANEL 192BR WING TO BODY FAIRING AT LOW
- [SDR SWAA2021091000853](https://openairdocs.org/sdr/SWAA2021091000853), Aug 2, 2021: FLOOR PANEL. BROKEN. BROKEN FLOOR PANEL 140CF SPLICE PLATE FWD CUT OUT OF DOOR AT AFT CARGO COMPARTMENT ; 2021-368266 / [01] REPLACED PANEL 140CF SPLICE PLATE FWD CUT OUT OF DOOR AT
- [SDR SWAA2021071994278](https://openairdocs.org/sdr/SWAA2021071994278), Jul 13, 2021: STIFFENER. CRACKED. STIFFENER CRACKED ; DIAGONAL STIFFENER CRACKED IN LH AC BAY LOCATED ON WING CENTER SECTION REAR SPAR FIBERGLASS VAPOR BARRIER BETWEEN LBL 6.15 AND LBL 31.83. / 
- [SDR SWAA2021071994280](https://openairdocs.org/sdr/SWAA2021071994280), Jul 13, 2021: PRESSURE DECK. CRACKED. VAPOR BARRIER INTERIM REPAIR APPLIED PER SRM 51-10-10-1A-2 ; APPLIED INTERIM SEAL OVER THE CRACK AT LBL 11.9; 45 FROM PRESSURE DECK THA IN PER SRM 57 -10-10 PAR

All 298: https://openairdocs.org/deregistered/N754SW-2024-10-04/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20170620006419I](https://openairdocs.org/incident/20170620006419I), Jun 20, 2017: Boeing 737-7H4 (N754SW), Latham, NY, No damage. Aircraft N754SW, flight #1766 taxied to runway 19, and began the take-off roll departing from alb to mco. While doing so, PIC received a radio call from ATC…

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