# N576US: 1988 Boeing 737-301, registration cancelled 2006-06-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 21, 2006 - Exported to: Spain - Status when cancelled: Valid registration - Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R) - Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23741 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: None - Airworthiness: Standard, normal - Airworthiness date: September 8, 1989 - Certificate issued: September 13, 2005 - Last registry action: September 13, 2005 - Mode S code: A76686 - Owner when cancelled: [Rpk Capital V LLC](https://openairdocs.org/faa-owner/RPK%20CAPITAL%20V%20LLC) - Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago) - Owner type: Corporation - Owner's area on the map: 41.9022° N, 87.6833° W: Placed by OpenAirDocs at the center of ZIP code 60622, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N576US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=576US - Page: https://openairdocs.org/deregistered/N576US-2006-06-21 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 (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SB04167](https://openairdocs.org/sdr/SB04167), Dec 13, 2004: CONTROL UNIT. UNRELIABLE. PIT FLT414 FLIGHT DEPARTED ORD, EN ROUTE TO PHL, WITH THE NR 2 GENERATOR ON MEL 24-1. DURING CRUISE, THE APU GENERATOR DROPPED OFF LINE, LEAVING ONLY THE NR 1 G - [SDR USAA040365](https://openairdocs.org/sdr/USAA040365), Jul 29, 2004: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 2.05 INCH, FS 129 LOWER SKIN AT AFT SPAR LEFT HORIZ STAB. INSTALLED DOUBLER PER SRM 55-10-01. (M) - [SDR USAA040096](https://openairdocs.org/sdr/USAA040096), Apr 1, 2004: BULKHEAD. CORRODED. FOUND AFT PRESSURE BULKHEAD CORRODED 2 FEET BY 2 INCH AREA, FROM LBL .5 TO RBL 5 INCHES IN FRONT OF CHANNEL STIFFENER. INSTALLED FILLERS, DOUBLERS AND STIFFENER - [SDR USAA040098](https://openairdocs.org/sdr/USAA040098), Apr 1, 2004: STRINGER. CRACKED. PIT - FOUND SHELF CRACKED 2 INCHES IN LENGTH, FROM AFT EDGE TO INBOARD FASTENER LEFT 18A SHELF. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (M) - [SDR USAA040099](https://openairdocs.org/sdr/USAA040099), Apr 1, 2004: STRINGER. CRACKED. PIT - FOUND SHELF CRACKED 2 INCHES IN LENGTH, AFT END OF RIGHT 18A SHELF INTO FIRST FASTENER. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (M) - [SDR USA2004F00024](https://openairdocs.org/sdr/USA2004F00024), Mar 28, 2004: CIRCUIT CARD. FAULTY. ON CLIMBOUT, THE LT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO - [SDR USAASB04033](https://openairdocs.org/sdr/USAASB04033), Mar 18, 2004: WARNING LIGHT. ILLUMINATED. ON CLIMB-OUT FROM PHL, THE LT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURT - [SDR USAASB04031](https://openairdocs.org/sdr/USAASB04031), Mar 16, 2004: UPLOCK SENSOR. FAILED. ORD - FLT 1082 - ON CLIMB-OUT FROM ORD, CAPTAIN REPORTED THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. AFTER FOLLOWING ABNORMAL PRO - [SDR USAASB02029](https://openairdocs.org/sdr/USAASB02029), Feb 6, 2002: BATTERY PACK. DISCHARGED. PHL - MAINTENANCE FOUND THE FORWARD SERVICE DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD RIGHT SIDE BATTERY PACK. OPERATIONAL - [SDR USAASB01318](https://openairdocs.org/sdr/USAASB01318), Nov 20, 2001: BLADE. DAMAGED. BUF - FLT 1563 - APPLIED T/O PWR, A SLIGHT NOISE AND VIBRATION WAS NOTED. ENG INDICATIONS WERE NORMAL WITH NO LIMITS EXCEEDED. SHORTLY AFTER BECOMING AIRBORNE, - [SDR USAA010849](https://openairdocs.org/sdr/USAA010849), Jun 29, 2001: ANGLE. CRACKED. PIT - FOUND ANGLE CRACKED 3 INCHES, STATION 294.5 RIGHT WL 208.1 CREASE BEAM TO FLOOR STRUCTURE. REPLACED ANGLE PER T/R. (M) - [SDR USAA010854](https://openairdocs.org/sdr/USAA010854), Jun 28, 2001: ANGLE. CORRODED. PIT - FOUND ANGLE CORRODED 1 INCH BY 18 INCH AREA, FORWARD SIDE FLOORBEAM STATION 270, WL 207.5 COCKPIT ENTRANCE. CORROSION LEVEL 1, TASK NR C53-107-01. REMOVED - [SDR USAA010852](https://openairdocs.org/sdr/USAA010852), Jun 28, 2001: SEAT TRACK. CORRODED. PIT - FOUND SEAT TRACK CORRODED 3 INCH BY 6 INCH, NR 2 GALLEY MIDDLE SEAT TRACK STATION 328 GOING AFT. (M) - [SDR USAA010851](https://openairdocs.org/sdr/USAA010851), Jun 28, 2001: SEAT TRACK. CORRODED. PIT - FOUND SEAT TRACK CORRODED 3 INCHES BY 6 INCHES, NR 2 GALLEY SEAT TRACK STATION 328 AFT. (M) - [SDR USAA010850](https://openairdocs.org/sdr/USAA010850), Jun 28, 2001: FLOORBEAM. CORRODED. PIT - FOUND FLOORBEAM CORRODED 3 INCHES BY 30 INCHES, STATION 328 NR 3 GALLEY 10 INCHES RIGHT OF C/L TO FORWARD SERVICE DOOR. CUT OUT CORROSION OF FLOORBEAM T-C - [SDR USAA010848](https://openairdocs.org/sdr/USAA010848), Jun 25, 2001: BEAM. CORRODED. PIT - FOUND BEAM CORRODED IN THREE AREAS 1 INCH BY 1 INCH, STATION 208.1 RIGHT UNDER GALLEY NR 1. CORROSION LEVEL 1, TASK NR C53-107-01. CLEANED AND TREATED PER - [SDR USAA010862](https://openairdocs.org/sdr/USAA010862), Jun 14, 2001: SUPPORT. CORRODED. PIT - FOUND CARGO PANEL SUPPORT ANGLE CORRODED 1 INCH BY 3 INCH, STATION 787 FROM S19L TO S24L. BLENDED PER 53-00-07. (M) - [SDR USAA010861](https://openairdocs.org/sdr/USAA010861), Jun 13, 2001: SUPPORT. CORRODED. PIT - FOUND SUPPORT CORRODED 1 INCH BY 1 INCH, STATION 967-986 AND 18.25 RBL. CORROSION LEVEL 1. REPLACED WITH PART NR 65-46812-169. (M) - [SDR USAA010860](https://openairdocs.org/sdr/USAA010860), Jun 13, 2001: FLOORBEAM. CORRODED. PIT - FOUND BEAM CORRODED 1 INCH BY 4 INCHES, BS 967 UPPER T-CAP. CORROSION LEVEL 1. REPLACED PER 53-00-51. (M) - [SDR USAA010859](https://openairdocs.org/sdr/USAA010859), Jun 13, 2001: BEAM. CORRODED. PIT - FOUND BEAM CORRODED 1 INCH BY 36 INCH AREA, BS 986.6. CORROSION LEVEL 1. REPAIRED PER TR 53-10-05, BAC 1505-100880. (M) - [SDR USAA010856](https://openairdocs.org/sdr/USAA010856), Jun 9, 2001: BELTFRAME. CRACKED. PIT - FOUND BELTFRAME CRACKED .25 INCH, STATION 480 S8. DOUBLER INSTALLED PER SRM T/R 53-10-14. (M) - [SDR USAA010857](https://openairdocs.org/sdr/USAA010857), Jun 9, 2001: BELTFRAME. CRACKED. PIT - FOUND BELTFRAME CRACKED 1 INCH, STATION 787 BELTFRAME ABOVE S9R. INSTALLED REPAIR DOUBLER PER T/R 53-1014. (M) - [SDR USAA010863](https://openairdocs.org/sdr/USAA010863), Jun 8, 2001: STRINGER. CRACKED. PIT - FOUND STRINGER CRACKED 1 INCH, STATION 440 STRINGER 8 RIGHT. INSTALLED DOUBLER PER SRM T/R 53-10-14. (M) - [SDR USAA010855](https://openairdocs.org/sdr/USAA010855), Jun 7, 2001: FLOOR SUPPORT. CORRODED. PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH SPOT, STATION 727C CHANNEL NR 5 FLOOR SUPPORT. BLENDED PER 53-60-51 FIG 101. CORROSION LEVEL 1. (M) - [SDR USAA010858](https://openairdocs.org/sdr/USAA010858), May 31, 2001: STRAP. CRACKED. PIT - FOUND STRAP CRACKED TWO PLACES .5 INCH ON BOTH FORWARD SIDES, STATION 312 BOTTOM FLOORBEAM SUPPORT STRAP 10 INCHES LEFT C/L. DEFECTIVE PART REPLACED WITH - [SDR USAA010853](https://openairdocs.org/sdr/USAA010853), May 29, 2001: SEAT TRACK. CORRODED. PIT - FOUND SEAT TRACK CORRODED 3 INCHES BY 6 INCHES, NR 2 GALLEY OUTBOARD SEAT TRACK STATION 328 GOING AFT. (M) - [SDR USAASB01132](https://openairdocs.org/sdr/USAASB01132), May 9, 2001: SWITCH. FAILED. CLT - MAINTENANCE FOUND THE EMERGENCY LIGHTS (NOT ARMED)INOPERATIVE/WON''T TEST. MAINTENANCE REMOVED AND REPLACED THE SOCKET/SWITCH ASSEMBLY ON THE P5 OVERHEAD - [SDR USAASB01101](https://openairdocs.org/sdr/USAASB01101), Apr 15, 2001: ENGINE. MALFUNCTIONED. TPA - FLT 1580 - EN ROUTE FROM PHL TO TPA, A BURNING OIL SMELL WAS REPORTED COMING FROM THE LEFT PACK DURING FLIGHT. FLIGHT CONTINUED AND LANDED AT TPA WITHOUT - [SDR USAASB01093](https://openairdocs.org/sdr/USAASB01093), Mar 29, 2001: BATTERY PACK. DISCHARGED. LGA - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EMERGENCY EXIT LIGHTS WEAK. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) - [SDR USAASB01071](https://openairdocs.org/sdr/USAASB01071), Mar 2, 2001: POWER SUPPLY. FAILED. GSO - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY ASSEMBLY. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB00179](https://openairdocs.org/sdr/USAASB00179), Jun 27, 2000: TRANSFORMER. OVERHEATED. MDT - FLT 1924 - EN ROUTE FROM ROC TO DCA, F/A NOTIFIED CAPTAIN THAT THERE WAS A STRONG BURNING ELECTRICAL ODOR IN THE CABIN. CAPT MADE A RAPID DESCENT, DECLARE - [SDR USAASB99207](https://openairdocs.org/sdr/USAASB99207), Aug 20, 1999: WINDOW. CRACKED. TPA - FLT 2335 - EN ROUTE FROM FLL TO CLT, THE CAPTINS L2 SLIDING WINDOW CRACKED. FLIGHT DIVERTED TO TPA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVE - [SDR USAASB98073](https://openairdocs.org/sdr/USAASB98073), Mar 21, 1998: BATTERY PACK. DISCHARGED. PIT - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP AT SEAT ROWS 2, 3, AND 4. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) - [SDR USAASB97312](https://openairdocs.org/sdr/USAASB97312), Nov 13, 1997: RELAY. FAILED. CLT - FLT 2183 - AFTER TAKEOFF AND MOVING THE LANDING GEAR LEVER TO THE UP POSITION, THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. NO VIBRATION WAS FELT. - [SDR USAASB97187](https://openairdocs.org/sdr/USAASB97187), Jul 13, 1997: COMPUTER. FAILED. BNA - FL2053 - FLIGHT WAS ON COUPLED APPROACH FOR BNA AT 1,000 FEET AGL WHEN THE CREW WAS UNABLE TO DISCONNECT AUTOPILOT WITH LEFT OR RIGHT CONTROL COLUMN. FLIG - [SDR USAASB96219](https://openairdocs.org/sdr/USAASB96219), Oct 26, 1996: CONTROLLER. FAILED. MCI - FLT 136 - CAPTAIN REPORTED PRESSURIZATION LOSS AND DESCENDED TO 10,000 FEET. CAPTAIN COULD NOT REGAIN CONTROL OF CABIN UNTIL LEVEL OFF AT 10,000 FEET. EME - [SDR USAASB96203](https://openairdocs.org/sdr/USAASB96203), Sep 30, 1996: OVERHEAT MODULE. FAILED. PIT - FL 133 - LEFT WING BODY OVERHEAT LIGHT ILLUMINATED ON TAKEOFF AND REMAINED ON IN CLIMB. CAPTAIN TURNED OFF LEFT BLEED SWITCH BUT LIGHT REMAINED ON. AT 10, ## FAA accident and incident reports (1) 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 20000627032639I](https://openairdocs.org/incident/20000627032639I), Jun 27, 2000: Boeing 737301 (N576US), Middletown, PA. (-23)Us air flight 1924 was enroute from rochester (roc) to Washington (dca) on an IFR flight when it diverted to Harrisburg, Pennsylvania (MDT) due to an… ## Other aircraft with N576US - [Registered now](https://openairdocs.org/aircraft/N576US): DJI T40, S/N 64TBL63002008N --- 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.