# N744SW: 1999 Boeing 737-7H4, registration cancelled 2024-09-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 18, 2024
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (registry code 1384404)
- Engine: [GE CFM56 series](https://openairdocs.org/engine/ge-cfm56-series) (registry code 30016)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 29490
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 10, 2000
- Certificate issued: April 27, 1999
- Last registry action: October 13, 2023
- Mode S code: AA030B
- 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/N744SW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=744SW
- Page: https://openairdocs.org/deregistered/N744SW-2024-09-18

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 (318, newest 50)

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

- [SDR SWAA2022071929626](https://openairdocs.org/sdr/SWAA2022071929626), Jul 15, 2022: SCUFF PLATE. CRACKED. RAMP AGENTS REPORT AFT CARGO CENTER THRESHOLD SCUFF PLATE CRACKED. / [01] R&R'ED AFT CARGO SCUFF PLATE PER AMM 53-11-02. NO DAMAGE NOTED UNDERNEATH.;[02] PER EE
- [SDR SWAA2022051005297](https://openairdocs.org/sdr/SWAA2022051005297), May 6, 2022: SLIDE. LOOSE. FOWARD ENTRY DOOR SLIDE FELT FROM COMPARTMENT / [01] REPACKED SLIDE INTO COMPARTMENT IAW AMM 25-66-01;OK FOR SERVICE
- [SDR SWAA2022012462636](https://openairdocs.org/sdr/SWAA2022012462636), Jan 20, 2022: LIGHT. INOPERATIVE. AFT RIGHT SERVICE DOOR EXTERIOR EMERGENCY LIGHT IS INOP ; / [01] REMOVED AND REPLACED THE AFT RIGHT EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-06. OPERATIONAL C
- [SDR SWAA2021090212616](https://openairdocs.org/sdr/SWAA2021090212616), Aug 29, 2021: MEGAPHONE. NO TEST. AFT MEGAPHONE WILL NOT TEST ; / [01] REMOVED AND REPLACED AFT MEGAPHONE IAW AMM 25-64-00. OP CHECK GOOD
- [SDR SWAA2021051271525](https://openairdocs.org/sdr/SWAA2021051271525), May 5, 2021: SKIN. CRACKED. FUSELAGE CRACK INDICATION AT BS 520 +13 AND S4R; REPAIRED PER EA 211531243
- [SDR SWAA2021051169225](https://openairdocs.org/sdr/SWAA2021051169225), May 5, 2021: SKIN. CRACKED. FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R; ISSUED EA 2115301243WIP1 AS A SUBTASK TO THE FAULT.
- [SDR SWAA2021051168968](https://openairdocs.org/sdr/SWAA2021051168968), May 5, 2021: SKIN. CRACKED. FUSELAGE CRACK INDICATION AT BS 500A +11 AND S4R
- [SDR SWAA2021051070442](https://openairdocs.org/sdr/SWAA2021051070442), May 5, 2021: SKIN. CRACKED. FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R ; / COMPLIED WITH EA
- [SDR SWAA2021051070441](https://openairdocs.org/sdr/SWAA2021051070441), May 5, 2021: SKIN. CRACKED. FUSELAGE CRACK INDICATION AT BS 500A +11 AND S-4R ; /
- [SDR SWAA2021051070440](https://openairdocs.org/sdr/SWAA2021051070440), May 5, 2021: SKIN. CRACKED. FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R ; / C/W STEP3.DO A HIGH FREQUENCY EDDY CURRENT (HFEC) HOLE PROBE INSPECTION OF ANY ADDITIONAL EXISTING FASTENER
- [SDR SWAA2021051069940](https://openairdocs.org/sdr/SWAA2021051069940), May 5, 2021: SKIN. CRACKED. FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R ; /
- [SDR SWAA2021051069667](https://openairdocs.org/sdr/SWAA2021051069667), May 5, 2021: SKIN. CRACKED. FUSELAGE CRACK INDICATION AT BS 500A +11 AND S-4R ; /
- [SDR SWAA2021051069666](https://openairdocs.org/sdr/SWAA2021051069666), May 5, 2021: SKIN. CRACKED. FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R ; /
- [SDR SWAA2021042866237](https://openairdocs.org/sdr/SWAA2021042866237), Apr 24, 2021: BATTERY. INOPERATIVE. AFT MEGAPHONE INOP / REPLACED AFT MEGAPHONE BATTERIES REF AMM 25-68-00. OPS CHECK GOOD.
- [SDR SWAA2021040260405](https://openairdocs.org/sdr/SWAA2021040260405), Mar 29, 2021: SLIDE. PULLED. CREW REPORTS:L1 DOOR SLIDE GIRL BAR MATERIAL PULLED OUT EXCESSIVE / REPOSITION SLIDE AND POSITIONS GIRL MATERIAL FOR L1 SLIDE ASSY ALL PER MT 7255-61-06 ALL C/W
- [SDR SWAA2020122137210](https://openairdocs.org/sdr/SWAA2020122137210), Dec 16, 2020: ENGINE. POWER LOSS. NR 1 ENGINE N1 ROLLED BACK APPROX 15% AT CRUISE AND THEN RECOVERED AFTER 5-7 SECS AND HAD ASSOCIATED GRUMBLING NOISE FOR REMAINDER OF FLIGHT. NO EEC LIGHT AND N
- [SDR SWAA2020092418217](https://openairdocs.org/sdr/SWAA2020092418217), Sep 24, 2020: SIGN. MISSING. INTERIOR: EMERGENCY LIGHT EXIT MISSING BULB AT AFT SERVICE DOOR. RELAMPED AND PERFORMED GOOD TEST OF AFT SERVICE DOOR EMERGENCY EXIT SIGN, PER AMM 33-51-01-960-
- [SDR SWAA2020092418216](https://openairdocs.org/sdr/SWAA2020092418216), Sep 24, 2020: SIGN. MISSING. INTERIOR: EMERGENCY LIGHT EXIT MISSING BULB AT LT OVERWING DOOR AT UPPER SIGN. RELAMPED AND PERFORMED GOOD TEST OF LT OVERWING UPPER EMERGENCY EXIT SIGN, PER AM
- [SDR SWAA2020092418215](https://openairdocs.org/sdr/SWAA2020092418215), Sep 24, 2020: SIGN. MISSING. INTERIOR: EMERGENCY LIGHT EXIT MISSING BULB AT L1 AND LT OVERWING. RELAMPED AND PERFORMED GOOD TEST OF LT OVERWING EMERGENCY EXIT SIGN. REPLACED AND PERFORMED G
- [SDR SWAA2021081615934](https://openairdocs.org/sdr/SWAA2021081615934), Sep 14, 2020: FLOOR SPLICE. CORRODED. ***CORROSION*** AFT CARGO BAY FLOOR SPLICE CORRODED AT BS 727D. RBL14; WL156 / RECEIVED NEW/SERVICABLE AFT CARGO BAY FLOOR SPLICE AT BS 727D TO BE INSTALLED ON 
- [SDR SWAA2021080315933](https://openairdocs.org/sdr/SWAA2021080315933), Sep 14, 2020: SPLICE PLATE. CORRODED. ***CORROSION*** AFT CARGO BAY FLOOR SPLICE CORRODED AT BS 767+5. / RECEIVED SERVICEABLE REPLACEMENT PART; PO NUMBER 801448. REPLACEMENT SPLICE PLATE TO BE INSTA
- [SDR SWAA2020092416076](https://openairdocs.org/sdr/SWAA2020092416076), Sep 14, 2020: BATTERY PACK. FAULTY. EMERGENCY SLIDE LIGHT AT FWD SERVICE DOOR ONLY ILLUMINATES FOR A FEW SECONDS. REMOVED AND INSTALLED NEW. PERFORMED A GOOD INSTALLATION TEST OF THE M01674 BATTER
- [SDR SWAA2020092416075](https://openairdocs.org/sdr/SWAA2020092416075), Sep 14, 2020: LAMP. INOPERATIVE. EMERGENCY LIGHT AFT OF RIGHT SIDE FLAP IS OUT. RELAMPED AND PERFORMED GOOD TEST OF RIGHT AFT SLIDE EMERGENCY LIGHT, PER AMM 33-51-04-960-801. 59019U 14SEP20.
- [SDR SWAA2020092416074](https://openairdocs.org/sdr/SWAA2020092416074), Sep 14, 2020: WIRE. DISCONNECTED. EXIT SIGN ABOVE AFT ENTRY DOOR IS INOP. PERFORMED CONTINUITY TEST FROM CONNECTOR D2982 TO D10744 AND GROUND, PER WDM 33-51-14 AND FOUND WIRE W3142-0474-20 DISCO
- [SDR SWAA2020092818356](https://openairdocs.org/sdr/SWAA2020092818356), Sep 9, 2020: SKIN. DENTED. FUSELAGE SKIN HAS A DENT AT BS 578+4.5'; 1.5' ABOVE S-4R. REPAIRED FUSELAGE SKIN DENT AT BS 578+4.5'; 1.5' ABOVE S-4R, PER EA 20-153-01719 REV IR AND ER 20-0326
- [SDR SWAA2020092417810](https://openairdocs.org/sdr/SWAA2020092417810), Sep 8, 2020: SKIN. DENTED. FUSELAGE SKIN HAS A DENT AT BS 203.8+4.5'; 4' BELOW S-17L. FUSELAGE SKIN DENT AT BS 203.8+4.5'; 4' BELOW S-17L. REPAIRED IAW ATS ER 20-03255 REV IR DATED 23-SEP
- [SDR SWAA2020092417624](https://openairdocs.org/sdr/SWAA2020092417624), Sep 8, 2020: SKIN. DENTED. FUSELAGE SKIN HAS A DENT AT BS 827+8.5; 3.8' ABOVE S-7L. REPAIRED FUSELAGE SKIN DENT AT BS 827+8.5; 3.8' ABOVE S-7L, PER 737-700 SRM 53-00-01-2R-3 (REPAIR 3).
- [SDR SWAA2021081714476](https://openairdocs.org/sdr/SWAA2021081714476), Sep 7, 2020: ATTACH BRACKET. BROKEN. ATTACH BRACKET FOR PANEL 551FB AT IRSS 209 ALONG LOWER REAR SPAR CORD IS BROKEN / REMOVED ATTACH BRACKET FOR PANEL 551FB IAW SRM 51-40-02-0G-0. LOCATED AND DRIL
- [SDR SWAA2021081614440](https://openairdocs.org/sdr/SWAA2021081614440), Sep 7, 2020: CARGO TRACK. CORRODED. ***CORROSION*** ON TRACK TIEDOWN AT FWD CARGO BAY BS500 LBL18 WL157. / REMOVED AND INSTALLED NEW TRACK TIEDOWN AT FWD CARGO BAY AT BS396 TO BS500D LBL 18; WL 15
- [SDR SWAA2021081514455](https://openairdocs.org/sdr/SWAA2021081514455), Sep 7, 2020: SHIELD. CORRODED. ***CORROSION*** ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL24 WL157. / REMOVED AND REPLACED SHIELD AT FWD CARGO BAY LOCATED BS420-BS440 RBL24 WL157 ITEM 75
- [SDR SWAA2021081314452](https://openairdocs.org/sdr/SWAA2021081314452), Sep 7, 2020: SUPPORT. CORRODED. ***CORROSION*** IN AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT B.S. 727-767; R.B.L. 21; W.L. 154. / REMOVED AND REPLACED SIDEWALL SUPPORT AT ACB BS727-767 WL1
- [SDR SWAA2021081314453](https://openairdocs.org/sdr/SWAA2021081314453), Sep 7, 2020: SUPPORT. CORRODED. ***CORROSION*** IN AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT B.S. 727-847; L.B.L. 21; W.L. 154. / REMOVED AND REPLACED FLOOR SIDEWALL SUPPORT AT ACB BS727-8
- [SDR SWAA2021081214432](https://openairdocs.org/sdr/SWAA2021081214432), Sep 7, 2020: BOOT. DAMAGED. NOSE RADOME BOOT IS DAMAGED / REMOVED DAMAGED RADOME BOOT AND INSTALLED A NEW RADOME BOOT IAW. AMM 53-52-00-400-802. 6042U 14SEP20. AND AMM 53-52-00-000-802 604
- [SDR SWAA2021072014466](https://openairdocs.org/sdr/SWAA2021072014466), Sep 7, 2020: ATTACH ANGLE. BENT. AFT SHIELD HAS BENT ATTACH ANGLE AT FWD CARGO BAY BS500A RBL25 WL157. / FABRICATED NEW FCB AFT SHIELD ATTACH ANGLE BS500A RBL-25 WL-157 MADE FROM BAC1503 - 1001
- [SDR SWAA2021071514464](https://openairdocs.org/sdr/SWAA2021071514464), Sep 7, 2020: SUPPORT ANGLE. CORRODED. ***CORROSION*** ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FWD CARGO BAY BS500D LBL22 TO RBL22 WL157. / REMOVED AND REPLACED ON AFT BULKHEAD TO FLOOR SUPPORT ANG
- [SDR SWAA2021071514465](https://openairdocs.org/sdr/SWAA2021071514465), Sep 7, 2020: SUPPORT ANGLE. CORRODED. ***CORROSION*** ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FWD CARGO BAY BS500D RBL25 WL157. / REMOVED AND REPLACED ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE 
- [SDR SWAA2021071414444](https://openairdocs.org/sdr/SWAA2021071414444), Sep 7, 2020: ATTACH ANGLE. CRACKED. CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 RBL25 WL156. / REMOVED AND REPLACED ON INTERCOSTAL ATTACH ANGLE AT FCB BS 400 RBL 25 NEW P/N 143A7502-15
- [SDR SWAA2021071414448](https://openairdocs.org/sdr/SWAA2021071414448), Sep 7, 2020: ATTACH ANGLE. CRACKED. CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500B FWD SIDE LBL25 WL156. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS 500B FWD SIDE LBL25 IAW
- [SDR SWAA2021052614469](https://openairdocs.org/sdr/SWAA2021052614469), Sep 7, 2020: GUSSET. CRACKED. FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / REMOVED AND REPLACED ON FCB AFT BULKHEAD SUPPORT GUSSET BS 500D S-19L P/N 143A
- [SDR SWAA2021052614470](https://openairdocs.org/sdr/SWAA2021052614470), Sep 7, 2020: GUSSET. CRACKED. FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / REMOVED AND REPLACED ON FCB AFT BULKHEAD SUPPORT GUSSET BS 500D S-19R P/N 143A
- [SDR SWAA2020092814447](https://openairdocs.org/sdr/SWAA2020092814447), Sep 7, 2020: ATTACH ANGLE. CRACKED. CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS 500C FWD SIDE RBL 25 WL 156. REMOVED AND REPLACED NEW ON INTERCOSTAL ATTACH ANGLE AT FCB BS 500C RBL 25 P/N
- [SDR SWAA2020092414468](https://openairdocs.org/sdr/SWAA2020092414468), Sep 7, 2020: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 540 S-23R WL 167. CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 540 - S-23R. REPAIRED, IAW ATS ER 20-03242 R
- [SDR SWAA2020092414467](https://openairdocs.org/sdr/SWAA2020092414467), Sep 7, 2020: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 540 S-27L WL151. CRACKED STRINGER AT BS 540 S-27L WL151 WAS REPAIRED, IAW SRM 53-00-03-2R-1 REPAIR 1.
- [SDR SWAA2020092414446](https://openairdocs.org/sdr/SWAA2020092414446), Sep 7, 2020: SKIN. BENT. FORWARD ENTRY DOOR UPPER AFT DOOR SKIN IS BENT. REPAIRED FORWARD ENTRY DOOR UPPER AFT DOOR SKIN, PER SRM 52-00-01-2R-2.
- [SDR SWAA2021062414427](https://openairdocs.org/sdr/SWAA2021062414427), Sep 5, 2020: SCUFF PLATE. CRACKED. FWD CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED / LOCATED AND DRILLED FWD CARGO AFT CORNER SCUFF PLATE IAW SRM 51-40-05-0G-0 SCUFF PLATE TO BE INSTALLED ON CUS
- [SDR SWAA2021062414426](https://openairdocs.org/sdr/SWAA2021062414426), Sep 5, 2020: SCUFF PLATE. CRACKED. FWD CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED / LOCATED AND DRILLED NEW FWD CARGO BAY FWD CORNER SCUFF PLATE IAW SRM 51-40-05-0G-0 SCUFF PLATE TO BE INSTALLE
- [SDR SWAA2021072014423](https://openairdocs.org/sdr/SWAA2021072014423), Sep 4, 2020: ATTACH ANGLE. CRACKED. RIGHT WING FIXED T/E PANEL LOWER WEB ATTACH ANGLE CRACKED; JUST IB OF DEFLECTION RIB ORSS278. MARKED / REMOVED AND REPLACED RIGHT WING FIXED T/E PANEL LOWER WEB
- [SDR SWAA2021041314397](https://openairdocs.org/sdr/SWAA2021041314397), Sep 4, 2020: SKIN. DENTED. TRANSFERRED FROM CARD V262886=FUSELAGE EXTERNAL SKIN DENT AT STA. 1006 + 3.5'; 2.5' BELOW STR. 16R HAS ADDITIONAL GOUGE DAMAGE NOTED IN DENTED AREA. / FUSELAGE 
- [SDR SWAA2020092814419](https://openairdocs.org/sdr/SWAA2020092814419), Sep 4, 2020: SEAT TRACK. DAMAGED. MECHANICAL DAMAGE ON SEAT TRACK AT PASSENGER CABIN BS 520 LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK AT PASSENGER CABIN FROM BS 480-520 LBL 45 WL 208, AS PE
- [SDR SWAA2020092814418](https://openairdocs.org/sdr/SWAA2020092814418), Sep 4, 2020: SEAT TRACK. DAMAGED. MECHANICAL DAMAGE ON SEAT TRACK AT PASSENGER CABIN BS 520 LBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK AT PASSENGER CABIN FROM BS 480-520 LBL 25 WL 208, AS PE

All 318: https://openairdocs.org/deregistered/N744SW-2024-09-18/reports.md

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