# N562WN: 2000 Boeing 737-790, registration cancelled 2024-10-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 4, 2024 - Status when cancelled: Valid registration - Airframe: [Boeing 737-790](https://openairdocs.org/model/boeing-737-790) (registry code 13844CN) - 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: 30778 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 12, 2000 - Certificate issued: April 25, 2014 - Last registry action: January 22, 2023 - Mode S code: A73059 - 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/N562WN - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=562WN - Page: https://openairdocs.org/deregistered/N562WN-2024-10-04 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 737-790: https://openairdocs.org/model/boeing-737-790.md ## Service difficulty reports (197, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA2023103015404](https://openairdocs.org/sdr/SWAA2023103015404), Oct 27, 2023: SKIN. PULLED. WHILE ACCOMPLISHING THE DVI ON TTG8Q00P7WPE; FOUND 1EA RIVET PULLING AND 2EA RIVETS ALMOST COMPLETELY PULLED THROUGH DUE TO DAMAGED LEADING EDGE RIB BEING BENT. - [SDR SWAA2023101108824](https://openairdocs.org/sdr/SWAA2023101108824), Oct 7, 2023: POWER SUPPLY. INOPERATIVE. AFT ENTRY DOOR EXIT EXIT SIGN LIGHT INOP<[01] REMOVED AND REPLACED LEFT AFT BATTERY POWER SUPPLY IAW AMM 33-51-06. OPS CHECK GOOD NO OTHER DEFECTS NOTED - [SDR SWAA2023052451464](https://openairdocs.org/sdr/SWAA2023052451464), May 23, 2023: RETAINER. LOOSE. FWD GIRT BAR CAPTIAN SIDE IS LOOSE<[01] AJUSTED GIRT BAR RETAINER AS REQUIRED AS PER SIP - [SDR SWAA2023050243344](https://openairdocs.org/sdr/SWAA2023050243344), Apr 28, 2023: GIRT BAR. OUT OF ADJUST. FWD ENRY DOOR ESCAPE SLIDE LOOKS SLIGHTLY PULLED WHEN GIRT BAR ARMED<[01] PERFORMED GVI OF FWD ENTRY DOOR ESCAPE SLIDE PER AMM 25-66-01 NORMAL OPERATION. - [SDR SWAA2023022409464](https://openairdocs.org/sdr/SWAA2023022409464), Feb 23, 2023: LIGHT. DISCONNECTED. EMERGENCY AISLE LIGHT AT ROW 14CBA INOP.<[01] UPON FURTHER INSPECTION FOUND EMERGENCY AISLE LIGHT AT ROW 14CBA PLUG IN OVERHEAD PANEL DISCONNECTED. RECONNECTED - [SDR SWAA2022100351575](https://openairdocs.org/sdr/SWAA2022100351575), Oct 1, 2022: SLIDE. OUT OF TOLERANCE. R1 DOOR SLIDE PRESSURE INDICATION IN THE RED / [01] R & R FWD SERVICE DOOR SLIDE PER MT 725-61-06 - [SDR SWAA2022090148814](https://openairdocs.org/sdr/SWAA2022090148814), Sep 1, 2022: NONE. INOPERATIVE. LH OVER WING EMERGENCY LIGHT INOP / [01] REMOVED AND REPLACED LH OVER WING EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK PER AMM 33-51-06 - [SDR SWAA2022041392524](https://openairdocs.org/sdr/SWAA2022041392524), Apr 9, 2022: LIGHT. CORRODED. LEFT EMERGENCY OVER WING EXIT SIDEWALL LIGHT INOP / [01] REMOVED AND REPLACED OVER WING EXIT LIGHT ASSEMBLY
REF AMM 33-21-00 - [SDR SWAA2021122046837](https://openairdocs.org/sdr/SWAA2021122046837), Nov 23, 2021: SUPPORT ANGLE. CRACKED. CRACK REAR SPAR SUPPORT ANGLE LOCATED BETWEEN ORSS 281 AND ORSS 328 AT LT WING ; 2021-546062 / [01] REPLACED REAR SPAR SUPPORT ANGLE LOCATED BETWEEN ORSS 281 AN - [SDR SWAA2021122046230](https://openairdocs.org/sdr/SWAA2021122046230), Nov 21, 2021: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 194E BODY FAIRING FASTENERS HOLES AT LOWER FUSELAGE ; 2021-546045 / [01] CALIPER PN: 700-113-10; SN: 0013356; DUE DATE: 30/SEP/22.; [02] TOOL - [SDR SWAA2021122046231](https://openairdocs.org/sdr/SWAA2021122046231), Nov 21, 2021: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 193D BODY FAIRING FASTENERS HOLES AT LOWER FUSELAGE ; 2021-546044 / [01] CALIPER PN: 700-113-10; SN: 0013356; DUE DATE: 30/SEP/22.; [02] TOOL - [SDR SWAA2021122045654](https://openairdocs.org/sdr/SWAA2021122045654), Nov 18, 2021: SUPPORT. CRACKED. CRACK SUPPORT ANGLE BS540 BETWEEN BL0 TO LBL24 AND WL208.1 AT PASSENGER CABIN ; 2021-545962 / [01] TOOL USED: CALIPER P/N: 500-752-20; S/N: B21037197; DUE DATE: - [SDR SWAA2021122045655](https://openairdocs.org/sdr/SWAA2021122045655), Nov 18, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE BS540 BETWEEN BL0 TO RBL24 AND WL208.1 AT PASSENGER CABIN ; 2021-545963 / [01] REPLACED SUPPORT ANGLE BS540 BETWEEN BL0 TO RBL24 AND WL208.1 - [SDR SWAA2021122045411](https://openairdocs.org/sdr/SWAA2021122045411), Nov 17, 2021: STRINGER. CRACKED. CRACK STRINGER 25R LOCATED BS540 FWD CARGO COMPARTMENT (1 EA) ; 2021-522219 / [01] TOOL USED 35DL;S/N:091419910;DUE DATE:30-NOV-21.[06] CORRECTED STEP 4 REPAIRE - [SDR SWAA2021122045412](https://openairdocs.org/sdr/SWAA2021122045412), Nov 17, 2021: STRINGER. CRACKED. CRACK STRINGER 26R LOCATED BS540 FWD CARGO COMPARTMENT (1 EA) REPAIRED STRINGER 26R AT BS 500D TO BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 - [SDR SWAA2021122045413](https://openairdocs.org/sdr/SWAA2021122045413), Nov 17, 2021: STRINGER. CRACKED. CRACKED STRINGER 26L, BS 540 IN FWD CARGO. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1. - [SDR SWAA2021122045414](https://openairdocs.org/sdr/SWAA2021122045414), Nov 17, 2021: STRINGER. CRACKED. CRACK STRINGER 27R LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-522237 / [01] TOOL USED 35DL;S/N:091419910; DUE DATE:30-NOV-2. REPAIRED STRINGER 27R AT BS 500D TO - [SDR SWAA2021122045415](https://openairdocs.org/sdr/SWAA2021122045415), Nov 17, 2021: STRINGER. CRACKED. CRACK STRINGER 27L LOCATED BS540 FWD CARGO COMPARTMENT (1 EA) ; 2021-522247 / [01] TOOL USED:35DL;S/N:091419910; DUE DATE:30-NOV-21.; [06] REPAIRED STRINGER 27L - [SDR SWAA2021122052868](https://openairdocs.org/sdr/SWAA2021122052868), Nov 17, 2021: PLATE. MISSING. MISSING MATERIAL ON PLATE LOCATED BS 790 STR 25R AFT CARGO COMPARTMENT ; 2021-522084 / [01] FABRICATED PLATE LOCATED BS 790 STR 25R AFT CARGO COMPARTMENT IAW B7 - [SDR SWAA2021122044583](https://openairdocs.org/sdr/SWAA2021122044583), Nov 17, 2021: STRINGER. CRACKED. CUSTOMER REQUEST CRACK ON STRINGER U8 WSTA 564.50 MORE 11 INCHES RH WING INTERNAL AREA. PERFORMED REPAIR ON STRINGER U8 WSTA 564.50 MORE 11 INCHES RH WING INTER - [SDR SWAA2021122045420](https://openairdocs.org/sdr/SWAA2021122045420), Nov 17, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOC. FRONT SPAR WEB FUEL BOOST PUMP AREA IFSS 120 APPROX AND WBL 88.24 APPROX AT RT WING. REPLACED SUPPORT ANGLE LOC. FRONT SPAR WEB FUEL BO - [SDR SWAA2021122043861](https://openairdocs.org/sdr/SWAA2021122043861), Nov 15, 2021: ANGLE. CRACKED. CRACK SUPPORT ANGLE LOC. BS 695 ; RBL 24 AND WL 208.1 CENTER SECTION ; 2021-521639 / [01] REPLACED SUPPORT ANGLE LOC. BS 695 ; RBL 24 AND WL 208.1 CENTER SECTIO - [SDR SWAA2021122043210](https://openairdocs.org/sdr/SWAA2021122043210), Nov 15, 2021: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT ; 2021-521637 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A21146537;DUE DATE:06-OCT-22.; [02] REPA - [SDR SWAA2021122043208](https://openairdocs.org/sdr/SWAA2021122043208), Nov 15, 2021: SCUFF PLATE. CRACKED. CRACK CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT ; 2021-521638 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A21146537;DUE DATE:06-OCT-22.; [02] REPAIRED - [SDR SWAA2021122043875](https://openairdocs.org/sdr/SWAA2021122043875), Nov 15, 2021: NONE. CRACKED. CRACK INDICATIONS FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.500 INCH FROM FRON SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.10 - [SDR SWAA2021122043876](https://openairdocs.org/sdr/SWAA2021122043876), Nov 15, 2021: NONE. CRACKED. CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 24.500 INCH FROM FRON SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.600 - [SDR SWAA2021122043189](https://openairdocs.org/sdr/SWAA2021122043189), Nov 14, 2021: BRACKET. BROKEN. BROKEN INBOARD TRAILING EDGE BRACKET LOCATED IRSS 211.0 LT WING ; 2021-521588 / [01] REPLACED INBOARD TRAILING EDGE BRACKET LOCATED IRSS 211.0 LT WING IAW B737- - [SDR SWAA2021122043196](https://openairdocs.org/sdr/SWAA2021122043196), Nov 14, 2021: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 274 AT RT WING ; 2021-521608 / [01] REPLACED ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 274 AT RT WIN - [SDR SWAA2021111843193](https://openairdocs.org/sdr/SWAA2021111843193), Nov 14, 2021: WEB. CORRODED. CORROSION FRONT SPAR WEB LOC. FUEL BOOST PUMP AREA L: 1.25 IN; W: 0.50 IN IFSS 120 APROX AND WBL 88.24 APROX AT LT WING. EVALUATED REWORKED AREA LOCATED FRONT S - [SDR SWAA2021111843192](https://openairdocs.org/sdr/SWAA2021111843192), Nov 14, 2021: SPAR WEB. CORRODED. CORROSION FRONT SPAR WEB LOC. FUEL BOOST PUMP AREA L: 1.50 IN W: 0.80 IN IFSS 120 APROX AND WBL 88.24 APROX AT RT WING. REPAIRED FRONT SPAR WEB LOC. FUEL BOOST - [SDR SWAA2021042866217](https://openairdocs.org/sdr/SWAA2021042866217), Apr 24, 2021: CONTROL PANEL. TRIPPED. "MA WARN AND CONT" CB P6-2-A21 TRIPPED DURING FLT / R&R F/O SIX PACK IND IAW 33-11-00. R&R NO. 1 FIRE WARN LIGHT/CUT OUT SWITCH IAW AMM 33-11-0. R&R M279 IAW AM - [SDR SWAA2021042867401](https://openairdocs.org/sdr/SWAA2021042867401), Apr 24, 2021: MODULE. TRIPPED. "MA WARN AND CONT" CB P6-2-A21 TRIPPED DURING FLT / R&R F/O SIX PACK IND IAW 33-11-00. R&R NO. 1 FIRE WARN LIGHT/CUT OUT SWITCH IAW AMM 33-11-0. R&R M279 IAW AM - [SDR SWAA2020021741402](https://openairdocs.org/sdr/SWAA2020021741402), Feb 15, 2020: SLIDE. LOOSE. B FLIGHT ATTENDANT STATUS RIGHT REAR SERVICE DOOR GIRT BAR REAR ATTACH PAINT DOES NOT CONTACT BAR PROPERLY. / RESECURED R2 AFT SERVICE DOOR GIRT BAR ADAPTER PLA - [SDR SWAA2021052509352](https://openairdocs.org/sdr/SWAA2021052509352), Feb 1, 2020: BRACKET. CRACKED. LEFT WING MLG CONDUIT GUIDE BRACKET HAS CRACK IN RADIUS. LOCATED JUST OTBD OF AFT TRUNNION BEARING AND TOWARD TOP OF WING SURFACE. MARKED. / REMOVED & REPLACED - [SDR SWAA2021052509350](https://openairdocs.org/sdr/SWAA2021052509350), Feb 1, 2020: TRUNNION. CORRODED. RIGHT MLG FWD TRUNNION SUPPORT FITTING LOWER OTBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11 - [SDR SWAA2021052509351](https://openairdocs.org/sdr/SWAA2021052509351), Feb 1, 2020: TRUNNION. CORRODED. RIGHT MLG FWD TRUNNION SUPPORT FITTING LOWER INBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11 - [SDR SWAA2021052509349](https://openairdocs.org/sdr/SWAA2021052509349), Feb 1, 2020: TRUNNION. CORRODED. RIGHT MLG FWD TRUNNION SUPPORT FITTING UPPER INBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11 - [SDR SWAA2021052509348](https://openairdocs.org/sdr/SWAA2021052509348), Feb 1, 2020: TRUNNION. CORRODED. RIGHT MLG FWD TRUNNION SUPPORT FITTING UPPER OTBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11 - [SDR SWAA2021052509347](https://openairdocs.org/sdr/SWAA2021052509347), Feb 1, 2020: TRUNNION. CORRODED. LEFT MLG FWD TRUNNION SUPPORT FITTING LOWER INBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11 - [SDR SWAA2021052509346](https://openairdocs.org/sdr/SWAA2021052509346), Feb 1, 2020: TRUNNION. CORRODED. LEFT MLG FWD TRUNNION SUPPORT FITTING LOWER OTBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11 - [SDR SWAA2021052509345](https://openairdocs.org/sdr/SWAA2021052509345), Feb 1, 2020: TRUNNION. CORRODED. LEFT MLG FWD TRUNNION SUPPORT FITTING UPPER INBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11 - [SDR SWAA2021052509344](https://openairdocs.org/sdr/SWAA2021052509344), Feb 1, 2020: TRUNNION. CORRODED. LEFT MLG FWD TRUNNION SUPPORT FITTING UPPER OTBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11 - [SDR SWAA2019111938932](https://openairdocs.org/sdr/SWAA2019111938932), Nov 15, 2019: LIGHT. INOPERATIVE. FORWARD ENTRY GROUND PROXIMITY EMERGENCY LIGHTS INOPERATIVE. / R&R LIGHT ASSEMBLY PER AMM. - [SDR SWAA2019111938931](https://openairdocs.org/sdr/SWAA2019111938931), Nov 15, 2019: LAMP. INOPERATIVE. R/H OVERWING EXIT GROUND LIGHT INOPERATIVE. / RELAMPED LIGHT PER AMM. - [SDR SWAA2022051165606](https://openairdocs.org/sdr/SWAA2022051165606), Nov 12, 2019: FLOORBEAM. DEFORMED. (SKYLINE DTIP) REPAIR ON CENTER SECTION LOWER BEAM CHORD AT BS 545 TO BS 550; RBL 41.5 TO RBL 42.5 REQUIRES REPLACEMENT. (REF ESR #19-05466) / REPAIRED CENTER S - [SDR SWAA2022040165596](https://openairdocs.org/sdr/SWAA2022040165596), Nov 7, 2019: SCUFF PLATE. CRACKED. FWD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / ACCOMPLISHED REPAIR EA 1-A53-2076 REV II - [SDR SWAA2022041965584](https://openairdocs.org/sdr/SWAA2022041965584), Nov 4, 2019: SKIN. CORRODED. T996953 CORROSION ON SKIN AT BS-907+10'; 2.5' ABOVE STR-22L AT LAV TANK VENT HOLE ; / B>ACTUALSLOADER; 24-APR-2021 11:51:13
T996953 CORROSION ON S - [SDR SWAA2019112539101](https://openairdocs.org/sdr/SWAA2019112539101), Nov 2, 2019: FRAME. CRACKED. FRAME CRACKED AT BS. 727D, RBL 21 FASTENER HOLE. / REPAIRED FRAME IAW EA AND ER. - [SDR SWAA2019112539100](https://openairdocs.org/sdr/SWAA2019112539100), Nov 2, 2019: FRAME. CRACKED. FRAME CRACKED AT BS 727B, RBL 23, FASTENER HOLE. / REPAIRED FRAME PER EA. - [SDR SWAA2019110738666](https://openairdocs.org/sdr/SWAA2019110738666), Nov 1, 2019: FLOOR SUPPORT. CRACKED. AFT CARGO BAY INTERCOSTAL CRACKED AT FASTENER HOLES BS 767 - BS 787 RBL 21 CRACKED. / REPLACED INTERCOSTAL IAW B737 SRM 51-40-02 AND DWG 146A0081. All 197: https://openairdocs.org/deregistered/N562WN-2024-10-04/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.