# N714CB: 1998 Boeing 737-7H4, registration cancelled 2024-10-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 15, 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: 27848
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 19, 1998
- Certificate issued: August 1, 1998
- Last registry action: April 21, 2023
- Mode S code: A98B1D
- 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/N714CB
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=714CB
- Page: https://openairdocs.org/deregistered/N714CB-2024-10-15

From the FAA registry file of October 31, 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 (270, newest 50)

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

- [SDR SWAA2021122154114](https://openairdocs.org/sdr/SWAA2021122154114), Dec 17, 2021: FLAP SYSTEM. FAULTED. ON APPROACH SELECTED FLAPS 15 AND THEN 30. AT WHICH TIME WE NOTICED FLAP INDICATOR WAS AT 5. EXC. GO AROUND AND USED QRH ALT FLAP EXT PROCEDURES. PERFORMED FSEU
- [SDR SWAA2021122053486](https://openairdocs.org/sdr/SWAA2021122053486), Dec 15, 2021: PANEL. ELONGATED. SUPPLEMENTAL INFORMATION: AFT WING-TO-BODY FAIRING PANEL 194E HAS ELONGATED FASTENER HOLES. ; / [01] TRIMMED; DRILLED; AND PAINTED NEW PNL; [02] REMOVED & REPLA
- [SDR SWAA2021122053205](https://openairdocs.org/sdr/SWAA2021122053205), Dec 15, 2021: PANEL. ELONGATED. CENTER WHEEL WELL PANEL 193D FASTENER HOLES ELONGATED. ; / [01] TRIMMED; DRILLED AND PAINTED NEW PNL; [02] REMOVED &REPLACE PANEL PER AMM 53-51-21
- [SDR SWAA2021092119554](https://openairdocs.org/sdr/SWAA2021092119554), Sep 17, 2021: HANDLE. LOOSE. AFT ENTRY DOOR SLIDE HANDLE EXPOSED ; / [01] SECURED AFT ENTRY DOOR SLIDE HANDLE IAW AMM 25-66-01
- [SDR SWAA2021092120453](https://openairdocs.org/sdr/SWAA2021092120453), Sep 17, 2021: HANDLE. LOOSE. AFT ENTRY DOOR SLIDE HANDLE EXPOSED ; / [01] SECURED AFT ENTRY DOOR SLIDE HANDLE IAW AMM 25-66-01
- [SDR SWAA2021061682904](https://openairdocs.org/sdr/SWAA2021061682904), Jun 13, 2021: LIGHT. INOPERATIVE. LH EMERGENCY EXIT SIDEWALL LIGHT INOP ; / OK TO CONTINUE PER MEL 33-2-03 SP1B; RR'D RH OVERWING EXIT SIDEWALL FUSE IAW AMM 33-51-01
- [SDR SWAA2021042967409](https://openairdocs.org/sdr/SWAA2021042967409), Apr 26, 2021: LIGHT. INOPERATIVE. ROW 12 DEF SIDEWALL LIGHT INOP ; ROW 12 DEF SIDEWALL LIGHT INOP /
- [SDR SWAA2021040159266](https://openairdocs.org/sdr/SWAA2021040159266), Mar 28, 2021: LENS. MISSING. EMERGENCY AISLE LIGHT BEZEL/LENS MISSING AT 13DEF / CLEARED ON DMA 0718865 REPLACED MISSING EMERGENCY LIGHT LENS AT SEAT ROW 13DEF IAW AMM 33-51-03 CL NO 74301
- [SDR SWAA2020112331793](https://openairdocs.org/sdr/SWAA2020112331793), Nov 20, 2020: LINKAGE. BROKEN. R1 DOOR SLIDE LINKAGE BROKEN. REPLACED LINKAGE, REF MT 725-61-06 AMM 25-66-01.
- [SDR SWAA2021051204424](https://openairdocs.org/sdr/SWAA2021051204424), Jul 28, 2020: SKATE ANGLE. CORRODED. #2 ENG FWD ENG STRUT FAIRING STRUCTURE INBD SKATE ANGLE HAS CORROSION AT APPROX NAC STA 252-256 UNDER PANEL 441DL. / REPAIRED PER EA 20-154-01219
- [SDR SWAA2020080304426](https://openairdocs.org/sdr/SWAA2020080304426), Jul 28, 2020: BATTERY PACK. NO TEST. EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY FUNCTIONAL CHECK AT LOCATION M01669. R&R EMERGENCY LIGHTING BATTERY PACK AND POWER SUPPLY AS PER AMM 33-51-06.
- [SDR SWAA2020072702817](https://openairdocs.org/sdr/SWAA2020072702817), Jul 22, 2020: BATTERY PACK. INOPERATIVE. EXIT LIGHTS CONNECTED TO M1674 BATTERY PACK DO NOT COME ON / REMOVED AND REPLACED M1674 BATTERY PACK AND OPS CHECKED PER AMM 33-51-06-960-805 CHECKED GOOD
- [SDR SWAA2020072702351](https://openairdocs.org/sdr/SWAA2020072702351), Jul 20, 2020: HOUSING. DAMAGED. AFT ENTRY WAY CENTER EMERGENCY EXIT LIGHT HOUSING IS DAMAGED. / REPLACED AFT ENTRY WAY CENTER EMERGENCY LIGHT HOUSING; OPS CHECK WAS GOOD IAW AMM 33-51-01-960-8
- [SDR SWAA2020072700652](https://openairdocs.org/sdr/SWAA2020072700652), Jul 14, 2020: SKIN. CORRODED. UPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 679 RBL 5 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND 2R. / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-
- [SDR SWAA2020072700651](https://openairdocs.org/sdr/SWAA2020072700651), Jul 14, 2020: SKIN. CORRODED. UPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 683 RBL 2;RBL 9 AT FASTENER HOLES. INBETWEEN STRINGER 1R AND 2R / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER 
- [SDR SWAA2020072700650](https://openairdocs.org/sdr/SWAA2020072700650), Jul 14, 2020: SKIN. CORRODED. UPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 694;RBL 9 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND STR2R / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 2
- [SDR SWAA2020072700649](https://openairdocs.org/sdr/SWAA2020072700649), Jul 14, 2020: SKIN. CORRODED. UPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 701; RBL3 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND 2R. / REPAIRED UPPER EXTERIOR FUSELAGE SKIN PER ATS ER 2
- [SDR SWAA2020072797632](https://openairdocs.org/sdr/SWAA2020072797632), Jul 4, 2020: FRAME. CORRODED. BS 847 FRAME UPPER SURFACE CORRODED. LBL20; WL156. REPAIRED THE FRAME IAW ER20-02837, REV IR, AND EA 20-153-01157, REV IR.
- [SDR SWAA2020072797627](https://openairdocs.org/sdr/SWAA2020072797627), Jul 2, 2020: BULKHEAD WEB. CORRODED. ***CORROSION*** ON BS 259.5 BULKHEAD WEB WL 207 LBL 10 - RBL 2. / BS 259.5 WEB REPAIRED IAW EA # 20-153-01002 REV IR AND ER # 20-02836 REV IR.
- [SDR SWAA2021080397612](https://openairdocs.org/sdr/SWAA2021080397612), Jul 1, 2020: FLOORBEAM. CRACKED. BREAK PANEL IS CRACKED STA 540; RBL 1; WL 208. (MARKED) / REMOVED AND REPLACED BREAK PANEL AT STA540 RBL1 IAW SRM 51-40-02 AND AIPC 53-31-00-05
- [SDR SWAA2021080397611](https://openairdocs.org/sdr/SWAA2021080397611), Jul 1, 2020: FLOORBEAM. CRACKED. BREAK PANEL IS CRACKED STA 540; LBL 1; WL 208. (MARKED) / REMOVED AND REPLACED BREAK PANEL AT STA540 LBL1 IAW SRM 51-40-02 AND AIPC 53-31-00-05
- [SDR SWAA2020072797614](https://openairdocs.org/sdr/SWAA2020072797614), Jul 1, 2020: STRUCTURE. CORRODED. ***CORROSION*** ON AFT CHORD OF BS 259.5 BULKHEAD WL 207 LBL 10-RBL 6. / THE DAMAGE IS REPAIRED PER EA 20-153-01002 REV IR AND ER #20-02836 REV IR. REFER TO NRC
- [SDR SWAA2020072797613](https://openairdocs.org/sdr/SWAA2020072797613), Jul 1, 2020: STRUCTURE. CORRODED. CORROSION ON FWD CHORD OF BS 259.5 BULKHEAD, WL 207, LBL 10 - RBL 3. REMOVED AND REPLACED CHORD IAW SRM 51-40-02-0G-0, DWG 141A5133, REV C, AND DWG 141A7430, RE
- [SDR SWAA2020072797623](https://openairdocs.org/sdr/SWAA2020072797623), Jul 1, 2020: STIFFENER. CORRODED. CORROSION ON VERTICAL STIFFENER AT BS 225 RBL 5 WL 160. FOUND CORROSION ON VERTICAL STIFFNER AT BS225 RBL5 WL160 TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. RE
- [SDR SWAA2020072797624](https://openairdocs.org/sdr/SWAA2020072797624), Jul 1, 2020: STIFFENER. CORRODED. CORROSION ON VERTICAL STIFFENER AT BS 225 LBL 5 WL 160. FOUND CORROSION ON VERTICAL STIFFNER AT BS 225, LBL 5, WL 160 TO BE OUT OF LIMITS DUE TO NO LIMITS IN SR
- [SDR SWAA2020072797602](https://openairdocs.org/sdr/SWAA2020072797602), Jul 1, 2020: STRINGER. CORRODED. FWD CARGO BAY STRINGER 23R HAS CORROSION AT END OF STRINGER BS536 WL164 RBL46 / REPAIRED STRINGER IN FWD CARGO BAY BS536. STR 23R WL164; RBL46 PER ER 20-02826 R
- [SDR SWAA2021081997560](https://openairdocs.org/sdr/SWAA2021081997560), Jun 30, 2020: BEAM. CRACKED. LT WING AFT LWR T/E PANEL BEAM JUST O/B OF THE #1 PYLON IS CRACKED. / REMOVED AND REPLACED LT WING AFT LWR T/E PANEL BEAM JUST O/B OF THE NO 1 PYLON IAW SRM 51-
- [SDR SWAA2021081797590](https://openairdocs.org/sdr/SWAA2021081797590), Jun 30, 2020: SUPPORT. CORRODED. AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUT PLATE HOLES BS727 TO BS767 RBL23 WL156 / REMOVED CORROSION DAMAGED FLOOR TO SIDEWALL 
- [SDR SWAA2021081797589](https://openairdocs.org/sdr/SWAA2021081797589), Jun 30, 2020: SUPPORT. CORRODED. AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUT PLATE HOLES BS727 TO BS847 LBL23 WL156 / EVALUATED CORROSION ON ACB L/H FLOOR TO SIDE
- [SDR SWAA2021081797591](https://openairdocs.org/sdr/SWAA2021081797591), Jun 30, 2020: SPLICE STRAP. CORRODED. AFT CARGO BAY FLOOR SPLICE STRAP AT BS767+4 HAS CORROSION AROUND NUT PLATE HOLES RBL10 TO LBL10 WL156 / RECEIVED NEW ACB FLOOR SPLICE STRAP BS767+4 ON PO# 79620
- [SDR SWAA2021081797592](https://openairdocs.org/sdr/SWAA2021081797592), Jun 30, 2020: SPLICE STRAP. CORRODED. AFT CARGO BAY FLOOR SPLICE STRAP AT BS887 HAS CORROSION AROUND NUT PLATE HOLES RBL10 TO LBL10 WL156 / EVALUATED CORROSION ON ACB FLOOR SPLICE STRAP; BS887; FOUN
- [SDR SWAA2021081597593](https://openairdocs.org/sdr/SWAA2021081597593), Jun 30, 2020: SUPPORT. CORRODED. AFT CARGO BAY LOWER BULKHEAD SUPPORT BS847 TO BS867 LBL10 TO WL156 HAS CORROSION / REMOVED AND REPLACED AFT CARGO BAY LOWER BULKHEAD SUPPORT BS847 TO 867 LBL10 
- [SDR SWAA2021081397594](https://openairdocs.org/sdr/SWAA2021081397594), Jun 30, 2020: WEB. CORRODED. AFT CARGO BAY WEB BETWEEN BS787 TO BS807 RBL6 WL150 HAS CORROSION / EVALUATED CORROSION ON WEB BETWEEN BS787-807; RBL6; FOUND TO BE OUT OF LIMITS; DUE TO NO LIM
- [SDR SWAA2021072997552](https://openairdocs.org/sdr/SWAA2021072997552), Jun 30, 2020: BOLT. BROKEN. BROKEN NUTPLATE FOR MOUNT BOLT ON DORSAL FIN. / REMOVED AND REPLACED NUT PLATE FOR MOUNT BOLT ON DORSAL FIN IAW SRM 51-40-02-0G-0 AND IPC 55-32-11-02. DWG #174A
- [SDR SWAA2020072797574](https://openairdocs.org/sdr/SWAA2020072797574), Jun 30, 2020: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK IN MULTIPLE AREAS AT PASSENGER CABIN BS480 - BS520 LBL45 WL208. MARKED / REMOVED CORROSION AND SEAT TRACK WAS FOUND TO BE OUT OF LIMITS 
- [SDR SWAA2020072797575](https://openairdocs.org/sdr/SWAA2020072797575), Jun 30, 2020: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK IN MULTIPLE AREAS AT PASSENGER CABIN BS 480 - 520, RBL 45, WL 208. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02-0G-0.
- [SDR SWAA2020072797598](https://openairdocs.org/sdr/SWAA2020072797598), Jun 30, 2020: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL 231XF UPPER SURFACE WAS DAMAGED. DUE TO THE EXTENT OF DAMAGE, FABRICATED A NEW CABIN FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1A, AND DWG 144A58
- [SDR SWAA2020072797599](https://openairdocs.org/sdr/SWAA2020072797599), Jun 30, 2020: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL 241AF UPPER SURFACE WAS DAMAGED. DUE TO THE EXTENT OF DAMAGE, FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1A AND DWG 144A5810-8.
- [SDR SWAA2020072797600](https://openairdocs.org/sdr/SWAA2020072797600), Jun 30, 2020: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL 241DF UPPER SURFACE WAS DAMAGED. DUE TO THE EXTENT OF DAMAGE, FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0, PARA 1A, AND DWG 144A5810-9.
- [SDR SWAA2020072797551](https://openairdocs.org/sdr/SWAA2020072797551), Jun 29, 2020: SKIN. CORRODED. CORROSION ON CROWN SKIN EXTERNAL SURFACE IN MULTIPLE AREAS FROM APPROXIMATELY BS 887- BS 996 STR 3L - STR 3R / REPAIRED DAMAGE ON CROWN SKIN EXTERNAL SURFACE IN
- [SDR SWAA2020072703504](https://openairdocs.org/sdr/SWAA2020072703504), Jun 29, 2020: FLOOR SKIN. DENTED. FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / REPAIRED FLIGHT DECK FLOOR EA #1-A53-33179 REV IR.
- [SDR SWAA2020012874817](https://openairdocs.org/sdr/SWAA2020012874817), Jan 24, 2020: FUSE. INOPERATIVE. EMERGENCY LIGHT ON CEILING IN FORWARD GALLEY AND LIGHT NEXT TO FORWARD JUMPSEAT INOP. REMOVED AND REPLACED BATTERY PACK AND FUSES FOR EMERGENCY LIGHT POWER SUPP
- [SDR SWAA2020012874775](https://openairdocs.org/sdr/SWAA2020012874775), Jan 24, 2020: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT ON CEILING IN FORWARD GALLEY AND LIGHT NEXT TO FORWARD JUMPSEAT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND FUSES FOR EMERGENCY LIGHT
- [SDR SWAA2019121739763](https://openairdocs.org/sdr/SWAA2019121739763), Dec 16, 2019: SLIDE. OUT OF POSITION. L2 DOOR SLIDE LOOSE AND WAS HANGING ON DOOR. / REPOSITIONED SLIDE PER MT.
- [SDR SWAA2019103138404](https://openairdocs.org/sdr/SWAA2019103138404), Oct 30, 2019: LAMP. INOPERATIVE. R/H AFT EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.
- [SDR SWAA2019103138403](https://openairdocs.org/sdr/SWAA2019103138403), Oct 30, 2019: LAMP. INOPERATIVE. L/H AFT EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.
- [SDR SWAA2019100237460](https://openairdocs.org/sdr/SWAA2019100237460), Sep 29, 2019: WIRE. BROKEN. FORWARD LT EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND A BROKEN WIRE, AFT OF THE FORWARD ENTRY DOOR, RETAINING LANYARD. REPAIRED LIGHT PER AMM. R&R LENS RETAINE
- [SDR SWAA2019100137431](https://openairdocs.org/sdr/SWAA2019100137431), Sep 27, 2019: OIL SYSTEM. LOW PRESSURE. INFLIGHT SHUTDOWN, DIVERTED, AND DECLARED AN EMERGENCY, OIL QUANTITY FOR THE NR 2 ENGINE DECREASED TO ZERO, FOLLOWED BY A LOW OIL PRESSURE LIGHT AND OIL PRESSUR
- [SDR SWAA2019091036733](https://openairdocs.org/sdr/SWAA2019091036733), Sep 5, 2019: GIRT BAR. LOOSE. R1 DOOR GIRT BAR LOOSE. SECURED GIRT BAR IAW AMM.
- [SDR SWAA2022031569917](https://openairdocs.org/sdr/SWAA2022031569917), Aug 22, 2019: BRACKET. CRACKED. LEFT WING FIXED UPPER TRAILING EDGE PANEL CENTER INNER BRACKET CRACKED ABOVE NACELLE STRUT FAIRING / REMOVED AND REPLACED PER SRM 51-40-02.

All 270: https://openairdocs.org/deregistered/N714CB-2024-10-15/reports.md

## 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.

- [Incident 20001211025069I](https://openairdocs.org/incident/20001211025069I), Dec 11, 2000: Boeing 7377H4 (N714CB), Kansas City, MO, Substantial damage. (-23)On December 11, 2000, at approximately 1324 CDT, southwest airlines flight 510, a Boeing 737-700, N714CB, from mdw, slid off the taxiway at the…

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