# N237US: Boeing 737-201, registration cancelled 2000-11-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 24, 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: 22353
- Type of aircraft: Fixed wing multi engine
- Certificate issued: August 15, 1989
- Last registry action: April 18, 2000
- Mode S code: A22454
- 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/N237US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=237US
- Page: https://openairdocs.org/deregistered/N237US-2000-11-24

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 (44)

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

- [SDR USAA991026](https://openairdocs.org/sdr/USAA991026), Sep 25, 1999: STRINGER. CORRODED. TPA - DURING A CX-4 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA LOCATED UNDER STR 27R, STA 930, CORROSION LEVEL 1. REPLACED CORRODED AREA PER SRM 53-10-3 FIG
- [SDR USAA991025](https://openairdocs.org/sdr/USAA991025), Sep 25, 1999: SKIN. CRACKED. TPA - DURING A CX-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN UPPER AFT CORNER OF TOP HINGE CUT-OUT SERVICE DOOR SKIN. INSTALLED DOUBLER PER TR 52-40-0
- [SDR USAASB99045](https://openairdocs.org/sdr/USAASB99045), Feb 19, 1999: COALESCER. DIRTY. PHL - FLT 712 - FLIGHT RETURNED TO FIELD AT PHL DUE TO A SMOKE SMELL IN THE COCKPIT. THE SMELL OF SMOKE WAS PRESENT AND TO WORSE ON TAKEOFF ROLL. CAPTAIN DECIDE
- [SDR USAASB98250](https://openairdocs.org/sdr/USAASB98250), Sep 22, 1998: BATTERY PACK. DISCHARGED. CMH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS AT THE AFT SERVICE DOORS DIM. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT M572. OPERATIONAL CHECK GOO
- [SDR USAASB97347](https://openairdocs.org/sdr/USAASB97347), Dec 23, 1997: WINDOW. CRACKED. CLT 851 - EN ROUTE PIT-BHM - WHEN AT FL3100, F/O'S NR 1 WINDOW SHATTERED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED F/O'S
- [SDR USAASB97068](https://openairdocs.org/sdr/USAASB97068), Mar 2, 1997: BATTERY PACK. DISCHARGED. PIT - MAINTENANCE FOUND THE LEFT INTERIOR OVERWING EMERGENCY EXIT LIGHT ON SIDEWALL PANEL INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOO
- [SDR USAASB97061](https://openairdocs.org/sdr/USAASB97061), Feb 22, 1997: POWER SUPPLY. FAILED. PHL - MAINTENANCE FOUND THE LEFT INTERIOR AND EXTERIOR OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE M192 POWER SUPPLY. OPS CHECK GOOD. (
- [SDR USAA960753](https://openairdocs.org/sdr/USAA960753), Nov 21, 1996: DOUBLER. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK SKIN DOUBLER BS 377.5 TO BS 379 LBL 3 WL 148.5. FABRICATED AND INSTALLED NEW DOUBLER, REPAIRED PE
- [SDR USAA960752](https://openairdocs.org/sdr/USAA960752), Nov 21, 1996: SKIN. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK WL 148.5 LBL 4, BS 279 SKIN. INSTALLED EXT DOUBELR WT ADDED 9.4 LBS AT BS 279, REPAIRED PER TR 5
- [SDR USAA960751](https://openairdocs.org/sdr/USAA960751), Nov 21, 1996: WEB. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK BS 708 STRINGER 18R, SHEAR BEAM WEB. INSTALLED REPAIR KIT, REPAIRED PER EO NR 5393G256 AND BOEING
- [SDR USAA960750](https://openairdocs.org/sdr/USAA960750), Nov 21, 1996: CHORD. CRACKED. INT - DURING Q-3 CHECK NDT INSPECTION, FOUND .25 INCH CRACK INBOARD AT FORWARD OUTBOARD HOE AT INTERSECTION OF STRINGER 18 A OUTBOARD STRAP AND BS 727 CHORD (RI
- [SDR USAA960749](https://openairdocs.org/sdr/USAA960749), Nov 21, 1996: SKIN. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK IN SKIN STATION 1156, LBL 12. INSTALLED DOUBLER (REPLACED DOUBLER), REPAIRED PER SRM 53-30-3, FIG 6
- [SDR USAA960748](https://openairdocs.org/sdr/USAA960748), Nov 21, 1996: SKIN. CORROSION. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA BS 967 BETWEEN STRINGER 27L AND STRINGER 27R SKIN. INSTALLED DOUBLER, REPAIRED PE
- [SDR USAA960747](https://openairdocs.org/sdr/USAA960747), Nov 21, 1996: BULKHEAD. CORROSION. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA AT BULKHEAD BS 1023 RBL 1 INCH WL 195. INSTALLED EXT REPAIR, REPAIRED PER SRM 53
- [SDR USAA960746](https://openairdocs.org/sdr/USAA960746), Nov 21, 1996: SPLICE. CORROSION. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA STRINGER SPLICE BS 362 TO 363, STRINGER 27L. INSTALLED NEW SPLICE WITH 2 ADDITIO
- [SDR USAA960745](https://openairdocs.org/sdr/USAA960745), Nov 21, 1996: CHORD. CRACK. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK INDICATION INSIDE FORWARD UPPER FASTENER HOLE OUTSIDE CHORD BS 727, STRINGER 18 A STRAP. INSTALLE
- [SDR USAA960744](https://openairdocs.org/sdr/USAA960744), Nov 21, 1996: FRAME. CORROSION. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION AT FRAME, BS 967. INSTALLED REPAIR ANGLE, REPAIRED PER SRM 53-10-4. CORROSION TASK NR
- [SDR USAA960743](https://openairdocs.org/sdr/USAA960743), Nov 21, 1996: STRINGER. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 5 INCH CORRODED AREA STRINGER 27R, BS 373 TO BS 378 (STRINGER). INSTALLED STRINGER REPAIR AND REPAIRED
- [SDR USAASB96230](https://openairdocs.org/sdr/USAASB96230), Nov 18, 1996: STATIC LINE. DISCONNECTED. MYR - FL 8033 - ON T/O AT INT, BOTH THE CAPTAINS AND F/O ALTIMETERS FROZE AT 1,200 FT ANT TRIPPED TO STANDBY. TRIED BOTH STANDBY STATIC SOURCES WITH NO RECOVERY
- [SDR USAASB96087](https://openairdocs.org/sdr/USAASB96087), May 9, 1996: LIGHT EMERGENCY. FAILED. FLT 916 - PHL - COCKPIT EMERGENCY LIGHT INOP. MX REPLACED COCKPIT EMERGENCY LIGHT ASSY. OPS CHECK SATISFACTORY. (M)
- [SDR USAA960191](https://openairdocs.org/sdr/USAA960191), Jan 30, 1996: SKIN. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK SKIN BS 347 AT STRINGER 17L. INSTALLED DOUBLERS. REPAIRED PER EO 5391G-694. (M)
- [SDR USAA960190](https://openairdocs.org/sdr/USAA960190), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK TIE CLIP, STRINGER 3R, BS 727. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960189](https://openairdocs.org/sdr/USAA960189), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK IN EACH OF 2 CLIPS BS 767 AT STRINGER 5L AND STRINGER 10L, STRINGER TIE CLIPS. REPAIRED PER EO 539
- [SDR USAA960188](https://openairdocs.org/sdr/USAA960188), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 685 STRINGER 3 RIGHT STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-353
- [SDR USAA960187](https://openairdocs.org/sdr/USAA960187), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK IN EACH OF 2 CLIPS, BS 727B AT STRINGER 2L AND STRINGER 7L, STRINGER TIE CLIPS. REPAIRED PER EO 53
- [SDR USAA960186](https://openairdocs.org/sdr/USAA960186), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK BS 767 AT STRINGER 10 RIGHT, STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-3535
- [SDR USAA960185](https://openairdocs.org/sdr/USAA960185), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK BS 767 AT STRINGER 6 RIGHT STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-
- [SDR USAA960184](https://openairdocs.org/sdr/USAA960184), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 747 STRINGER 5 RIGHT, STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35
- [SDR USAA960183](https://openairdocs.org/sdr/USAA960183), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 578 AT STRINGER 3 LEFT STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-3
- [SDR USAA960182](https://openairdocs.org/sdr/USAA960182), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK IN 2 STRINGER TIE CLIPS BS 616 AT STRINGER 2L AND STRINGER 4L. REPAIRED PER EO 5393G227. MOD
- [SDR USAA960181](https://openairdocs.org/sdr/USAA960181), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STATION 639 STRINGERS 4L, 6L. REPAIRED PER EO 5393G227. MODIFIED PART NR 6
- [SDR USAA960180](https://openairdocs.org/sdr/USAA960180), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STATION 685, STRINGER 2L AND STRINGER 5L. REPAIRED PER EO 5393G227. MODIFI
- [SDR USAA960179](https://openairdocs.org/sdr/USAA960179), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 706, STRINGER 10L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-
- [SDR USAA960178](https://openairdocs.org/sdr/USAA960178), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STATION 727 A STRINGERS 3L, STRINGER 4L, STRINGER 5L. REPAIRED PER EO 5393
- [SDR USAA960177](https://openairdocs.org/sdr/USAA960177), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 747 STRINGER 7L AND STRINGER 10L. REPAIRED PER EO 5393G227. MODIFIED PA
- [SDR USAA960176](https://openairdocs.org/sdr/USAA960176), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 787 STRINGER 10L. REPAIRED PER EO 5353G227. MODIFIED PART NR 69-35352-1
- [SDR USAA960175](https://openairdocs.org/sdr/USAA960175), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 827 STRINGER 5 LEFT. REPAIRED PER EO 5393G227. MODIFIED PER NR 69-35352
- [SDR USAA960173](https://openairdocs.org/sdr/USAA960173), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 578 STRINGER 3 RIGHT. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-353
- [SDR USAA960172](https://openairdocs.org/sdr/USAA960172), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 639 STRINGER 4 RIGHT. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-353
- [SDR USAA960171](https://openairdocs.org/sdr/USAA960171), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT STRINGER TIE CLIP BS 727A STRINGER 4 RIGHT. REPAIRED PER EO 5393G227. MODIFIED PART NR 69
- [SDR USAA960170](https://openairdocs.org/sdr/USAA960170), Jan 30, 1996: TIE CLIP. CRACKED. INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 727 B S-1, STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR INSTALLED 69-353
- [SDR USAA951428](https://openairdocs.org/sdr/USAA951428), Dec 30, 1995: SKIN. CRACKED. ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK SHEET METAL AT LOWER CORNER MED. INSTALLED INTERIM REPAIR PER EA 31854 AND TBC. REPAIRED PER EA
- [SDR USAA950927](https://openairdocs.org/sdr/USAA950927), Jul 28, 1995: STRINGER. CORRODED. ROA - DURING 'BX CHECK' VISUAL INSPECTION, FOUND 13 .125 INCH LONG STRINGER CORRODED FUSELAGE STATION 967 JUST TO THE LEFT OF WATER TANK. REMOVED CORRODED STRIN
- [SDR USAA950029](https://openairdocs.org/sdr/USAA950029), Jan 15, 1995: EEL. INOPERATIVE. PHL - COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY. (Z)

## FAA accident and incident reports (4)

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 19970413008589I](https://openairdocs.org/incident/19970413008589I), Apr 13, 1997: Boeing 737201 (N237US), Syracuse, NY. Narrative: on April 13, 1997 at 0950 EST local time, a Boeing 737-200, N237US, s/n 22353, registered to us airways, inc., landed on runway 28 in Syracuse, NY…
- [Incident 19961118041829I](https://openairdocs.org/incident/19961118041829I), Nov 18, 1996: Boeing 737201 (N237US), Myrtle Beach, SC. Maintenance check flight. Altimeter froze at FL120. Then operated on desent. Static lines off. Failed prior check.
- [Incident 19921011046099I](https://openairdocs.org/incident/19921011046099I), Oct 11, 1992: Boeing 737201 (N237US), Atlanta, GA. Oil filter light on. Shut engine down. Diverted to Atlanta. Changed NR1 engine oil system.
- [Incident 19890214009409I](https://openairdocs.org/incident/19890214009409I), Feb 14, 1989: Boeing 737201 (N237US), Houston, TX. Aircraft hit seagulls at rotation. Returned and landed safely. No damage found. Bird hit engine and top of radome.

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