# N373US: 1985 Boeing 737-3B7, registration cancelled 2006-07-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 3, 2006 - Exported to: Indonesia - Status when cancelled: Valid registration - Airframe: [Boeing 737-3B7](https://openairdocs.org/model/boeing-737-3b7) (registry code 138447F) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 22952 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 11, 1985 - Certificate issued: June 13, 2006 - Last registry action: June 13, 2006 - Mode S code: A440C3 - Owner when cancelled: [Wells Fargo Bank Northwest Na (Trustee)](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20(TRUSTEE)) - 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/N373US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=373US - Page: https://openairdocs.org/deregistered/N373US-2006-07-03 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 737-3B7: https://openairdocs.org/model/boeing-737-3b7.md ## Service difficulty reports (67, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA200511006](https://openairdocs.org/sdr/USAA200511006), Nov 15, 2005: SKIN. CRACKED. A 2 INCH CRACK IN FUSELAGE SKIN AT STA 892, 6 INCH BELOW STR 24R. INSTALLED REPAIR DOUBLERS PER SRM 53-00-01 FIG 201. - [SDR SAA200511006](https://openairdocs.org/sdr/SAA200511006), Nov 15, 2005: SKIN. CRACKED. A 2 INCH CRACK IN FUSELAGE SKIN AT STA 892, 6 INCHES BELOW STR 24R. INSTALLED REPAIR DOUBLERS PER SRM 53-00-01 FIG 201. - [SDR USAA050675](https://openairdocs.org/sdr/USAA050675), May 22, 2005: SKIN. GOUGED. CLT - FOUND FLAP SKIN GOUGED 1 INCH BY .5 INCH, TOP SKIN OF RIGHT OUTBOARD FOREFLAP. COMPOSITE REPAIR IAW 737-3 SRM 57-53-02 DETAIL XV, TABLE VI. (M) - [SDR USAA050668](https://openairdocs.org/sdr/USAA050668), May 20, 2005: SKIN. DEBONDED. CLT - FOUND ELEVATOR SKIN DISBOND 1 INCH, LEFT ELEVATOR LOWER SURFACE 6.2 INCHES FROM THE OUTBOARD EDGE. COMPOSITE REPAIR IAW SRM 51-70-17. (M) - [SDR USAA050667](https://openairdocs.org/sdr/USAA050667), May 20, 2005: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .750 INCH, STATION 330, STRINGER 17R. FABRICATED AND INSTALLED SKIN DOUBLERS PER SRM 53-10-01. (M) - [SDR SB0534](https://openairdocs.org/sdr/SB0534), Mar 3, 2005: SOCKET. INOPERATIVE. MCO - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 12ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET AT SEAT 12ABC. OPERATIONAL CHECK GOO - [SDR SB05035](https://openairdocs.org/sdr/SB05035), Mar 3, 2005: SOCKET. INOPERATIVE. MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 12ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET AT SEAT 12ABC. OPERATIONAL CHECK GOOD. - [SDR USAA040112](https://openairdocs.org/sdr/USAA040112), Apr 5, 2004: SKIN. CRACKED. FOUND SKIN CRACKED .600 INCH LONG, S-23L AT FS 744. REPAIR DOUBLER INSTALLED PER SRM 53-00-01, FIG 229. (M) - [SDR USAA040113](https://openairdocs.org/sdr/USAA040113), Apr 5, 2004: SKIN. CRACKED. FOUND SKIN CRACKED 1.250 INCH LONG, 3 INCHES FORWARD OF FS 727E ADJACENT TO S-24L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) - [SDR USAA040107](https://openairdocs.org/sdr/USAA040107), Apr 5, 2004: SKIN. CRACKED. FOUND SKIN CRACKED 1.250 INCH LONG, INSTALLED DOUBLER PER SRM. 53-00-01, FIG 229. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) - [SDR USAA040111](https://openairdocs.org/sdr/USAA040111), Apr 4, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .600 INCH LONG, S22R 12 INCHES AFT OF FS 727D. INSTALLED DOUBLER PER SRM 53-00-01. (M) - [SDR USAA040110](https://openairdocs.org/sdr/USAA040110), Apr 3, 2004: SKIN. CRACKED. FOUND SKIN CRACKED 1.450 INCH LONG, FS 891 ADJACENT OT S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M) - [SDR USAA030223](https://openairdocs.org/sdr/USAA030223), Nov 11, 2003: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 2.5 INCHES STATION 765 ABOVE STRINGER 19R. CRACK CUT OUT AND DOUBLER INSTALLED PER SRM 53-00-01. (M) - [SDR USAA030204](https://openairdocs.org/sdr/USAA030204), Sep 26, 2003: SKIN. CRACKED. PIT - FOUND SKIN CRACKED .25 INCH, AFT SERVICE DOOR UPPER HINGE STATION 951. INSTALLED DOUBLER PER SRM 53-60-01 FIG 205. (M) - [SDR USAASB03115](https://openairdocs.org/sdr/USAASB03115), Jul 19, 2003: CLAMP. LOOSE. ON CLIMB-OUT FROM PIT, AT FL170, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED WHEN THROTTLE WAS RETARDED. FLIGHT RETURNED TO FIELD AT PIT AND - [SDR USAASB03102](https://openairdocs.org/sdr/USAASB03102), Jul 5, 2003: CHARGER. INOPERATIVE. PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT AISLE LIGHTS AT SEAT ROWS 12 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, P/N 201301 - [SDR USAASB03072](https://openairdocs.org/sdr/USAASB03072), May 31, 2003: LIGHT. INOPERATIVE. PILOT REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 12C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) - [SDR USAA020464](https://openairdocs.org/sdr/USAA020464), Nov 21, 2002: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 2 INCHES, RIGHT SIDE STATION 727E STRINGER 24 RT. CUTOUT DAMAGE, INSTALLED DOUBLER AND FILLER PER SRM 53-00-01 FIG 225. (M) - [SDR USAASB02162](https://openairdocs.org/sdr/USAASB02162), Aug 27, 2002: SOCKET. SHORTED. GSO - MAINTENANCE FOUND THE BULLNOSE EMERGENCY LIGHTS AT SEAT ROWS 12, 16 AND 20 INOPERATIVE. MAINTENANCE FOUND THE LIGHT SOCKET AT SEAT ROW 16 SHORTED. REPAIRE - [SDR USAA020327](https://openairdocs.org/sdr/USAA020327), Aug 14, 2002: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 3.5 INCH, S25R BETWEEN STATION 727E AND 747. INSTALLED DOUBLER PER SRM 53-00-01 FIG 2. (M) - [SDR USAA020252](https://openairdocs.org/sdr/USAA020252), Jun 18, 2002: BULKHEAD. CORRODED. PIT - FOUND Y-CHORD AND BULKHEAD CORRODED, BS 1016 AFT PRESSURE BULKHEAD AT FLOOR LINE CENTER. CORROSION LEVEL 2, REMOVED CORROSION AND INSTALLED DOUBLERS PER E - [SDR USAA020210](https://openairdocs.org/sdr/USAA020210), Jun 5, 2002: STIFFENER. CORRODED. PIT - FOUND STIFFENER CORRODED 3 INCH BY 3 INCH AREA, AFT PRESS BULKHEAD STIFFENER BS 1018 BL 00. INSTALLED DOUBLER, SPLICED SECTION OF STIFFENER PER BOEING DRA - [SDR USAA020209](https://openairdocs.org/sdr/USAA020209), Jun 5, 2002: BULKHEAD. CORRODED. PIT - FOUND CHORDS AND WEBS CORRODED 5 INCH BY 6 INCH AREA, FORWARD SIDE AFT PRESSURE BULKHEAD BS 1018 BL 00 4 INCH BY 5 INCH. CORROSION LEVEL 2. BULKHEAD WEB A - [SDR USAA020208](https://openairdocs.org/sdr/USAA020208), Jun 4, 2002: BULKHEAD. CRACKED. PIT - FOUND SKIN CRACKED 1.125 INCH BY 6.625 INCH CRACK, BETWEEN STRINGER 16 AND 17 OUTERSKIN STATION 178. DOUBLER INSTALLED PER EO 5300V157. (M) - [SDR USAA020207](https://openairdocs.org/sdr/USAA020207), Jun 4, 2002: BULKHEAD. CRACKED. PIT - FOUND SKIN CRACKED 7.875 INCH BY 6.75 INCH, BETWEEN STRINGER 16/17, OUTER SKIN STATION 178. DOUBLER INSTALLED PER EO 5300V157. (M) - [SDR USAA020224](https://openairdocs.org/sdr/USAA020224), May 31, 2002: FLOOR SUPPORT. CORRODED. PIT - FOUND SUPPORT CORRODED ENTIRE SURFACE, DIAGONAL FLOOR SUPPORT RBBL 12, STATION 987-1016. FOUND DEFECTIVE PART REPLACED WITH IDENT PART NR. CORRODED LEVEL - [SDR USAA020254](https://openairdocs.org/sdr/USAA020254), May 30, 2002: CLIP. CORRODED. PIT - FOUND CLIP CORRODED, STATION 727E BETWEEN S26R AND S27R. DOUBLER TREATED PER SRM 53-00-07 PAGES 210-212. (M) - [SDR USAA020260](https://openairdocs.org/sdr/USAA020260), May 18, 2002: STRINGER. CRACKED. PIT - FOUND STRINGER CRACKED .25 INCH, STATION 663 STRINGER 2R. INSTALLED DOUBLERS PER SRM 53-00-07 FIG 209. (M) - [SDR USAA020259](https://openairdocs.org/sdr/USAA020259), May 15, 2002: INTERCOSTAL. CRACKED. PIT - FOUND INTERCOSTAL CRACKED 1 INCH, UPPER AFT FLANGE INTERCOSTAL BL 0 STATION 294.5-312. INSTALLED NEW INTERCOSTAL PER SRM 51-10-02. (M) - [SDR USAA020205](https://openairdocs.org/sdr/USAA020205), May 15, 2002: INTERCOSTAL. CRACKED. PIT - FOUND INTERCOSTAL CRACKED 1.5 INCH, JUST ABOVE AFT ENTRANCE DOOR BS 967. INSTALLED NEW ATTACH ANGLE. (M) - [SDR USAA020261](https://openairdocs.org/sdr/USAA020261), May 14, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED TWO PLACES .125 INCH AND .25 INCH, STATION 380 BETWEEN S8R AND S9R. INSTALLED DOUBLER PER SRM 53-00-07. (M) - [SDR USAA020256](https://openairdocs.org/sdr/USAA020256), May 14, 2002: SEAT TRACK. CORRODED. PIT - FOUND LEFT INBOARD SEAT TRACK, STATION 827-945 LBBL 24. CORROSION LEVEL 2. SPLICED IN SECTION OF TRACK PER SRM 53-00-52. (M) - [SDR USAA020204](https://openairdocs.org/sdr/USAA020204), May 10, 2002: KEELBEAM. CORRODED. PIT - FOUND KEEL BEAM CORRODED 3 INCHES BY 1 INCH CORRODED, 13.5.546 STRINGER 28L. CORROSION LEVEL 2, TASK NR C53-212-01. REMOVED DAMAGED AREA, INSTALLED NEW SE - [SDR USAA020253](https://openairdocs.org/sdr/USAA020253), May 8, 2002: CREASE BEAM. CORRODED. PIT - FOUND CREASE BEAM CORRODED, STATION 277-360. DEFECTIVE PART REPLACED WITH IDENT PART. (M) - [SDR USAA020175](https://openairdocs.org/sdr/USAA020175), May 6, 2002: SKIN. CRACKED. PIT - FOUND SKIN CRACKED IN 13 SMALL CONTINUOUS PLACES, RIGHT WING, NR 6 SLAT, LOWER SURFACE SLAT STATION 299.10-314. REMOVED DAMAGED SKIN PER SRM 57-43-01. (M) - [SDR USAA020257](https://openairdocs.org/sdr/USAA020257), May 4, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .25 INCH, STATION 767 BETWEEN S8L AND S9L AT PSU SUPPORT BRACKET. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14A. (M) - [SDR USAA020258](https://openairdocs.org/sdr/USAA020258), May 2, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .25 INCH, STATION 480 BETWEEN S8R AND S9R. CUT OUT CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14A. (M) - [SDR USAA020176](https://openairdocs.org/sdr/USAA020176), May 2, 2002: FRAME. CRACKED. PIT - FOUND Z-FRAME CRACKED .25 INCH, STATION 807 BETWEEN S8R AND S9R. CUT OUT CRACKED, INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14A. (M) - [SDR USAA020255](https://openairdocs.org/sdr/USAA020255), May 1, 2002: FLOOR SUPPORT. CORRODED. IT - FOUND FLOOR SUPPORT CORRODED, STATION 727-787 AND 787-827 ABOVE S25L. SPLICED IN NEW SECTION PER SRM 53-60-53. (M) - [SDR USAA020174](https://openairdocs.org/sdr/USAA020174), Apr 29, 2002: ARM. CORRODED. PIT - FOUND RUDDER BALANCE ARM WITH CORROSION 3 INCH BY 12 INCH AREA, RUDDER BALANCE ARM STRUCTURE. CORROSION LEVEL 2. RUDDER REPLACED AND INSTALLED PER JOB CAR - [SDR USAA020173](https://openairdocs.org/sdr/USAA020173), Apr 18, 2002: ANGLE. CRACKED. PIT - FOUND DRAG ANGLE CRACKED .5 INCH, SECTION 48, RIGHT SIDE, AFT OF AFT LUGS FOR VERTICAL STABILIZER. FILLERS AND STRAPS INSTALLED ON BOTH SIDES OF DRAG ANGL - [SDR USAA020206](https://openairdocs.org/sdr/USAA020206), Apr 17, 2002: ANGLE. CRACKED. PIT - FOUND DRAG ANGLE CRACKED .25 INCH, SECT 48 DRAG ANGLE LIGHT SIDE 10 INCH BEHIND ATTACH LUG. REPAIRED FILLER AND STRAPS ON OUTSIDE AND INSIDE OF DRAG ANGLE - [SDR USAASB01175](https://openairdocs.org/sdr/USAASB01175), Jun 15, 2001: FUEL CELL. LEAKING. CLT - FLT 1290 - AFTER TAKEOFF, FUEL WAS REPORTED STREAMING OUT OF THE LEFT WING BY AN AMERICAN FLIGHT BEHIND AND WAS ALSO CONFIRMED BY THE CLT TOWER. AN EMERGE - [SDR USAASB01116](https://openairdocs.org/sdr/USAASB01116), Apr 27, 2001: CHARGER. FAILED. PHL - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS AT ROWS 1 THROUGH 4 INOPERATIVE AND THE EMERGENCY LIGHTS AT THE FORWARD ENTRY AND SERVICE DOORS INOPERATI - [SDR USAASB1017](https://openairdocs.org/sdr/USAASB1017), Jan 22, 2001: THROTTLE CABLE. FAILED. EWR - FLT 1024 - EN ROUTE FROM DCA TO ALB, THE NR 2 THRUST LEVER STUCK AT CLIMB POWER. CREW DISENGAGED AUTO THROTTLES BUT WAS STILL UNABLE TO RETARD THRUST LEVE - [SDR USAASB00274](https://openairdocs.org/sdr/USAASB00274), Sep 25, 2000: SWIVEL. BROKEN. BOS - FLT 1090 - EN ROUTE FROM PHL TO BOS, FLT LOST A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE. MX CONTROL ADVISED THAT FLIGHT SHOULD PROCEED TO ORIGIN OR DESTINA - [SDR USAA001319](https://openairdocs.org/sdr/USAA001319), Aug 24, 2000: BULKHEAD. CRACKED. CLT - FOUND BULKHEAD WEB CRACKED .75 INCH, STATION 178 RBL .5, WL 188. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-10-08. (M) - [SDR USAA000959](https://openairdocs.org/sdr/USAA000959), Jun 26, 2000: FRAME. CORRODED. PIT - FOUND FRAME CORRODED 4 INCHES BY 3 INCHES, STATION 1006 AT STRINGER 18 AND 19 RIGHT SIDE. CORROSION LEVEL 2, TASK NR C53-206-01. CUT FRAME AND REPLACED PE - [SDR USAASB00098](https://openairdocs.org/sdr/USAASB00098), Apr 3, 2000: LIGHT. SHORTED. IAH - FLT 2231 - ON CLIMB-OUT FROM IAH, AT APPROXIMATELY 9,000 FEET, CAPTAIN REPORTED THERE WAS A LOUD POP AND SPARKS THAT DROPPED DOWN ON THE FIRST OFFICER FRO - [SDR USAA990180](https://openairdocs.org/sdr/USAA990180), Mar 5, 1999: WEB. CRACKED. CLT - DURING DROP IN VISUAL INSPECTION, FOUND A 4 INCH CRACK AT BS 233, BL 0, WL 192.5 WEB. INSTALLED DOUBLER PER BOEING SRM 51-70-13. (M) All 67: https://openairdocs.org/deregistered/N373US-2006-07-03/reports.md ## NTSB investigations (2) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB NYC96IA022](https://openairdocs.org/ntsb/NYC96IA022), Nov 2, 1995: Boeing 737-3B7 (N373US), Portland, ME, incident, minor damage. Probable cause: a bird strike during takeoff, which resulted in failure of several fan blades in the right engine and a partial loss of engine power. - [NTSB MIA95IA214](https://openairdocs.org/ntsb/MIA95IA214), Aug 25, 1995: Boeing 737-3B7 (N373US), Fort Lauderdale, FL, incident, no damage. Probable cause: LOW ELECTRICAL RESISTANCE OF THE AUTOPILOT AILERON ACTUATOR FOR UNSPECIFIED REASONS WHICH RESULTED IN AN UNCOMMANDED ROLL TO THE RIGHT. ## FAA accident and incident reports (2) 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 19951102038739I](https://openairdocs.org/incident/19951102038739I), Nov 2, 1995: Boeing 7373B7 (N373US), Portland, ME, Substantial damage. Loud bang right engine on takeoff. Vibration. Shutdown. Vectored low over ocean to clear runway. Injested ducks. - [Incident 19950825033929I](https://openairdocs.org/incident/19950825033929I), Aug 25, 1995: Boeing 7373B7 (N373US), Ft Lauderdale, FL. Descending to land. Uncommanded roll to right. Disconnected auto pilot. Landed safely. ## Other aircraft with N373US - [Registered now](https://openairdocs.org/aircraft/N373US): Costruzioni Aeronautiche Tecna P2006T, S/N 373/US, built 2023 --- 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.