# N228US: Boeing 737-201, registration cancelled 2001-01-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 31, 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: 21817
- Type of aircraft: Fixed wing multi engine
- Certificate issued: August 16, 1996
- Last registry action: April 18, 2000
- Mode S code: A2008C
- 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/N228US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=228US
- Page: https://openairdocs.org/deregistered/N228US-2001-01-31

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 (36)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR USAA001205](https://openairdocs.org/sdr/USAA001205), Aug 7, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .75 INCH, LEFT FUSE EXT SKIN STATION 766, STRINGER 18L. INSTALLED DOUBLER PER EA 67770. (M)
- [SDR USAA000833](https://openairdocs.org/sdr/USAA000833), Jun 13, 2000: SKIN. CRACKED. TPA - FOUND DOOR EXT SKIN CRACKED 1.75 INCH, AFT ENTRY DOOR FWD LOWER CORNER. INSTALLED DOUBLER PER SRM 52-10-1. (M)
- [SDR USAASB00144](https://openairdocs.org/sdr/USAASB00144), May 17, 2000: CONNECTOR. DIRTY. CLT - WHILE A/C WAS ON THE GROUND, PILOT REPORTED THE EMERGENCY EXIT LIGHTS ILLUMINATED MOMENTARILY AND EXTINGUISHED ON THEIR OWN. HOWEVER, DURING FLT, THE EMER
- [SDR USAA000309](https://openairdocs.org/sdr/USAA000309), Mar 6, 2000: SKIN. CRACKED. CLT - FOUND TWO CRACKS, 3.5 INCH AND 1 INCH, LT FUSE EXT STATION 759-763 AND STATION 780-781 STRINGER 17L. REPAIRED PER EA 66792. (M)
- [SDR USAASB00007](https://openairdocs.org/sdr/USAASB00007), Jan 8, 2000: BULB. FAULTY. PHL - FLT 1223 - DURING DESCENT INTO PHL, BOTH MASTER CAUTION FIRE WARNING LIGHTS ILLUMINATED FOR APPROXIMATELY FIVE SECONDS. NO OTHER LIGHTS OR BELLS WERE NOTE
- [SDR USAA991383](https://openairdocs.org/sdr/USAA991383), Nov 24, 1999: SKIN. CRACKED. TPA - DURING CX-3 CHECK, FOUND 2 INCH CRACK IN FUSELAGE SKIN AT STATION 727A PLUS 8 AT STRINGER 18R. INSTALLED REPAIR DOUBLER PER SRM, DOUBLE MADE FROM 2024-T3 
- [SDR USAASB99110](https://openairdocs.org/sdr/USAASB99110), Apr 26, 1999: POWER SUPPLY. INOPERATIVE. CLE - MAINTENANCE FOUND THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. ALSO, FOUND THE INTERIOR LOWER EXIT SIGNS INOPERA
- [SDR 99ZZZM358](https://openairdocs.org/sdr/99ZZZM358), Apr 26, 1999: BATTERY PACK. DISCHARGED. CLE - MAINTENANCE FOUND THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. ALSO, FOUND THE INTERIOR LOWER EXIT SIGNS INOPERA
- [SDR USAA980625](https://openairdocs.org/sdr/USAA980625), Dec 2, 1998: SKIN. CRACKED. TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 1.1 INCH CRACK IN EXTERNAL SKIN .5 INCH ABOVE STRINGER 18R AT STATION 754 SKIN. INSTALLED DOUBLER PER SRM 53-
- [SDR USAA980404](https://openairdocs.org/sdr/USAA980404), Sep 12, 1998: SKIN. CRACKED. CLT - DURING RON CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK OUT OF FORWARD EDGE OF EQUIPMENT COOLING DUCT CUT OUT STA 368 ON SKIN. INSTALLED DOUBLER PER TR
- [SDR USAA980403](https://openairdocs.org/sdr/USAA980403), Sep 12, 1998: SKIN. CRACKED. CLT - DURING RON CHECK VISUAL INSPECTION VERIFIED BY EDDY CURRENT, FOUND APPROXIMATELY .75 INCH CRACK FUSELAGE SKIN STA 727A JUST ABOVE STR 16R. CUT OUT DAMAGED
- [SDR USAASB98001](https://openairdocs.org/sdr/USAASB98001), Jan 2, 1998: BATTERY. FAILED. ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE AFT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPS CHECK GOOD. (M)
- [SDR USAA970364](https://openairdocs.org/sdr/USAA970364), Dec 7, 1997: FLOORBEAM. CORRODED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM UPPER CHORD BS 947 LBL 41 TO LBL 48. INSTALLED BEAM SPLICE, REPAIRED EPR TR 53-10-05C. CO
- [SDR USAA970363](https://openairdocs.org/sdr/USAA970363), Dec 7, 1997: WEB. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK IN CREASE BEAM WEB BS 637 LBL 71, WL 208. INSTALLED NEW WEB PER SRM 51-10-1. (M)
- [SDR USAA970362](https://openairdocs.org/sdr/USAA970362), Dec 7, 1997: FRAME. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK BS 360 2 INCH ABOVE STRINGER 20R FRAME. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-2 AND SRM 51-40-3
- [SDR USAA970361](https://openairdocs.org/sdr/USAA970361), Dec 7, 1997: STRINGER. CORRODED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA BS 370 STRINGER 27R ON SIDE OF STRINGER. INSTALLED STRINGER REPAIR, REPAIRED PER 
- [SDR USAA970360](https://openairdocs.org/sdr/USAA970360), Dec 7, 1997: SKIN. CORRODED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND BULGE IN 2 PLACES LOWER FUSELAGE SKIN BS 727 PLUS 16 INCHES, 6 INCHES LBL AND 6 INCHES RBL. INSTALLED DOUBLER, R
- [SDR USAA970359](https://openairdocs.org/sdr/USAA970359), Dec 7, 1997: FRAME. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK BS 328 FRAME 2 INCH BELOW STRINGER 20R. INSTALLED DOUBLER AND FILLER, REPAIRED PER SRM 51-40-2. (M)
- [SDR USAA970358](https://openairdocs.org/sdr/USAA970358), Dec 7, 1997: FLOORBEAM. CORRODED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 22 INCH BY 1 INCH STATION 259, LBL 11 TO RBL 11 FLOORBEAM. INSTALLED DOUBLER, REPAIRED PER TR 53-10-16
- [SDR USAA970245](https://openairdocs.org/sdr/USAA970245), Jul 31, 1997: SKIN. CRACKED. ROA - DURING CX-6 CHECK VISUAL INSPECTION, FUOND 1.75 INCH CRACK BS 792 STRINGER 18L FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-
- [SDR USAA970244](https://openairdocs.org/sdr/USAA970244), Jul 31, 1997: SKIN. CRACKED. ROA - DURING CX-6 VISUAL/EDDY CURRENT INSPECTION, FOUND 1.25 INCH CRACK BS 747 STRINGER 18L FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER PER SRM 53-30-3 F
- [SDR USAA970243](https://openairdocs.org/sdr/USAA970243), Jul 31, 1997: SKIN. CRACKED. ROA - DURING CX-6 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .75 INCH CRACK AND .25 INCH CRACK BS 727A PLUS 8 INCHES STRINGER 18L FUSELAGE SKIN. INSTALLED DOUB
- [SDR USAASB97017](https://openairdocs.org/sdr/USAASB97017), Jan 15, 1997: HEAT MANIFOLD. FAILED. TPA - FL 232, FLIGHT WAS CLIMBING THRU 12,000 FT WHEN THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CAPT RETARDED THROTTLE AND THE LGIHT WENT OUT. ADVANCED THROTT
- [SDR 97ZZZM223](https://openairdocs.org/sdr/97ZZZM223), Jan 15, 1997: ANTI-ICE TUBE. FAILED. TPA - FL 232, FLIGHT WAS CLIMBING THRU 12,000 FT WHEN THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CAPT RETARDED THROTTLE AND THE LGIHT WENT OUT. ADVANCED THROTT
- [SDR USAASB96225](https://openairdocs.org/sdr/USAASB96225), Nov 8, 1996: CONNECTOR. LOOSE. RSW - FL 1429 - ON APPROACH TO RSW, CREW RECEIVED THE FIRE WARNING FOR THE NR 2 ENGINE. CREW SHUT DOWN ENGINE AND FIRED BOTH BOTTLES. FLIGHT LANDED AT RSW WITH 
- [SDR USAA960688](https://openairdocs.org/sdr/USAA960688), Oct 21, 1996: SKIN. CRACKED. ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 1.375 INCH CRACK AFT GALLEY DOOR CUT OUT FORWARD LOWER CORNER (STRINGER 17 R BS 857) FUSELAGE SKIN. INSTALLED T
- [SDR USAA960687](https://openairdocs.org/sdr/USAA960687), Oct 21, 1996: SKIN. CRACKED. ROA - DURING CX-5 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2 CRACKS 3.1875 INCH AND .5 INCH FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER (STRINGER 17R BS 328
- [SDR USAA960468](https://openairdocs.org/sdr/USAA960468), Jun 1, 1996: STRINGER. CORROSION. ROA - DURING 'BX TRANSIT' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION STRINGER 27L BS 986.5. INSTALLED DOUBLER AND STRINGER, REPAIRED PER SRM 53-1
- [SDR USAA960467](https://openairdocs.org/sdr/USAA960467), Jun 1, 1996: SKIN. CRACKED. ROA - DURING 'TRANSIT CHECK' VISUAL INSPECTION VERIFIED WITH HFEC, FOUND TWO .75 INCH CRACK IN FUSELAGE SKIN JUST ABOVE STRINGER 18L, FORWARD OF BS 787. INSTALL
- [SDR USAA960014](https://openairdocs.org/sdr/USAA960014), Jan 4, 1996: SHEAR BEAM. CRACKED. ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK STRINGER 18A LEFT SHEAR BEAM WEB AT BS 706. INSTALLED DOUBLER. REPAIRED PER EO 5393G259 REV 'A'
- [SDR USAA960013](https://openairdocs.org/sdr/USAA960013), Jan 4, 1996: SHEAR BEAM. CRACKED. ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND ONE .375 INCH CRACK STRINGER 18A LEFT SHEAR BEAM AT BS 727. INSTALLED DOUBLER. REPAIRED PER EO 5393G256 REV 'A'
- [SDR USAA951334](https://openairdocs.org/sdr/USAA951334), Dec 15, 1995: SKIN. DELAMINATION. INT - DURING 'TRANSIT CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 727-908 BETWEEN STRINGER 10 AND 14 RHS, ON FUSELAGE SKIN. REPLACED UPPE
- [SDR USAA951333](https://openairdocs.org/sdr/USAA951333), Dec 15, 1995: SKIN. DELAMINATION. INT - DURING 'TRANS CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 727-908 BETWEEN STRINGER 10 AND 14 LHS, ON FUSELAGE SKIN. REPLACED UPPER 
- [SDR USAA951332](https://openairdocs.org/sdr/USAA951332), Dec 15, 1995: SKIN. DELAMINATION. INT - DURING 'TRANS CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 360-540 BETWEEN STRINGER 10 AND 14 LHS, ON FUSELAGE SKIN. REPLACED UPPER 
- [SDR USAA950614](https://openairdocs.org/sdr/USAA950614), Jun 19, 1995: STRAP. LOOSE. EWR - FLT 371 - LOUD BANGING NOISE ON CLIMB-OUT. WARNING STRAP CAUGHT IN FORWARD GALLEY SERVICE DOOR. FLIGHT RETURNED TO EWR WHERE LANDING WAS WITHOUT FURTHER I
- [SDR USAA950596](https://openairdocs.org/sdr/USAA950596), Jun 4, 1995: R/T UNIT. FAILED. CLT - FLT 97 - FLIGHT EN ROUTE PIT TO MIA WHEN RADAR QUIT WORKING. FLIGHT DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENACNE REPLACED 

## Other aircraft with N228US

- [Registered now](https://openairdocs.org/aircraft/N228US): Diamond Aircraft Ind DA 42, S/N 42.347, built 2008

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