# N585US: 1988 Boeing 737-301, registration cancelled 2006-09-12 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 12, 2006 - Exported to: Belgium - Status when cancelled: Valid registration - Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R) - Engine: [GE CFM56 series](https://openairdocs.org/engine/ge-cfm56-series) (registry code 30016) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23930 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 20, 1988 - Certificate issued: January 6, 2000 - Last registry action: December 7, 2005 - Mode S code: A78A4E - Owner when cancelled: [Wachovia Bank Na Trustee](https://openairdocs.org/faa-owner/WACHOVIA%20BANK%20NA%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N585US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=585US - Page: https://openairdocs.org/deregistered/N585US-2006-09-12 From the FAA registry file of October 31, 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 737-301: https://openairdocs.org/model/boeing-737-301.md ## Service difficulty reports (62, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA050281](https://openairdocs.org/sdr/USAA050281), Feb 11, 2005: DOOR FRAME. CRACKED. PIT - FOUND DOOR WITH THREE .5 INCH CRACKS, AFT CARGO DOOR FORWARD FRAME. REMOVED AND REPLACED DOOR PER JOB CARD J3-57-52301. (M) - [SDR USAA040413](https://openairdocs.org/sdr/USAA040413), Aug 7, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1.25 INCH, BS 727D S-23R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229 DETAIL XI. (M) - [SDR USAA040414](https://openairdocs.org/sdr/USAA040414), Aug 4, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1.5 INCH, BS 727E S23L. INSTALLED DOUBLERS PER SRM 53-00-01 FIG 229. (M) - [SDR USAA040232](https://openairdocs.org/sdr/USAA040232), May 3, 2004: FRAME. CRACKED. FRAME CRCKED, 1 INCH LONG CRACK, STA 616 JUST BELOW STRINGER 17L. FABRICATED FILLER IAW T/R 53-62-01, 53-60-01 AND J NR 58-53503-004. - [SDR USAA040200](https://openairdocs.org/sdr/USAA040200), May 3, 2004: STRINGER. CRACKED. STRINGER (.2500 INCH X .1250 INCH CRACKS) CRACKED STA 908 AND STR 4R. REPLACED STRINGER SPLICE IAW SRM 51-20-02. - [SDR USAA040182](https://openairdocs.org/sdr/USAA040182), May 3, 2004: FLOORBEAM. CORRODED. PIT - FOUND FLOORBEAM CORRODED, STATION 986.5. CORROSION LEVEL 1, TASK NR C53-107-01. REPLACED INTERCOSTAL STRUCTURE BETWEEN STATION 986.5 AND 100.6 PER SRM 52- - [SDR USAA040181](https://openairdocs.org/sdr/USAA040181), May 3, 2004: SUPPORT FITTING. CRACKED. PIT - FOUND MLG SUPPORT FITTING CRACKED .5 INCH, RT MLG SUPPORT FITTING REAR SPAR OF RIGHT WING. REPLACED RIGHT MLG SUPPORT FITTING PER EA 78221. (M) - [SDR USAA040179](https://openairdocs.org/sdr/USAA040179), May 3, 2004: WEB. CRACKED. PIT - FOUND FLOOR WEB CRACKED 1 INCH AND 1.5 INCHES, BETWEEN STATION 559 AND 578 AT STRINGER 17L. REPLACED FLOOR WEB PER SRM 51-10-2. (M) - [SDR USAA040180](https://openairdocs.org/sdr/USAA040180), May 3, 2004: SUPPORT FITTING. CRACKED. PIT - FOUND MLG SUPPORT FITTING CRACKED .25 INCH LONG, LEFT MLG SUPPORT FITTING REAR SPAR OF LEFT WING. REPLACED LEFT MLG SUPPORT FITTING PER EA 78221. (M) - [SDR USAA040160](https://openairdocs.org/sdr/USAA040160), Apr 9, 2004: STRINGER SPLICE. CRACKED. PIT - FOUND STRINGER SPLICE WITH TWO .125 INCH CRACKS, FS 907, S4R STRINGER SPLICE. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M) - [SDR USAASB03153](https://openairdocs.org/sdr/USAASB03153), Aug 25, 2003: CONTROL UNIT. MALFUNCTIONED. AFTER TAKEOFF FROM TPA, CREW REPORTED UNABLE TO RETRACT FLAPS BEYOND 2 UNITS. CREW RECYCLED FLAP HANDLE AND FLAPS CIRCUIT BREAKER SEVERAL TIMES WITH NO HELP. FL - [SDR USAASB03033](https://openairdocs.org/sdr/USAASB03033), Mar 2, 2003: INDICATOR. FAILED. CLT - FLT 953 - ON APPROACH TO CLT FROM BOS, CREW REPORTED THAT WHEN FLAPS WERE EXTENDED TO 10 UNITS, THE RIGHT TRAILING EDGE FLAP STOPPED AT 6 UNITS. CREW EXTE - [SDR USAA020476](https://openairdocs.org/sdr/USAA020476), Dec 31, 2002: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 2 INCHES, STATION 727 STRINGER 24L. CUT OUT DAMAGE, NDT'D AREA, INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 201 AND TR 53-60-06. - [SDR USAASB02185](https://openairdocs.org/sdr/USAASB02185), Oct 3, 2002: WIRE. BROKEN. EWR - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT 1C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER SEATS 2A AND C. OPERATIONAL CHECK GOOD. (M) - [SDR USAA020370](https://openairdocs.org/sdr/USAA020370), Sep 26, 2002: SKIN. CRACKED. PIT - FOUND SKIN WITH TWO CRACKED .25 INCH LONG, STATION 380 BODYLINE 0 AT RIVET FASTENER. INSTALLED DOUBLER, ROUTED OUT CRACK PER TYPICAL REPAIR 53-30-07 AND E - [SDR USA2002F00077](https://openairdocs.org/sdr/USA2002F00077), Aug 3, 2002: WIRE. BROKEN. MAINTENANCE FOUND THE EMERGENCY LIGHT ON SEAT ROW 13 ABC INOPERATIVE. MAINTENANCE REPAIRED WIRING AT SEAT ROW 13 ABC. OPERATIONAL CHECK NORMAL. - [SDR USAASB02117](https://openairdocs.org/sdr/USAASB02117), Jun 17, 2002: SOLENOID. FAULTY. SYR - FLT 251 - AFTER T/O FROM SYR, COULD NOT GET THE GEAR HANDLE TO MOVE PAST THE 'OFF' POSITION. CREW DID NOT OVERRIDE THE GEAR HANDLE BECAUSE OF A FLAPPING N - [SDR USAA020134](https://openairdocs.org/sdr/USAA020134), Apr 11, 2002: BULKHEAD. CRACKED. TPA - FOUND BULKHEAD WEB CRACKED TWO PLACES 2.5 INCH EACH, FS 663.75, RBL 45, W/W FORWARD BULKHEAD WEB. INSTALLED TWO DOUBLERS PER EA 94296A. (M) - [SDR USAA020133](https://openairdocs.org/sdr/USAA020133), Apr 9, 2002: SKIN. CRACKED. TPA - FOUND SKIN CRACKED .25 INCH, LOWER AFT CORNER OF LOWER HINGE CUT OUT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 52-10-12. (M) - [SDR USA2001F00006](https://openairdocs.org/sdr/USA2001F00006), May 31, 2001: PANEL. DEPARTED. AFTER TAKEOFF, FLIGHT ENCOUNTERED COMPLETE LOSS OF SYSTEM A HYDRAULICS AND PRESSURE. LOST LG TRIANGULAR PANEL OFF TOP OF RT WING. NOSE GEAR WOULD RETRACT BUT MA - [SDR USAASB01046](https://openairdocs.org/sdr/USAASB01046), Feb 10, 2001: INDICATOR. FAILED. BUF - FLT 638 - DURING DESCENT INTO BUF, CREW EXTENDED FLAPS TO 5 DEGREES AND THEN TO 10 DEGREES BUT RECEIVED A FLAP LIGHT. FLAPS WOULD NOT EXTEND BEYOND 5 DEGR - [SDR USAASB00352](https://openairdocs.org/sdr/USAASB00352), Dec 20, 2000: JACKSCREW. WORN. CLT - FLT 1974 - ON DESCENT INTO CLT, FROM MBJ, CAPTAIN NOTIFIED TOWER THAT THE FLAPS WOULD NOT EXTEND BEYOND FIVE DEGREES. CREW ACCOMPLISHED QUICK REFERENCE HA - [SDR USAASB00314](https://openairdocs.org/sdr/USAASB00314), Nov 14, 2000: FLAP. MALFUNCTIONED. BWI - FLT 2046 - ON APPROACH TO DCA, FROM MCI, THE TRAILING EDGE FLAPS STOPPED AT 8-10 DEGREES WITH NEEDLES SPLIT ON INDICATOR. CREW FOLLOWED QUICK REFERENCE HA - [SDR USAASB00243](https://openairdocs.org/sdr/USAASB00243), Sep 3, 2000: WARNING LIGHT. ILLUMINATED. PIT - FLT 1624 - ON CLIMB-OUT FROM PIT, THE LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED AS LEADING EDGE SLATS AND FLAPS DID NOT FULLY RETRACT. FLIGHT RETURNED T - [SDR USAASB00256](https://openairdocs.org/sdr/USAASB00256), Aug 29, 2000: BATTERY PACK. DISCHARGED. RDU - WHILE ACCOMPLISHING OVERNIGHT CHECK, MAINTENANCE FOUND THE LEFT OVERHEAD EXIT LIGHTS, THE OVERWING DOOR EXIT LIGHTS, THE SEAT MOUNTED EXIT LIGHT AT OVERWI - [SDR USAASB00185](https://openairdocs.org/sdr/USAASB00185), Jul 4, 2000: CONTROL PANEL. FAILED. PHL - FLT 637 - EN ROUTE FROM BOS-PHL, AT FL280, THE CABIN PRESSURE BEGAN TO SLOWLY CREEP UP TO 10,000 FEET. THE ALTITUDE WARNING HORN SOUNDED AND THE CREW BEGA - [SDR USAA000888](https://openairdocs.org/sdr/USAA000888), Jun 20, 2000: FRAME. WORN. CLT - FOUND FRAME WORN 3 INCHES WEAR AREA CAUSED BY APU DUCT CLAMP, STATION 1040. REPAIRED PER EA 67421/SRM 53-00-03. (M) - [SDR USAA000878](https://openairdocs.org/sdr/USAA000878), Jun 20, 2000: ANGLE. CRACKED. CLT - FOUND CHORD ANGLE CRACKED 4 INCHES, STATION 1138, STRINGER 5R INSIDE UPPER STRAP CHORD ANGLE. FABRICATED REPAIR AND INSTALLED PER SRM 53-00-01 FIG 221. (M - [SDR USAA000868](https://openairdocs.org/sdr/USAA000868), Jun 19, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCHES, STATION 480, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER AND FILLER PER TR 53-10-14A. (M) - [SDR USAA000869](https://openairdocs.org/sdr/USAA000869), Jun 19, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, STATION 440, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER AND FILLER PER TR 53-10-14A. (M) - [SDR USAA000870](https://openairdocs.org/sdr/USAA000870), Jun 19, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCHES, STATION 500A, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M) - [SDR USAA000871](https://openairdocs.org/sdr/USAA000871), Jun 19, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, STATION 400, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M) - [SDR USAA000858](https://openairdocs.org/sdr/USAA000858), Jun 16, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, STATION 400, STRINGER 9L AT OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER SRM 53-10-14A. (M) - [SDR USAA000859](https://openairdocs.org/sdr/USAA000859), Jun 16, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, STATION 440, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M) - [SDR USAA000861](https://openairdocs.org/sdr/USAA000861), Jun 16, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, STATION 727D, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M) - [SDR USAA000862](https://openairdocs.org/sdr/USAA000862), Jun 16, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, STATION 747, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M) - [SDR USAA000863](https://openairdocs.org/sdr/USAA000863), Jun 16, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED, STATION 747 STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M) - [SDR USAA000864](https://openairdocs.org/sdr/USAA000864), Jun 16, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, STATION 787, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M) - [SDR USAA000865](https://openairdocs.org/sdr/USAA000865), Jun 16, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, STATION 827, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M) - [SDR USAA000866](https://openairdocs.org/sdr/USAA000866), Jun 16, 2000: FRAME. CRACKED. CLT - FOUND FRAME .5 INCH CRACKED, STATION 827, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M) - [SDR USAA000867](https://openairdocs.org/sdr/USAA000867), Jun 16, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, STATION 867, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M) - [SDR USAA000860](https://openairdocs.org/sdr/USAA000860), Jun 16, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCHES, STATION 480, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M) - [SDR USAA000848](https://openairdocs.org/sdr/USAA000848), Jun 14, 2000: DOOR FRAME. CRACKED. CLT - FOUND FRAME CRACKED .125 INCH, FORWARD SERVICE DOOR JAMB FRAME UPPER FORWARD DOOR STOP FITTING. REMOVED AND REPLACED PART PER BOEING DWG 65-55878. (M) - [SDR USAA000815](https://openairdocs.org/sdr/USAA000815), Jun 12, 2000: BULKHEAD. CRACKED. CLT - FOUND TWO CRACKS IN BULKHEAD .25 INCH AND .75 INCH, WL 201, LBL 5. FABRICATED AND INSTALLED REPAIR PART PER TR 53-10-08 FIG 209. (M) - [SDR USAA000814](https://openairdocs.org/sdr/USAA000814), Jun 12, 2000: ANGLE. CRACKED. CLT - FOUND ANGLE CRACKED 1 INCH, LOWER FORWARD WING TO BS 540 ABOVE RT RAM AIR DUCT. INSTALLED DOUBLER PER TR 53-50-03. (M) - [SDR USAA000884](https://openairdocs.org/sdr/USAA000884), Jun 4, 2000: CHANNEL. CRACKED. CLT - FOUND U-CHANNEL CRACKED .375 INCH, STRINGER 18A SHAFT LEFT W/W PLUS 727. REPLACED STRINGER 18A SHELF. (M) - [SDR USAA000885](https://openairdocs.org/sdr/USAA000885), Jun 3, 2000: FRAME. CORRODED. CLT - FOUND 1 INCH CORROSION, STATION 807 BETWEEN STRINER 23R-24R. FABRICATED REPLACEMENT STIFFENER PER DWG 69-38178. CORROSION LEVEL 1, TASK NR C53-202-01. (M) - [SDR USAA000883](https://openairdocs.org/sdr/USAA000883), Jun 3, 2000: SUPPORT BRACKET. CRACKED. CLT - FOUND DOOR SUPPORT CRACKED 2 INCHES, LOWER CORNER AT FORWARD DOOR SUPPORT. INSTALLED DOUBLER PER SRM 51-70-11. (M) - [SDR USAA000882](https://openairdocs.org/sdr/USAA000882), Jun 3, 2000: DRAG BRACE. CRACKED. CLT - FOUND DRAG BRACE ANGLE CRACKED .5 INCH, BS 536, STRINGER 21L. INSTALLED FABRICATED SUPPORT ANGLE SECTION PER TR 53-50-03. (M) - [SDR USAA000887](https://openairdocs.org/sdr/USAA000887), Jun 2, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH IN FRAME AT INBOARD RIVET HOLE, STATION 787, STRINGER 9L AT OVERHEAD BIN SUPPORT. INSTALLED REPAIR DOUBLER PER TR 53-10-14A. ( All 62: https://openairdocs.org/deregistered/N585US-2006-09-12/reports.md ## 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 20020617019159I](https://openairdocs.org/incident/20020617019159I), Jun 17, 2002: Boeing 737301 (N585US), Syracuse, NY. (-23) On Monday, June 17, 2002, after takeoff from runway 28 at Syracuse Hancock International Airport, the nose gear would not retract on N585US, a Boeing… - [Incident 20010531015299I](https://openairdocs.org/incident/20010531015299I), May 31, 2001: Boeing 737301 (N585US), Tampa, FL, Minor damage. (-23) On may 31, 2001 a B-737-301, N585US operated by us airways airlines, on departure from Tampa International Airport, Florida, (tpa) report "a" hydraulic… - [Incident 20010210002709I](https://openairdocs.org/incident/20010210002709I), Feb 10, 2001: Boeing 737301 (N585US), Buffalo, NY. (-23) On Saturday, February 10, 2001 at 2009 EST, a usairways B-737, N585US, flight 638, landed on runway 23 at the Buffalo niagra international airport after… ## Other aircraft with N585US - [Registered now](https://openairdocs.org/aircraft/N585US): Nil Rotorcraft Club MAGNI M24, S/N 24106104, built 2011 --- 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.