# N86SW: 1982 Boeing 737-2H4, registration cancelled 2013-03-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 19, 2013 - Status when cancelled: Sale reported, canceled - Airframe: [Boeing 737-2H4](https://openairdocs.org/model/boeing-737-2h4) (registry code 138448C) - Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 22827 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: June 4, 1982 - Last registry action: August 24, 2004 - Mode S code: ABCE23 - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Individual - Owner's area on the map: 35.0795° N, 89.8454° W: Placed by OpenAirDocs at the center of ZIP code 38119, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N86SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=86SW - Page: https://openairdocs.org/deregistered/N86SW-2013-03-19 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 737-2H4: https://openairdocs.org/model/boeing-737-2h4.md ## Service difficulty reports (28) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA000385](https://openairdocs.org/sdr/SWAA000385), Mar 1, 2000: SKIN. CRACKED. DURING SCHEDULED SPECIAL VISIT, FOUND 1.25 INCH HOLE WITH CRACKS ON LEFT INBD MIDFLAP UPPER SURFACE AROUND TRACK CUTOUT. REMOVED AND REPLACED MIDFLAP ASSY PER M - [SDR SWAA000021](https://openairdocs.org/sdr/SWAA000021), Jan 3, 2000: SKIN. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 775, STRINGER 22L. REPAIRED SKIN PER SRM. - [SDR SWAA000020](https://openairdocs.org/sdr/SWAA000020), Jan 3, 2000: SKIN. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 298, STRINGER 18R. REPAIRED SKIN PER SRM. - [SDR SWAA990795](https://openairdocs.org/sdr/SWAA990795), May 3, 1999: CABLE. OUT OF POSITION. DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR SLIDE PACK CABLE ROUTED INCORRECTLY. REROUTED CABLE PER MM. - [SDR SWAA990695](https://openairdocs.org/sdr/SWAA990695), Apr 13, 1999: BATTERY PACK. DISCHARGED. DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS (INNER AND OUTER) INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER MM. - [SDR SWAA990490](https://openairdocs.org/sdr/SWAA990490), Mar 10, 1999: SLIDE. LOOSE. PLASTIC SHROUD AROUND ESCAPE SLIDE ON FWD SERVICE DOOR WAS LOOSE AT THE BOTTOM AND SLIDE FELL OUT. REPACKED SLIDE PER SWA WORK CARD. - [SDR SWAA980441](https://openairdocs.org/sdr/SWAA980441), Mar 29, 1998: VALVE. INOPERATIVE. DIVERTED TO HOU DUE TO ANTI-SKID INOP GEAR DOWN. COULD NOT GO TO AUS DUE TO WET RUNWAYS. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PARKING BRAKE VALVE, NO L - [SDR SWAA970555](https://openairdocs.org/sdr/SWAA970555), Jun 19, 1997: MODULE. INOPERATIVE. DURING SCHEDULED C1 CHECK, FOUND COCKPIT EMERGENCY LIGHTING INOP. REMOVED AND REPLACED M560 MODULE PER BOEING M/M. - [SDR SWAA970080](https://openairdocs.org/sdr/SWAA970080), Jan 17, 1997: DOOR FRAME. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR LOWER FWD DOORWAY STUB FRAME CRACKED 1.5 INCH VERTICALLY AND .5 INCH HORIZONTALLY PROTRUDING FROM LOWER L - [SDR SWAA970079](https://openairdocs.org/sdr/SWAA970079), Jan 17, 1997: FRAME. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND FRAME CRACKED .5 INCH AT BS 639 FLOOR LEVEL, RT BELTFRAME. REPLACED FRAME PER BOEING SRM. - [SDR SWAA960616](https://openairdocs.org/sdr/SWAA960616), Jul 6, 1996: BATTERY. DISCHARGED. DURING SCHEDULED A1 CHECK, FOUND ALL ENTRY SERVICE DOOR EMERGENCY EXIT LIGHT BATTERY PACKS WEAK. REPLACED BATTERY PACKS PER BOEING M/M. - [SDR SWAA960602](https://openairdocs.org/sdr/SWAA960602), Jun 27, 1996: SUPPORT. CORRODED. DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY FLOOR SUPPORT CORRODED AT BS 504, FROM S25L TO 26R. REPAIRED PER BOEING SRM. - [SDR SWAA960601](https://openairdocs.org/sdr/SWAA960601), Jun 27, 1996: WEB. CORRODED. DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR SEAL WEB CORRODED AT BS 492 AND 490, WL 166, RBL 32. REPLACED WEB PER BOEING SRM. - [SDR SWAA960600](https://openairdocs.org/sdr/SWAA960600), Jun 27, 1996: BULKHEAD. CRACKED. DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT WL 218, LBL 7 TO 10. REPAIRED PER BOEING SRM. - [SDR SWAA960599](https://openairdocs.org/sdr/SWAA960599), Jun 27, 1996: STRINGER. CORRODED. DURING SCHEDULED D-CHECK, FOUND STRINGER 25R AT BS 947 CORRODED. REPLACED CORRODED SECTION PER BOEING SRM. - [SDR SWAA960590](https://openairdocs.org/sdr/SWAA960590), Jun 24, 1996: CHORD. CORRODED. DURING SCHEDULED D CHECK, FOUND FLOORBEAM ANGLED CHORD CORRODED AROUND FASTENER HOLES BETWEEN BS 1006 AND 986.5, WL 208, LBL 10 TO 19. REPAIRED PER BOEING SRM. - [SDR SWAA960589](https://openairdocs.org/sdr/SWAA960589), Jun 24, 1996: FLOOR BEAM. CORRODED. DURING SCHEDULED D CHECK, FOUND FLOORBEAM CHORD CORRODED AROUND FASTENER HOLES BETWEEN BS 1006 AND 1016, WL 208, UNDER WEB. REPAIRED PER BOEING SRM. - [SDR SWAA960588](https://openairdocs.org/sdr/SWAA960588), Jun 24, 1996: SPLICE. CORRODED. DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907+5. REPAIRED PER BOEING SRM AND BOEING T1-A51-004. - [SDR SWAA960587](https://openairdocs.org/sdr/SWAA960587), Jun 24, 1996: FLOOR BEAM. CORRODED. DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 344, LBL 7 TO 10, AND AT RBL 2 TO 31. REPAIRED PER BOEING SRM. - [SDR SWAA960586](https://openairdocs.org/sdr/SWAA960586), Jun 24, 1996: BULKHEAD. CRACKED. DURING SCHEDULED D CHECK, FOUND BULKHEAD BS 178 CRACKED AT WL 218, RBL 7 TO 12, AND AT RBL 9.5 TO 12. REPAIRED PER BOEING SRM. - [SDR SWAA960585](https://openairdocs.org/sdr/SWAA960585), Jun 24, 1996: ANGLE. CRACKED. DURING SCHEDULED D CHECK, FOUND BULKHEAD SUPPORT ANGLE CRACKED AT BS 727+8, WL 156 BL ZERO-LBL 5. REPAIRED PER BOEING SRM. - [SDR SWAA960584](https://openairdocs.org/sdr/SWAA960584), Jun 24, 1996: CLIP. CRACKED. DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727B, S18R AND S20R. REPLACED PER BOEING SRM. - [SDR SWAA960583](https://openairdocs.org/sdr/SWAA960583), Jun 24, 1996: SKIN. DENTED. DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT THE FOLLOWING LOCATIONS: BS 823, AT S26L, BS 341 AT S25R, BS 504, BETWEEN 21R AND 22R, BS 203, 4 INCHES - [SDR SWAA960568](https://openairdocs.org/sdr/SWAA960568), Jun 18, 1996: SKIN. DENTED. DURING SCHEDULED HD CHECK, FOUND FUSELAGE SKIN DENTED AT BS 370, S25L, AT BS 980, S22L AND AT BS 936 AT S19L. REPAIRED ALL PER BOEING SRM. - [SDR SWAA950706](https://openairdocs.org/sdr/SWAA950706), Nov 12, 1995: INTERCOSTAL. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND INTERCOSTAL CRACKED AT FWD CARGO THRESHOLD AT BS 469. REPAIRED PER BOEING SRM. - [SDR SWAA950603](https://openairdocs.org/sdr/SWAA950603), Aug 25, 1995: SKIN. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND 3 SKIN CRACK ALONG S25L AT BS 720. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. - [SDR SWAA950171](https://openairdocs.org/sdr/SWAA950171), Feb 13, 1995: SKIN. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED JUST ABOVE POTABLE WATER SERVICE PANEL AT S25L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. - [SDR SWAA950062](https://openairdocs.org/sdr/SWAA950062), Jan 20, 1995: EEL. INOPERATIVE. DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY PER BOEING MM. ## 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 FTW86MA030](https://openairdocs.org/ntsb/FTW86MA030), Jan 3, 1986: Boeing 737-2H4 (N86SW), Dallas, TX, incident, minor damage ## FAA accident and incident reports (2) 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 19921228054859I](https://openairdocs.org/incident/19921228054859I), Dec 28, 1992: Boeing 7372H4 (N86SW), Kansas City, MO. Experienced loss of a system hydraulic quantity. Landed at destination. Found a chafed hydraulic pressure line. - [Incident 19860103068529I](https://openairdocs.org/incident/19860103068529I), Jan 3, 1986: Boeing 7372H4 (N86SW), Dallas, TX, Substantial damage. NR2 engine aft mount cone bolt broke on rotation. Aft portion of engine dropped down. Safe landing. --- 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.