# N85SW: 1982 Boeing 737-2H4, registration cancelled 2006-05-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 23, 2006 - Exported to: Venezuela - Status when cancelled: Valid registration - 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: 22826 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: June 3, 1982 - Certificate issued: November 5, 2004 - Last registry action: November 9, 2005 - Mode S code: ABA6A4 - Owner when cancelled: [Jet Midwest Inc](https://openairdocs.org/faa-owner/JET%20MIDWEST%20INC) - Location: [Kansas City, KS](https://openairdocs.org/faa-place/KS/Kansas%20City) - Owner type: Corporation - Owner's area on the map: 39.1483° N, 94.6051° W: Placed by OpenAirDocs at the center of ZIP code 66115, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N85SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=85SW - Page: https://openairdocs.org/deregistered/N85SW-2006-05-23 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 (46) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA000390](https://openairdocs.org/sdr/SWAA000390), Mar 2, 2000: INDICATOR. DISLODGED. DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. - [SDR SWAA000389](https://openairdocs.org/sdr/SWAA000389), Mar 2, 2000: CABLE. MISROUTED. DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE RELEASE CABLE IMPROPERLY ROUTED. REROUTED CABLE PER MM. - [SDR SWAA991996](https://openairdocs.org/sdr/SWAA991996), Dec 1, 1999: INDICATOR. DISLODGED. FWD SERVICE DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. - [SDR SWAA990820](https://openairdocs.org/sdr/SWAA990820), May 6, 1999: BATTERY PACK. DISCHARGED. DURING SCHEDULED SERVICE CHECK, FOUND 2 CENTER EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. - [SDR SWAA990178](https://openairdocs.org/sdr/SWAA990178), Jan 27, 1999: SLIDE. LOW PRESS. DURING SCHEDULED A1 CHECK, FOUND FWD ENTRY DOOR SLIDE PRESSURE LOW. REPLACED PER BOEING M/M. - [SDR SWAA981838](https://openairdocs.org/sdr/SWAA981838), Aug 24, 1998: FUEL CONTROL. FAILED. AT CRUISE, NR 2 ENGINE ROLLED BACK TO 1.56 EPR, 79 PERCENT N1, 83.5 PERCENT N2 2150 FF AND FROZE THERE. ENGINE DID NOT RESPOND TO THROTTLE MOVEMENT, ENGINE SHUT - [SDR SWAA980059](https://openairdocs.org/sdr/SWAA980059), Jan 14, 1998: BATTERY. DISCHARGED. DURING SCHEDULED A2 CHECK, FOUND MID CABIN OVERHEAD EMEGENCY EXIT LIGHT FLASHING DURING OP CHECK. REPLACED BATTERY PACK PER BOEING M/M. - [SDR SWAA971078](https://openairdocs.org/sdr/SWAA971078), Dec 12, 1997: PCU. LEAKING. AFTER TAKEOFF, EXPERIENCED B-SYSTEM HYDRAULIC FAILURE. RETURNED TO TPA AND MADE AN UNEVENTFUL LANDING. REPLACED ELEVATOR PCU PER BOEING M/M. - [SDR SWAA970847](https://openairdocs.org/sdr/SWAA970847), Sep 15, 1997: SLIDE. WORN. DURING SCHEDULED C3, FOUND AFT GALLEY DOOR SLIDE PACK MATERIAL WORN OFF AT AFT END OF GIRT BAR. REPLACED SLIDE PER BOEING M/M. - [SDR SWAA970836](https://openairdocs.org/sdr/SWAA970836), Sep 5, 1997: PLUG. CRACKED. AFTER TAKEOFF, EXPERIENCED A' SYSTEM HYD PRESSURE LOSS. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. REPLACED NR 3 SPOILER PLUG CRACKED. REPLACED AN - [SDR SWAA970817](https://openairdocs.org/sdr/SWAA970817), Sep 1, 1997: SKIN. CRACKED. DURING SCHEDULED RON CHECK, FOUND CRACKED AT PREVIOUS PATCH AT RT AFT FUSELAGE AREA. REPAIRED PER BOEING SRM. - [SDR SWAA970693](https://openairdocs.org/sdr/SWAA970693), Aug 10, 1997: THROTTLES. OUT OF ADJUST. RETURNED TO HOU DUE TO NR 2 ENGINE NOT MAKING 9 POWER. WITH A 1.5 KNOB THROTTLE SPLIT. AIRCRAFT LANDED WITHOUT INCIDENT. RIGGED THROTTLES AND TRIMMED ENGINE PER - [SDR SWAA970410](https://openairdocs.org/sdr/SWAA970410), Apr 22, 1997: ACTUATOR. INOP. AFTER TAKEOFF, RT O/B L/E SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO SMF AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED RT O/B L/E SLAT ACTUATOR AND OP - [SDR SWAA970143](https://openairdocs.org/sdr/SWAA970143), Jan 30, 1997: VALVE. FAILED. IN FLIGHT, YAW DAMPER KICKED VIOLENTLY LEFT ONE TIME. CREW TURNED OFF YAW DAMPER FOR REMAINDER OF FLIGHT. LANDED WITHOUT INCIDENT IN HOU. AFTER LANDING, YAW DAM - [SDR SWAA960483](https://openairdocs.org/sdr/SWAA960483), Jun 4, 1996: BATTERY. DISCHARGED. DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT FWD EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK PER BOEING M/M. - [SDR SWAA960452](https://openairdocs.org/sdr/SWAA960452), May 20, 1996: CHORD. CRACKED. DURING SCHEDULED D-CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178, WL 184, LBL 4.7. REPAIRED PER BOEING SRM. - [SDR SWAA960451](https://openairdocs.org/sdr/SWAA960451), May 20, 1996: STRINGER. DAMAGED. DURING SCHEDULED D-CHECK, FOUND STRINGER 27L DAMAGED AT BS 997. REPLACED DAMAGED SECTION PER BOEING SRM. - [SDR SWAA960450](https://openairdocs.org/sdr/SWAA960450), May 20, 1996: LIGHT. DAMAGED. DURING SCHEDULED D-CHECK, AFT LEFT ENTRY DOOR EXTERNAL EMERGENCY EXIT LIGHT ASSEMBLY DAMAGED. REPLACED AND PERFORMED EMERGENCY LIGHT TEST PER BOEING M/M. - [SDR SWAA960449](https://openairdocs.org/sdr/SWAA960449), May 20, 1996: SPLICE CAP. CORRODED. DURING SCHEDULED D-CHECK, FOUND CHORD SPLICE CAP CORRODED AT BS 1016, LBL 4, WL 188. REPAIRED PER BOEING SRM. - [SDR SWAA960448](https://openairdocs.org/sdr/SWAA960448), May 20, 1996: SKIN. DENTED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED JUST FWD OF FWD ENTRY, BS 308 BETWEEN S10 AND 13L. REPAIRED PER BOEING SRM AND EWO 96-0187. - [SDR SWAA960447](https://openairdocs.org/sdr/SWAA960447), May 20, 1996: GATE BEAM. CRACKED. DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR LOWER GATE BEAM CRACKED AT LOWER FORWARD CORNER. REPAIRED PER BOEING SRM. - [SDR SWAA960446](https://openairdocs.org/sdr/SWAA960446), May 20, 1996: FRAME. CRACKED. DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED AT NR 3 STOP FITTING CUTOUT. REPAIRED PER BOEING SRM. - [SDR SWAA960445](https://openairdocs.org/sdr/SWAA960445), May 20, 1996: FRAME. DAMAGED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME AT BS 400 DENTED AT LBL 28, WL 157, LBL 36, LBL 161, LBL 53, WL 173. REPAIRED PER BOEING SRM. - [SDR SWAA960444](https://openairdocs.org/sdr/SWAA960444), May 20, 1996: DOOR FRAME. CRACKED. DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR FRAME WEB CRACKED AT BS 847, RBL 26, WL 166. REPAIRED PER BOEING SRM. - [SDR SWAA960443](https://openairdocs.org/sdr/SWAA960443), May 20, 1996: SPLICE. CORRODED. DURING SCHEDULED D-CHECK, FOUND CORROSION ON O/B SIDE OF STRINGER PRODUCTION SPLICE AT BS 907, S25L. REPAIRED PER BOEING SRM. - [SDR SWAA960442](https://openairdocs.org/sdr/SWAA960442), May 20, 1996: STR CLIP. CRACKED. DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 867 AT S20R. REPLACED PER BOEING SRM. - [SDR SWAA960441](https://openairdocs.org/sdr/SWAA960441), May 20, 1996: SHEAR TIE. GOUGED. DURING SCHEDULED D-CHECK, FOUND SHEAR TIE GOUGED AT BS 947.5 BETWEEN STRINGER 22 AND 23R. REPAIRED PER BOEING SRM. - [SDR SWAA960440](https://openairdocs.org/sdr/SWAA960440), May 20, 1996: WEB. CRACKED. DURING SCHEDULED D-CHECK, FOUND WEB CRACK AT BS 727, LBL 15, WL 176. REPAIRED PER BOEING SRM. - [SDR SWAA960265](https://openairdocs.org/sdr/SWAA960265), Apr 25, 1996: CLIP. CRACKED. DURING SCHEDULED HD CHECK, FOUND STRINGER CLIPS CRACKED AT BS 520 S19L AND AT BS 400 S27L. REPLACED PER BOEING SRM. - [SDR SWAA960264](https://openairdocs.org/sdr/SWAA960264), Apr 25, 1996: FRAME. DENTED. DURING SCHEDULED HD CHECK, FOUND FUSELAGE FRAME DENTED AT BS 500A S24L. REPAIRED PER BOEING SRM. - [SDR SWAA960263](https://openairdocs.org/sdr/SWAA960263), Apr 25, 1996: ANGLE. CRACKED. DURING SCHEDULED HD CHECK, FOUND Z-ANGLE CRACKED BS 663, AFT SIDE LBL 6 WL 170 LEFT WHEEL WELL. REPAIRED PER BOEING SRM. - [SDR SWAA960262](https://openairdocs.org/sdr/SWAA960262), Apr 25, 1996: ANGLE. CRACKED. DURING SCHEDULED HD CHECK, FOUND CRACKED ANGLE ABOVE STRINGER 10L AT BS 302. REPAIRED PER BOEING SRM. - [SDR SWAA960261](https://openairdocs.org/sdr/SWAA960261), Apr 25, 1996: ANGLE. CRACKED. DURING SCHEDULED HD CHECK, FOUND CRACKED ANGLE AND STRAP AT FWD ENTRY DOOR STOP FITTINGS NR 9 AND 10 BS 348. REPAIRED PER BOEING SRM. - [SDR SWAA960260](https://openairdocs.org/sdr/SWAA960260), Apr 25, 1996: STRAP. CRACKED. DURING SCHEDULED HD CHECK, FOUND TENSION STRAP CRACKED AT BS 326 RBL 31 WL 200. REPAIRED PER BOEING SRM. - [SDR SWAA960259](https://openairdocs.org/sdr/SWAA960259), Apr 25, 1996: FLOOR BEAM. CRACKED. DURING SCHEDULED HD CHECK, FOUND FLOOR BEAM CRACKED AT BS 294 RBL 55 WL 208. REPLACED BEAM PER BOEING SRM. - [SDR SWAA960258](https://openairdocs.org/sdr/SWAA960258), Apr 25, 1996: FRAME. CRACKED. DURING SCHEDULED HD CHECK, FOUND CRACK LOWER FWD DOOR FRAME AT BS 296 RBL 57, WL 216. REPLACED FRAME PER BOEING SRM. - [SDR SWAA960257](https://openairdocs.org/sdr/SWAA960257), Apr 25, 1996: ANGLE. CRACKED. DURING SCHEDULED HD CHECK, FOUND ANGLE CRACKED AT BS 291 RBL 60 WL 248. REPLACED PER BOEING SRM. - [SDR SWAA960256](https://openairdocs.org/sdr/SWAA960256), Apr 25, 1996: FRAME. CRACKED. DURING SCHEDULED HD CHECK, FOUND CRACKED DOOR FRAME AT BS 296 RBL 57 WL 216. REPLACED PER BOEING SRM. - [SDR SWAA960255](https://openairdocs.org/sdr/SWAA960255), Apr 25, 1996: ANGLE. CRACKED. DURING SCHEDULED HD CHECK, FOUND ANGLE CRACK AT BS 291 RBL 60 WL 248 208. REPLACED PER BOEING SRM. - [SDR SWAA960254](https://openairdocs.org/sdr/SWAA960254), Apr 25, 1996: FLOOR BEAM. CORRODED. DURING SCHEDULED HD CHECK, FOUND UPPER FLOOR BEAM CORRODED AT BS 1016 RBL 10, 20 TO 34, WL 208. REPLACED PER BOEING SRM. - [SDR SWAA960253](https://openairdocs.org/sdr/SWAA960253), Apr 25, 1996: CHORD. CRACKED. DURING SCHEDULED HD CHECK, FOUND O/B CHORD CRACKED AT BS 1156 WL 240 RBL 18. REPAIRED PER BOEING SRM. - [SDR SWAA960252](https://openairdocs.org/sdr/SWAA960252), Apr 25, 1996: SILL. CORRODED. DURING SCHEDULED HD CHECK, FOUND AFT SERVICE DOORWAY MOPSILL CORRODED AT BS 955 TO 996 RBL 47TO 52 WL 208 TO 209. REPLACED PER BOEING SRM. - [SDR SWAA960251](https://openairdocs.org/sdr/SWAA960251), Apr 25, 1996: SILL. CORRODED. DURING SCHEDULED HD CHECK, FOUND FWD ENTRY DOORWAY MOPSILL CORRODED AT BS 316 TO 344 LBL 57 TO 59 WL 208. REPLACED PER BOEING SRM. - [SDR SWAA960250](https://openairdocs.org/sdr/SWAA960250), Apr 25, 1996: SUPPORT. CORRODED. DURING SCHEDULED HD CHECK, FOUND FLOOR BEAM SUPPORT CORRODED AT BS 284 TO 286 LBL 11 WL 208. REPLACED PER BOEING SRM. - [SDR SWAA950794](https://openairdocs.org/sdr/SWAA950794), Dec 22, 1995: WINDOW. CRACKED. EXPERIENCED BIRDSTRIKE TO FIRST OFFICER'S NR 1 WINDOW. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. PERFORMED BIRDSTRIKE INSPECTION. ALSO, FOUND NR - [SDR SWAA950556](https://openairdocs.org/sdr/SWAA950556), Jul 30, 1995: PROX SENSOR. INOP. AFTER GEAR RETRACTION, RIGHT MAIN GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND LIGHT EXTINGUISHED, THEN ILLUMINATED AGAIN. AIRCRAFT RETURNED TO M ## Other aircraft with N85SW - [Registered now](https://openairdocs.org/aircraft/N85SW): Sapkos Stan W RV-7A, S/N 73459, built 2009 --- 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.