# N729SW: 1999 Boeing 737-7H4, registration cancelled 2024-09-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 16, 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: 27861 - Year built: 1999 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 24, 1999 - Certificate issued: June 23, 1999 - Last registry action: March 10, 2023 - Mode S code: A9C6A0 - 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/N729SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=729SW - Page: https://openairdocs.org/deregistered/N729SW-2024-09-16 From the FAA registry file of November 12, 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 (268, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA2022072531022](https://openairdocs.org/sdr/SWAA2022072531022), Jul 19, 2022: FLOOR PANEL. CRACKED. AFT CARGO FLOOR PANEL AFT FROM THE FWD PANEL HAS A CRACK APPROX 20 INCHES LONG / [01] R&R AFT CARGO FLOOR PANEL AFT OF FWD FLOOR PANEL REF MM 25-52-10
P/N 45 - [SDR SWAA2022071327247](https://openairdocs.org/sdr/SWAA2022071327247), Jul 9, 2022: LIGHT. MISSING. EMERGENCY EXIT SIGN LENS COVER MISSING AT LEFT OVERWING EXIT DOOR SIDEWALL. / [01] REPLACED LENS PER AMM 33-51-01. - [SDR SWAA2022062420857](https://openairdocs.org/sdr/SWAA2022062420857), Jun 20, 2022: GIRT BAR. OUT OF POSITION. AFT ENTRY DOOR SLIDE GIRT BAR LOOSE ON STOW HOOK / [01] RESECURED AFT ENTRY DOOR MOUNTED SLIDE GIRT BAR PER AMM 25-66-01. NO FURTHER DEFECTED NOTED. - [SDR SWAA2022021671814](https://openairdocs.org/sdr/SWAA2022021671814), Feb 12, 2022: FLAP. DELAMINATED. ON WALK AROUND FOUND R/H; OUTBOARD; AFT FLAP; LOWER SKIN DELAMINATED. / [01] ADDED EA 22-157-00450 TO FAULT.;[02] REMOVED R/H OUTBOARD AFT FLAP PER AMM 27-51-22 - [SDR SWAA2021081707181](https://openairdocs.org/sdr/SWAA2021081707181), Aug 13, 2021: FUSE. INOPERATIVE. AFT ENTRY ESCAPE SLIDE EMERGENCY LIGHT INOP ; / [01] R+R AFT ENTRY LEFT ESCAPE SLIDE EMERGENCY LIGHT FUSE AT POWER SUPPLY OPS OKAY PER AMM 33-51-06 - [SDR SWAA2021070688861](https://openairdocs.org/sdr/SWAA2021070688861), Jun 29, 2021: LENS. MISSING. FWD SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING DIRECTIONAL ARROW ; / [01] REMOVED AND REPLACED FWD SERVICE DOOR EMERGENCY LIGHT LENS REF AMM 33-51-01. - [SDR SWAA2021070688853](https://openairdocs.org/sdr/SWAA2021070688853), Jun 29, 2021: LENS. MISSING. RIGHT OVERWING EMERGENCY EXIT LOWER FWD LIGHT LENS MISSING DIRECTIONAL ARROW MISSING ; / [01] REMOVED AND REPLACED R/H OVER WING EMERGENCY EXIT FWD LIGHT LENS. - [SDR SWAA2021011140210](https://openairdocs.org/sdr/SWAA2021011140210), Jan 7, 2021: BULB. INOPERATIVE. RT OWE UPPER EMERGENCY EXIT LIGHT, BULB INOPERABLE. RE-LAMPED RT OWE UPPER EMERGENCY EXIT LIGHT BULBS AS NEEDED. PERFORMED GOOD FUNCTIONAL TEST, IAW AMM 33-51-0 - [SDR SWAA2021011140211](https://openairdocs.org/sdr/SWAA2021011140211), Jan 7, 2021: BULB. INOPERATIVE. LT OWE FWD EMERGENCY EXIT LIGHT, BULB INOPERABLE. RELAMPED LT OWE FWD EMERGENCY EXIT LIGHT BULBS AS NEEDED. PERFORMED GOOD FUNCTIONAL TEST, IAW AMM 33-51-01-960 - [SDR SWAA2021080339252](https://openairdocs.org/sdr/SWAA2021080339252), Dec 31, 2020: ISOLATOR. DAMAGED. DAMAGED ISOLATOR ON FRAME STA 360; AT STR 10 L/H. / REPLACED DAMAGED ISOLATOR ON FRAME STA 360 AT STR 10 L/H PER SRM 51-40-02-0G-0; REF IPC 53-11-00-56. - [SDR SWAA2021011137431](https://openairdocs.org/sdr/SWAA2021011137431), Dec 17, 2020: FRAME. CRACKED. WHILE WORKING CRACK ON FWD ENTRY DOOR DISCOVERED FRAME TO BE CRACKED COMMON TO NR 7 STOP PIN ON AFT FRAME. THE DAMAGE WAS REPAIRED, PER ATS ER 20-03739 REV IR A - [SDR SWAA2021080336895](https://openairdocs.org/sdr/SWAA2021080336895), Dec 15, 2020: ISOLATOR. DAMAGED. 1 EACH DAMAGED ISOLATOR ON FWD ENTRY DOOR FWD MID UPPER COVE PANEL. / REMOVED AND REPLACED DAMAGED ISOLATOR ON FWD ENTRY DOOR; FWD MID UPPER COVE PANEL PER SRM - [SDR SWAA2021071436891](https://openairdocs.org/sdr/SWAA2021071436891), Dec 15, 2020: ANGLE. CRACKED. CRACKED VERTICAL ANGLE ON CABLE GUARD INTERCOSTAL BS 693 RBL 1 WL 204-208. / REMOVED AND REPLACED VERTICAL ANGLE ON CABLE GUARD INTERCOSTAL BS693 RBL1 WL204-208 - [SDR SWAA2021011136951](https://openairdocs.org/sdr/SWAA2021011136951), Dec 15, 2020: FLOORBEAM. CORRODED. CORROSION ON BS 259.5 LATERAL BEAM AFT FLANGE UPPER SURFACE WL 208.1 LBL 10 TO RBL 10. CORROSION WAS FOUND TO BE OUT OF LIMITS ON BS 259.5 LATERAL BEAM AFT FLAN - [SDR SWAA2021011136928](https://openairdocs.org/sdr/SWAA2021011136928), Dec 15, 2020: STRINGER. CRACKED. FCB STRINGER 25R CRACKED AT BS 536 ATTACH POINT, MARKED. REPAIRED FWD CARGO BAY STR 25 RT AT BS 536 PER ER 20-03717 REV IR AND EA 21-153-00002 REV IR. - [SDR SWAA2021011136926](https://openairdocs.org/sdr/SWAA2021011136926), Dec 15, 2020: STRINGER. CRACKED. FCB STRINGER 26L CRACKED AT BS 536 ATTACH POINT, MARKED. REPAIRED FCB STRINGER 26L AT BS 500D+10-540, IAW SRM 53-00-03-2R-1 PARA 4 STEPS A-L. - [SDR SWAA2021011136925](https://openairdocs.org/sdr/SWAA2021011136925), Dec 15, 2020: STRINGER. CRACKED. FCB STRINGER 25L CRACKED AT BS 536 ATTACH POINT, MARKED. REPAIRED FCB STRINGER 25L AT BS 500D+10-540, IAW SRM 53-00-03-2R-1 PARA 4 STEPS A-L. - [SDR SWAA2021011136927](https://openairdocs.org/sdr/SWAA2021011136927), Dec 15, 2020: STRINGER. CRACKED. FCB STRINGER 27L CRACKED AT BS 536 ATTACH POINT, MARKED. REPAIRED FCB STRINGER 27L AT BS 500D+10-540, IAW SRM 53-00-03-2R-1 PARA 4 STEPS A-L. - [SDR SWAA2021011136929](https://openairdocs.org/sdr/SWAA2021011136929), Dec 15, 2020: STRINGER. CRACKED. FCB STRINGER 26R CRACKED AT BS 536 ATTACH POINT, MARKED. REPAIRED FCB STRINGER 26R AT BS 500D+10-540, IAW SRM 53-00-03-2R-1 PARA 4 STEPS A-L. - [SDR SWAA2021011136933](https://openairdocs.org/sdr/SWAA2021011136933), Dec 15, 2020: LENS. DAMAGED. RT NR 2 BIN EMERGENCY LIGHT LENS IS DAMAGED. INSTALLED A NEW RT NR 2 BIN EMERGENCY LIGHT LENS, PER AMM NR 33-51-03-960-801 STEP 2D ITEMS (1)(A)(C) 2666C 17DEC20 - [SDR SWAA2021011136949](https://openairdocs.org/sdr/SWAA2021011136949), Dec 15, 2020: CAP. MISSING. AFT ENTRY DOOR SLIDE COVER BUMPER MISSING AFT END CAP. INSTALLED NEW BUMPER END CAP ON AFT ENTRY DOOR SLIDE COVER, PER SRM 51-40-02. - [SDR SWAA2021051236484](https://openairdocs.org/sdr/SWAA2021051236484), Dec 14, 2020: SKATE ANGLE. CHAFED. R/H AFT SKATE ANGLE CHAFFED BS 1028; RBL 12; WL 308; / REMOVED & REPLACED R/H AFT SKATE ANGLE BS1028 RBL 12 WL 308 IAW SRM'S 51-40-02-0G-0; SRM 51-40-05-0G-0; S - [SDR SWAA2021051236483](https://openairdocs.org/sdr/SWAA2021051236483), Dec 14, 2020: SKATE ANGLE. CHAFED. L/H AFT SKATE ANGLE CHAFFED BS 1028; LBL 12; WL 308 / REMOVED & REPLACED L/H AFT SKATE ANGLE BS1028 LBL12 WL308 IAW SRM'S 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM - [SDR SWAA2021011136504](https://openairdocs.org/sdr/SWAA2021011136504), Dec 14, 2020: WEB. CRACKED. FWD ENTRY DOOR INNER WEB IS CRACKED AFT FRAME AT NR 7 STOP PIN CUTOUT. FWD ENTRY DOOR INNER WEB CRACK AT AFT FRAME AT NR 7 STOP PIN CUTOUT WAS REPAIRED, PER ER - [SDR SWAA2021011139969](https://openairdocs.org/sdr/SWAA2021011139969), Dec 11, 2020: PRESSURE DECK. DENTED. FLIGHT DECK FLOOR IS DENTED AT BS 255, RBL 4-LBL 14, WL 207.54. THE DAMAGE IS REPAIRED, PER EA 1-A53-33179 REV 1 AND EA 20-153-02588 REV IR. 56040C 04JAN21. - [SDR SWAA2021080429519](https://openairdocs.org/sdr/SWAA2021080429519), Nov 8, 2020: NUT PLATE. BROKEN. BROKEN NUTPLATE ON RADOME AT 6 OCLOCK POSITION / REMOVEED AND REPLACED NUTPLATE AT 6 OCLOCK POSITION IAW AMM 53-52-00 - [SDR SWAA2020090814128](https://openairdocs.org/sdr/SWAA2020090814128), Sep 4, 2020: LAMP. INOPERATIVE. CABIN EMERGENCY LIGHT INOPERABLE AT ROW 13DEF. RELAMPED EMERGENCY LIGHT AT ROW 13DEF IAW AMM 33-51-03. - [SDR SWAA2020082711794](https://openairdocs.org/sdr/SWAA2020082711794), Aug 26, 2020: DOUBLER. DAMAGED. EXTERNAL GROUND POWER RECEPTICAL DOOR SURROUND DOUBLER DAMAGED. REPAIRED PER SRM 53-10-15-2R-4. SEE ATTACHED SAM 326 FOR WORK IN PROGRESS DETAILS - [SDR SWAA2020071600660](https://openairdocs.org/sdr/SWAA2020071600660), Jul 15, 2020: LENS. LOOSE. EMERGENCY EXIT LIGHT LENS IS LOOSE 4ABC. SECURED LOOSE EMERGENCY LIGHT LENS PER AMM 33-51-03. - [SDR SWAA2020032634348](https://openairdocs.org/sdr/SWAA2020032634348), Mar 16, 2020: SKIN. CRACKED. RES NRC D393391 CRACK IND FROM BS 706+7 TO 706+10 1' TO 2' ABOVE S-4L USING C SCAN 737 NDT MANUAL PART 6; 53-30-25 AND 737 NDT MANUAL PART 6; 53-30-18 / C/W EA - [SDR SWAA2019112939224](https://openairdocs.org/sdr/SWAA2019112939224), Nov 27, 2019: BATTERY. NO TEST. EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1673. / R&R BATTERY PER MM. - [SDR SWAA2019112939223](https://openairdocs.org/sdr/SWAA2019112939223), Nov 27, 2019: BATTERY. NO TEST. EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1672. / R&R BATTERY PER MM. - [SDR SWAA2019112939222](https://openairdocs.org/sdr/SWAA2019112939222), Nov 27, 2019: BATTERY. NO TEST. EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1675. / R&R BATTERY PER MM. - [SDR SWAA2019112939208](https://openairdocs.org/sdr/SWAA2019112939208), Nov 27, 2019: BATTERY. NO TEST. EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1669. R&R BATTERY PER MM. - [SDR SWAA2022032974991](https://openairdocs.org/sdr/SWAA2022032974991), Oct 2, 2019: STRINGER. CORRODED. LOGBOOK DEFECT NO.1250576 AIRCRAFT N729SW FOUND CORROSION AT STA.364 ON STRINGER 27R / FOUND CORROSION ON STR 27R TO BE 100% MATERIAL LOSS ON STR AND STR END FI - [SDR SWAA2019100937693](https://openairdocs.org/sdr/SWAA2019100937693), Oct 2, 2019: STRINGER. CORRODED. STRINGER CORRODED AT BS. 364, STR. 27R. / REPAIRED STRINGER IAW EA. - [SDR SWAA2022030874794](https://openairdocs.org/sdr/SWAA2022030874794), Apr 15, 2019: RETAINER. CRACKED. LEFT WING TRAILING EDGE FIXED PANEL BEHIND NACELLE STRUT FAIRING CENTER SEAL RETAINER CRACKED / REMOVED AND REPLACED SEAL RETAINER PER SRM 51-40-02 - [SDR SWAA2022030874795](https://openairdocs.org/sdr/SWAA2022030874795), Apr 15, 2019: STIFFENER. CRACKED. RIGHT WHEEL WELL; RBL 26 VERTICAL STIFFENER CRACKED AT LOWER END. / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02. - [SDR SWAA2019040231247](https://openairdocs.org/sdr/SWAA2019040231247), Mar 31, 2019: LENS. MISSING. RT EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 6. INSTALLED LENS PER MM. - [SDR SWAA2022030375213](https://openairdocs.org/sdr/SWAA2022030375213), Feb 26, 2019: RETAINER. CRACKED. RIGHT WING INBOARD LEADING EDGE JUST AFT OF #4 KRUGER FLAP HAS CRACKED SEAL RETAINER / REMOVED CRACKED SEAL RETAINER ON RIGHT WING I/B LEADING EDGE AFT OF #4 FR - [SDR SWAA2019030630370](https://openairdocs.org/sdr/SWAA2019030630370), Feb 19, 2019: RIB. CRACKED. RT HORIZONTAL STABILIZER RIB CRACKED AT STA 120.3, FORWARD WEB, LOWER SIDE INBOARD LOWER FLANGE FORWARD END FASTENER HOLE. REPAIRED RIB IAW EA. - [SDR SWAA2019022630012](https://openairdocs.org/sdr/SWAA2019022630012), Feb 19, 2019: RIB. CRACKED. RT HORIZONTAL STABILIZER RIB STA 120.3, 4TH FROM FORWARD VERTICAL STIFFENER CRACKED. REPAIRED RIB IAW SRM. - [SDR SWAA2022030275209](https://openairdocs.org/sdr/SWAA2022030275209), Feb 18, 2019: PANEL. CRACKED. WTB FAIRING PANEL 195CR HAS CRACK AT FWD END IN RADIUS / REPAIRED WTB FAIRING PANEL 195CR AT FWD END IN RADIUS IAW 3737-700-SRM 53-6070-2R-1 REPAIR 1 REV 66 - [SDR SWAA2019022730096](https://openairdocs.org/sdr/SWAA2019022730096), Feb 13, 2019: SUPPORT CHANNEL. CRACKED. RT WING AFT LOWER PANEL SUPPORT CHANNEL CRACKED NEAR ORRS 288. R&R CHANNEL IAW SRM AND DWG. - [SDR SWAA2019022129891](https://openairdocs.org/sdr/SWAA2019022129891), Feb 13, 2019: PLATE. CRACKED. LT WING AFT SPAR WIGGLE PLATE CRACKED AT ORRS 261. R&R WIGGLE PLATE IAW SRM. - [SDR SWAA2019030530308](https://openairdocs.org/sdr/SWAA2019030530308), Feb 6, 2019: RIB. CRACKED. RT HORIZONTAL STABILIZER RIB 120.30, THIRD FROM FORWARD VERTICAL STIFFENER CRACKED. R&R RIB IAW SRM & DWG. - [SDR SWAA2022030275187](https://openairdocs.org/sdr/SWAA2022030275187), Feb 2, 2019: STIFFENER. CRACKED. R/H A/C BAY STA 663; RBL 8 VERTICAL ATTACH ANGLE CRACKED / REMOVED VERTICAL STIFFNER RBL 8 STA 663 FWD SIDE OF VAPOR BARRIER IAW B737-700 SRM 51-40-02-0G-0. REC - [SDR SWAA2019021829756](https://openairdocs.org/sdr/SWAA2019021829756), Feb 2, 2019: FRAME SPLICE. CORRODED. FORWARD CABIN FRAME FACTORY SPLICE CORRODED AT BS 294.5, STR 1. R&R SPLICE IAW SRM & DWG. - [SDR SWAA2019022029854](https://openairdocs.org/sdr/SWAA2019022029854), Feb 1, 2019: STRINGER. CORRODED. STRINGER CORRODED AT BS 365, STR 28L. REPAIRED STRINGER IAW SRM AND EA. - [SDR SWAA2022030275158](https://openairdocs.org/sdr/SWAA2022030275158), Jan 29, 2019: WEB. CORRODED. E/E COMPARTMENT STUB FRAME STA 336 ABOVE STR 23L WEB HAS CORROSION / EVALUATED CORROSION + FOUND TO BE 100% MATERIAL LOSS. OUT OF LIMITS. REMOVED STUB FRAME AT All 268: https://openairdocs.org/deregistered/N729SW-2024-09-16/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.