# N236US: Boeing 737-201, registration cancelled 2000-08-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 11, 2000 - Exported to: Canada - Status when cancelled: Triennial form not returned - Airframe: [Boeing 737-201](https://openairdocs.org/model/boeing-737-201) (registry code 1384454) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 22352 - Type of aircraft: Fixed wing multi engine - Certificate issued: August 15, 1989 - Last registry action: April 18, 2000 - Mode S code: A2209D - Owner when cancelled: [US Airways Inc](https://openairdocs.org/faa-owner/US%20AIRWAYS%20INC) - Location: [Arlington, VA](https://openairdocs.org/faa-place/VA/Arlington) - Owner type: Corporation - Owner's area on the map: 38.8783° N, 77.1007° W: Placed by OpenAirDocs: center of Arlington, VA, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N236US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=236US - Page: https://openairdocs.org/deregistered/N236US-2000-08-11 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 737-201: https://openairdocs.org/model/boeing-737-201.md ## Service difficulty reports (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA000192](https://openairdocs.org/sdr/USAA000192), Feb 11, 2000: SKIN. CRACKED. TPA - FOUND .5 INCH SKIN CRACK, STATION 540, JUST BELOW LAP AND STRINGER 14L SKIN. INSTALLED FILLER AND DOUBLER PER SRM 53-30-3 AND EA 66144. (M) - [SDR USAA990736](https://openairdocs.org/sdr/USAA990736), Jul 17, 1999: SKIN. CRACKED. PIT - DURING RON CHECK, FOUND .5 INCH LONG CRACK AT STATION 727A STRINGER 18 RT ON SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 6. (M) - [SDR USAA990735](https://openairdocs.org/sdr/USAA990735), Jul 17, 1999: SKIN. CRACKED. PIT - DURING RON CHECK, FOUND A .75 INCH CRACK AT STATION 747 STRINGER 18 RT AND A .75 INCH LONG CRACK AT STATION 767 STRINGER 19 RT ON SKIN. INSTALLED EXTERNAL - [SDR USAA990734](https://openairdocs.org/sdr/USAA990734), Jul 17, 1999: WEB. CRACKED. PIT - DURING RON CHECK, FOUND 6 INCH CRACK AT PRESSURE SIDEWALL WEB, NOSE WHEEL WELL AT BS 259.5, WL 175.6. INSTALLED SHEETMETAL DOUBLERS AND FILLERS PER TYPICA - [SDR USAASB99142](https://openairdocs.org/sdr/USAASB99142), Jun 14, 1999: CHARGER. FAILED. ORD - MAINTENANCE FOUND THE LEFT AND RIGHT FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD BATTERY CHARGER ASSEMBLY. OP - [SDR USAA990039](https://openairdocs.org/sdr/USAA990039), Jan 14, 1999: SKIN. CRACKED. CLT - DURING PCI CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK ON FUSE SKIN STATION 727 BELOW STRINGER 17R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M) - [SDR USAASB98167](https://openairdocs.org/sdr/USAASB98167), Jul 2, 1998: SEAL. OUT OF POSITION. PIT - FLT 856 - AFTER TAKEOFF FROM PIT, AIRCRAFT FAILED TO PRESSURIZE. A LOUD AIR NOISE WAS HEARD COMING FROM DOOR R1. FLIGHT RETURNED TO PIT AND LANDED WITHOUT - [SDR USAASB98153](https://openairdocs.org/sdr/USAASB98153), Jun 21, 1998: ENGINE. OVERTEMP. PIT - FLT 1894 - AFTER TAKEOFF FROM PIT, THE NR 1 ENGINE ENCOUNTERED HIGH OIL TEMPERATURE. FLT RETURNED TO FIELD AT PIT AND LANDED WITHOUT INCIDENT. NO EMERGENC - [SDR USAASB98035](https://openairdocs.org/sdr/USAASB98035), Feb 10, 1998: ANTI-ICE DUCT. LEAKING. TPA - FLT 1874 - THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT APPROXIMATELY 25 MILES NORTH OF TPA. CREW FOLLOWED EMERGENCY PROCEDURES FOR OVERHEA - [SDR USAASB98025](https://openairdocs.org/sdr/USAASB98025), Jan 30, 1998: WINDSHIELD. DEFECTIVE. ORF - FLT 1279 - CAPT REPORTED VIA ACARS THAT FLIGHT WAS RETURNING TO FIELD AT ORF DUE TO A LOUD AIRLEAK COMING FROM THE F/O'S WINDSHIELD. NOISE WAS TOO LOUD TO - [SDR USAA970303](https://openairdocs.org/sdr/USAA970303), Oct 24, 1997: SKIN. CRACKED. ROA - DURNG BX CHECK VISUAL INSPECTION, FOUND 1.125 INCH CRACK AFT ENTRY DOOR SKIN AFT UPPER CORNER. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM - [SDR USAA970302](https://openairdocs.org/sdr/USAA970302), Oct 24, 1997: SKIN. CRACKED. ROA - DURING BX CHECK VISUAL INSPECTION, FOUND 3 INCH SKIN CRACK STATION 950 STRINGER 24L FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 5 - [SDR USAASB96175](https://openairdocs.org/sdr/USAASB96175), Aug 31, 1996: BATTERY PACK. FAILED. CLT - MAINTENANCE FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS FLASHING. MAINTENANCE REMOVED AND REPLACD THE BATTERY PACK FOR THE OVERWING EMERGENCY EXIT LIGHTS. O - [SDR USAASB96171](https://openairdocs.org/sdr/USAASB96171), Aug 30, 1996: LIGHT BALLAST. BURNED. IAH - FL 1183 - ON DESCENT INTO IAH, CREW DETECTED SMELL OF SMOKE IN THE COCKPIT. WHILE LOOKING FOR THE SOURCE, THE SMOKE ALARM IN THE FORWARD LAV WENT OFF. SHO - [SDR USAA960568](https://openairdocs.org/sdr/USAA960568), Aug 22, 1996: FLOOR BEAM. CRACKED. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND ONE .25 INCH CRACK BS 520 AT RBL 45 INCH FLOOR BEAM. INSTALLED NEW CHANNEL AND DOUBLERS, REPAIRED PER EA 41421. - [SDR USAA960567](https://openairdocs.org/sdr/USAA960567), Aug 22, 1996: FLOOR BEAM. CRACKED. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND ONE .25 INCH CRACK BS 520 AT RBL 25 CABIN FLOOR BEAM. INSTALLED NEW CHANNELS AND DOUBLERS PER EA 41421. (M) - [SDR USAA960565](https://openairdocs.org/sdr/USAA960565), Aug 22, 1996: FLOOR BEAM. BROKEN. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND UPPER 'T' OF FLOOR BEAM BROKEN INTO STATION 663 BL0. INSTALLED DOUBLER ON T-CAP AND WEB. REPAIRED PER BOEING DRA - [SDR USAA960564](https://openairdocs.org/sdr/USAA960564), Aug 22, 1996: STRINGER. CORRODED. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 7 INCH CORRODED AREA STRINGER 27L, STATION 967. CUT OUT DAMAGE AND INSTALLED STRINGER SPLICE REPAIR. R - [SDR USAA960563](https://openairdocs.org/sdr/USAA960563), Aug 22, 1996: FLOOR BEAM. CORROSION. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 6 INCH AT STATION 947.5 FLOOR BEAM. REPAIRED T-CAP, DOUBLERS AND REPAIR ANGLES. REPAIRED PE - [SDR USAA960562](https://openairdocs.org/sdr/USAA960562), Aug 22, 1996: STRINGER. CRACKED. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS IN FASTENER HOLES FOR STRINGER 15R TO STATION 532. CUT OUT DAMAGED AREA AND FABRICATED AND R - [SDR USAA960561](https://openairdocs.org/sdr/USAA960561), Aug 22, 1996: ANGLE. CORROSION. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 40 INCH STATION 277 TO 340 'Z' ANGLE RIGHT SIDE. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3 - [SDR USAA960560](https://openairdocs.org/sdr/USAA960560), Aug 22, 1996: BEAM. CORRODED. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS BS 420 TO BS 500, STRINGER 26R BEAM. FABRICATED AND REPLACED WITH NEW BE - [SDR USAA960559](https://openairdocs.org/sdr/USAA960559), Aug 22, 1996: STRINGER. CRACKED. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS AT FASTENER HOLES STATION 532, STRINGER 15R. REMOVED DAMAGED SECTION OF STRINGER AND PERFORM ## 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 19951216044239I](https://openairdocs.org/incident/19951216044239I), Dec 16, 1995: Boeing 737201 (N236US), Rochester, NY, Minor damage. Narrative: amended report. Aircraft struck two deer while landing on runway 22 at Rochester international airport. Aircraft was ferried to greensboro for… --- 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.