# N514SW: 1991 Boeing 737-5H4, registration cancelled 2016-07-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 13, 2016 - Exported to: China - Status when cancelled: Valid registration - Airframe: [Boeing 737-5H4](https://openairdocs.org/model/boeing-737-5h4) (registry code 138449D) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 25153 - Year built: 1991 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 2, 1991 - Certificate issued: May 13, 2016 - Last registry action: May 13, 2016 - Mode S code: A671F0 - Owner when cancelled: [Infinity Trading & Solutions LLC](https://openairdocs.org/faa-owner/INFINITY%20TRADING%20%26%20SOLUTIONS%20LLC) - Location: [Chandler, AZ](https://openairdocs.org/faa-place/AZ/Chandler) - Owner type: Corporation - Owner's area on the map: 33.3178° N, 111.8305° W: Placed by OpenAirDocs at the center of ZIP code 85225, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N514SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=514SW - Page: https://openairdocs.org/deregistered/N514SW-2016-07-13 From the FAA registry file of October 27, 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 737-5H4: https://openairdocs.org/model/boeing-737-5h4.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 SWAA2015113046545](https://openairdocs.org/sdr/SWAA2015113046545), Nov 17, 2015: SKIN. CRACKED. SKIN CRACKED AT BS 380+4, STRINGER 15L. REPAIRED SKIN IAW EA. - [SDR SWAA2015112546454](https://openairdocs.org/sdr/SWAA2015112546454), Nov 17, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT BS 360-10, STRINGER 2L. R & R SKIN IAW SRM. - [SDR SWAA2015112546453](https://openairdocs.org/sdr/SWAA2015112546453), Nov 16, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT BS 807-2, STRINGER 22L. REPAIRED SKIN IAW SRM & EA. - [SDR SWAA2015100944736](https://openairdocs.org/sdr/SWAA2015100944736), Oct 7, 2015: LENS. LOOSE. LEFT EMER LIGHT LENS LOOSE. REPAIRED LENS IAW MM. - [SDR SWAA2015070941676](https://openairdocs.org/sdr/SWAA2015070941676), Jul 5, 2015: COVER. LOOSE. R2 DOOR EMER EXIT SIGN COVER LOOSE. SECURED COVER IAW SIP. - [SDR SWAA2015062541129](https://openairdocs.org/sdr/SWAA2015062541129), Jun 2, 2015: SUPPORT FITTING. CRACKED. LEFT WING NR 2 FLAP TRACK SUPPORT FITTING CRACKED. REPAIRED FITTING IAW EA. - [SDR SWAA2015050739401](https://openairdocs.org/sdr/SWAA2015050739401), May 6, 2015: SENSOR. FAULTY. AIR TURN BACK & DECLARED EMER. NR 1 ENG OVERHEAT ON CLIMB OUT, ALL ENG PARAMETERS WERE NORMAL. ENG OVERHEAT EXTINGUISHED UPON THRUST REDUCTION. R & R LOWER FIRE - [SDR SWAA2015031037302](https://openairdocs.org/sdr/SWAA2015031037302), Mar 9, 2015: CABLE. MISROUTED. R2 DOOR ESCAPE SLIDE GIRT BAR RELEASE CABLE MISROUTED. REROUTED CABLE IAW MT. - [SDR SWAA2015031037301](https://openairdocs.org/sdr/SWAA2015031037301), Mar 9, 2015: LIGHT. INOPERATIVE. FORWARD ENTRY DOOR ON AFT FACE OF FWD LAVATORY EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM. - [SDR SWAA2015030937221](https://openairdocs.org/sdr/SWAA2015030937221), Mar 5, 2015: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 400, STRINGER 15R. R & R CLIP IAW SRM & DWG. - [SDR SWAA2015031037300](https://openairdocs.org/sdr/SWAA2015031037300), Feb 20, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED BETWEEN BS 913.5 TO 914, STRINGER 10L. REPAIRED SKIN IAW ER & EA. - [SDR SWAA2015031037299](https://openairdocs.org/sdr/SWAA2015031037299), Feb 20, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED BETWEEN BS 790 TO 792, STRINGER 18L. REPAIRED SKIN IAW ER & EA. - [SDR SWAA2015030937220](https://openairdocs.org/sdr/SWAA2015030937220), Feb 20, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED BETWEEN BS 810 TO 812, STRINGER 19L. REPAIRED SKIN IAW SRM & EA. - [SDR SWAA2015030937219](https://openairdocs.org/sdr/SWAA2015030937219), Feb 20, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED BETWEEN BS 831 TO 832, STRINGER 17L. REPAIRED SKIN IAW SRM. - [SDR SWAA2015030537133](https://openairdocs.org/sdr/SWAA2015030537133), Feb 20, 2015: SKIN. CRACKED. SKIN CRACKED BETWEEN BS 820.5 TO 821.5, STRINGER 19L. REPAIRED SKIN IAW SRM. - [SDR SWAA2015030237002](https://openairdocs.org/sdr/SWAA2015030237002), Feb 20, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED BETWEEN BS 749.5 TO 751, STRINGER 19L. REPAIRED SKIN IAW SRM. - [SDR SWAA2015031937218](https://openairdocs.org/sdr/SWAA2015031937218), Feb 19, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT BS 804, STRINGER 23L. REPAIRED SKIN IAW SRM & EA. - [SDR SWAA2015031037293](https://openairdocs.org/sdr/SWAA2015031037293), Feb 18, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED BETWEEN BS 442 TO 446, STRINGER 1. REPAIRED SKIN IAW ER & EA. - [SDR SWAA2015031037292](https://openairdocs.org/sdr/SWAA2015031037292), Feb 18, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED BETWEEN BS 482B+14 TO 482B+15.5, STRINGER 16L. REPAIRED SKIN IAW ER & EA. - [SDR SWAA2015031037291](https://openairdocs.org/sdr/SWAA2015031037291), Feb 18, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED BETWEEN BS 384.5 TO 386.75, STRINGER 15R. REPAIRED SKIN IAW ER & EA. - [SDR SWAA2015031037290](https://openairdocs.org/sdr/SWAA2015031037290), Feb 18, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT BS 360, BETWEEN STRINGER 7R TO 8R. REPAIRED SKIN IAW ER & EA. - [SDR SWAA2015022736957](https://openairdocs.org/sdr/SWAA2015022736957), Feb 18, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED BETWEEN BS 393.5 TO 395.5, STRINGER 15R. REPAIRED SKIN IAW SRM. - [SDR SWAA2015022736956](https://openairdocs.org/sdr/SWAA2015022736956), Feb 18, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT BS 942, STRINGER 22L. REPAIRED SKIN IAW SRM. - [SDR SWAA2015021636635](https://openairdocs.org/sdr/SWAA2015021636635), Feb 13, 2015: SLIDE. OUT OF POSITION. R2 DOOR EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM. - [SDR SWAA2015012736113](https://openairdocs.org/sdr/SWAA2015012736113), Jan 26, 2015: SLIDE. LOOSE. R1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT. - [SDR SWAA2015012636084](https://openairdocs.org/sdr/SWAA2015012636084), Jan 14, 2015: SKIN. CRACKED. SKIN CRACKED AT BS 332, STRINGER 4L. REPAIRED SKIN IAW ER & SRM. - [SDR SWAA2015012235954](https://openairdocs.org/sdr/SWAA2015012235954), Jan 14, 2015: SKIN. CRACKED. SKIN CRACKED AT BS 787+5, STRINGER 17L. REPAIRED SKIN IAW EA & SRM. - [SDR SWAA2015011535802](https://openairdocs.org/sdr/SWAA2015011535802), Jan 13, 2015: STIFFENER. CRACKED. RIGHT WING AILERON STIFFENER CRACKED AT NR 2 HINGE. R & R STIFFENER IAW SRM. - [SDR SWAA2014102833385](https://openairdocs.org/sdr/SWAA2014102833385), Oct 26, 2014: SIGN. BROKEN. FORWARD ENTRY EMER EXIT SIGN BROKEN. R & R FWD ENTRY EMER EXIT LIGHT ASSEMBLY IAW MM. - [SDR SWAA2014090431597](https://openairdocs.org/sdr/SWAA2014090431597), Sep 2, 2014: SKIN. LOOSE. LEFT WING INBD FORE FLAP LOWER SURFACE LOOSE, 38 INCHES FROM INBD END. SECURED FORE FLAP IAW SRM. - [SDR SWAA2014082731307](https://openairdocs.org/sdr/SWAA2014082731307), Aug 24, 2014: WIRE. CHAFED. L1 DOOR EMER EVAC SLIDE LIGHT WIRE CHAFED AT BS 355L. REPAIRED WIRE IAW SWPM. - [SDR SWAA2014082731306](https://openairdocs.org/sdr/SWAA2014082731306), Aug 13, 2014: TIE. CRACKED. STRINGER TIE CRACKED AT BS 727 STRINGER 23R. REPAIRED TIE IAW SRM. - [SDR SWAA2014090431596](https://openairdocs.org/sdr/SWAA2014090431596), Aug 11, 2014: CREASE BEAM. CRACKED. RIGHT CREASE BEAM WEB CRACKED BETWEEN BS 847 TO 867 STRINGER 17R. REPAIRED WEB IAW ER & EA. - [SDR SWAA2014082731305](https://openairdocs.org/sdr/SWAA2014082731305), Aug 8, 2014: SKIN. CRACKED. FORWARD SIDE OF AFT CARGO DOOR CUT OUT CRACKED AT BS 793 STRINGER 21R. REPAIRED CUT OUT IAW SRM. - [SDR SWAA2014082731304](https://openairdocs.org/sdr/SWAA2014082731304), Aug 8, 2014: TIE CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT BS 727A STRINGER 7L. R & R TIE CLIP IAW SRM. - [SDR SWAA2014082731303](https://openairdocs.org/sdr/SWAA2014082731303), Aug 8, 2014: TIE CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT BS 727A STRINGER 9L. R & R TIE CLIP IAW SRM. - [SDR SWAA2014082731302](https://openairdocs.org/sdr/SWAA2014082731302), Aug 8, 2014: TIE CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT BS 380 STRINGER 6L. R & R TIE CLIP IAW SRM. - [SDR SWAA2014082731301](https://openairdocs.org/sdr/SWAA2014082731301), Aug 5, 2014: CHANNEL. CORRODED. STIFFENER CHANNEL CORRODED AT BS 227.8 LBL 3. R & R CHANNEL IAW SRM & DWG. - [SDR SWAA2014090231531](https://openairdocs.org/sdr/SWAA2014090231531), Jul 31, 2014: STRUCTURE. CORRODED. CHORD CORRODED AT BS 227 LBL 2. REPAIRED CHORD IAW EA & ER. - [SDR SWAA2014082631241](https://openairdocs.org/sdr/SWAA2014082631241), Jul 31, 2014: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 847 STRINGER 3L. R & R CLIP IAW SRM. - [SDR SWAA2014082631240](https://openairdocs.org/sdr/SWAA2014082631240), Jul 31, 2014: SEAT TRACK. DAMAGED. SEAT TRACK DAMAGED BETWEEN BS 555 TO 727 LBL 45.5. R & R SEAT TRACK IAW SRM. - [SDR SWAA2014082631239](https://openairdocs.org/sdr/SWAA2014082631239), Jul 31, 2014: SEAT TRACK. DAMAGED. SEAT TRACK DAMAGED BETWEEN BS 555 TO 727 LBL 25. R & R SEAT TRACK IAW SRM. - [SDR SWAA2014090231530](https://openairdocs.org/sdr/SWAA2014090231530), Jul 30, 2014: BULKHEAD. CORRODED. PRESSURE WEB CORRODED AT BS 1016 BETWEEN STRINGER 26L TO 26R. REPAIRED WEB IAW ER & EA. - [SDR SWAA2014082631238](https://openairdocs.org/sdr/SWAA2014082631238), Jul 30, 2014: FLOOR SUPPORT. CRACKED. LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 707 TO 710 LBL 0.07. REPAIRED WEB IAW EA. - [SDR SWAA2014082631237](https://openairdocs.org/sdr/SWAA2014082631237), Jul 30, 2014: CREASE BEAM. CORRODED. RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 827 TO 847 WL 208. R & R WEB IAW DWG & SRM. - [SDR SWAA2014082631236](https://openairdocs.org/sdr/SWAA2014082631236), Jul 30, 2014: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BETWEEN BS 344 TO 360 RBL 25. R & R SEAT TRACK IAW SRM. - [SDR SWAA2014082631235](https://openairdocs.org/sdr/SWAA2014082631235), Jul 30, 2014: ANGLE. CRACKED. AFT DOOR FRAME ANGLE CRACKED AT BS 342 STRINGER 15L. REPAIRED ANGLE IAW SRM. - [SDR SWAA2014082631234](https://openairdocs.org/sdr/SWAA2014082631234), Jul 30, 2014: CREASE BEAM. CORRODED. LEFT CREASE BEAM WEB CORRODED BETWEEN BS 847 TO 867 WL 208. R & R WEB IAW SRM. - [SDR SWAA2014082631233](https://openairdocs.org/sdr/SWAA2014082631233), Jul 30, 2014: CREASE BEAM. CORRODED. LEFT CREASE BEAM WEB CORRODED BETWEEN BS 807 TO 827 WL 208. REPAIRED BEAM IAW SRM & DWG. - [SDR SWAA2014082631232](https://openairdocs.org/sdr/SWAA2014082631232), Jul 30, 2014: CREASE BEAM. CORRODED. LEFT CREASE BEAM WEB CORRODED BETWEEN BS 482 TO 482A WL 208. R & R WEB IAW SRM. All 318: https://openairdocs.org/deregistered/N514SW-2016-07-13/reports.md ## FAA accident and incident reports (3) 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 20010702018369I](https://openairdocs.org/incident/20010702018369I), Jul 2, 2001: Boeing 737500 (N514SW), Omaha, NE. (-23) Swaa flight 1594 was enroute las vegas, NV, to Omaha, NE, at FL370 when the aircraft lost pressurization. The crew began an emergency descent and leveled… - [Incident 19990923027119I](https://openairdocs.org/incident/19990923027119I), Sep 23, 1999: Boeing 737500 (N514SW), Kansas City, MO. (-23) On 9/23/99, swaa, B-737-500, N514SW, departed st. louis international airport (stl) and declared an emergency for landing at mci, due to fire indication… - [Incident 19980319010899I](https://openairdocs.org/incident/19980319010899I), Mar 19, 1998: Boeing 737500 (N514SW), Birmingham, AL. Narrative: the aircraft was descending out of 14,000 feet about 40 west of Birmingham, Alabama. The aircraft hit light to moderate turbulence for 5 to 7… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.