# N24SW: Boeing 737-2H4, registration cancelled 1997-10-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 7, 1997 - Exported to: Aruba - Status when cancelled: Valid registration - Airframe: [Boeing 737-2H4](https://openairdocs.org/model/boeing-737-2h4) (registry code 138448C) - Serial number: 20925 - Type of aircraft: Fixed wing multi engine - Certificate issued: June 6, 1997 - Last registry action: June 6, 1997 - Mode S code: A22F4B - Owner when cancelled: [First Security Bank Na Owner Trustee](https://openairdocs.org/faa-owner/FIRST%20SECURITY%20BANK%20NA%20OWNER%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N24SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=24SW - Page: https://openairdocs.org/deregistered/N24SW-1997-10-07 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 737-2H4: https://openairdocs.org/model/boeing-737-2h4.md ## Service difficulty reports (18) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA961072](https://openairdocs.org/sdr/SWAA961072), Oct 8, 1996: CHORD. CRACKED. DURING SCHEDULED TERMINAL CHECK, FOUND BS 727 OUTBOARD CHORD CRACKED AT S18A, LEFT SIDE. FORWARD HOLE. REPAIRED PER BOEING SRM. - [SDR SWAA961025](https://openairdocs.org/sdr/SWAA961025), Sep 27, 1996: GUIDE PLATE. CRACKED. DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR FRAME UPPER HINGE GUIDE PLATE CRACKED BETWEEN FASTENERS TO EDGE. REPLACED WEB PER BOEING SRM. - [SDR SWAA960980](https://openairdocs.org/sdr/SWAA960980), Sep 17, 1996: FLOORBEAM. CRACKED. DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM T-CAP AT BS 312 CRACKED ABOVE FWD UPPER AIRSTAIR DOOR STOP AT LWR RADIUS. REPAIRED PER BOEING SRM. - [SDR SWAA960979](https://openairdocs.org/sdr/SWAA960979), Sep 17, 1996: SKIN. CRACKED. DURING SCHEDULED C1 CHECK, FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT FWD ENTRY DOOR CUTOUT UPPER FWD CORNER. REPAIRED PER SWA ACO 6317-53. - [SDR SWAA960978](https://openairdocs.org/sdr/SWAA960978), Sep 17, 1996: CEILING. CRACKED. DURING SCHEDULED C1 CHECK, FOUND A 4.5 CRACK IN NOSE WHEEL WELL CEILING RIGHT SIDE JUST AFT OF MANUAL GEAR EXTENSION RETURN SPRING BRACKET. REPAIRED PER BOEING - [SDR SWAA960965](https://openairdocs.org/sdr/SWAA960965), Sep 15, 1996: PWR SUPPLY. INOPERATIVE. DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN CEILING LIGHT INOP. REPLACED POWER SUPPLY PER BOEING M/M. - [SDR SWAA960865](https://openairdocs.org/sdr/SWAA960865), Aug 24, 1996: STRINGER. CRACKED. DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 9R CRACKED AT BS 727B. REPAIRED PER BOEING SRM. - [SDR SWAA960864](https://openairdocs.org/sdr/SWAA960864), Aug 24, 1996: CLIPS. CRACKED. DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER TIE CLIPS CRACKED AT 10R, BS 727, AND AT 9R, BS 727B. REPLACED PER BOEING SRM. - [SDR SWAA960863](https://openairdocs.org/sdr/SWAA960863), Aug 24, 1996: CLIPS. CRACKED. DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER TIE CLIPS 3L CRACKED AT BS 559, S3R, S4R AND S5R CRACKED AT BS 559, AND S5L AT BS 578. REPLACED ALL PER BOE - [SDR SWAA960862](https://openairdocs.org/sdr/SWAA960862), Aug 24, 1996: CLIP. CRACKED. DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER TIE CLIP 10R CRACKED AT BS 597. REPLACED PER BOEING SRM. - [SDR SWAA960861](https://openairdocs.org/sdr/SWAA960861), Aug 24, 1996: STRINGER. CRACKED. DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 10R CRACKED AT BS 727B. REPAIRED PER BOEING SRM. - [SDR SWAA950677](https://openairdocs.org/sdr/SWAA950677), Oct 22, 1995: OIL TEMP IND. MALFUNCTIONED. EXPERIENCED NR 1 ENGINE OIL HIGH OIL TEMP. CREW PERFORMED ENGINE SHUT-DOWN CHECK LIST. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. INSPECTED ENGINE - [SDR SWAA950391](https://openairdocs.org/sdr/SWAA950391), May 16, 1995: BULKHEAD. CRACKED. FOUND PRESSURE BULKHEAD CRACKED AT BS 727, AFT WALL OF WHEEL WELL. REPAIRED PER SWA RA 253-1194. - [SDR SWAA95293](https://openairdocs.org/sdr/SWAA95293), Apr 8, 1995: SKIN. CRACKED. DURING SCHEDULED B-CHECK, FOUND FUSELAGE SKIN CRACKED .75 INCH AT BS 767 AND STRINGER 19R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. - [SDR SWAA950190](https://openairdocs.org/sdr/SWAA950190), Feb 28, 1995: BLKHD ANGLE. CRACKED. DURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION AT BS 178 PRESSURE BULKHEAD VERTICAL T-ANGLE AT LBL 5.7 AT WL 184, IN THE I/B AND O/B FLANGE RADIUS. REPAIRED - [SDR SWAA950189](https://openairdocs.org/sdr/SWAA950189), Feb 28, 1995: SKIN. CRACKED. DURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION NEAR SEVERAL FASTENERS IN PRESSURE WEB AT I/B SIDE OF STRAP, BS 178, LBL 5.7, FROM WL 205 TO 186. REPAIRED PER - [SDR SWAA950188](https://openairdocs.org/sdr/SWAA950188), Feb 28, 1995: SKIN. CRACK. DURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION AT FUSELAGE SKIN LAP, BS 480, S10L, AT BS 500B+10, S14L AND AT BS 530, S10R. REPAIRED PER SWA RA 1-253-1251 AN - [SDR SWAA950182](https://openairdocs.org/sdr/SWAA950182), Feb 15, 1995: CONTROL VALVE. FAILED. AFTER LEVELING AT 28,000, CABIN PRESSURE WARNING HORN SOUNDED. CABIN ALTITUDE CONTINUED TO CLIMB. USING STANDBY OR MANUAL SYSTEM, NO HELP. CREW INITIATED DESCEN ## 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 19800303028239I](https://openairdocs.org/incident/19800303028239I), Mar 3, 1980: Boeing 7372H4 (N24SW), Dallas, TX. During descent in turbulance, the yaw damper malfunctioned, was disconnected, and descent with auto pilot continued - [Incident 19800210028789I](https://openairdocs.org/incident/19800210028789I), Feb 10, 1980: Boeing 7372H4 (N24SW), New Orleans, LA. On climbout, engine oil filter bypass light came on. Emergency declared and flight returned to msy. - [Incident 19780201005159I](https://openairdocs.org/incident/19780201005159I), Feb 1, 1978: Boeing 737/ (N24SW), Houston, TX. Pilot made an uneventful landing after failure of the main hydraulic system. Found a hydraulic line cracked. ## Other aircraft with N24SW - [Registered now](https://openairdocs.org/aircraft/N24SW): Piper PA-28R-200, S/N 28R-7535213, built 1975 --- 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.