# N394US: 1986 Boeing 737-3B7, registration cancelled 2006-07-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 18, 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: 23316 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 31, 1986 - Certificate issued: July 14, 2006 - Last registry action: July 14, 2006 - Mode S code: A49378 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - 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/N394US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=394US - Page: https://openairdocs.org/deregistered/N394US-2006-07-18 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 (47) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SB05116](https://openairdocs.org/sdr/SB05116), Sep 19, 2005: BRACKET. MISSING. ORD - PILOT REPORTED MISSING HARDWARE FOR THE FORWARD BRACKET OF THE R2 SERVICE DOOR ESCAPE SLIDE. MAINTENANCE REPLACED MISSING HARDWARE FOR THE FORWARD BRACKET - [SDR USAA050452](https://openairdocs.org/sdr/USAA050452), Apr 2, 2005: FRAME. BROKEN. CLT - FOUND FORMER BROKEN, STATION 535 WL 165, LBL 60. REPLACED FORMER. (M) - [SDR SB05032](https://openairdocs.org/sdr/SB05032), Feb 23, 2005: CIRCUIT BREAKER. BURNED. AFTER LANDING CREW STOPPED A/C ON TAXIWAY & REPORTED TO INBOUND RAMP, FIRE & SMOKE IN COCKPIT. CREW STATED, "ON TAXI-IN, FIRE ERUPTED FROM F/O LWR C/B PNL. USED - [SDR USAA040834](https://openairdocs.org/sdr/USAA040834), Oct 8, 2004: SKIN. CRACKED. SKIN, 1 INCH CRACK, BS 727D, STR 22R. INSTALLED DOUBLER IAW SRM 53-00-01. INSTALLED DOUBLER IAW SRM 53-00-01. - [SDR USAA040507](https://openairdocs.org/sdr/USAA040507), Aug 12, 2004: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 1.250 INCH, STATION 727D, STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) - [SDR USAA040360](https://openairdocs.org/sdr/USAA040360), Jul 26, 2004: SKIN. CRACKED. PIT - FOUND SKIN CRACKED APPROXIMATELY .375 INCH CRACK, AFT CARGO DOOR FORWARD FRAME CUTOUT. REMOVED EXISTING REPAIR AND INSTALLED DOUBLER PER EA 78434. (M) - [SDR USAA040344](https://openairdocs.org/sdr/USAA040344), Jul 16, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 2 INCHES, TWO 4.5 INCHES AFT OF 867, 1 INCH BELOW STRINGER 15R. INSTALLED DOUBLER PER SRM 53-00-01 DETAIL XI. (M) - [SDR USAA040206](https://openairdocs.org/sdr/USAA040206), May 6, 2004: SKIN. CRACKED. SERVICE DOOR CUTOUT (.2500 INCH CRACK) AFT CORNER AT STA 332.101 FWD TO DOOR CUTOUT. REPAIRED IAW 53-10-01 FIG 202, PAGE 207. - [SDR USAA030218](https://openairdocs.org/sdr/USAA030218), Oct 28, 2003: SKIN. CRACKED. FOUND SKIN CRACKED 2.375 INCH, STATION 740 AND S23R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M) - [SDR USAASB03074](https://openairdocs.org/sdr/USAASB03074), Jun 7, 2003: ODOR. DETECTED. TEN MINUTES AFTER TAKEOFF FROM CLT, FLIGHT ATTENDANT REPORTED AN ELECTICAL ODOR ALONG WITH A SLIGHT HAZE IN THE CABIN FROM SEAT ROWS 4 THROUGH 14. AS A PRECAUTI - [SDR USAA030080](https://openairdocs.org/sdr/USAA030080), May 22, 2003: SKIN. CRACKED. FOUND SKIN CRAKCED .75 INCH LONG CRACK, SKIN AFT ENTRY DOOR LOWER HINGE CUTOUT STATION 947.5, STRINGER 14L. DOUBLER AND TRIPLER INSTALLED AND PAINTED PER SRM 53 - [SDR USAA030081](https://openairdocs.org/sdr/USAA030081), May 22, 2003: SKIN. CRACKED. PIT - FOUND SKIN CRACKED .75 INCH LONG, SKIN AFT SERVICE DOOR LOEWR HINGE CUTOUT STATION 947.5, STRINGER 14R. DOUBLE AND TRIPLER INSTALLED AND PAINTED PER SRM 5 - [SDR USAASB02186](https://openairdocs.org/sdr/USAASB02186), Sep 30, 2002: SLIDE. MALFUNCTIONED. DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE APPEARED TO HAVE PREMATURELY INFLATED AND BECAME TWISTED 90 DEGREES. D - [SDR USA2002F00092](https://openairdocs.org/sdr/USA2002F00092), Sep 30, 2002: SLIDE. FAILED. DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE APPEARED TO HAVE PREMATURELY INFLATED AND BECAME TWISTED 90 DEGREES. D - [SDR USAASB02115](https://openairdocs.org/sdr/USAASB02115), Jun 16, 2002: WIRE. BROKEN. CLT - FOUND MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 20C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER SEAT ROW 20C. OPERATIONAL CHEC - [SDR USAA020198](https://openairdocs.org/sdr/USAA020198), May 22, 2002: STRINGER. CRACKED. PIT - FOUND SHELF WITH .25 INCH CRACK ON EACH SIDE OF FASTENER, AFT END OF S18 LEFT SHELF AT AFT INBOARD FASTENER. REPLACED 18A SHELF ASSEMBLY PER SRM 51-40-02. - [SDR USAA020191](https://openairdocs.org/sdr/USAA020191), May 21, 2002: FRAME. CORRODED. PIT - FOUND FRAME CRACKED 1 INCH BY 3 INCH CORRODED AREA, FS 500B, BETWEEN STRINGERS 27L AND 28L. REMOVED CORROSION PER SRM 51-40-02. (M) - [SDR USAA020199](https://openairdocs.org/sdr/USAA020199), May 21, 2002: STRINGER. CORRODED. PIT - FOUND SHELF WITH 3 AREAS OF CORROSION, 1 INCH ROUND, 2 INCH BY 2 INCH, 2 INCH BY 3 INCH, 6 INCHES TO 8 INCHES AFT OF STATION 706 ON LEFT 18A SHELF. REMOVE - [SDR USAA020200](https://openairdocs.org/sdr/USAA020200), May 21, 2002: STRINGER. CORRODED. PIT - FOUND 1 INCH ROUND CORRODED AREA, BETWEEN STATION 695 AND 706 ON LEFT SIDE 18A SHELF INBOARD. REMOVED CORROSION PER SRM 51-10-02. (M) - [SDR USAA020192](https://openairdocs.org/sdr/USAA020192), May 21, 2002: FRAME. CORRODED. PIT - FOUND FRAME CORRODED 1 INCH BY 1 INCH CORRODED AREA, STATION 500B, BETWEEN STRINGERS 28L AND 28R. INSTALLED FABRICATED SHEAR TIE PER SRM 51-70-11. (M) - [SDR USAA020193](https://openairdocs.org/sdr/USAA020193), May 21, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .5 INCH, FS 887 RIGHT AT STRINGER 9R. INSTALLED FRAME DOUBLER PER T/R 53-10-14A. (M) - [SDR USAA020194](https://openairdocs.org/sdr/USAA020194), May 21, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .5 INCH, FS 827 RIGHT AT STRINGER 9R. INSTALLED FRAME DOUBLER PER T/R 53-10-14A. (M) - [SDR USAA020195](https://openairdocs.org/sdr/USAA020195), May 21, 2002: SUPPORT. CRACKED. PIT - FOUND ANTENNA SUPPORT ZEE 1.25 INCH CRACK, HORIZONTAL LEG OF ANTENNA ZEE SUPPORT STATION 727D AND 727C. REPLACED ZEE SUPPORT PER SRM 51-40-05. (M) - [SDR USAA020196](https://openairdocs.org/sdr/USAA020196), May 21, 2002: DOUBLER. CRACKED. PIT - FOUND DOUBLER CRACKED 1 INCH, ANTENNA DOUBLER BETWEEN STATION 727D AND 727E. REPLACED ZEE SUPPORT AND MOUNT BRACKET PER SRM 51-40-05. (M) - [SDR USAA020197](https://openairdocs.org/sdr/USAA020197), May 21, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED 1 INCH, FRAME 807 LEFT AT FASTENER STRINGER 9. INSTALLED ANGLES, SHIMS, STRAP PER T/R 53-10-14A. (M) - [SDR USAA020216](https://openairdocs.org/sdr/USAA020216), May 21, 2002: DOUBLER. CORRODED. PIT - FOUND ANTENNA DOUBLER CORRODED SIX .25 INCH BY .25 INCH AREAS, ANTENNA MOUNT NUTPLATE BRACKETS BETWEEN STATION 727D. REMOVED CORROSION AND REPLACED CHANNE - [SDR USAA020171](https://openairdocs.org/sdr/USAA020171), Apr 24, 2002: SKIN. CORRODED. PIT - FOUND RIB AND SKIN WITH HEAVY CORROSION 4 INCHES LONG BY 1 INCH WIDE, RUDDER COUNTER BALANCE STRUCTURE, RUDDER STATION 121.64. LEVEL 2 CORROSION. (M) - [SDR USAA020170](https://openairdocs.org/sdr/USAA020170), Apr 15, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .062 INCH, FRAME 480 LEFT SIDE BETWEEN S8L AND S9L. REPAIRED PER TYPICAL REPAIR 53-10-14A. (M) - [SDR USAA020172](https://openairdocs.org/sdr/USAA020172), Apr 15, 2002: FRAME. CRACKED. PIT - FOND FRAME CRACKED .064 INCHES LONG, FRAME 400 RIGHT SIDE BETWEEN S8R AND S9R. ACCOMPLISHED TYPICAL REPAIR 53-10-14A. (M) - [SDR USAASB01115](https://openairdocs.org/sdr/USAASB01115), Apr 27, 2001: FUSE. BLOWN. TPA - MAINTENANCE FOUND THE FORWARD EMERGENCY EGRESS LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TWO 5 AMPS FUSES. OPS CHECK GOOD. (M) - [SDR USAASB01114](https://openairdocs.org/sdr/USAASB01114), Apr 27, 2001: LIGHT. INOPERATIVE. TPA - MAINTENANCE FOUND SEAT 5C EMERGENCY SEAT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SPLICE. OPS CHECK GOOD. (M) - [SDR USAASB01106](https://openairdocs.org/sdr/USAASB01106), Apr 20, 2001: TRANSMISSION. FAILED. IAD - FLT 1083 - ON APPROACH TO DCA, CAPTAIN REPORTED THAT THE FLAPS WERE STUCK AT 10 DEGREES. CREW CHECKED ALL CIRCUIT BREAKERS AND TRIED ALTERNATE METHOD WITH - [SDR USAA000850](https://openairdocs.org/sdr/USAA000850), Jun 14, 2000: SKIN. CRACKED. CLT - FOUND SKIN FUSELAGE CRACKED 1.5 INCH, BS 727D PLUS 17.5 INCH JUST ABOVE STRINGER 23R. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 202 AND - [SDR USAA000451](https://openairdocs.org/sdr/USAA000451), Mar 23, 2000: SKIN. CRACKED. CLT - FOUND FUSELAGE SKIN CRACKED 2.125 INCHES, STRINGER 24L JUST FORWARD OF BS 727E. INSTALLED EXTERNAL DOUBLER PER EA 66901. (M) - [SDR USAASB99215](https://openairdocs.org/sdr/USAASB99215), Aug 31, 1999: STUD. LOOSE. DFW - FLT 870 - CAPTAIN REPORTED THAT AFTER TAKEOFF FROM DFW AND CLIMBING THROUGH 17,000 FT, THE NR 1 ENGINE OIL TEMPERATURE ROSE ABOVE THE RED RADIAL. CREW SHU - [SDR USAA990798](https://openairdocs.org/sdr/USAA990798), Aug 3, 1999: SKIN. CRACKED. TPA - DURING CX-1 CHECK EDDY CURRENT, FOUND A .25 INCH CRACK BELLY SKIN AFT EQUIPMENT COOLING EXHAUST STA 380 FUSELAGE SKIN. INSTALLED REPAIRED DOUBLER PER TR 5 - [SDR USAA990279](https://openairdocs.org/sdr/USAA990279), Mar 31, 1999: SKIN. CRACKED. CLT - DURING A RON VISUAL INSPECTION, FOUND A 1.25 INCH CRACK LEFT SIDE OF FUSELAGE AT STRINGER 24L, 24 INCHES AFT OF AFT WING TO BODY FAIRING SKIN. REMOVED DAM - [SDR USAA980371](https://openairdocs.org/sdr/USAA980371), Aug 27, 1998: BEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON UPPER SURFACE OF CREASEBEAM INNER CHORD RBBL BETWEEN STATION 294.5 TO STATION 331. CORROSION TASK N - [SDR USAA980370](https://openairdocs.org/sdr/USAA980370), Aug 27, 1998: FLOORBEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 11 INCH AREA OF CORROSION ON UPPER FLOORBEAM CHORD STATION 1016 LBL 15, CORROSION TASK N - [SDR USAA980369](https://openairdocs.org/sdr/USAA980369), Aug 27, 1998: FLOORBEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON 'T' CAP OF FLOORBEAM 65 INCH BY 3.5 INCH STATION 312 LBL 8 RBL 56 FLOORBEAM UPPER CHORD. CORROSION - [SDR USAA980368](https://openairdocs.org/sdr/USAA980368), Aug 27, 1998: FLOORBEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FLOORBEAM BOARD SCREW HOLES .5 INBY .5 BY 70 INCH STATION 328 BETWEEN RBL 14 TO RBL 56 UPPER CH - [SDR USAA980367](https://openairdocs.org/sdr/USAA980367), Aug 27, 1998: FLOORBEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FLOORBOARD SCREW HOLES .5 INCH BY .5 INCH BY 25 INCH STATION 344 BETWEEN LBL 14 TO RBL 11 UPPER - [SDR USAA980366](https://openairdocs.org/sdr/USAA980366), Aug 27, 1998: SKIN. CRACKED. CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AFT SERVICE DOOR INSIDE UPPER FRAME SKIN, UPPER HINGE ARM CLOSEOUT. INSTALLED DOUBLER PER TYPICAL - [SDR USAA980174](https://openairdocs.org/sdr/USAA980174), Apr 25, 1998: SKIN. CRACKED. CLT - DURING RON VISUAL INSPECTION, FOUND A 2.675 INCH CRACK IN THE SKIN AT RIGHT BS 727D AT S23R. INSTALLED DOUBLER PER REPAIR DOCUMENT EA 61668. (X) - [SDR USAASB97318](https://openairdocs.org/sdr/USAASB97318), Nov 21, 1997: BATTERY PACK. DISCHARGED. PVD - MAINTENANCE FOUND THE AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) - [SDR USAASB97046](https://openairdocs.org/sdr/USAASB97046), Feb 12, 1997: SEAL. LEAKING. LGA - FLT 2238 - DURING CLIMB, AIRCRAFT WOULD NOT PRESSURIZE AND RETURNED TO FIELD AT LGA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE E/E DOO - [SDR USAASB96246](https://openairdocs.org/sdr/USAASB96246), Nov 26, 1996: ENGINE. BIRD STRIKE. DAB - FLT 282 - UPON ROTATION WITH THE NOSE JUST OFF THE RUNWAY, THE AIRCRAFT STRUCK A FLOCK OF BIRDS. SEVERE VIBRATION WAS FELT FROM THE NR 2 ENGINE. THE CAPTA ## NTSB investigations (1) 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 NYC05IA095](https://openairdocs.org/ntsb/NYC05IA095), Jun 9, 2005: Boeing 737-3B7 (N394US), Boston, MA, incident, no damage. Probable cause: The local east controller's failure to follow FAA Order 7110.65, para 3-9-8 and Boston Tower Order 7110.11, Standard Operating Procedures, which resulted in a runway incursion during takeoff… ## 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 19891116061069I](https://openairdocs.org/incident/19891116061069I), Nov 16, 1989: Boeing 7373B7 (N394US), Philadelphia, PA, Minor damage. Both nose wheels blew on landing. Strong crosswind at time. Pilot declined to give a statement. ## Other aircraft with N394US - [Registered now](https://openairdocs.org/aircraft/N394US): Costruzioni Aeronautiche Tecna P2006T, S/N 394/US, built 2024 --- 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.