# N320SW: 1987 Boeing 737-3H4, registration cancelled 2008-06-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 3, 2008 - Status when cancelled: Valid registration - Airframe: [Boeing 737-3H4](https://openairdocs.org/model/boeing-737-3h4) (registry code 138447K) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 23341 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 6, 1987 - Certificate issued: April 8, 2008 - Last registry action: April 8, 2008 - Mode S code: A36FF5 - Owner when cancelled: [Aar Parts Trading Inc](https://openairdocs.org/faa-owner/AAR%20PARTS%20TRADING%20INC) - Location: [Wood Dale, IL](https://openairdocs.org/faa-place/IL/Wood%20Dale) - Owner type: Corporation - Owner's area on the map: 41.9744° N, 87.9865° W: Placed by OpenAirDocs at the center of ZIP code 60191, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N320SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=320SW - Page: https://openairdocs.org/deregistered/N320SW-2008-06-03 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 737-3H4: https://openairdocs.org/model/boeing-737-3h4.md ## Service difficulty reports (211, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA080160](https://openairdocs.org/sdr/SWAA080160), Jan 7, 2008: SLIDE. OUT OF ADJUST. DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. - [SDR SWAA080161](https://openairdocs.org/sdr/SWAA080161), Jan 7, 2008: TAB. DELAMINATED. DURING SCHEDULED HC1 CHECK, FOUND LT ELEVATOR TAB DELAMINATED AT OUTBOARD T/E. REMOVED AND REPLACED TAB PER MM. - [SDR SWAA076513](https://openairdocs.org/sdr/SWAA076513), Dec 27, 2007: BATTERY. DISCHARGED. DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. - [SDR SWAA075409](https://openairdocs.org/sdr/SWAA075409), Oct 28, 2007: SKIN. CRACKED. DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 15L. REPAIRED SKIN PER SWA EA. - [SDR SWAA075408](https://openairdocs.org/sdr/SWAA075408), Oct 28, 2007: DOOR FRAME. CRACKED. DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR LOWER FRAME CRACKED AT AFT END. REMOVED AND REPLACED DOOR PER MM. - [SDR SWAA075407](https://openairdocs.org/sdr/SWAA075407), Oct 28, 2007: SKIN. CRACKED. DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 792, STR 18L. REPAIRED SKIN PER SWA EA. - [SDR SWAA075237](https://openairdocs.org/sdr/SWAA075237), Oct 23, 2007: SKIN. CRACKED. DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506C, STR 14R. REPAIRED SKIN PER SWA EA. - [SDR SWAA075112](https://openairdocs.org/sdr/SWAA075112), Oct 15, 2007: ACTUATOR. FAULTY. DIVERSION / DECLARED EMERGENCY. AFTER CROSS FEEDING FUEL, TURNED OFF CROSS FEED VALVE, NOTICED LIGHT STAYED ILLUMINATED. NOTICED START OF FUEL IMBALANCE. REMOVE - [SDR SWAA074646](https://openairdocs.org/sdr/SWAA074646), Sep 18, 2007: BATTERY PACK. DISCHARGED. DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. - [SDR SWAA070929](https://openairdocs.org/sdr/SWAA070929), Feb 17, 2007: SKIN. CRACKED. DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, STR 15R. REPAIRED SKIN PER SWA EA. - [SDR SWAA064689](https://openairdocs.org/sdr/SWAA064689), Dec 3, 2006: SKIN. CRACKED. DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 495, STR 16L. REPAIRED SKIN PER SRM. - [SDR SWAA064007](https://openairdocs.org/sdr/SWAA064007), Oct 17, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 13R. REPAIRED FRAME SECTION PER SWA EA. - [SDR SWAA064006](https://openairdocs.org/sdr/SWAA064006), Oct 17, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 13L. REPAIRED FRAME SECTION PER SWA EA. - [SDR SWAA063974](https://openairdocs.org/sdr/SWAA063974), Oct 13, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 14L. REPAIRED FRAME SECTION PER SWA EA. - [SDR SWAA063973](https://openairdocs.org/sdr/SWAA063973), Oct 13, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 14R. REPAIRED FRAME SECTION PER SWA EA. - [SDR SWAA063972](https://openairdocs.org/sdr/SWAA063972), Oct 13, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 14R AND STR 14L. REPAIRED FRAME SECTION PER SWA EA. - [SDR SWAA063971](https://openairdocs.org/sdr/SWAA063971), Oct 13, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 14R. REPAIRED FRAME SECTION PER SWA EA. - [SDR SWAA063970](https://openairdocs.org/sdr/SWAA063970), Oct 13, 2006: TORQUE TUBE. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM. - [SDR SWAA063936](https://openairdocs.org/sdr/SWAA063936), Oct 12, 2006: SHEAR TIE. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 559, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM. - [SDR SWAA063935](https://openairdocs.org/sdr/SWAA063935), Oct 12, 2006: RIB. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB LOWER RIB CRACKED AT STA 138.70. REMOVED AND REPLACED RIB PER SRM AND BOEING DRAWING. - [SDR SWAA063934](https://openairdocs.org/sdr/SWAA063934), Oct 12, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED FRAME SECTION PER ER. - [SDR SWAA063933](https://openairdocs.org/sdr/SWAA063933), Oct 12, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 13L. REMOVED AND REPLACED FRAME SECTION PER ER. - [SDR SWAA063932](https://openairdocs.org/sdr/SWAA063932), Oct 12, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2L. REMOVED AND REPLACED FRAME SECTION PER ER. - [SDR SWAA063931](https://openairdocs.org/sdr/SWAA063931), Oct 12, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REMOVED AND REPLACED FRAME SECTION PER SWA EA. - [SDR SWAA063930](https://openairdocs.org/sdr/SWAA063930), Oct 12, 2006: SKIN. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD CARGO DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER ER. - [SDR SWAA063916](https://openairdocs.org/sdr/SWAA063916), Oct 11, 2006: SKIN. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB LOWER AFT INBOARD SKIN CRACKED. REPAIRED SKIN PER ER. - [SDR SWAA063915](https://openairdocs.org/sdr/SWAA063915), Oct 11, 2006: FITTING. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. - [SDR SWAA063914](https://openairdocs.org/sdr/SWAA063914), Oct 11, 2006: FLOORBEAM. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 270, LBL 11 TO RBL 11. REPAIRED FLOORBEAM CHORD PER SRM. - [SDR SWAA063913](https://openairdocs.org/sdr/SWAA063913), Oct 11, 2006: FLOORBEAM. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 259, LBL 8 TO RBL 8. REPAIRED FLOORBEAM CHORD PER ER. - [SDR SWAA063900](https://openairdocs.org/sdr/SWAA063900), Oct 10, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 908, STR 13R. REPAIRED FRAME SECTION PER SWA EA. - [SDR SWAA063899](https://openairdocs.org/sdr/SWAA063899), Oct 10, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 578, STR 13R. REPAIRED FRAME SECTION PER SWA EA. - [SDR SWAA063898](https://openairdocs.org/sdr/SWAA063898), Oct 10, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 420, STR 13R. REPAIRED FRAME SECTION PER SWA EA. - [SDR SWAA063897](https://openairdocs.org/sdr/SWAA063897), Oct 10, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 13R. REPAIRED FRAME SECTION PER SWA EA. - [SDR SWAA063896](https://openairdocs.org/sdr/SWAA063896), Oct 10, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13L. REPAIRED FRAME SECTION PER SWA EA. - [SDR SWAA063895](https://openairdocs.org/sdr/SWAA063895), Oct 10, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 13L. REPAIRED FRAME SECTION PER SWA EA. - [SDR SWAA063894](https://openairdocs.org/sdr/SWAA063894), Oct 10, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 13L. REPAIRED FRAME SECTION PER SWA EA. - [SDR SWAA063893](https://openairdocs.org/sdr/SWAA063893), Oct 10, 2006: FITTING. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED STAB FITTING PER SRM. - [SDR SWAA063892](https://openairdocs.org/sdr/SWAA063892), Oct 10, 2006: SHEAR TIE. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, STR 3L. REMOVED AND REPLACED SHEAR TIE PER SRM. - [SDR SWAA063891](https://openairdocs.org/sdr/SWAA063891), Oct 10, 2006: FLOORBEAM. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, LBL 12 TO RBL 40. REPAIRED FLOORBEAM PER ER. - [SDR SWAA063890](https://openairdocs.org/sdr/SWAA063890), Oct 10, 2006: STRINGER CLIP. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA063889](https://openairdocs.org/sdr/SWAA063889), Oct 10, 2006: BEARING. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND RT ELEVATOR TAB FWD CONTROL ROD ENDS CORRODED. REMOVED AND REPLACED ROD END BEARINGS PER MM. - [SDR SWAA063888](https://openairdocs.org/sdr/SWAA063888), Oct 10, 2006: BEARING. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND LT ELEVATOR TAB FWD CONTROL ROD ENDS CORRODED. REMOVED AND REPLACED ROD END BEARINGS PER MM. - [SDR SWAA063887](https://openairdocs.org/sdr/SWAA063887), Oct 10, 2006: DOOR FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 4 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM. - [SDR SWAA063883](https://openairdocs.org/sdr/SWAA063883), Oct 9, 2006: PRESSURE PANEL. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND NLG W/W UPPER LT CEILING PANEL CUTOUT CRACKED AT AFT RT CORNER. REPAIRED CEILING PANEL PER ACO. - [SDR SWAA063882](https://openairdocs.org/sdr/SWAA063882), Oct 9, 2006: FLOORBEAM. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 744A, RBL 45. REPAIRED FLOORBEAM PER ER. - [SDR SWAA063881](https://openairdocs.org/sdr/SWAA063881), Oct 9, 2006: FLOORBEAM. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 744A, RBL 25. REPAIRED FLOORBEAM PER ER. - [SDR SWAA063880](https://openairdocs.org/sdr/SWAA063880), Oct 9, 2006: STRAP. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD UPPER AFT STRAP CORRODED AT BS 1016, LBL 16. REMOVED AND REPLACED AFT STRAP PER SRM. - [SDR SWAA063879](https://openairdocs.org/sdr/SWAA063879), Oct 9, 2006: SHEAR TIE. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, STR 3R. REMOVED AND REPLACED SHEAR TIE PER SRM. - [SDR SWAA063878](https://openairdocs.org/sdr/SWAA063878), Oct 9, 2006: STRINGER SPLICE. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. - [SDR SWAA063877](https://openairdocs.org/sdr/SWAA063877), Oct 9, 2006: CREASE BEAM. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BS 747 TO BS 767, WL 208. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. All 211: https://openairdocs.org/deregistered/N320SW-2008-06-03/reports.md ## FAA accident and incident reports (4) 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 20071015022079I](https://openairdocs.org/incident/20071015022079I), Oct 15, 2007: Boeing 7373H4 (N320SW), Omaha, NE, No damage. (-23) N320SW, operated as swaa flight 1436 from sea to mci, diverted to oma after a fuel imbalance problem. The crew noted after they turned the crossfeed… - [Incident 20050318004739I](https://openairdocs.org/incident/20050318004739I), Mar 18, 2005: Boeing 7373H4 (N320SW), Ontario, CA. (-23) On takeoff roll at ont (runway 26R) pilot aborted takeoff at approximately 80KTS. Reverse thrust and light braking used to stop aircraft. Aircraft taxied… - [Incident 20000303003399I](https://openairdocs.org/incident/20000303003399I), Mar 3, 2000: Boeing 7373H4 (N320SW), Seattle, WA, Minor damage. #2 Engine failed after takeoff. Maintenance found #2 turbine failed, also found rt. Horizontal stabilizer leading edge had puncture. Maintenance r&r engine and… - [Incident 19881207066319I](https://openairdocs.org/incident/19881207066319I), Dec 7, 1988: Boeing 7373H4 (N320SW), St Louis, MO. Nose gear would not retract after takeoff. Returned. Found a ruptured hydraulic line to the down lock actuator. ## Other aircraft with N320SW - [Registered now](https://openairdocs.org/aircraft/N320SW): Cessna 414A, S/N 414A0451, built 1980 --- 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.