# N575US: 1987 Boeing 737-301, registration cancelled 2010-04-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 8, 2010 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23740 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 8, 1989 - Certificate issued: February 8, 2007 - Last registry action: February 16, 2010 - Mode S code: A762CF - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N575US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=575US - Page: https://openairdocs.org/deregistered/N575US-2010-04-08 From the FAA registry file of October 29, 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 (29) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SB05074](https://openairdocs.org/sdr/SB05074), Jun 20, 2005: OUTFLOW VALVE. FAULTY. AT FL330, CREW REPORTED CABIN BEGAN A 6,000 FPM CLIMB. AUTO FAIL LIGHT ILLUMINATED ALONG WITH STANDBY ON LIGHT. CREW SWITCHED TO MANUAL AC/DC PRESSURIZATION MOD - [SDR SB05073](https://openairdocs.org/sdr/SB05073), Jun 19, 2005: OUTFLOW VALVE. FAILED. EN ROUTE FROM CLT TO BUF, 100 MILES SOUTH OF PIT, AIRCRAFT LOST AUTO AND STANDBY PRESSURIZATION MODES. HOWEVER, CREW WAS ABLE TO REGAIN CONTROL IN MANUAL PRESSU - [SDR SB05070](https://openairdocs.org/sdr/SB05070), Jun 14, 2005: OUTFLOW VALVE. INOPERATIVE. EN ROUTE WITH THE AUTO PRESSURIZATION ON MEL, LOST CONTROL OF STANDBY PRESSURIZATION MODE. CABIN ALTITUDE BEGAN TO CLIMB, PILOT REQUESTED AN EMERGENCY DESCENT. - [SDR USAA050750](https://openairdocs.org/sdr/USAA050750), Jun 9, 2005: SKIN. CRACKED. CLT - FOUND FORWARD SERVICE DOOR SKIN CRACKED .620 INCH, UPPER HINGE CUTOUT. REPAIR DOUBLER INSTALLED IAW TR 52-10-13. (M) - [SDR SB05058](https://openairdocs.org/sdr/SB05058), May 8, 2005: CABLE. INOPERATIVE. PIT - THE R2 DOOR SLIDE LANYARD WOULD NOT RELEASE. MAINTENANCE REPLACED THE SLIDE. - [SDR USAA040362](https://openairdocs.org/sdr/USAA040362), Jul 26, 2004: FRAME. CRACKED. PIT - FOUND FRAME CRACKED APPROX 1.025 INCH, STATION 663.75. INSTALLED REPAIR ANGLE PER EA 78568. (M) - [SDR USAA04337](https://openairdocs.org/sdr/USAA04337), Jun 22, 2004: SKIN. DAMAGED. FOUND PROBLEM WITH PREVIOUS REPAIR AT BS 470, STRINGER 8L TO 9L. REPAIRED PER SRM 53-00-01 FIGURE 201. (M) - [SDR USAA04336](https://openairdocs.org/sdr/USAA04336), Jun 22, 2004: SPAR. DAMAGED. PIT - FOUND PROBLEM WITH PREVIOUS REPAIR ON LOWER SKIN OF THE RIGHT HORIZONTAL STAB AT REAR SPAR LOWER SURFACE. REPAIRED PER SRM FIUTE 204 DETAIL NR 1. (M) - [SDR USAA040304](https://openairdocs.org/sdr/USAA040304), Jun 15, 2004: SKIN. DELAMINATED. PIT - FOUND WING DELAMINATION 1 SQUARE INCH, NR 3 SLAT INBOARD END TRAILING EDGE. REMOVED DAMAGE, INSTALLED FILLER INTERNAL DOUBLER AND NEW CORE AND TOP DOUBLER - [SDR USAA040305](https://openairdocs.org/sdr/USAA040305), Jun 15, 2004: SKIN. DELAMINATED. PIT - FOUND WING DELAMINATED 1.5 SQUARE INCH, TOP SURFACE AT OUTBOARD TRACK AREA TRAILING EDGE OF NR 3 SLAT. REMOVED DAMAGE. INSTALLED FILLER/CORE MATERIAL, INS - [SDR USAA040281](https://openairdocs.org/sdr/USAA040281), Jun 8, 2004: STIFFENER. CORRODED. PIT - FOUND BULKHEAD STIFFENER 1 INCH BY 2 INCH AREA, STATION 1016 LBL 0. REMOVED CORROSION AND INSTALLED REPAIR PER BOEING DWG 65C28106. (M) - [SDR USAA040303](https://openairdocs.org/sdr/USAA040303), Jun 3, 2004: SKIN. DENTED. PIT - FOUND SKIN DENTED WITH DELAMINATION TWO AREAS 2 INCHES BY 1.5 INCH AND 1 INCH BY 1.375 INCH AREA, LEFT ELEVATOR LOWER SURFACE BETWEEN 176/200. REMOVED DIS - [SDR USAASB03169](https://openairdocs.org/sdr/USAASB03169), Sep 17, 2003: BATTERY. WEAK. FOUND LT OVERWING AND FORWARD ENTRY EMERGENCY LIGHT BATTERIES WEAK. MAINTENANCE REPLACED THE BATTERIES. (M) - [SDR USAASB03069](https://openairdocs.org/sdr/USAASB03069), May 25, 2003: CHARGER. INOPERATIVE. CLT - MAINTENANCE REPORTED THE RIGHT EMERGENCY LIGHTS AT THE OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATION - [SDR USAASB02119](https://openairdocs.org/sdr/USAASB02119), Jun 22, 2002: SPLICE. DAMAGED. TPA - MAINTENANCE FOUND THE SEAT END EMERGENCY EXIT LIGHT AT THE EMERGENCY EXIT ROW INOPERATIVE. MAINTENANCE REPLACED A BAD SPLICE. OPERATIONAL CHECK GOOD. (M) - [SDR USA2002F00055](https://openairdocs.org/sdr/USA2002F00055), Jun 9, 2002: UPLOCK SENSOR. FAULTY. ENROUTE, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND REPORTED THE GEAR OPERATED NORMALLY. LIGHT E - [SDR USA2002F00047](https://openairdocs.org/sdr/USA2002F00047), Jun 1, 2002: CONNECTOR. FAULTY. AFTER TAKEOFF, THE NR 2 ENGINE EGT RED LIGHT ILLUMINATED AS EGT WENT TO 1,067 DEGREES. CREW REDUCED THROTTLE AND EGT RETURNED TO NORMAL. ALL OTHER ENGINE INDICA - [SDR USAASB01305](https://openairdocs.org/sdr/USAASB01305), Nov 1, 2001: BATTERY PACK. DISCHARGED. PHL - MAINTENANCE FOUND THE AISLE EMERGENCY LIGHTS, IN THE CABIN, INOPERATIVE. MAINTENANCE FOUND SEVERAL BATTERY PACKS DISCHARGED. REMOVED AND REPLACED BATTERY - [SDR USAASB01218](https://openairdocs.org/sdr/USAASB01218), Aug 1, 2001: POWER UNIT. FAILED. CLT - DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE DEPLOYED NORMALLY BUT THE SLIDE MOUNTED EMERGENCY LIGHTS FAILED - [SDR USAASB01065](https://openairdocs.org/sdr/USAASB01065), Feb 27, 2001: SWITCH. FAULTY. CLT - FLT 1625 - EN ROUTE FROM CLT-JAX, AS CREW RETRACTED THE FLAPS/SLATS, THE NR 6 LEADING EDGE SLAT INTRANSIT LIGHT ILLUMINATED ON THE FORWARD AND OVERHEAD PA - [SDR USAASB01060](https://openairdocs.org/sdr/USAASB01060), Feb 25, 2001: CONTROLLER. FAULTY. CLT - FLT 1262 - ON CLIMB-OUT FROM PBI, EN ROUTE TO PHL, PRESSURIZATION WAS UNCONTROLLABLE WITH THE RIGHT PACK AS THE LEFT PACK WAS ON MEL. FLIGHT DIVERTED TO C - [SDR USAASB00025](https://openairdocs.org/sdr/USAASB00025), Jan 28, 2000: INDICATOR. FAILED. GSO - FLT 1462 - ON APPROACH INTO GSO, A FLAP ASYMMETRY OCCURRED. SPLIT FLAPS OF 1 DEGREE LEFT AND 25 DEGREES RIGHT WAS INDICATED. FLAP HANDLE WAS LOCKED OUT AL - [SDR USAASB99084](https://openairdocs.org/sdr/USAASB99084), Mar 31, 1999: MECHANISM. NOT LATCHED. EWR - FLT 605 - AFTER TAKEOFF, CLIMBING THROUGH 2000 FEET, THE AUTO FAIL LIGHT ILLUMINATED. CREW COULD NOT CONTROL CABIN PRESSURIZATION IN STANDBY OR MANUAL MOD - [SDR USAASB98207](https://openairdocs.org/sdr/USAASB98207), Aug 11, 1998: AIR DISTR. ODOR. CLT - FLT 1267 - ON TAKEOFF FROM LGA, CREW NOTICED A STRONG SMELL OF RUBBER BURNING IN THE COCKPIT AND THE CABIN. THERE WERE NO SIGNS OF SMOKE SMELL AND THE APU - [SDR USAASB98195](https://openairdocs.org/sdr/USAASB98195), Jul 22, 1998: BATTERY PACK. DISCHARGED. ROC - MAINTENANCE FOUND ALL THE EMERGENCY LIGHTS CONTROLLED BY POWER SUPPLY M1132 FAIL AFTER 10-15 SECONDS OF OPERATION. ALSO FOUND THE AISLE BULLNOSE EMERGENCY - [SDR USAA970001](https://openairdocs.org/sdr/USAA970001), Jan 4, 1997: BULKHEAD. CRACKED. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO CRACKS APPROXIMATELY 2 INCHES IN LENGTH AT BS 178 LBL 6 INCHES WL 200 BULKHEAD. REPAIRED PER T/R 53-10-07 RE - [SDR USAA970000](https://openairdocs.org/sdr/USAA970000), Jan 4, 1997: BULKHEAD. CRACKED. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO CRACKS APPROXIMATELY 2 INCHES AT BS 178 BULKHEAD RBL 6 INCHES WL 200. REPAIRED PER T/R 53-10-07 REV A SRM 51 - [SDR USAASB97005](https://openairdocs.org/sdr/USAASB97005), Jan 3, 1997: OIL LINE. LEAKING. INT - FL 7901 - FLIGHT WAS IN THE PROCESS OF COMPLYING WITH TEST HOP PROCEDURES, AFTER A HEAVY MAINTENANCE VISIT, WHEN THE CREW NOTICED A RAPID OIL QTY LOSS IN - [SDR USAASB96174](https://openairdocs.org/sdr/USAASB96174), Sep 1, 1996: POWER SUPPLY. INOPERATIVE. PHL - MAINTENANCE FOUND THE EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT INOP AT THE AFT RIGHT SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY IN THE A ## 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 19950717023039I](https://openairdocs.org/incident/19950717023039I), Jul 17, 1995: Boeing 737300 (N575US), Buffalo, NY, Minor damage. On takeoff right engine injested a bird. Returned safely. Fan blades damaged. 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