# N390US: Boeing 737-3B7, registration cancelled 2021-10-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 30, 2021 - Status when cancelled: Registration expired, pending cancellation - 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: 23312 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 8, 1985 - Certificate issued: July 26, 2018 - Last registry action: July 26, 2018 - Mode S code: A4849C - Owner when cancelled: [Aerothrust Holdings Leasing LLC](https://openairdocs.org/faa-owner/AEROTHRUST%20HOLDINGS%20LEASING%20LLC) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: LLC - Owner's area on the map: 25.8166° N, 80.3105° W: Placed by OpenAirDocs at the center of ZIP code 33166, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N390US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=390US - Page: https://openairdocs.org/deregistered/N390US-2021-10-30 From the FAA registry file of November 5, 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 (61, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA050506](https://openairdocs.org/sdr/USAA050506), Apr 17, 2005: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 2.25 INCH, 727E STRINGER 24L. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. (M) - [SDR SB05048](https://openairdocs.org/sdr/SB05048), Apr 16, 2005: WIRE. BROKEN. CLT - PILOT REPORTED THE EMERGENCY EXIT LIGHT AT THE R1 DOOR WAS ILLUMINATED. MAINTENANCE FOUND A BROKEN WIRE BETWEEN BATTERY PACKS. RESPLICED WIRE. OPERATIONAL - [SDR USAA050348](https://openairdocs.org/sdr/USAA050348), Mar 7, 2005: HINGE. CRACKED. CLT - UNSCHED - HINGE CASTING, 1 INCH X 1 INCH CRACK, LT AFT SERVICE DOOR HINGE BOX. (K) - [SDR SB05029](https://openairdocs.org/sdr/SB05029), Feb 20, 2005: SOCKET. DIRTY. BDL - MAINTENANCE REPORTED THE EXTERIOR EMERGENCY LIGHT AT THE L1 DOOR INOPERATIVE. MAINTENANCE CLEANED SOCKET AND RELAMPED. OPERATIONAL CHECK NORMAL. - [SDR USAA050224](https://openairdocs.org/sdr/USAA050224), Feb 7, 2005: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1 INCH, AFT LEFT SERVICE DOOR CUTOUT LOWER HINGE AREA. INSTALLED DOUBLER PER TR 53-60-10. (M) - [SDR SB04150](https://openairdocs.org/sdr/SB04150), Oct 28, 2004: ODOR. DETECTED. PIT - FLT470 - ON CLIMB-OUT FROM PIT, EN ROUTE TO ORD, THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN THE FORWARD GALLEY. FLIGHT RETURNED TO FIELD AT PIT A - [SDR SB04146](https://openairdocs.org/sdr/SB04146), Oct 17, 2004: LIGHT. INOPERATIVE. CLT - PILOT REPORTED THE EMERGENCY EXIT ROW EVACUATION LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. - [SDR USAA040118](https://openairdocs.org/sdr/USAA040118), Apr 10, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1.5 INCH, STATION 933 STRINGER 24R. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (M) - [SDR USAA040119](https://openairdocs.org/sdr/USAA040119), Apr 9, 2004: SKIN. CRACKED. CLT - FOUND SKIN WITH TWO CRACKS .5 INCH AND 2 INCHES LONG, STATION 727E +4 AT STRINGER 22R, RIGHT FUSELAGE. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (M) - [SDR USAA040117](https://openairdocs.org/sdr/USAA040117), Apr 9, 2004: SKIN. CRACKED. FOUND SKIN CRACKED 2.5 INCHES, STATION 727E AT STRINGER 18R, RT FUSELAGE. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (M) - [SDR USAA030202](https://openairdocs.org/sdr/USAA030202), Sep 24, 2003: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 4.5 INCH HORIZONTALLY, BS 727E STRINGER 24 LT. INSTALLED TEMPORARY REPAIR DOUBLER PER SRM 53-00-01 FIG 202. (M) - [SDR USAASB03028](https://openairdocs.org/sdr/USAASB03028), Feb 17, 2003: CIRCUIT CARD. FAILED. ATL - FLT 520 - AFTER TAKEOFF FROM ATL, EN ROUTE TO PIT, CREW REPORTED THE RIGHT MLG RED LIGHT REMAINED ILLUMINATED WITH THE GEAR HANDLE IN THE OFF PAND UP POSI - [SDR USAASB03027](https://openairdocs.org/sdr/USAASB03027), Feb 16, 2003: UPLOCK SENSOR. DIRTY. ATL - FLT 1711 - AFTER 15 MINUTES AFTER TAKEOFF FROM CLT, EN ROUTE TO MSY, CAPTAIN REPORTED THE RIGHT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR HAD BEEN - [SDR USA2002F00042](https://openairdocs.org/sdr/USA2002F00042), Jun 4, 2002: DOOR. UNLATCHED. SHORTLY AFTER TAKEOFF, ENROUTE, CAPTAIN REPORTED A LOUD NOISE COMING FROM UNDER THE INSTRUMENT PANEL. HE ALSO REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT - [SDR USAASB02008](https://openairdocs.org/sdr/USAASB02008), Jan 13, 2002: CONTROL PANEL. FAULTY. DTW - FLT 765 - EN ROUTE TO DTW, CLIMBING TO FL350, CABIN ALTITUDE BEGAN CLIMBING APPROX 2,000 FPM. SWITCHED BOTH PACKS TO HIGH FLOW AND CABIN RETURNED TO NORMA - [SDR USAA020009](https://openairdocs.org/sdr/USAA020009), Jan 10, 2002: BULKHEAD. CORRODED. PIT - FOUND AFT BULKHEAD 4 INCHES BY 1 INCH TOTAL DIMENSION, STATION 1016 BL 00 FORWARD END OF LOWER PRESSURE BULKHEAD STIFFENER. REMOVED DAMAGE, INSTALLED MANU - [SDR USAA020016](https://openairdocs.org/sdr/USAA020016), Jan 10, 2002: SKIN. CRACKED. PIT - FOUND SKIN CRACKED .5 INCH LONG, FRAME POST SKIN OF F/O'S R-1 WINDOW UPPER OUTBOARD CORNER. CUT OUT DAMAGED AREA INSTALLED FILLER AND DOUBLER PER SRM 53-1 - [SDR USAA020017](https://openairdocs.org/sdr/USAA020017), Jan 10, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED 2 INCHES, STATION 303.3 AT STR 4L UNDER BULKHEAD MOUNT FITTING. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-2. (M) - [SDR USAA020015](https://openairdocs.org/sdr/USAA020015), Jan 10, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .5 INCH, CORNER FORWARD GALLEY DOOR STATION 296 BETWEEN S7R-8R. INSTALLED MANUAL DOUBLER PER SRM 51-70-11 AND EA 73057. (M) - [SDR USAA020014](https://openairdocs.org/sdr/USAA020014), Jan 10, 2002: INTERCOSTAL. CRACKED. PIT - FOUND INTERCOSTAL CRACKED .5 INCH, FORWARD TOP END OF INTERCOSTAL AT STATION 344, BL0. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02. (M) - [SDR USAA020013](https://openairdocs.org/sdr/USAA020013), Jan 10, 2002: FRAME. CRACKED. PIT - FOUND FRAME WEB CRACKED .75 INCH, AT STATION 277 S14R SUPPORT WEB. MANUFACTURED AND REPLACED WEB PER SRM 53-10-15. (M) - [SDR USAA020012](https://openairdocs.org/sdr/USAA020012), Jan 10, 2002: ANGLE. CRACKED. PIT - FOUND ANGLE CRACKED .75 INCH, ANGLE SUPPORT FORWARD OF STATION 291.5 BETWEEN S12R-13R. REMOVED AND REPLACED SUPPORT WITH IDENTICAL PART PER SRM 51-40-02. - [SDR USAA020011](https://openairdocs.org/sdr/USAA020011), Jan 10, 2002: STRINGER. CRACKED. PIT - FOUND STRINGER CRACKED 1.5 INCH, STRINGER 5L AT STATION 380. CUT OUT CRACKED SECTION, INSTALLED NEW STRINGER SECTION AND DOUBLERS PER SRM 53-00-03. (M) - [SDR USAA020010](https://openairdocs.org/sdr/USAA020010), Jan 10, 2002: SKIN. CRACKED. PIT - FOUND SKIN CRACKED .812 INCH LONG, FRAME POST SKIN OF CAPT L1 WINDOW UPPER OUTBOARD CORNER. INSTALLED DOUBLER PER EA 73010 AND SRM 53-10-01 FIG 210. (M) - [SDR USAA011408](https://openairdocs.org/sdr/USAA011408), Dec 21, 2001: INTERCOSTAL. CRACKED. PIT - FOUND INTERCOSTAL PLATE WITH 1 INCH CRACK, AFT OF RT FRAME 947 AND STRINGER 11R. INSTALLED DOUBLER PER SRM 51-70-13. (M) - [SDR USAA011396](https://openairdocs.org/sdr/USAA011396), Dec 19, 2001: INTERCOSTAL. CRACKED. PIT - INTERCOSTAL CRACKED.125 INCH, CABIN FLOOR STATION 344 BL 0 FLOORBEAM AT STATION 344. DRILLED AND INSTALLED 525 INTERCOSTAL (NEW PART) PER SRM 51-10-2 AND - [SDR USAA011397](https://openairdocs.org/sdr/USAA011397), Dec 19, 2001: INTERCOSTAL. CRACKED. PIT - FOUND INTERCOSTAL .125 INCH CRACKED, CABIN FLOOR INTERCOSTAL STATION 344 LBL 12. FABRICATED AND INSTALLED PER SRM 51-10-1 AND 53-10-51. (M) - [SDR USAA011412](https://openairdocs.org/sdr/USAA011412), Dec 14, 2001: SKIN. CRACKED. PIT - FOUND BOTTOM SKIN CRACKED .25 INCH LONG, AFT SPAR RIGHT STAB, STATION 152. INSTALLED DOUBLER PER SRM 55-10-01 FIG 204. (M) - [SDR USAA011411](https://openairdocs.org/sdr/USAA011411), Dec 11, 2001: CAP. CORRODED. PIT - FOUND STRIP CAP CORRODED 1 INCH CIRCLE AROUND NUT PLATE, SIDE PLATE FORWARD CARGO AT STATION 500 S26C. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (M) - [SDR USAA011413](https://openairdocs.org/sdr/USAA011413), Dec 11, 2001: FRAME. CORRODED. PIT - FOUND FRAME CORRODED 1 INCH CIRCLE UPPER AND LOWER SURFACE, BELTFRAME AT STATION 500 S-26R. BLENDED AND TREATED PER SRM 53-00-07 FIG 101. (M) - [SDR USAA011392](https://openairdocs.org/sdr/USAA011392), Dec 11, 2001: FITTING. CRACKED. PIT - FOUND FITTING CRACKED .75 INCH, L ANGLE TOP CENTER FITTING STATION 312 (RS) FORWARD SERVICE DOOR. INSTALLED DOUBLER STRAP PER 51-40-02 AND 51-40-03. (M) - [SDR USAA011414](https://openairdocs.org/sdr/USAA011414), Dec 7, 2001: FLOOR SUPPORT. CORRODED. PIT - FOUND FLOOR SUPPORT .125 INCH BY .125 INCH AROUND 2 NUT PLACE HOLES, FLOOR SUPPORT ANGLE BETWEEN 1006 AND 1016, LBL 37. DEFECTIVE PART REPLACED WITH IDENT - [SDR USAA011388](https://openairdocs.org/sdr/USAA011388), Dec 3, 2001: ANGLE. CRACKED. PIT - FOUND MED JAMB WEB ANGLE CRACKED 2 INCH, STRINGER 10L STATION 303.9. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-20-01, 51-40-00, 51-10-02. - [SDR USAA011389](https://openairdocs.org/sdr/USAA011389), Dec 3, 2001: STRINGER. CRACKED. PIT - FOUND STRINGER CRACKED 1.5 INCH STRINGER 5L AT FRAME JUNCTION STATION 380. DOUBLER INSTALLED PER SRM 53-00-03. (M) - [SDR USAA011390](https://openairdocs.org/sdr/USAA011390), Dec 3, 2001: INTERCOSTAL. CORRODED. PIT - FOUND INTERCOSTAL 1 SQUARE INCH, FORWARD END OF INTERCOSTAL 525L, BS 947. CLEANED AND TREATED PER SRM 51-20-01. (M) - [SDR USAA011405](https://openairdocs.org/sdr/USAA011405), Nov 28, 2001: SKIN. CRACKED. PIT - FOUND PYLON SKIN CRACKED .75 INCH, NR 1 ENGINE PYLON UPPER SKIN STRUCTURE AT ACCESS PANEL. STOP DRILLED AND INSTALLED DOUBLER PER TYP REPAIR 54-30-07. (M) - [SDR USAA011406](https://openairdocs.org/sdr/USAA011406), Nov 21, 2001: FRAME. CRACKED. PIT - FOUND FRAME .5 INCH CRACK, STATION 663.75 AT STRINGER 1 CUTOUT RIGHT SIDE. REPAIR ANGLE AND STRINGER SPLICE PER SRM 53-00-07. (M) - [SDR USAASB01262](https://openairdocs.org/sdr/USAASB01262), Sep 19, 2001: SEAL. OUT OF POSITION. PHL - FLT 867 - ON CLIMB-OUT FROM GSO, AT FL240, THE CABIN ALTITUDE CLIMBED TO 9,700 FEET. NO AUTO FAIL INDICATION WAS NOTED. CREW COULD NOT CONTROL CABIN IN ST - [SDR USAA011154](https://openairdocs.org/sdr/USAA011154), Aug 27, 2001: PRESSURE PANEL. CRACKED. CLT - FOUND FLOOR SKIN CRACKED 1 INCH, PRESSURE FLOOR RIGHT WHEEL WELL. INSTALLED DOUBLER PER TR 53-60-4. (M) - [SDR USAA011155](https://openairdocs.org/sdr/USAA011155), Aug 27, 2001: PRESSURE PANEL. CRACKED. CLT - FOUND PRESSURE FLOOR SKIN CRACKED 1 INCH, PRESSURE FLOOR LEFT WHEEL WELL. INSTALLED DOUBLER PER TR 53-60-4. (M) - [SDR USAASB01063](https://openairdocs.org/sdr/USAASB01063), Feb 24, 2001: BATTERY PACK. DISCHARGED. GSO - MAINTENANCE FOUND SOME CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) - [SDR USAA001834](https://openairdocs.org/sdr/USAA001834), Oct 31, 2000: FRAME. CRACKED. TPA - FOUND FORWARD CARGO DOOR CRACKED .50 INCH, FORWARD CARGO DOOR FRAME JUST BELOW LOWER LATCH ROLLER. INSTALLED REPAIR DOUBLER PER SRM 51-70-11 FIG 1. (M) - [SDR USAA002192](https://openairdocs.org/sdr/USAA002192), Sep 15, 2000: FRAME. CRACKED. PIT - FOUND FRAME CHORD CRACKED APPROX .25 INCH, RT 178 WL 212. SPLICED IN NEW SECTION OF CHORD PER EO 5300V157. (M) - [SDR USAA002191](https://openairdocs.org/sdr/USAA002191), Sep 15, 2000: FRAME. CRACKED. PIT - FOUND CHORD ANGLE CRACKED .5 INCH, LEFT 178 WL 212. SPLICED IN NEW SECTION OF CHORD PER EO 5300V157. (M) - [SDR USAA991343](https://openairdocs.org/sdr/USAA991343), Dec 9, 1999: SKIN. CRACKED. TPA - DURING CX-3 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .5 INCH CRACK IN SKIN AT STATION 380, BL 3LT. INSTALLED DOUBLER PER TR 53-30-07. (M) - [SDR USAASB98318](https://openairdocs.org/sdr/USAASB98318), Dec 1, 1998: BATTERY PACK. DISCHARGED. GSO - MAINTENANCE FOUND A SECTION OF THE FORWARD EMERGENCY LIGHTS INOP AT THE FORWARD ENTRY DOOR AND THE LEFT BULLNOSE. MAINTENANCE REMOVED AND REPLACED THE BAT - [SDR 98ZZZM966](https://openairdocs.org/sdr/98ZZZM966), Dec 1, 1998: BATTERY CHARGER. INOP. GSO - MAINTENANCE FOUND A SECTION OF THE FORWARD EMERGENCY LIGHTS INOP AT THE FORWARD ENTRY DOOR AND THE LEFT BULLNOSE. MAINTENANCE REMOVED AND REPLACED THE BAT - [SDR USAASB98199](https://openairdocs.org/sdr/USAASB98199), Jul 30, 1998: HARNESS. FAILED. IAH - FLT 1934 - SHORTLY AFTER TAKEOFF, THE NR 2 ENGINE OVERHEAT LIGHT AND THE MASTER CAUTION LIGHT ILLUMINATED. CREW WENT THROUGH EMERGENCY PROCEDURES, DISCHAR - [SDR USAASB98141](https://openairdocs.org/sdr/USAASB98141), Jun 4, 1998: SWITCH. OUT OF ADJUST. PHL - FLT 701 - AFTER TAKEOFF OUT OF BTV, THE LANDING GEAR WOULD NOT RETRACT. CREW TRIED TO RECYCLE GEAR BUT IT WOULD NOT RETRACT. USED LANDING GEAR OVERRIDE TR - [SDR USAA980128](https://openairdocs.org/sdr/USAA980128), Mar 20, 1998: FLOORBEAM. CORROSION. CLT - DURING Q-6 VISUAL INSPECTION, FOUND CORROSION AT SCREW HOLES STATION 1016 BEAM IN LEFT LAV AREA. INSTALLED REPAIR STRAP REPAIR DOCUMENT SRM 53-00-51 FIG 2 All 61: https://openairdocs.org/deregistered/N390US-2021-10-30/reports.md ## 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 MIA95IA187](https://openairdocs.org/ntsb/MIA95IA187), Jul 18, 1995: Boeing 737-3B7 (N390US), Orlando, FL, incident, no damage. Probable cause: CONTAMINATION OF THE WIRING HARNESS AND ELECTRICAL CONNECTORS TO THE E-1-2 AND E-1-3 SHELF DISCONNECT BRACKETS IN THE ELECTRONICS COMPARTMENT, WHICH RESULTED IN AN ELECTRICAL FAULT AND AN UNCOMMANDED… ## 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 19950718026339I](https://openairdocs.org/incident/19950718026339I), Jul 18, 1995: Boeing 737300 (N390US), Orlando, FL. Uncommanded roll at FL280. Descending. Disconnected autopilot and yaw dampner. Descent at 290 knots at 1000 fpm. --- 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.