# N774SW: 2000 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: 27882 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 18, 2000 - Certificate issued: August 14, 2000 - Last registry action: April 21, 2023 - Mode S code: AA7988 - 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/N774SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=774SW - Page: https://openairdocs.org/deregistered/N774SW-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 737-7H4: https://openairdocs.org/model/boeing-737-7h4.md ## Service difficulty reports (290, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA2022121381038](https://openairdocs.org/sdr/SWAA2022121381038), Dec 13, 2022: PANEL. DAMAGED. WING TO BODY FAIRING PANEL 193B HAS ELONGATED & CRACKED HOLES. R & R THE FAIRING PANEL 193B IAW AMM.53-51-21. - [SDR SWAA2022060614177](https://openairdocs.org/sdr/SWAA2022060614177), Jun 1, 2022: LIGHT. INOPERATIVE. FO SIDE EMERGENCY EXIT WINDOW LIGHT INOP (WING) / [01] OK TO CONTINUE PER MEL 33-2-03 SP1B C/W. R AND R BULB AND FUSE FO SIDE EMERGENCY EXIT WINDOW LIGHT IAW AM - [SDR SWAA2022052509394](https://openairdocs.org/sdr/SWAA2022052509394), May 19, 2022: BRACKET. CRACKED. I/B T/E SUPPORT BRACKET FOR PANEL 551EB L/H WING IS CRACK. / [01] REMOVED I/B TRAILING EDGE SUPPORT BRACKET FOR ACCESS PANEL 551 EB AS PER BOEING 737 SRM 51-40- - [SDR SWAA2022052509215](https://openairdocs.org/sdr/SWAA2022052509215), May 18, 2022: GIRT LACING. OUT OF ADJUST. CUSTOMER REQUEST- L1 DOOR SLIDE HAS EXCESSIVE GIRT HANGING DOWN. / [01] READJUSTED L1 DOOR SLIDE GIRT REF B737 AMM 25-66-01-400-803;[02] VERIFIED 1;COMPLETE - [SDR SWAA2022052508857](https://openairdocs.org/sdr/SWAA2022052508857), May 17, 2022: ANGLE. CRACKED. SUPPORT ANGLE AT VAPOR BARRIER LH STA 663 CRACKED / [01] LOCATED AND DRILLED NEW SUPPORT ANGLE AT VAPOR BARRIER L/H STA 663 PER REF B737-700 SRM51-40-05-0G-0.;[ - [SDR SWAA2022052508625](https://openairdocs.org/sdr/SWAA2022052508625), May 14, 2022: VAPOR BARRIER. CRACKED. L/H STA 663 VAPOR BARRIER CRACKED AT LBL 10 LOWER CORNER. STOP DRILL CRACK AS PER B737 SRM 51-70-04-2R-10; ACCOMPLISH DRY OUT ON DAMAGE AREA OF L/H VAPOR BARRIE - [SDR SWAA2021111643351](https://openairdocs.org/sdr/SWAA2021111643351), Nov 12, 2021: LENS. BROKEN. CUSTOMER WALK: FORWARD CABIN EMERGENCY EXIT LENS FALLING WONT STAY UP CLIP LOCK BROKEN. ; / [01] SECURED FORWARD CABIN EMERGENCY EXIT LENS AS PER B737 AMM 33-51 - [SDR SWAA2021111642174](https://openairdocs.org/sdr/SWAA2021111642174), Nov 10, 2021: SLIDE. OUT OF POSITION. R2 DOOR SIDE SCURT TOUCHING SCUFF PLATE WHEN CLOSED ; / [01] REPOSITIONED R2 DOOR SLIDE SKIRT PER B737 AMM 25-66-01-400-803; [02] VERIFIED STEP 1. - [SDR SWAA2021111542172](https://openairdocs.org/sdr/SWAA2021111542172), Nov 10, 2021: SCUFF PLATE. CRACKED. AFT CARGO CENTER SCUFF PLATE CRACKED ; AFT CARGO CENTER SCFF PLATE CRACKED / [01] RECEIVED NEW SCUFF PLATE PART #146A8342-8 TO BE INSTALLED ON WORK ORDER #TTG8Q - [SDR SWAA2021111641203](https://openairdocs.org/sdr/SWAA2021111641203), Nov 7, 2021: LIGHT. INOPERATIVE. R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. ; / [01] RELAMPED R1 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF. B737 AMM 33-51-04-960-801. TEST OK; [02] VERIFIED STEP 1. - [SDR SWAA2021111641206](https://openairdocs.org/sdr/SWAA2021111641206), Nov 7, 2021: NONE. MISSING. EMERGENCY EXIT SIGN LENS MISSING AT G4 GALLEY ; / [01] REPLACED EMERGENCY EXIT SIGN LIGHT ASSEMBLY AND PERFORMED TEST FOR NEW ASSEMBLY AS PER B737 AMM 33-51-019 - [SDR SWAA2021111641197](https://openairdocs.org/sdr/SWAA2021111641197), Nov 6, 2021: SKIN. INOPERATIVE. L2 DOOR LOWER EMERGENCY INDICATOR EXIT SIGN INOP. ; / [01] PERFORMED BATTERY PACK REPLACEMENT AT M1673 L2 DOOR (S/N ON: 36688) ; AND ACCOMPLISHED OPS CHECK AS P - [SDR SWAA2021111641198](https://openairdocs.org/sdr/SWAA2021111641198), Nov 6, 2021: LIGHT. INOPERATIVE. EMERGENCY OVERHEAD BIN LIGHTS INOP AT POSITIONS: 14L/H THRU 23L/H AND 22R/H. ; / [01] WORK TO BE ACCOMPLISHED IN ITEM TTG8Q0096A91; OPS CHECK FOUND NORMAL AS PE - [SDR SWAA2021111641199](https://openairdocs.org/sdr/SWAA2021111641199), Nov 6, 2021: LIGHT. INOPERATIVE. L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. ; / [01] WORK TO BE ACCOMPLISHED IN ITEM TTG8Q009A91; OPS CHECK FOUND NORMAL AS PER B737 AMM 33-51-06-960-805.; [02] VERI - [SDR SWAA2021111641201](https://openairdocs.org/sdr/SWAA2021111641201), Nov 6, 2021: SIGN. BURNED OUT. R/H OVER-WING EMERGENCY EXIT INDICATOR SIGN HAS 1 BULB BURNED OUT. ; / [01] REPLACED EXIT SIGN; LAMP AT R/H OVER WING INDICATOR; AS PER B737 AMM 33-51-01-960-80 - [SDR SWAA2021111041200](https://openairdocs.org/sdr/SWAA2021111041200), Nov 6, 2021: NONE. INOPERATIVE. R2 DOOR UPPER EMERGENCY INDICATOR EXIT SIGN INOP. ; / [01] WORK TO BE ACCOMPLISHED IN ITEM TTG8Q0096A91; OPS CHECK FOUND NORMAL AS PER B737 AMM 33-51-06-960-805 - [SDR SWAA2021111738631](https://openairdocs.org/sdr/SWAA2021111738631), Oct 31, 2021: DOUBLER. CORRODED. FOUND CORROSION AT FWD CARGO COMP BILGE AREA M2134 'NATS AIRPHONE ANTENNA' DOBBLER BETWEEN STA 500 AND 500A STGR 28L AND STGR 28R .INSTALLED PROTECTION OF EWIS - [SDR SWAA2021111632322](https://openairdocs.org/sdr/SWAA2021111632322), Oct 21, 2021: NONE. MISSING. EMERGENCY EXIT DOOR L & R SIDE INDICATOR ASSY -LIGHTED EXIT FOUND MISSING ; / [01] INSTALLED EMERGENCY EXIT DOOR L/H SIDE AND R/H SIDE INDICATOR ASSY LIGHT AS P - [SDR SWAA2021111731584](https://openairdocs.org/sdr/SWAA2021111731584), Oct 19, 2021: INTERCOSTAL. CRACKED. ENG 2 O/B FAN COWL INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL AT NR 2 ENGINE O/B FAN COWL IAW SRM 51-40-02-0G-0. - [SDR SWAA2021111731793](https://openairdocs.org/sdr/SWAA2021111731793), Oct 19, 2021: ACCESS PANEL. DELAMINATED. NR 2 PYLON ACCESS PANEL 431ER EDGE DELAMINATED. PREPARED PANEL 431ER FOR REPAIR OF THE FIBER GLASS IAW SRM 51-70-062R-7. REPAIRED AT PANEL 431ER IAW SRM 51-70-0 - [SDR SWAA2021111730939](https://openairdocs.org/sdr/SWAA2021111730939), Oct 18, 2021: CHANNEL. CORRODED. CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR SUPPORT Z CHANNEL NUTPLATES BETWEEN BS 767 & 787. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS I - [SDR SWAA2021111730941](https://openairdocs.org/sdr/SWAA2021111730941), Oct 18, 2021: SUPPORT. CORRODED. CORROSION ON AFT CARGO BAY BILGE FRAME SUPPORT UPPER FLANGE BS 787, S26R. REMOVED CORROSION IAW SRM 51-10-02-0G-0. EVALUATED REWORKED AREA ORG MAT 0.088 MAT REM - [SDR SWAA2021111728694](https://openairdocs.org/sdr/SWAA2021111728694), Oct 11, 2021: STRINGER. CORRODED. CORROSION FOUND AFT FUSELAGE INTERNAL STINGER 27L, BS 1006 & 1016. REMOVED CORROSION AT AFT FUSELAGE & FOUND OUT OF LIMITS DUE TO ITS ALL THE WAY THROUGH STRING - [SDR SWAA2021111728693](https://openairdocs.org/sdr/SWAA2021111728693), Oct 11, 2021: HINGE. CORRODED. CORROSION AT UPPER FUSELAGE UNDER VERTICAL FIN AREA BETWEEN VERTICAL STAB. FWD HINGE & AFT HINGE. OTBD S1L & 1R. REMOVED CORROSION AT UPPER FUSELAGE UNDER VERTI - [SDR SWAA2021111728691](https://openairdocs.org/sdr/SWAA2021111728691), Oct 9, 2021: PANEL. DELAMINATED. PANEL 192BL HAS EDGES DELAMINATED IN TWO SPOTS. REMOVED DAMAGED PLIES & PREPARED THE DAMAGED AREA TO APPLY FABRIC REPAIR PLIES NO WATER NOTE AT ACCESS PANEL 192 - [SDR SWAA2021111727968](https://openairdocs.org/sdr/SWAA2021111727968), Oct 7, 2021: STIFFENER. CRACKED. LEFT HORIZONTAL STAILIZER INSPAR RIB ASSY #4 STIFFENER #2 LOWER CRACK NOTED. PERFORMED HFEC INSP ON STIFFENER#2 LOWER CHORD IAW B737 NDT P6 51-00-00 PROC.23; 2E - [SDR SWAA2021111727969](https://openairdocs.org/sdr/SWAA2021111727969), Oct 7, 2021: STIFFENER. CRACKED. LEFT HORIZONTAL STAILIZER INSPAR RI ASSY #4 STIFFENER #4 LOWER CRACK NOTED / REMOVED DAMAGED AT LT HORIZONTAL STAB #4 RIB #4 STIFFENER LOWER IAW 7 SRM 55-10-09- - [SDR SWAA2021111726866](https://openairdocs.org/sdr/SWAA2021111726866), Oct 5, 2021: RIB. CRACKED. DORSAL FIN FWD RIB CRACKED ; / [01] REMOVED DORSAL FIN FWD RIB AS PER B737-700 SRM 5-40-02-0G-0; [02] LOCATED AND DRILLED NEW RIB ASSEMBLY AS PER B737-700 SRM 5 - [SDR SWAA2021111626860](https://openairdocs.org/sdr/SWAA2021111626860), Oct 5, 2021: WEB. CRACKED. CRACK FOUND AT EXTERNAL WHEEL WELL WEB LOCATED AT RT SIDE STA 663 BETWEEN RBL 31.83 & RBL 40.00. CRACK LENGTH : 0.512'. / [01] INSTALLED EWIS PROTECTION AT EXTE - [SDR SWAA2021111725744](https://openairdocs.org/sdr/SWAA2021111725744), Oct 3, 2021: PANEL. DELAMINATED. NO-2 PYLON ACCESS PANEL 441EL EDGE AREA DELAMINATED MKD DOT ; / [01] PREPARED FOR REPAIR AT PANEL 441 EL AS PER B737-700 SRM. 51-70-06-2R-7; [02] VERIFIED STEP - [SDR SWAA2021111725737](https://openairdocs.org/sdr/SWAA2021111725737), Oct 2, 2021: GUSSET. CRACKED. FWD CARGO L/H STA 500D S-19L GUSSET BRACKET CRACK. ; / [01] REMOVED GUSSET AT FWD CARGO DOOR L/H STA 500D S19L B737-700 ARM 51-40-02-0G-0; [02] LOCATED. HOLE AN - [SDR SWAA2021111725738](https://openairdocs.org/sdr/SWAA2021111725738), Oct 2, 2021: GUSSET. CRACKED. FWD CARGO R/H STA 500D S-19R GUSSET BRACKET CRACK. ; / [01] REMOVED GUSSET AT FWD CARGO R/H SAT 500D S-19 B737-700 ARM 51-40 -02 0G-0; [02] LOCATED HOLE NEW GUS - [SDR SWAA2021111725727](https://openairdocs.org/sdr/SWAA2021111725727), Oct 1, 2021: PANEL. DEFORMED. PANEL 211AF OUT OF SHAPE. LOCATED AND DRILLED NEW PART REF B-737-700 SRM 41-40-05-0G-0; [02] VERIFIED NEW PART.INSTALLATION ON CARD TTG8Q002YL6X - [SDR SWAA2021111725191](https://openairdocs.org/sdr/SWAA2021111725191), Oct 1, 2021: PANEL. DELAMINATED. ACCESS PANEL 193D AFT EDGE DELAMINATED. / [01] PREPARED FOR REPAIR PLIES THE AREA AT PANEL 193D AS PER B737-700 SRM51-70-04-2R-9; [02] OK TO INSTALL REPAIR.; [0 - [SDR SWAA2021111725206](https://openairdocs.org/sdr/SWAA2021111725206), Oct 1, 2021: CHANNEL. CORRODED. CORROSION ON AFT CARGO BILGE AREA, LT SIDE ZEE CHANNEL, BS 727D+9 - 847. REMOVED CORROSION IAW SRM 51-51-10-02-0G-0. PERFORMED UT THIKNESS INSP. ON REWORKED ARE - [SDR SWAA2021111725731](https://openairdocs.org/sdr/SWAA2021111725731), Oct 1, 2021: SKIN. CORRODED. LIGHT CORROSION AT AFT PRESSURE DOME FWD SIDE BS 1016, CIRCUMFERENTIAL SKIN SPLICE BETWEEN STRINGERS 26L TO 26R. REMOVED SKIN ATTACH RIVETS AT AFT PRESSURE DOME - [SDR SWAA2021111725215](https://openairdocs.org/sdr/SWAA2021111725215), Oct 1, 2021: SPLICE. CORRODED. AFT CARGO BILGE AREA; FLOOR-PANEL SPLICE AT STA#727D+5; SPOTS OF CORROSION. DOT#208-16