# N226US: Boeing 737-201, registration cancelled 2001-03-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 13, 2001 - 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: 21815 - Type of aircraft: Fixed wing multi engine - Certificate issued: August 15, 1996 - Last registry action: April 18, 2000 - Mode S code: A1F91E - 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/N226US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=226US - Page: https://openairdocs.org/deregistered/N226US-2001-03-13 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 737-201: https://openairdocs.org/model/boeing-737-201.md ## Service difficulty reports (30) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 99ZZZX2744](https://openairdocs.org/sdr/99ZZZX2744), Jun 30, 1999: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK RT OUTBOARD STA 344 - STA 380. - [SDR USAASB99129](https://openairdocs.org/sdr/USAASB99129), May 24, 1999: BATTERY PACK. DISCHARGED. GSO - MAINTENANCE FOUND THE AISLE SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A WIRE SPLICE AND TWO BATTERY PACKS. OPERATIONAL CHECK GOO - [SDR USAASB99103](https://openairdocs.org/sdr/USAASB99103), Apr 19, 1999: BATTERY PACK. DISCHARGED. BOS - PILOT REPORTED THAT THE AFT BATTERY PACK UNDER SEAT 16 LEFT NEEDS REPLACED DUE TO THE EMERGENCY LIGHTS ILLUMINATING DIM. MAINTENANCE REMOVED AND REPLACED - [SDR USAASB99102](https://openairdocs.org/sdr/USAASB99102), Apr 17, 1999: BATTERY PACK. DISCHARGED. EWR - MAINTENANCE FOUND SEVERAL CABIN SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS AT SEATS 5A AND 16A AND RERACKED REM - [SDR USAA990311](https://openairdocs.org/sdr/USAA990311), Apr 13, 1999: DOUBLER. CRACKED. TPA - DURING HFEC CHECK INSPECTION, FOUND A .25 INCH CRACK IN MED REPAIR DOUBLER AFT LOWER CORNER OF MAIN ENTRY DOOR CUTOUT. INSTALLED NEW DOUBLER PER EO 5391G6 - [SDR USAASB99101](https://openairdocs.org/sdr/USAASB99101), Apr 11, 1999: BATTERY PACK. DISCHARGED. TPA - MAINTENANCE FOUND THE LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT BATTERY PACKS IN - [SDR USAASB99076](https://openairdocs.org/sdr/USAASB99076), Mar 20, 1999: HOSE. RUPTURED. CLT - FLT 462 - ON CLIMB-OUT OF JAX, F/O NOTICED NR 2 ENG HYD PUMP LOW PRESSURE LIGHT ILLUMINATED. ACCOMP QUICK REF HANDBOOK PROCEDURES. APPROX 1 MIN LATE, THE - [SDR USAASB98241](https://openairdocs.org/sdr/USAASB98241), Sep 13, 1998: SENSOR. OUT OF ADJUST. ATL - FLT 496 - AFTER TAKEOFF AT APPROXIMATELY 500 FT, THE FORWARD CARGO DOOR WARNING LIGHT ILLUMINATED. FLIGHT RETURNED TO FIELD AT ATL AND LANDED WITHOUT FURT - [SDR USAA980160](https://openairdocs.org/sdr/USAA980160), Apr 12, 1998: SKIN. CRACKED. ROA - DURING C-5 CHECK, FOUND 2 INCH CRACK AT STA 740, S17R FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER PER EA 51596. (X) - [SDR USAA980159](https://openairdocs.org/sdr/USAA980159), Apr 12, 1998: SKIN. CRACKED. ROA - DURING C-5 CHECK, FOUND 1 INCH CRACK IN FUSELAGE SKIN AT LOWER HINGE CUTOUT OF AFT SERVICE DOOR. REMOVED CRACK AND INSTALLED DOUBLER PER EA 61580. (M) - [SDR USAASB98014](https://openairdocs.org/sdr/USAASB98014), Jan 17, 1998: B-NUT. LOOSE. SAV - FLT 1481 - AT FL 310, THE 'A' SYSTEM HYDRAULIC QTY SLOWLY DROPPED TO 1.2 GALLONS. CAPTAIN NOTICED THE QTY HAD BEEN SLOWLY DROPPING OVER THE LAST HOUR. THE - [SDR USAASB98004](https://openairdocs.org/sdr/USAASB98004), Jan 6, 1998: SEPARATOR BAGS. DIRTY. CLT - FLT 776 - CLIMBING THROUGH 4,000 FEET, CREW SMELLED A SMOKY ODOR THAT RESEMBLED A BURNING CANDLE SMELL IN THE COCKPIT. ODOR WAS ALSO PRESENT IN THE CABIN. - [SDR USAASB97336](https://openairdocs.org/sdr/USAASB97336), Dec 7, 1997: BATTERY PACK. DISCHARGED. ATL - MAINTENANCE FOUND THE INTERIOR AND EXTERIOR EMERGENCY LIGHTS AT THE FORWARD ENTRY AND SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE FORWARD BATT - [SDR USAASB97335](https://openairdocs.org/sdr/USAASB97335), Dec 2, 1997: POWER SUPPLY. FAILED. MCO - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTING AT ROWS 1 THROUGH 5, LEFT SIDE, INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AT SEAT ROW 5. OPS C - [SDR USAA970215](https://openairdocs.org/sdr/USAA970215), May 24, 1997: SKIN. CRACKED. INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK IN SKIN AT LOWER FORWARD CORNER OF DOOR CUTOUT AFT ENTRY DOOR BS 964. INSTALLED EXT SKIN REPAIR AND - [SDR USAA970214](https://openairdocs.org/sdr/USAA970214), May 24, 1997: SKIN. DENTED. INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND DENTS 2.5 INCH BY 3 INCH AND 1.5 INCH BY 1.5 INCH STATION 807 BETWEEN STRINGER 19L AND 20L SKIN. INSTALLED DOUBL - [SDR USAA970213](https://openairdocs.org/sdr/USAA970213), May 24, 1997: FRAME. CRACKED. INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK FORWARD CARGO FRAME BS 500 BL '0'. INSTALLED DOUBLER AND FILLER, REPAIRED PER SRM 51-40-3 FIG 1. ( - [SDR USAA970212](https://openairdocs.org/sdr/USAA970212), May 24, 1997: BEAM. CRACKED. INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BL '0' BL 660 WL 208 BEAM. INSTALLED REPAIR ANGLES, REPAIRED PER BOEING DRAWING NR 65C34537. (M) - [SDR USAA970211](https://openairdocs.org/sdr/USAA970211), May 24, 1997: SKIN. CRACKED. INT - DURING Q-2 CHECK CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 380 BETWEEN STRINGER 28L AND BL '0' SKIN. INSTALLED DOUBLER DOUBLER, REPAIRED PER TR 53-30 - [SDR USAA970210](https://openairdocs.org/sdr/USAA970210), May 24, 1997: STRINGER. CORRODED. INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORRODED AREA AFT CARGO BS 907 STRINGER 26R. INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1 SRM 53-10 - [SDR USAA970209](https://openairdocs.org/sdr/USAA970209), May 24, 1997: STRINGER. CORRODED. INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA BS 907, STRINGER 24L. INSTALLED STRINGER SPLICE, REPAIRED PER SRM 51-10-1. CORROS - [SDR USAA970208](https://openairdocs.org/sdr/USAA970208), May 24, 1997: SKIN. CORROSION. INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 4 INCHES APPROX BS 927 BETWEEN STRINGER 24L AND 25L SKIN. INSTALLED FILLER AND DOUBLER, RE - [SDR USAA970207](https://openairdocs.org/sdr/USAA970207), May 24, 1997: FRAME. CORRODED. INT - DURING Q2-CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA AFT CARGO LOWER LEG OF FRAME BS 767 STRINGER 26R-25R. INSTALLED FRAME REPAIR CONSI - [SDR USAA970206](https://openairdocs.org/sdr/USAA970206), May 24, 1997: SKIN. CRACKED. INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 INCH BY .25 INCH CRACK FORWARD LOWER CORNER AFT ENTRY DOOR SKIN. INSTALLED DOUBLER AND TRIPLER, REPAIRED PER E - [SDR USAA970205](https://openairdocs.org/sdr/USAA970205), May 24, 1997: STRINGER. CORROSION. INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 12 INCHES STATION 962 , STRINGER 27L. INSTALLED DOUBLER (SPLICE), REPAIRED PER SRM 53-10-3. CORROSION - [SDR USAASB97094](https://openairdocs.org/sdr/USAASB97094), Apr 4, 1997: GARLOCK SEAL. FAILED. BWI - FLT 1243 - FLIGHT HAD JUST LEVELED OFF AT 28,000 FEET WHEN CREW NOTICED THE NR 1 ENGINE OIL QUANTITY BEGAN TO DECREASE TOWARDS ZERO. FLIGHT DIVERTED TO BW - [SDR USAA960609](https://openairdocs.org/sdr/USAA960609), Sep 13, 1996: SKIN. CRACKED. ROA - DURING 'CX-3' CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .125 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN. REMOVED CRACK AND IN - [SDR USAASB96181](https://openairdocs.org/sdr/USAASB96181), Sep 6, 1996: AIR DISTR. ODOR. PIT - FL 553 - FLIGHT ATTENDANTS ADVISED COCKPIT CREW THAT THEY SMELLED SMOKE OR FUMES IN THE REAR OF THE AIRCRAFT. THEY DID NOT DETECT ANY SIGHT OF SMOKE. CAPT - [SDR USAASB96124](https://openairdocs.org/sdr/USAASB96124), Jul 9, 1996: FLOW CONTROL VLV. FAILED. MSP - FLT 824 - ON CLIMB-OUT ABOVE 15,000 FEET, A LOUD RUMBLING NOISE BEGAN. CREW DECIDED TO RETURN TO FIELD AT MSP. ALL AIRCRAFT INDICATORS WERE NORMAL. CREW S - [SDR USAA951331](https://openairdocs.org/sdr/USAA951331), Dec 15, 1995: STRINGER. CORRODED. ROA - DURING 'CX-2' CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED STRINGER CAUSED BY LAVATORY SPILL, STRINGER 27L AT BS 947. REMOVED CORRODED STRINGER SECTION ## 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 19890709040599I](https://openairdocs.org/incident/19890709040599I), Jul 9, 1989: Boeing 737201 (N226US), Albany, NY. Wall panel below seat hot with burning smell. Diverted to Albany. Left temperature control valve malfunctioned. --- 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.