# N94SW: 1983 Boeing 737-2H4, registration cancelled 2013-05-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 22, 2013 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Boeing 737-2H4](https://openairdocs.org/model/boeing-737-2h4) (registry code 138448C) - Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 23053 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 25, 1983 - Certificate issued: June 15, 2006 - Last registry action: October 1, 2009 - Mode S code: AD0C74 - Owner when cancelled: [Jet Midwest Inc](https://openairdocs.org/faa-owner/JET%20MIDWEST%20INC) - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Corporation - 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/N94SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=94SW - Page: https://openairdocs.org/deregistered/N94SW-2013-05-22 From the FAA registry file of November 5, 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 (43) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA000477](https://openairdocs.org/sdr/SWAA000477), Mar 13, 2000: SKIN. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND 3 CRACKS ON FUSELAGE EXTERNAL SKIN, BS 475, BS 505 AND BS 538, ABOVE STRINGER 10R. REPAIRED SKIN PER SRM. - [SDR SWAA000030](https://openairdocs.org/sdr/SWAA000030), Jan 5, 2000: STOP. OUT OF RIG. DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT DOOR RELEASE HANDLE DIFFICULT TO OPERATE. ADJUSTED STOP PINS PER MM. - [SDR SWAA000029](https://openairdocs.org/sdr/SWAA000029), Jan 5, 2000: COVER. BROKEN. DURING SCHEDULED C3 CHECK, FOUND EEPLS FWD END COVER BROKEN. REMOVED AND REPLACED FWD END COVER PER MM. - [SDR SWAA992127](https://openairdocs.org/sdr/SWAA992127), Dec 23, 1999: INDICATOR. MOVED. AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. - [SDR SWAA990602](https://openairdocs.org/sdr/SWAA990602), Mar 29, 1999: BATTERY PACK. DISCHARGED. DURING SCHEDULED OVERNIGHT CHECK, FOUND OVERHEAD EXIT LIGHTS FLICKERING AT REAR OF CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. - [SDR SWAA971050](https://openairdocs.org/sdr/SWAA971050), Dec 18, 1997: HOSE. RUPTURED. AFTER GEAR RETRACTION, NR 2 ENGINE LOW PRESS LIGHT ILLUMINATED FOR APPROX 5 SECONDS WITH LOW A SYSTEM HYD QUANTITY. APPROX 10 MINUTES LATER, A SYSTEM QUANTITY F - [SDR SWAA970973](https://openairdocs.org/sdr/SWAA970973), Nov 5, 1997: SKIN. CRACKED. DURING WALKAROUND CHECK, FOUND A FUSELAGE SKIN CRACKED 3 ABOVE #10 WINDOW RIGHT SIDE \N\NREPAIRED PER BOEING SRM - [SDR SWAA970974](https://openairdocs.org/sdr/SWAA970974), Oct 27, 1997: EPR LINE. CHAFED. RETURNED TO BWI DUE TO #1 ENGINE LOW EPR INDICATION \N\NINSPECTED AND FOUND EPR LINE CHAFING IN A CLAMP IN KRUGER FLAP AREA. R&R LINE PER BOEING M/M - [SDR SWAA970814](https://openairdocs.org/sdr/SWAA970814), Sep 2, 1997: BATTERY. DISCHARGED. DURING SCHEDULED TERMINAL CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. - [SDR SWAA970505](https://openairdocs.org/sdr/SWAA970505), May 23, 1997: SKIN. CRACKED. DURING SCHEDULED TERMINAL CHECK, FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT BS 460. REPAIRED PER BOEING SRM. - [SDR SWAA970342](https://openairdocs.org/sdr/SWAA970342), Mar 27, 1997: SKIN. DAMAGED. DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR FUSELAGE TORQUE TUBE CAVITY OUTER SKIN GOUGED AND DENTED ON INBOARD SIDE. REPAIRED PER BOEING SRM. - [SDR SWAA970341](https://openairdocs.org/sdr/SWAA970341), Mar 27, 1997: WEB. CORRODED. DURING SCHEDULED D CHECK, FOUND CORROSION AT EXISTING WEB REPAIR AT BS 496, RBL 25, WL 156. REPAIRED PER BOEING SRM. - [SDR SWAA970340](https://openairdocs.org/sdr/SWAA970340), Mar 27, 1997: STRINGER. CORRODED. DURING SCHEDULED D CHECK, FOUND STRINGER END CORRODED AT BS 322.5, S28R. REPAIRED PER BOEING SRM. - [SDR SWAA970339](https://openairdocs.org/sdr/SWAA970339), Mar 27, 1997: TEARSTRAP. CORRODED. DURING SCHEDULED D CHECK, FOUND TEARSTRAP CORRODED AT BS 787-847, RBL 20, WL 156. REPAIRED PER BOEING SRM. - [SDR SWAA970338](https://openairdocs.org/sdr/SWAA970338), Mar 27, 1997: BULKHEAD. CRACKED. DURING SCHEDULED D CHECK, FOUND BULKHEAD BS 178 CRACKED AT WL 234, LBL 10 AND AT RBL 10. REPAIRED PER BOEING SRM. - [SDR SWAA970337](https://openairdocs.org/sdr/SWAA970337), Mar 27, 1997: TEE CHORD. CRACKED. DURING SCHEDULED D CHECK, FOUND T CHORD CRACKED AT BS 178, LBL 4, WL 185. REPLACED DAMAGED SECTION PER BOEING SRM. - [SDR SWAA970336](https://openairdocs.org/sdr/SWAA970336), Mar 27, 1997: FLOORBEAM. CORRODED. DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 59 TO RBL 11, WL 208 AROUND NUTCLIP HOLES, AND AT BS 328, RBL 23-60, WL 208. REPAIRED PER BOEI - [SDR SWAA970335](https://openairdocs.org/sdr/SWAA970335), Mar 27, 1997: FLOORBEAM. CORRODED. DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 312, LBL 11-RBL 11, WL 208. REPAIRED PER BOEING SRM. - [SDR SWAA970334](https://openairdocs.org/sdr/SWAA970334), Mar 27, 1997: SUPPORT. CORRODED. DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 277-294.5, LBL 11, WL 208. REPAIRED PER BOEING SRM. - [SDR SWAA970333](https://openairdocs.org/sdr/SWAA970333), Mar 27, 1997: FRAME. CORRODED. DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, RBL 25, WL 156. REPAIRED PER BOEING SRM. - [SDR SWAA970332](https://openairdocs.org/sdr/SWAA970332), Mar 27, 1997: SKIN. DAMAGED. DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AND CREASED AT BS 993, WL 231. REPAIRED PER BOEING SRM. - [SDR SWAA970331](https://openairdocs.org/sdr/SWAA970331), Mar 27, 1997: DOUBLER. CRACKED. DURING SCHEDULED D CHECK, FOUND FWD GALLEY DOOR LOWER AFT FRAME INNER DOUBLER CRACKED. REPAIRED PER BOEING SRM. - [SDR SWAA970330](https://openairdocs.org/sdr/SWAA970330), Mar 27, 1997: SKIN. DAMAGED. DURING SCHEDULED D CHECK, FOUND FWD GALLEY DOOR OUTER SKIN LOWER HINGE CUTOUT, DAMAGED. REPAIRED PER BOEING SRM. - [SDR SWAA970329](https://openairdocs.org/sdr/SWAA970329), Mar 27, 1997: ANGLE. CORRODED. DURING SCHEDULED D CHECK, FOUND L ANGLE CORRODED UNDER MOPSILL AT BS 344 TO 360 , LBL 61, WL 207.5. REPLACED PER BOEING SRM. - [SDR SWAA970328](https://openairdocs.org/sdr/SWAA970328), Mar 27, 1997: FRAME. CRACKED. DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 695, LBL 65, WL 203.5. REPAIRED PER BOEING SRM. - [SDR SWAA970307](https://openairdocs.org/sdr/SWAA970307), Mar 20, 1997: STRINGER. CRACKED. DURING SCHEDULED D-CHECK, FOUND STRINGER 16R CRACKED AT BS 500B. REPLACED DAMAGED SECTION PER BOEING SRM. - [SDR SWAA970306](https://openairdocs.org/sdr/SWAA970306), Mar 20, 1997: ANGLE. CORRODED. DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR Z-ANGLE CORRODED AT BS 270, LBL 11-RBL 11, WL 208. REPAIRED PER BOEING SRM. - [SDR SWAA970305](https://openairdocs.org/sdr/SWAA970305), Mar 20, 1997: BULKHEAD SUPPORT. CORRODED. DURING SCHEDULED D-CHECK, FOUND SIDEWALL TO BULKHEAD SUPPORT CORRODED AT BS 520, LBL 25, WL 157. REPLACED PER BOEING SRM. - [SDR SWAA970304](https://openairdocs.org/sdr/SWAA970304), Mar 20, 1997: STRAP. CORRODED. DURING SCHEDULED D-CHECK, FOUND TEAR STRAP CORRODED AT BS 440 TO 500, WL 156, RBL 22 AROUND FASTENER HOLES. REPLACED PER BOEING SRM. - [SDR SWAA970303](https://openairdocs.org/sdr/SWAA970303), Mar 20, 1997: WEB. CRACKED. DURING SCHEDULED D-CHECK, FOUND SHEAR WEB CRACKED AT BS 986.5, RBL 42, WL 208. REPAIRED PER BOEING SRM. - [SDR SWAA970302](https://openairdocs.org/sdr/SWAA970302), Mar 20, 1997: ANGLE. CORRODED. DURING SCHEDULED D-CHECK, FOUND WEB ATTACH ANGLE COMMON TO SKIN CRACKED AT WL 240 RIGHT, BS 303. REPLACED PER BOEING SRM. - [SDR SWAA970301](https://openairdocs.org/sdr/SWAA970301), Mar 20, 1997: MOPSILL. CORRODED. DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR MOPSILL CORRODED. REPLACED PER BOEING SRM. - [SDR SWAA970300](https://openairdocs.org/sdr/SWAA970300), Mar 20, 1997: THRESHOLD. CORRODED. DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR THRESHOLD U-CHANNEL SUPPORT CORRODED. REPLACED CHANNEL PER BOEING SRM. - [SDR SWAA970299](https://openairdocs.org/sdr/SWAA970299), Mar 20, 1997: ANGLE. CRACKED. DURING SCHEDULED D-CHECK, FOUND WEB ATTACH ANGLE CRACKED AT BS 289, WL 255, RIGHT SIDE. REPLACED ANGLE PER BOEING SRM. - [SDR SWAA961320](https://openairdocs.org/sdr/SWAA961320), Nov 26, 1996: SKIN. CRACKED. DURING SCHEDULED C2 CHECK, FOUND AFT RADIUS OF AFT CARGO DOOR HANDLE CUTOUT CRACKED. REPAIRED PER BOEING SRM. - [SDR SWAA960482](https://openairdocs.org/sdr/SWAA960482), May 31, 1996: WEB. CRACKED. DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR OUTER WEB CRACKED 1.5 INCH ON LOWER FWD SIDE. REPAIRED PER BOEING SRM. - [SDR SWAA960294](https://openairdocs.org/sdr/SWAA960294), Feb 25, 1996: BATTERY PACK. DISCHARGED. DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. - [SDR SWAA960002](https://openairdocs.org/sdr/SWAA960002), Jan 3, 1996: ACTUATOR. LEAKING. NOTED A-SYSTEM FLUID LOSS EN ROUTE. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED TAIL AREA AND PERFORMED LEAK CHECK. REPLACED ELEVATOR FEE - [SDR SWAA950406](https://openairdocs.org/sdr/SWAA950406), May 22, 1995: ANGLE. CRACKED. DURING SCHEDULED B2 CHECK, FOUND AFT CARGO DOOR WEB ANGLE CRACKED AT 4TH RIVET AT LOWER FWD STOP. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. - [SDR SWAA950230](https://openairdocs.org/sdr/SWAA950230), Mar 9, 1995: WEB. CRACKED. DURING SCHEDULED QUARTER D CHECK, FOUND WEB CRACKED 1 INCH AT I/B RADIUS ABOVE RAM AIR DUCT AT FWD END ATTACH POINT, LEFT AC BAY. REPAIRED PER BOEING STRUCTURAL - [SDR SWAA950229](https://openairdocs.org/sdr/SWAA950229), Mar 9, 1995: BELTFRAME. CRACKED. DURING SCHEDULED QUARTER D CHECK, FOUND BELTFRAME CRACKED AT BS 360, STRINGER 26L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. - [SDR SWAA950200](https://openairdocs.org/sdr/SWAA950200), Mar 3, 1995: BELTFRAME. CRACKED. DURING SCHEDULED 1/4 D-CHECK, FOUND BELTFRAME CRACKED AT BS 360, S26L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. - [SDR SWAA950183](https://openairdocs.org/sdr/SWAA950183), Feb 14, 1995: ACCESS PANEL. CRACKED. DURING SCHEDULED CHECK, FOUND NOSE WHEEL WELL CEILING LEFT PRESSURE ACCESS PANEL CRACKED AT AFT I/B RADIUS. REPAIRED PER SWA RA 1-253-1249. --- 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.