# N238WN: 2005 Boeing 737-7H4, registration cancelled 2026-06-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 5, 2026 - Status when cancelled: Valid registration - Airframe: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (registry code 1384404) - Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 34713 - Year built: 2005 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 21, 2006 - Certificate issued: June 27, 2006 - Last registry action: March 10, 2023 - Mode S code: A22839 - 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/N238WN - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=238WN - Page: https://openairdocs.org/deregistered/N238WN-2026-06-05 From the FAA registry file of October 29, 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 (273, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA2025120341772](https://openairdocs.org/sdr/SWAA2025120341772), Dec 1, 2025: SLIDE. DISLODGED. FWD ENTRY DOOR SLIDE FELL OUT OF DOOR COMPARTMENT. REINSTALLED FWD ENTRY IAW AMM 25-66-00 AND TASK CARD 725-61-06. - [SDR SWAA2025111133130](https://openairdocs.org/sdr/SWAA2025111133130), Nov 8, 2025: BRACKET. OUT OF ADJUST. FORWARD SERVICE DOOR GIRT BAR WILL NOT STAY ARMED. ADJUSTED THE BRACKETS IAW SIP. - [SDR SWAA2025091113291](https://openairdocs.org/sdr/SWAA2025091113291), Sep 9, 2025: GIRT BAR. NO DISCREPANCY. FORWARD PROVISIONING DOOR LEFT SIDE GIRT BAR BRACKET ON SLIDE BROKEN. INSPECTED FORWARD SERVICE DOOR GIRT BAR LATCH AND BRACKET ATTACHMENTS. EVERYTHING IS INTAC - [SDR SWAA2025082909183](https://openairdocs.org/sdr/SWAA2025082909183), Aug 28, 2025: LAMP. INOPERATIVE. EMER LIGHT 3D INOPERATIVE. REMOVED AND REPLACED THE LAMPS IAW AMM 33-51-03-960-801-NG - [SDR SWAA2025081198853](https://openairdocs.org/sdr/SWAA2025081198853), Aug 5, 2025: HMU. FAILED. NR 1 ENGINE FAILED UPON EXITING THE RUNWAY. SHUTDOWN ENG IAW QRH. R&R HMU;FUEL PUMP PACKAGE REF 773-11-00; R&R MW03102 HARNESS PER AMM 71-51-03; R&R J10;J6 HARN - [SDR SWAA2025081100402](https://openairdocs.org/sdr/SWAA2025081100402), Aug 5, 2025: PUMP. FAILED. NR 1 ENGINE FAILED UPON EXITING THE RUNWAY. SHUTDOWN ENG IAW QRH. R&R HMU;FUEL PUMP PACKAGE REF 773-11-00; R&R MW03102 HARNESS PER AMM 71-51-03; R&R J10;J6 HARN - [SDR SWAA2025081100403](https://openairdocs.org/sdr/SWAA2025081100403), Aug 5, 2025: WIRE HARNESS. FAILED. NR 1 ENGINE FAILED UPON EXITING THE RUNWAY. SHUTDOWN ENG IAW QRH. R&R HMU;FUEL PUMP PACKAGE REF 773-11-00; R&R MW03102 HARNESS PER AMM 71-51-03; R&R J10;J6 HARN - [SDR SWAA2025081100404](https://openairdocs.org/sdr/SWAA2025081100404), Aug 5, 2025: EEC. FAILED. NR 1 ENGINE FAILED UPON EXITING THE RUNWAY. SHUTDOWN ENG IAW QRH<[01] C/W. R&R HMU;FUEL PUMP PACKAGE REF 773-11-00; R&R MW03102 HARNESS PER AMM 71-51-03; R&R J1 - [SDR SWAA2025031003751](https://openairdocs.org/sdr/SWAA2025031003751), Mar 9, 2025: STRUCTURE. CRACKED. BIRD STRIKE ON CLIMBOUT. NOTED NO ABNORMAL SMELL IN COCKPIT.AS CLIMB CONTINUED; EGT ON #1 ENGINE CONTINUED TO RISE PAST 860 LARGE EGT SPLIT WITH OTHER ENGINE (+ - [SDR SWAA2025022597750](https://openairdocs.org/sdr/SWAA2025022597750), Feb 19, 2025: HANDLE. OUT OF ADJUST. L1 DOOR ASSIST HANDLE NEEDS SECURED <[01]. ADJUSTED L1 DOOR ASSIST HANDLE IAW B737-700 AMM 52-11-31-400-802-NG; [02] ADJUSTED L1 DOOR ASSIST HANDLE IAW B737-700 - [SDR SWAA2025022597747](https://openairdocs.org/sdr/SWAA2025022597747), Feb 19, 2025: HANDLE. LOOSE. L2 DOOR ASSIST HANDLE NEEDS SECURED <[01]. SECURED L2 DOOR ASSIST HANDLE IAW B737-700 AMM 52-13-31-400-802-NG (TOOL# T-0070023-0003); [02] SECURED L2 DOOR ASSIS - [SDR SWAA2025022597751](https://openairdocs.org/sdr/SWAA2025022597751), Feb 19, 2025: HANDLE. LOOSE. R1 DOOR AND AIRFRAME SIDE ASSIST HANDLES NEED SECURED <[01]. SECURED R1 DOOR AND AIRFRAME SIDE ASSIST HANDLES IAW B737-700 AMM 52-11-31-400-802-NG (TOOL# T-0070 - [SDR SWAA2024101447207](https://openairdocs.org/sdr/SWAA2024101447207), Oct 10, 2024: CIRCUIT BREAKER. TRIPPED. ON DECENT ELECTRICAL SMELL IN AFT GALLEY. SELECTED GALLEY POWER OFF; SMELL DISSIPATED.<[01] C/W CONDITIONAL INSPECTION IAW AMM 05-51-56 & FIM 21-60 TASK 806. NO - [SDR SWAA2024071211614](https://openairdocs.org/sdr/SWAA2024071211614), Jul 12, 2024: BATTERY PACK. NO TEST. M1673 FAILED CAPACITY CHECK<[01] R&R M1673 BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2024071211612](https://openairdocs.org/sdr/SWAA2024071211612), Jul 12, 2024: BATTERY PACK. NO TEST. M1675 FAILED CAPACITY CHECK<[01] R&R M1675 BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2024071211613](https://openairdocs.org/sdr/SWAA2024071211613), Jul 12, 2024: BATTERY PACK. NO TEST. M1672 FAILED CAPACITY CHECK<[01] R&R M1672 BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2024071211591](https://openairdocs.org/sdr/SWAA2024071211591), Jul 12, 2024: STOP FITTING. CRACKED. FWD SERVICE DOOR AFT LOWER STOP FITTING CRACKED.<[01] REMOVED FWD SERVICE DOOR AND INSTALLED NEW DOOR UP TO AMM TASK 52-41-00 GALLEY SERVICE DOOR INSTALLATION S - [SDR SWAA2024052890772](https://openairdocs.org/sdr/SWAA2024052890772), May 20, 2024: B-NUT. LOOSE. #2 BRAKE LEAKING HYDRAULIC FLUID<[01] TIGHTENED B-NUT @ MLG BRAKE QUICK DISCONNECT PER AMM 32-41-11 LEAK CHECK GOOD. SERVICED B HYD SYS TO FULL PER AMM 12-12-00 - [SDR SWAA2024032666886](https://openairdocs.org/sdr/SWAA2024032666886), Mar 23, 2024: DOOR. CRACKED. LEFT MLG CENTER GEAR DOOR CRACKED AT LWR FWD ATTACH POINT. CONFIGURED AIRCRAFT FOR GEAR SWING AND PULLED BREAKERS PER AMM 32-00-00; INSTALLED L/H GEAR CENTER DO - [SDR SWAA2024030559386](https://openairdocs.org/sdr/SWAA2024030559386), Mar 3, 2024: MODULE. FLUCTUATES. AT FL400 AIRSPEED AND ALTITUDE INDICATIONS BEGAN TO FLUCTUATE AND DISAGREE FLAG. DETERMINED CA SIDE WAS UNRELIABLE/BAD. FO SIDE RELIABLE AND STANDBY RELIABLE. I - [SDR SWAA2024030458535](https://openairdocs.org/sdr/SWAA2024030458535), Mar 2, 2024: MODULE. FLUCTUATES. FL390 A/S & ALT DISAGREE INDICATIONS WITH A/S & ALT FLUCUATIONS. DETERMINED CA SIDE WAS THE BAD SIDE. INDICATIONS CONTINUED THROUGH DESCENT. NO OVERWEIGHT LANDI - [SDR SWAA2024030458805](https://openairdocs.org/sdr/SWAA2024030458805), Mar 2, 2024: MODULE. FLUCTUATES. FL390 A/S & ALT DISAGREE INDICATIONS WITH A/S & ALT FLUCUATIONS. DETERMINED CA SIDE WAS THE BAD SIDE. INDICATIONS CONTINUED THROUGH DESCENT. NO OVERWEIGHT LANDI - [SDR SWAA2024030457268](https://openairdocs.org/sdr/SWAA2024030457268), Feb 29, 2024: LAMP. INOPERATIVE. L/H EMERGENCY EXIT GROUND ILLUMINATION LIGHT INOP<[01] REPLACED LAMP AND PERFORMED GOOD FUNCTIONAL TEST OF L/H EMERGENCY EXIT GROUND ILLUMINATION LIGHT PER AMM - [SDR SWAA2024030457267](https://openairdocs.org/sdr/SWAA2024030457267), Feb 29, 2024: LAMP. INOPERATIVE. L/H OWE EMERGENCY EXIT LOCATOR SIGN HAS INOP BULBS<[01] REPLACED LAMPS AND PERFORMED GOOD FUNCTIONAL CHECK OF L/H OWE EMERGENCY EXIT LOCATOR SIGN PER AMM 33-51- - [SDR SWAA2024030456460](https://openairdocs.org/sdr/SWAA2024030456460), Feb 26, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1670 ARE INOP<[01] OK TO CLOSE SIDEWALL CARPET RISER.;[02] OK TO CLOSE GIVEN.;[03] REPLACED POWER SUPPLY - B - [SDR SWAA2024030453804](https://openairdocs.org/sdr/SWAA2024030453804), Feb 20, 2024: SCUFF PLATE. CRACKED. FWD CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED<[01] REMOVED AND REPAIRED CRACK FCB CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER BAC5975.A - [SDR SWAA2024030551057](https://openairdocs.org/sdr/SWAA2024030551057), Feb 10, 2024: HINGE BOX. CORRODED. FWD ENTRY DOOR LOWER HINGE BOX IS CORRODED ON UPPER SURFACE COMMON TO OUTBOARD; AFT BOLT HOLE FOR BEARING PLATE<[01] REMOVED CORROSION ON LOWER HINGE BOX FOUND - [SDR SWAA2024030449329](https://openairdocs.org/sdr/SWAA2024030449329), Feb 6, 2024: INTERCOSTAL. CRACKED. BS 295 INTERCOSTAL AT STR 15L CRACKED; IB RADIUS<[01] REMOVED AND INSTALLED NEW INTERCOSTAL PER SRM 51-40-02 AND DWG 141A8180 - [SDR SWAA2024030548060](https://openairdocs.org/sdr/SWAA2024030548060), Feb 2, 2024: FORMER. CRACKED. L/H FAIRING FORMER I/B OF #2 K-FLAP IS CRACKED AT UPPER FASTENER (MARKED)<[01] REMOVED AND REPLACED LEFT WING FAIRING FORMER ON I/B FIXED L/E; BS 500D IAW SRM 5 - [SDR SWAA2024030447950](https://openairdocs.org/sdr/SWAA2024030447950), Feb 2, 2024: INTERCOSTAL. CRACKED. BS 295 INTERCOSTAL AT STR 16L CRACKED; IB RADIUS; MARKED<[01] REMOVED AND REPLACED INTERCOSTAL ON BS295 TO BS 303.8 STR 16L IAW SRM 51-40-02 AND DWG 141A8180;[0 - [SDR SWAA2024030547290](https://openairdocs.org/sdr/SWAA2024030547290), Feb 1, 2024: SUPPORT BRACKET. BROKEN. CABLE ATTACH ANGLE SUPPORT BRACKET BROKEN; BS 685+8; RB 24.5; WL 204.<[01] REMOVED AND REPLACED ATTACH ANGLE SUPPORT BRACKET I.A.W SRM 51-10-02-0G-0; SRM 51-40- - [SDR SWAA2024030547292](https://openairdocs.org/sdr/SWAA2024030547292), Feb 1, 2024: WEB. CORRODED. REJECT; ADDITIONAL CORROSION EXIST ON WEB BS 1016+11; LBL 4; WL208; ADJACENT TO TENSION STRAP ON UPPER SURFACE.<[01] REMOVED AND REPLACED WEB IN TTG8Q00R9MW3;[0 - [SDR SWAA2024030547294](https://openairdocs.org/sdr/SWAA2024030547294), Feb 1, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION ON FWD CARGO BAY LH FLOOR-TO-SIDEWALL SUPPORT AT WL 156; LBL 24; BS 494; BS 500+4 TO 500A; AND BS 500B+5 TO 500C+11<[01] ALL PROCESS WILL BE CLOSED WI - [SDR SWAA2024030547295](https://openairdocs.org/sdr/SWAA2024030547295), Feb 1, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION ON FWD CARGO BAY RH FLOOR-TO-SIDEWALL SUPPORT AT WL 156; RBL 24; BS 500B+14; BS 500C+10; AND BS 500C+14<[01] REMOVED AND REPLACED ON FWD CARGO BAY RH - [SDR SWAA2024030547298](https://openairdocs.org/sdr/SWAA2024030547298), Feb 1, 2024: SHIELD. CORRODED. CORROSION ON FWD CARGO DOORWAY AFT SHIELD AT RBL 24; WL 156; BS 500+6; AND BS 500+13 TO 500+18<[01] VERIFIED STEP 2; COMPLETE; STEP 2 IN PARTIAL; OK TO APPLY CO - [SDR SWAA2024030547296](https://openairdocs.org/sdr/SWAA2024030547296), Feb 1, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION ON FWD CARGO BAY RH FLOOR-TO-SIDEWALL SUPPORT AT WL 156; RBL 24; BS 414<[01] VERIFIED STEP 3 IN PARTIAL.;[02] REMOVED ; FABRICATED AND INSTALLED FWD C - [SDR SWAA2024030547300](https://openairdocs.org/sdr/SWAA2024030547300), Feb 1, 2024: SHIELD. CORRODED. CORROSION OF FWD CARGO DOORWAY FWD SHIELD AT RBL 24; WL 156; BS 426<[01] REMOVED AND REPLACED ON FWD. CARGO DOORWAY FWD. SHIELD AT WL 156; RBL 24; BS. 420 - BS. - [SDR SWAA2024030547302](https://openairdocs.org/sdr/SWAA2024030547302), Feb 1, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION ON FWD CARGO BAY LH FLOOR-TO-SIDEWALL SUPPORT AT WL 156; LBL 24; BS 458; AND BS 466 TO 479<[01] REMOVED AND REPLACED LH FLOOR TO SIDEWALL SUPPORT AT L - [SDR SWAA2024030547685](https://openairdocs.org/sdr/SWAA2024030547685), Feb 1, 2024: SIDEWALL SUPPORT. CORRODED. AFT CARGO LH SIDEWALL SUPPORT SECTION FROM BS 727F TO 787 HAS MULTIPLE CORROSION AROUND NUTPLATE HOLES; WL 150; LBL 21.0<[01] VERIFIED STEP 9 COMPLETE; STEP 10 - [SDR SWAA2024030547686](https://openairdocs.org/sdr/SWAA2024030547686), Feb 1, 2024: SIDEWALL SUPPORT. CORRODED. AFT CARGO RH FLOOR TO SIDEWALL SUPPORT FROM BS 727D TO 767 HAS MULTIPLE CORROSION AROUND NUTPLATE HOLES; WL 150.6; RBL 21.0 [TTG8Q00R9J22]<[01] REMOVED AND REPL - [SDR SWAA2024030547548](https://openairdocs.org/sdr/SWAA2024030547548), Feb 1, 2024: FLOORBEAM. CORRODED. WHILE WORKING CUST. CARD TTG8Q00R9ETN CORROSION FOUND ON LOWER FLANGE AT BS986.5 FLOORBEAM AT NUTPLATE HOLE RBL 40 WL 208.<[01] 'REFER TO FAULT TTG8Q00R9ETN WHE - [SDR SWAA2024030447687](https://openairdocs.org/sdr/SWAA2024030447687), Feb 1, 2024: SHIELD. CORRODED. FWD AFT CARGO DOOR SHIELD HAS CORROSION IN MULTIPLE PLACES BS 767-787+3; WL 150; RBL 21<[01] REMOVED AND REPLACED FWD AFT CARGO DOOR SHIELD AT WL 150; RBL 21; B - [SDR SWAA2024030547091](https://openairdocs.org/sdr/SWAA2024030547091), Jan 31, 2024: FLOORBEAM. CORRODED. CORROSION ON BS 986 FLOOR BEAM AT NUTPLATE HOLE RBL 42; WL 208<[01] UPDATED LINE 22 OF MEASUREMENTS TABLE - PHOTOGRAPH IS NOT AVAILABLE OF THE CORROSION.;[02] U - [SDR SWAA2024030547092](https://openairdocs.org/sdr/SWAA2024030547092), Jan 31, 2024: FLOORBEAM. CORRODED. CORROSION ON BS 986 FLOOR BEAM AT NUTPLATE HOLE LBL 42; WL 208<[01] REPAIRED BS 986 FLOOR BEAM AT NUTPLATE HOLE LBL 42; WL 208 PER REF SRM 53-70-51-2R-6;[02] VE - [SDR SWAA2024030547277](https://openairdocs.org/sdr/SWAA2024030547277), Jan 31, 2024: WEB. CORRODED. AFT PASSENGER CABIN 1016 WEB HAS CORROSION AT BS 1016 - 1016+16; LBL 6 - 29; WL 208<[01] REMOVED AND INSTALLED NEW SHEAR WEB PER SRM 51-40-02-0G-0 AND DWG#147A5 - [SDR SWAA2024030547278](https://openairdocs.org/sdr/SWAA2024030547278), Jan 31, 2024: STRAP. CORRODED. AFT PASSENGER CABIN 1016 TENSION STRAP HAS CORROSION AT BS 1016 - 1016+14; LBL 3; WL 208<[01] REMOVED AND REPLACED TENSION STRAP BS 1016; LBL 3; WL 208
IAW S - [SDR SWAA2024030547283](https://openairdocs.org/sdr/SWAA2024030547283), Jan 31, 2024: INTERCOSTAL. CORRODED. FWD PASSENGER CABIN INTERCOSTAL IS CORRODED COMMON TO ATTACH FITTING AT BS 294.5 + 10; LBL 13; WL 208<[01] REMOVED AND INSTALLED ON FWD PASSENGER CABIN INTERCOS - [SDR SWAA2024022647280](https://openairdocs.org/sdr/SWAA2024022647280), Jan 31, 2024: STRAP. CORRODED. AFT PASSENGER CABIN 1016 TENSION STRAP HAS CORROSION AT BS 1016 + 10 - 1016 + 14; RBL 17 -18; WL 208<[01] REMOVED AND REPLACED BS1016 TENSION STRAP AT RBL 17 IA - [SDR SWAA2024030546405](https://openairdocs.org/sdr/SWAA2024030546405), Jan 30, 2024: PANEL. CRACKED. LT WING T/E PANEL 561AB AFT ROW OF FASTENER HOLES HAVE CRACKS AROUND THEM<[01] PANEL 561AB FASTENER HOLES HAVE BEEN REPAIRED IAW SRM 51-70-04-2R-9.

ATTAC - [SDR SWAA2024030546419](https://openairdocs.org/sdr/SWAA2024030546419), Jan 30, 2024: PANEL. CRACKED. RT WING T/E PANEL 661CB AFT ROW OF FASTENER HOLES HAS HOLES WITH CRACKS AROUND THEM<[01] PANEL 661CB FASTENER HOLES HAVE BEEN REPAIRED IAW SRM 51-70-04-2R-9.