# N784SW: 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: 29810
- Year built: 2000
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 8, 2000
- Certificate issued: October 25, 2000
- Last registry action: June 3, 2023
- Mode S code: AAA107
- 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/N784SW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=784SW
- Page: https://openairdocs.org/deregistered/N784SW-2024-10-04

From the FAA registry file of October 28, 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 (271, newest 50)

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

- [SDR SWAA2023080384717](https://openairdocs.org/sdr/SWAA2023080384717), Aug 2, 2023: LIGHT. UNSECURE. FWD CABIN FLOOR EMERGENCY LUMINESCENT STRIP NEEDS TO BE SECURED AT FWD RH BULKHEAD.<[01] SECURED FWD CABIN FLOOR EMERGENCY LUMINESCENT STRIP AT FWD RH BULKHEAD 
- [SDR SWAA2023050846629](https://openairdocs.org/sdr/SWAA2023050846629), May 6, 2023: MEGAPHONE. FAILED. AFT MEGAPHONE WILL NOT TEST<[01] REPLACED BATTERIES FOR AFT MEGAPHONE PER AMM 25-64-00. OPS CHECK IS GOOD
- [SDR SWAA2023040322416](https://openairdocs.org/sdr/SWAA2023040322416), Mar 31, 2023: LENS. STAINED. BOTH OVER WING EXITS LIGHT LENSES ARE STAINED.<[01] REPLACED LENSES PER AMM 33-51-01
- [SDR SWAA2023040322418](https://openairdocs.org/sdr/SWAA2023040322418), Mar 31, 2023: SLIDE. LOOSE. FWD SERVICE DOOR AFT SLIDE ISOLATOR LOOSE<[01] R&R FWD SERVICE DOOR AFT SLIDE ISOLATOR IAW AMM 20-50-11.;[02] INSPECTION C/W R&R FWD SERVICE DOOR AFT SLIDE ISOL
- [SDR SWAA2023030110296](https://openairdocs.org/sdr/SWAA2023030110296), Feb 26, 2023: BATTERY PACK. INOPERATIVE. THREE AFT EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED AFT RH EMERGENCY BATTERY PACK IN REF TO AMM 33-51-06. OPS CHECK GOOD
- [SDR SWAA2023020297768](https://openairdocs.org/sdr/SWAA2023020297768), Feb 2, 2023: LIGHT. INOPERATIVE. EMERGENCY LIGHT AFT OF THE AFT SERVICE DOOR INOP<[01] RELAMP'ED EMER. LITE AFT OF THE AFT SERVICE DOOR REF M/M 33-51-22
- [SDR SWAA2023010588315](https://openairdocs.org/sdr/SWAA2023010588315), Jan 4, 2023: MEGAPHONE. INOPERATIVE. FWD MEGA PHONE HANDLE LOOSE AND INOPERATIVE. REMOVED AND REPLACED FWD MEGA PHONE PER AMM 25-64-00.
- [SDR SWAA2022112875595](https://openairdocs.org/sdr/SWAA2022112875595), Nov 25, 2022: MEGAPHONE. INOPERATIVE. FA WRITE UP - FWD MEGAPHONE NEEDS BATTERY / [01] REMOVED AND REPLACED BATTERIES PER AMM SIP
- [SDR SWAA2022111068411](https://openairdocs.org/sdr/SWAA2022111068411), Nov 6, 2022: SLIDE. OUT OF ADJUST. AFT A/C LEFT: EMERGENCY ESCAPE SLIDE HAS MANUAL PULL HANDLE EXPOSED / [01] ATTACHED PULLHANDLE COVER TO VELCRO PER SIP
- [SDR SWAA2022062822651](https://openairdocs.org/sdr/SWAA2022062822651), Jun 24, 2022: SLIDE. OUT OF POSITION. FWD ENTRY DOOR SLIDE PULLED OUT OF NORMAL / [01] SLIDE SKIRT DROOPING REFOLDED SLIDE SKIRT OK FOR SERVICE. SLIDE WAS NOT DEPLOYED IAW SIP
- [SDR SWAA2022041995225](https://openairdocs.org/sdr/SWAA2022041995225), Apr 17, 2022: COVER. LOOSE. SLIDE PULL HANDLE COVERS- FWD ENTRY & BOTH REAR DOORS NEED TO BE RESECURED / [01] RESECURED SLIDE PULL HANDLE COVERS ON FWD ENTRY AND BOTH DOORS PER SIP.;[02] R
- [SDR SWAA2022041492842](https://openairdocs.org/sdr/SWAA2022041492842), Apr 10, 2022: COVER. LOOSE. F/O OVER WING EXIT LIGHT FELL OFF / [01] RESECURE F/O OVERWING EXIT LIGHT COVER PER SIP
- [SDR SWAA2022032385654](https://openairdocs.org/sdr/SWAA2022032385654), Mar 19, 2022: LIGHT. LOOSE. R/H OVERWING UPPER RIGHT EXIT/SALIDA SIGN COVER LOOSE. / [01] REPOSITION AND RE TIGHTEN SCREW ON R/H OVER WING UPPER RIGHT EXIT/SALIDA SIGN COVER; OPS CHECK GOO
- [SDR SWAA2022031783218](https://openairdocs.org/sdr/SWAA2022031783218), Mar 13, 2022: LIGHT. INOPERATIVE. LOWER EMERGENCY EXIT LIGHT INOP LOWER EMERGENCY EXIT LIGHT INOP (F/O) SIDE CENTER DOOR / [01] R&R LOWER EMERGENCY EXIT LIGHT ASSY PER AMM 33-51-01. OPS CHECK GO
- [SDR SWAA2022031582758](https://openairdocs.org/sdr/SWAA2022031582758), Mar 11, 2022: NONE. NONE. ON TAKEOFF ROLL TOWER OBSERVED FLAMES COMING OUT OF THE #2 ENGINE. ALL ENGINE PARAMETERS NORMAL. / [01] PERFORMED FIM TASK 71-05 TASK 811 WITH NO FAULTS FOUND. 
- [SDR SWAA2022030379862](https://openairdocs.org/sdr/SWAA2022030379862), Mar 3, 2022: LIGHT. BROKEN. AIRCRAFT RIGHT FO OVER WING FWD EXIT SIGN COVER BROKEN / [01] RESECURRED COVER PER SIP
- [SDR SWAA2022010457054](https://openairdocs.org/sdr/SWAA2022010457054), Dec 29, 2021: LIGHT. INOPERATIVE. EMERGENCY LIGHT INOP AT OVERHEAD BIN SEAT 22 RH. ; EMERGENCY LIGHT INOP AT OVERHEAD IN SEAT 22 RH. / [01] RELAMPED EMERGENCY LIGHT AT OVERHEAD BIN SEAT 22 RH PE
- [SDR SWAA2022010555180](https://openairdocs.org/sdr/SWAA2022010555180), Dec 21, 2021: FLOOR SUPPORT. CRACKED. SUPPLEMENTAL INFORMATION: MAIN CABINE FLOOR SUPPORT CRACK AT STA.540 AND I/B OF SEAT TRACK RBL 24.75 ; / [01] LOCATED AND DRILLED NEW MAIN CABIN FLOOR SUPPORT P
- [SDR SWAA2021122754661](https://openairdocs.org/sdr/SWAA2021122754661), Dec 18, 2021: INTERCOSTAL. CRACKED. FWD CARGO BILGE INTERCOSTAL CRACKED AT BS500B TO BS500C AND S25L. REMOVED INTERCOSTAL AT FWD CARGO BS 500B TO BS 500C IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED
- [SDR SWAA2021122754660](https://openairdocs.org/sdr/SWAA2021122754660), Dec 18, 2021: ANGLE. CRACKED. FWD CARGO BILGE BS500B AND S25R ANGLE CLIP CRACKED. ; / [01] REMOVED AND REPLACED CLIP AT STA 500B AND STR 25R PER SRM 51-40-02-0G-0; [02] VERIFIED 1
- [SDR SWAA2022011254145](https://openairdocs.org/sdr/SWAA2022011254145), Dec 16, 2021: CAP. CORRODED. AFT CARGO L/H CAP STRIPS WITH CORROSION ; / [01] ORDERED NEW PARTS; [02] REMOVED DAMAGED AS PER B737-7 SRM 51-10-02-0G-0. CORROSION THROUGH MATERIAL FOUND OUT O
- [SDR SWAA2022011254146](https://openairdocs.org/sdr/SWAA2022011254146), Dec 16, 2021: CAP. CORRODED. AFT CARGO R/H CAP STRIPS WITH CORROSION ; / [01] RECIEVED NEW PARTS; [02] REMOVED DAMAGED AS PER B737-7 SRM 51-10-02-0G-0. CORROSION THROUGH MATERIAL FOUND OUT 
- [SDR SWAA2022011253499](https://openairdocs.org/sdr/SWAA2022011253499), Dec 15, 2021: SUPPORT BEAM. ELONGATED. RIGHT WING ACCESS PANEL 651GB UPPER SUPPORT BEAN FASTENER HOLE ELONGATED ( MARKED) ; / [01] PERFORMED HFEC INSP. IAW B737 NDT<BR>PART 6; 51-00-00; PROCEDURE 23.
- [SDR SWAA2022010552363](https://openairdocs.org/sdr/SWAA2022010552363), Dec 11, 2021: SHIELD. CRACKED. FWD CARGO AFT SHIELD IS CRACK ; / [01] RECEIVED NEW SHIELD LOCATED AND DRILL HOLES NEW SHIELD INSTALLED NUTPLATES AS PER SRM 51-40-05 AND 51-40-02; [02] VERIFIE
- [SDR SWAA2022011051936](https://openairdocs.org/sdr/SWAA2022011051936), Dec 10, 2021: SKIN. DELAMINATED. L/H WING SPOILER #6 HAS A DELAMINATED DENT LOCATED AT 9.75' FROM I/B EDGE AND 6.5' FROM AFT EDGE MEASURES L=0.5';W=O.5';Y=0.004';W/Y=125 ; / [01] PREPARED THE D
- [SDR SWAA2022011249854](https://openairdocs.org/sdr/SWAA2022011249854), Dec 3, 2021: RIB. CRACKED. SUPPLEMENTAL INFORMATION: VERTICAL DORSAL FIN FWD RIB CRACKED ; / [01] REMOVED AND REPLACED VERTICAL DORSAL FIN FWD RIB AS PER B737-700 SRM 51-40-02-0G-0 AND BO
- [SDR SWAA2022011249442](https://openairdocs.org/sdr/SWAA2022011249442), Dec 2, 2021: NONE. CRACKED. SUPPLEMENTAL INFORMATION: R/H STAB INSPAR RIB ASSY NO. 5 AT STAB STA 129.50 STIFFENER NO.4 CRACKED ; / [01] TRIMMED OUT DAMAGED AREA ON RH STAB INSPAR RIB ASSY 
- [SDR SWAA2022010549440](https://openairdocs.org/sdr/SWAA2022010549440), Dec 2, 2021: FLOOR PANEL. DELAMINATED. SUPPLEMENTAL INFORMATION: PAX CABIN FLOOR PANEL 222AF AFT O/B CORNER DELAMINATED ; / [01] MEASUREMENTS; [02] PREPARED DAMAGED AREA FOR REPAIR AT CABIN FLOOR PAN
- [SDR SWAA2022010449061](https://openairdocs.org/sdr/SWAA2022010449061), Dec 1, 2021: FLOOR PANEL. DELAMINATED. PAX CABIN FLOOR PANEL 221GF UPPER LAMINATE WITH SOME DELAMINATION ; / [01] RECEIVED FLOOR PANEL 221GF P/N:141A5810-181 REF. TASK CARD TTG8Q006QHXA FOR PANEL INS
- [SDR SWAA2022010449065](https://openairdocs.org/sdr/SWAA2022010449065), Dec 1, 2021: FLOOR PANEL. CRACKED. PAX CABIN FLOOR PANEL 221BF AFT O/B CORNER CRACKED ; / [01] PREPARED DAMAGED AREA AT FLOOR PANEL 221BF PER B737 SRN<BR>53-00-50-2R-0; [02] REPAIRED DAMAGED AREA
- [SDR SWAA2022011247580](https://openairdocs.org/sdr/SWAA2022011247580), Nov 25, 2021: ANGLE. CRACKED. SUPPLEMENTAL INFORMATION: CABIN FLOOR ANGLE AT STA 540 LBL 64 IS CRACK (228-007) ; CAIN FLOOR ANGLE AT STA 540 LBL 64 IS CRACK (228-007) / [01] INSTALLED PARCIA
- [SDR SWAA2022011247312](https://openairdocs.org/sdr/SWAA2022011247312), Nov 24, 2021: SUPPORT. CORRODED. AFT CARGO, BS 727 TO 847 LBL 21, S25L SIDEPLATE SUPPORT ZEE CORROUDED. REMOVED CORROSION IAW SRM 51-10-02-0G-0. REMOVED CORROSION ON LT Z-CHANNEL BS 727-847 LBL
- [SDR SWAA2021112947308](https://openairdocs.org/sdr/SWAA2021112947308), Nov 24, 2021: BEAM. CORRODED. CABIN FLOORBEAM AT BS 986.5, RBL 30, AND RBL 34 HAS SURFACE CORROSION ON THE UPPER AND LOWER SURFACES. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THI
- [SDR SWAA2021112947309](https://openairdocs.org/sdr/SWAA2021112947309), Nov 24, 2021: FLOORBEAM. CORRODED. CABIN FLOOR BEAM AT STA 986.5 LBL 32 AND LBL 35 HAS SURFACE CORROSION ON THE UPPER AND LOWER SURFACES OF THE FASTENER HOLE. REMOVED CORROSION IAW SRM 51-10-02-0
- [SDR SWAA2021112446375](https://openairdocs.org/sdr/SWAA2021112446375), Nov 20, 2021: TRACK. CORRODED. CABIN L/H SEAT TRACK I/B TRACK AT ABOUT STA 500A +6' WITH CORROSION. REMOVED LIGHT CORROSION AT CABIN L/H SEAT TRACK I/B TRACK STA 500A +6' CORRECTION TO STEP 1
- [SDR SWAA2021112446392](https://openairdocs.org/sdr/SWAA2021112446392), Nov 20, 2021: SEAT TRACK. CORRODED. CABIN L/H SEAT TRACK AT ABOUT STA 500D +14' WITH CORROSION. FAULT FOUND AT OB TRACK. REMOVED SURFACE CORROSION ON L/H I/B TRACK STA 500D+14 PER B737-700 SRM 51-
- [SDR SWAA2021112446397](https://openairdocs.org/sdr/SWAA2021112446397), Nov 20, 2021: TRACK. CORRODED. CABIN L/H SEAT TRACK O/B TRACK AT ABOUT STA 559+14' WITH CORROSION. REMOVED CORROSION ON SEAT TRACK STA 559B+14' LBL 45 AS PER B737-700 SRM 51-10-02-0G-0 VERIFI
- [SDR SWAA2022010545508](https://openairdocs.org/sdr/SWAA2022010545508), Nov 17, 2021: STUB FRAME. CRACKED. POSSIBLE CRACK AT CABIN R-1 DOOR FUSELAGE CUTOUT FWD EDGE BETWEEN S-8R AND S-9R. REMOVED SEALANT TO GAIN ACCESS FOR NDT INSPECTIONS TO CHECK FOR CRACK REF SRM 5
- [SDR SWAA2022010444684](https://openairdocs.org/sdr/SWAA2022010444684), Nov 17, 2021: FLOOR PANEL. DELAMINATED. FLOOR PANEL 241DF UPPER SURFACE DELAMINATED ; / [01] RECEIVED NEW FLOOR PANEL 241DF P/N 144A5810-128 P/O:1728471 REF. TASK CARD TTG8Q006QHHG FOR PANEL INSTALLAT
- [SDR SWAA2022010445113](https://openairdocs.org/sdr/SWAA2022010445113), Nov 17, 2021: FLOOR PANEL. DELAMINATED. FLOOR PANEL 241DF UPPER SURFACE DELAMINATED ; / [01] RECEIVED NEW FLOOR PANEL 241DF P/N 144A5810-128 P/O:1728471 REF. TASK CARD TTG8Q006QHHG FOR PANEL INSTALLAT
- [SDR SWAA2022011244681](https://openairdocs.org/sdr/SWAA2022011244681), Nov 16, 2021: FITTING. CRACKED. SUPPLEMENTAL INFORMATION: L/H WING T/E AT LWR DEFLECTOR RIB SEAL BRACKET INNER SIDE CRACKED ; / [01] REMOVED LWR DEFLECTOR RIB; FITTING AND SEAL; L/H WING T/E L
- [SDR SWAA2022011245110](https://openairdocs.org/sdr/SWAA2022011245110), Nov 16, 2021: FITTING. CRACKED. SUPPLEMENTAL INFORMATION: L/H WING T/E AT LWR DEFLECTOR RIB SEAL BRACKET INNER SIDE CRACKED ; / [01] REMOVED LWR DEFLECTOR RIB; FITTING AND SEAL; L/H WING T/E L
- [SDR SWAA2022010443989](https://openairdocs.org/sdr/SWAA2022010443989), Nov 15, 2021: BATTERY PACK. INOPERATIVE. SUPPLEMENTAL INFORMATION: FOUND EMERGENCY LIGHT POWER SUPPLY M1673 INOP ;(AFT GALLEY CEILING). ; / [01] REMOVED AND REPLACED BATTERY PACK AT AFT GALLEY CEILING 
- [SDR SWAA2022010443983](https://openairdocs.org/sdr/SWAA2022010443983), Nov 15, 2021: FLOOR PANEL. DETERIORATED. SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT;FLOOR PANEL 140AF IS DETERIORATED ; / [01] FABRICATED AFT CARGO FLOOR PANEL 140AF AS PER B737-700 AMM 25-52-01-2
- [SDR SWAA2022010443428](https://openairdocs.org/sdr/SWAA2022010443428), Nov 15, 2021: NONE. OUT OF TOLERANCE. SUPPLEMENTAL INFORMATION: L2 DOOR EMERGENCY ESCAPE SYSTEM; RETAINER CLIPS (BOTH); MEASUREMENTS OUT OF LIMITS ; / [01] DUPLICATE. REF TASK CARD# TTG8Q009B258.; [
- [SDR SWAA2022010443427](https://openairdocs.org/sdr/SWAA2022010443427), Nov 15, 2021: RETAINER CUP. OUT OF TOLERANCE. L1 DOOR EMERGENCY ESCAPE SYSTEM; RETAINER CLIPS (BOTH); MEASUREMENTS OUT OF LIMITS ; / [01] REMOVED AND REPLACED BOTH FLOOR-MOUNTED ESCAPE SLIDE BRACKET/CLIP ON
- [SDR SWAA2020020544161](https://openairdocs.org/sdr/SWAA2020020544161), Jan 31, 2020: SLIDE. DISLODGED. R1 DOOR SLIDE DISLODGED. / RESECURED SLIDE PER AMM.
- [SDR SWAA2020013040919](https://openairdocs.org/sdr/SWAA2020013040919), Jan 25, 2020: FITTING. CORRODED. LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTBOARD FACE HAD CORROSION. REPAIRED PER WO SSR1207.
- [SDR SWAA2020013040918](https://openairdocs.org/sdr/SWAA2020013040918), Jan 25, 2020: FITTING. CORRODED. LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG INBOARD FACE HAD CORROSION. REPAIRED FACE PER WO 1207.
- [SDR SWAA2020013040917](https://openairdocs.org/sdr/SWAA2020013040917), Jan 25, 2020: FITTING. CORRODED. LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG OUTBOARD FACE HAD CORROSION. REPAIRED FACE PER WO SSR1207.

All 271: https://openairdocs.org/deregistered/N784SW-2024-10-04/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA16CA094](https://openairdocs.org/ntsb/DCA16CA094), Feb 17, 2016: Boeing 737 7H4 (N784SW), Detroit, MI, substantial damage. Probable cause: N925NN flight crew's incorrect evaluation of the clearance between the two aircraft, leading to the inadvertent collision of the winglet with the horizontal stabilizer and elevator of N784SW.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20160217002962A](https://openairdocs.org/incident/20160217002962A), Feb 17, 2016: Boeing 737-7H4 (N784SW), Detroit, MI, Substantial damage. On February 17th, 2016, at approximately 0600 local time, the emi-fsdo was notified of an accident at dtw airport involving two Boeing 737 aircraft contacting…

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