# N392US: 1985 Boeing 737-3B7, registration cancelled 2006-04-10 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 10, 2006 - 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: 23314 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 19, 1985 - Certificate issued: April 25, 2002 - Last registry action: May 18, 2005 - Mode S code: A48C0A - Owner when cancelled: [J P Morgan Trust Co Na Trustee](https://openairdocs.org/faa-owner/J%20P%20MORGAN%20TRUST%20CO%20NA%20TRUSTEE) - Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York) - Owner type: Corporation - Owner's area on the map: 40.6898° N, 74.0174° W: Placed by OpenAirDocs at the center of ZIP code 10004, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N392US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=392US - Page: https://openairdocs.org/deregistered/N392US-2006-04-10 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 (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA200507004](https://openairdocs.org/sdr/USAA200507004), Jul 12, 2005: SKIN. CRACKED. 5 IN CRACK FOUND BETWEEN FRAME 727D AND 727E STR 24L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. - [SDR USAA200507003](https://openairdocs.org/sdr/USAA200507003), Jul 11, 2005: FRAME. CRACKED. 1.5 IN CRACK FOUND AT FRAME 767, STR 24L. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 229. - [SDR SB05059](https://openairdocs.org/sdr/SB05059), May 11, 2005: BATTERY. DISCHARGED. CLT FOUND EXTERIOR EMERGENCY LIGHTS AFT OF THE WINGS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. - [SDR USAA041077](https://openairdocs.org/sdr/USAA041077), Dec 10, 2004: SKIN. DELAMINATED. PIT - WALKAROUND- WING T/E, 8 INCH X 12 INCH AREA, DELAMINATION, UPPER PANEL OB RT FIXED T/E OF WING. REPLACED PANEL IAW SRM AND EA. - [SDR SB04142](https://openairdocs.org/sdr/SB04142), Oct 10, 2004: LIGHT. LOOSE. CLT - MAINTENANCE REPORTED THE EXTERIOR EMERGENCY EXIT LIGHT AT THE R1 DOOR INOPERATIVE. MAINTENANCE FOUND THE BULB LOOSE IN SOCKET. SECURED BULB. OPERATIONAL C - [SDR USAA040243](https://openairdocs.org/sdr/USAA040243), Jun 1, 2004: SKIN. CRACKED. SKIN CRACKED (1 INCH X Q.22 INCH) LOWER AFT CORNER FORWARD SERV CUTOUT STA 322, 4 INCH/ 14 INCH. INSTALLED DOUBLERS IAW SRM. - [SDR USA2004F00007](https://openairdocs.org/sdr/USA2004F00007), Feb 9, 2004: INDICATOR. FAILED. SHORTLY AFTER TAKEOFF, ENROUTE, THE F/O ADI FAILED. CREW REPORTED THE CIRCUIT BREAKER WAS TRIPPED AND THAT A SLIGHT ELECTRICAL ODOR WAS PRESENT IN THE COCKPIT. - [SDR USAASB03216](https://openairdocs.org/sdr/USAASB03216), Dec 16, 2003: CHARGER. FAILED. MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 17 THROUGH 22 AND AT BOTH AFT DOORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASS - [SDR USAA030132](https://openairdocs.org/sdr/USAA030132), Jul 25, 2003: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 2 INCHES, S23L AND BS 727E. INSTALLED DOUBLER PER EA 94536. (M) - [SDR USAA030208](https://openairdocs.org/sdr/USAA030208), May 15, 2003: SKIN. CORRODED. PIT - FOUND ON WALKAROUND SKIN AND KEEL BEAMS CORRODED 1 FT BY .5 INCH AREA, AT FASTENERS STATION 727, L STR 27 AND R STR 28. REPLACED LEFT AND RIGHT BEAMS SPLI - [SDR USAA030028](https://openairdocs.org/sdr/USAA030028), Mar 21, 2003: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 1 INCH IN LENGTH, AFT SERVICE DOOR, UPPER HINGE CUTOUT. REMOVED CRACK AND INSTALLED DOUBLER PER TR 52-10-13 AND EA 75742. (M) - [SDR USAASB03019](https://openairdocs.org/sdr/USAASB03019), Feb 6, 2003: SENSOR. MALFUNCTIONED. PIT - FLT 1963 - AFTER TAKEOFF, CREW REPORTED LANDING GEAR LEVER WOULD NOT MOVE TO RETRACT GEAR. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCI - [SDR USAASB03018](https://openairdocs.org/sdr/USAASB03018), Feb 5, 2003: SENSOR. MALFUNCTIONED. PIT - FLT 231 - AFTER TAKEOFF, CREW REPORTED LANDING GEAR LEVER WOULD NOT MOVE TO RETRACT GEAR. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND RETURN - [SDR USAASB02229](https://openairdocs.org/sdr/USAASB02229), Dec 23, 2002: IRU. FAILED. PIT - FLT 1004 - AFTER TAKEOFF FROM PIT, EN ROUTE TO MKE, THE LEFT IRS FAILED IN FLIGHT. DECISION WAS MADE TO RETURN TO FIELD AT PIT. FLIGHT LANDED WITHOUT FURT - [SDR USAA020106](https://openairdocs.org/sdr/USAA020106), Feb 17, 2002: ANGLE. CRACKED. PIT - FOUND ANGLE CRACKED 2 INCHES, FORWARD OF STATION 345. REPLACED ANGLE PER SRM 31-70-12. (M) - [SDR USAA020107](https://openairdocs.org/sdr/USAA020107), Feb 17, 2002: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 2.75 INCH, STATION 727E PLUS 3 INCHES AT S18R. INSTALLED DOUBLER PER SRM 53-00-01 AND 51-20-05. (M) - [SDR USAA020108](https://openairdocs.org/sdr/USAA020108), Feb 17, 2002: FLOORBEAM. BROKEN. PIT - FOUND WEB BROKEN IN HALF, MAIN FRAME BROKE IN HALF STATION 639 FLOOR LEVEL. REMOVED AND REPLACED WEB PER EA 73114. (M) - [SDR USAA020103](https://openairdocs.org/sdr/USAA020103), Feb 4, 2002: FRAME. CORRODED. PIT - FOUND FRAME CORRODED 6 INCHES BY .5 INCHES, RBL 8.10 BETWEEN STATION 727E AND 772. CORROSION LEVEL 1. REPAIRED PER TYPICAL REPAIR 53-10-06B. (M) - [SDR USAA020070](https://openairdocs.org/sdr/USAA020070), Jan 24, 2002: DOUBLER. CRACKED. PIT - FOUND DOUBLER CRACKED .5 INCHES AREA AND 1 INCH AREA BENT, LIP FOR A/C DOOR, STATION 490 BL 0. INSTALLED DOUBLER PER TR 53-30-05 AND EA 73180. (M) - [SDR USAA020071](https://openairdocs.org/sdr/USAA020071), Jan 24, 2002: WEB. CORRODED. FOUND SUPPORTS AND WEB CORRODED 36 INCHES BY 3 INCHES AREA, STATION 300-340 MAIN ENTRY THRESHOLD. CORROSION LEVEL 2, TASK NR C53-107-0. REMOVED AND REPLACED SUP - [SDR USAA020105](https://openairdocs.org/sdr/USAA020105), Dec 30, 2001: CHANNEL. CRACKED. PIT - FOUND CHANNEL CRACKED 12 INCHES, STATION 345-363. DEFECTIVE PART REPLACED WITH IDENTICAL P/N, REPLACED CHANNEL PER NR 313A1355. (M) - [SDR USAASB00146](https://openairdocs.org/sdr/USAASB00146), May 21, 2000: RELIEF VALVE. MISINSTALLED. CLT - WHILE ON THE GATE AT CLT, THE A SYSTEM HYDRAULIC RESERVOIR EXPLODED. MAINTENANCE FOUND THE PRESSURE RELIEF VALVE INSTALLED IMPROPERLY. THE VALVE AND RESER - [SDR USAA990622](https://openairdocs.org/sdr/USAA990622), Jun 21, 1999: SKIN. CRACKED. CLT - DURING METRO MOD, FOUND 2 INCH LONG CRACK ON SKIN AT STATION 727B STRINGER 16L. INSTALLED DOUBLER PER SRM 53-30-3. (M) - [SDR USAASB99079](https://openairdocs.org/sdr/USAASB99079), Mar 21, 1999: ENGINE. FAILED. CLT - FLT 858 - FLIGHT RETURNED TO FIELD AT CLT DUE TO A 6 INCH THROTTLE SPLIT AND A NR 1 EGINE OVERTEMP. DURING TAKEOFF ROLL, THE CREW GOT THE THROTTLE SPLIT A - [SDR USAASB98311](https://openairdocs.org/sdr/USAASB98311), Nov 23, 1998: LIGHT. INOPERATIVE. GSO - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT AT THE SERVICE DOOR INOP AND THE EMERGENCY LIGHT OVER THE RIGHT WING INOP. MAINTENANCE REMOVED AND REPLACED - [SDR 98ZZZM948](https://openairdocs.org/sdr/98ZZZM948), Nov 23, 1998: BATTERY PACK. DISCHARGED. GSO - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT AT THE SERVICE DOOR INOP AND THE EMERGENCY LIGHT OVER THE RIGHT WING INOP. MAINTENANCE REMOVED AND REPLACED - [SDR 98ZZZM947](https://openairdocs.org/sdr/98ZZZM947), Nov 23, 1998: CHARGER. INOPERATIVE. GSO - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT AT THE SERVICE DOOR INOP AND THE EMERGENCY LIGHT OVER THE RIGHT WING INOP. MAINTENANCE REMOVED AND REPLACED - [SDR USAA980320](https://openairdocs.org/sdr/USAA980320), Jul 26, 1998: FLOORBEAM. CORRODED. CLT - DURING Q-3 CHECK VISUAL INSPECTION FOUND A 4 INCH BY 4 INCH CORROSION TOP OF FLANGE STA 312 CENTERLINE FLOORBEAM. CORROSION TASK NR C 53-107-01. INSTALLED - [SDR USAA980319](https://openairdocs.org/sdr/USAA980319), Jul 26, 1998: FLOORBEAM. CORRODED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 4 INCH AREA OF CORROSION TOP OF FLANGE FLOORBEAM AT STA 312 RBL 30. CORROSION TASK NR C53-107-01. INSTALLED SP - [SDR USAA980318](https://openairdocs.org/sdr/USAA980318), Jul 26, 1998: FRAME. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1.50 INCH CRACK 727D BETWEEN STRINGERS 27 LT AND RT OF FRAME. INSTALLED DOUBLER, NEW SHEAR TIES AND FLOOR ANGL - [SDR USAASB98149](https://openairdocs.org/sdr/USAASB98149), Jun 12, 1998: BATTERY PACK. DISCHARGED. PIT - MAINTENANCE FOUND THE EMERGENCY LIGHT AT THE AFT LEFT ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB97029](https://openairdocs.org/sdr/USAASB97029), Jan 25, 1997: TR UNIT. FAILED. ILM - FL 1505 - EN ROUTE FROM BOS-FLL OVER ILM, AT FL 310, FLT LOST A TRANSFORMER/RECTIFIER. RESULT WAS COMPLETE INSTRUMENTATION LOSS ON CAPTAINS SIDE AND PARTI - [SDR USAASB95016](https://openairdocs.org/sdr/USAASB95016), Nov 19, 1995: BLEED VLV. FAILED. MCO - FLT NR 378 - NR 2 ENGINE OVERTEMPED ON TAKEOFF TO 944 DEGREES FOR 2 SECONDS. FLIGHT CREW REDUCED POWER AFTER TAKEOFF TO BELOW RED LINE. CREW COULD NOT SEL ## 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 MIA96LA220](https://openairdocs.org/ntsb/MIA96LA220), Aug 29, 1996: Boeing 737-300 (N392US), Chattanooga, TN, minor damage. Probable cause: clear air turbulence, which was encountered during cruise flight and resulted in injuries to passengers. ## 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. - [Accident 19960829029759A](https://openairdocs.org/incident/19960829029759A), Aug 29, 1996: Boeing 7373B7 (N392US), Chattanooga, TN, Minor damage. (.4)The airplane encountered severe turbulence, while in cruise flight. The seat belt signs were not illuminated. The airplane weather avoidance radar was on,… - [Incident 19950626022909I](https://openairdocs.org/incident/19950626022909I), Jun 26, 1995: Boeing 7373B7 (N392US), Washington, DC. Uncommonded right roll on approach. Turned 45 degrees. Used auto pilot kill switch and recovered control. --- 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.