# N2310: 1986 Boeing 737-347, registration cancelled 2006-03-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 17, 2006 - Status when cancelled: Valid registration - Airframe: [Boeing 737-347](https://openairdocs.org/model/boeing-737-347) (registry code 138447U) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23596 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 29, 1986 - Certificate issued: August 13, 2004 - Last registry action: August 13, 2004 - Mode S code: A20E8F - Owner when cancelled: [U S Bank Na Trustee](https://openairdocs.org/faa-owner/U%20S%20BANK%20NA%20TRUSTEE) - Location: [Boston, MA](https://openairdocs.org/faa-place/MA/Boston) - Owner type: Corporation - Owner's area on the map: 42.3582° N, 71.0519° W: Placed by OpenAirDocs at the center of ZIP code 02110, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N2310 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=2310 - Page: https://openairdocs.org/deregistered/N2310-2006-03-17 From the FAA registry file of October 31, 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 737-347: https://openairdocs.org/model/boeing-737-347.md ## Service difficulty reports (20) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL733050035](https://openairdocs.org/sdr/DL733050035), Jan 15, 2005: OUTFLOW VALVE. CONTAMINATED. AIRCRAFT FAILED TO PRESSURIZE. FOUND PRESSURE RELIEF VALVE STUCK OPEN. - [SDR DL733030478](https://openairdocs.org/sdr/DL733030478), May 19, 2003: FITTING. CORRODED. CORROSION WAS FOUND IN THE LUG BORE AND AFT LUG FACE OF THE LT MLG SIDE STRUT FITTING AT FS 685. THE BORE WAS OVERSIZED AND THE FACE SPOTFACED TO REMOVE ALL COR - [SDR DL733030434](https://openairdocs.org/sdr/DL733030434), May 7, 2003: SKIN. DENTED. FUSELAGE / SKIN / DENTING AND CREASE AT STA 380 BETWEEN STRINGERS 17L AND 18L. DENTED AND CREASED SKIN WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER - [SDR DL733030408](https://openairdocs.org/sdr/DL733030408), May 1, 2003: FRAME. CRACKED. FUSELAGE / COCKPIT FLOOR STRUCTURE / CRACKED WEB AND INTERCOSTAL / STA 178, WL 207, RBL 28, THE INTERCOSTAL OUTBOARD STRUCTURE AND HORIZONTAL WEB WERE FOUND CRA - [SDR DL733020892](https://openairdocs.org/sdr/DL733020892), Jul 30, 2002: SMOKE DETECTOR. FAULTY. LAV SMOKE AMBER LIGHT AND CHIME CAME ON DURING CRUISE FLIGHT. ALL LAVS CHECKED WITH NO SIGN OF SMOKE, FUMES, EXCESSIVE HEAT. CIRCUIT BREAKER PULLED TO SILENCE C - [SDR DL733020877](https://openairdocs.org/sdr/DL733020877), Jul 27, 2002: ENGINE. OVERTEMP. ON TAKEOFF (NORMAL POWER) CLIMBOUT BOTH ENGINE INDICATIONS SHOWED RED LIGHT ILLUMINATED ON DIGITAL READOUT AT 970 DEGREES (C) PLUS ON BOTH ENGINES AT LEAST 5 SE - [SDR DL733020874](https://openairdocs.org/sdr/DL733020874), Jul 26, 2002: TRANSMITTER. MALFUNCTIONED. DURING FLAP EXTENSION RIGHT FLAP IND REMAINED NEAR ZERO AND LEFT INDICATED NEAR ONE DEGREE. L/E INDICATIONS NORMAL. FOLLOWED QRH PROCEDURES AND LANDED AT 170 KI - [SDR DL733010703](https://openairdocs.org/sdr/DL733010703), May 1, 2001: SKIN. CRACKED. THE FUSELAGE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT WAS FOUND WITH A SMALL CRACK AT STRINGER 22R. THE CRACK WAS REMOVED WITH A 1.1 IN X .85 IN EDGE TRIM AND - [SDR DL733001662](https://openairdocs.org/sdr/DL733001662), Aug 29, 2000: BATTERY. INOPERATIVE. 1L DOOR AND 1R EXIT SIGN EMERGENCY LIGHT INOP. REPLACED BATTERY. - [SDR DL733001622](https://openairdocs.org/sdr/DL733001622), Aug 21, 2000: WIRE. FAILED. AFTER LANDING WITH APU RUNNING AND POWER ON RT ENG ON APU GEN, SHUT DOWN RT ENG AND APU GEN IMMEDIATELY DROPPED OFF LINE. RECONNECTED APU GEN TO RT SIDE SIMULTA - [SDR DL733001552](https://openairdocs.org/sdr/DL733001552), Aug 12, 2000: ATTACH FITTING. CORRODED. REMOVAL OF A MIGRATED SPHERICAL BEARING ON THE AFT LUG FITTING OF THE NR 2 ENGINE STRUT CROWN BEAM REVEALED CORROSION IN THE LUG BORE. THE LUG BORE WAS OVERSIZE - [SDR DL733001134](https://openairdocs.org/sdr/DL733001134), Jun 10, 2000: ACTUATOR. FAILED. AT FL 270, BEGINNING DESCENT, EXPERIENCED UNCOMMANDED ABRUPT ROLL APPROX 35-40 DEGREES TO THE LEFT. AUTOPILOT REVERTED TO CWS PITCH AND ROLL. YAW DAMPER IND SHO - [SDR DL733000984](https://openairdocs.org/sdr/DL733000984), May 18, 2000: VALVE. OPEN. START VALVE CAME OPEN DURING TAXI ON NUMBER 2 ENGINE. STARTER DESTROYED. REPLACED STARTER AND START VALVE. - [SDR DL733981470](https://openairdocs.org/sdr/DL733981470), Jul 12, 1998: SKIN. CRACKED. A .75 INCH CRACK WAS FOUND IN THE SKIN AND UNDERLYING CORNER GUSSET AT UPPER OUTBD CORNER OF THE L1 COCKPIT WINDOW (C-D WINDOW POST LOCATION). THE CRACK WAS ROU - [SDR DL733970502](https://openairdocs.org/sdr/DL733970502), Mar 18, 1997: BRAKES. FAILED. NR 4 BRAKE FAILED. FOUND PARTS OF STATORS AND PADS IN WHEEL ASSY. REPLACED BRAKE AND WHEEL ASSY. - [SDR DL733970005](https://openairdocs.org/sdr/DL733970005), Jan 1, 1997: HYD HOSE. RUPTURES. NOSE GEAR WOULD NOT RETRACT. FOUND RUPTURED HYD HOSE ON NOSE GEAR UPLOCK ACTUATOR. REPLACED HOSE, SWUNG GEAR AND OPERATIONAL CHECK GOOD. - [SDR DL733953335](https://openairdocs.org/sdr/DL733953335), Jul 21, 1995: SKIN. DENTED. DURING HMV INSPECTION, THE SKIN WAS FOUND DENTED AT FS 765 JUST BELOW THE STRINGER 20R LAP SPLICE. IN ACCORDANCE WITH B737-300 SRM 53-00-01, FIG 202, THE DAMAGE - [SDR DL733953126](https://openairdocs.org/sdr/DL733953126), Jul 12, 1995: SKIN. WORN. AT HMV, INSP FOUND THE O/B SIDE OF NR 2 PYLON WORN AT WING L/E AREA. ACCOMPLISHED REPAIRS PER SRM 54-50-01 PG 219. - [SDR DL733953114](https://openairdocs.org/sdr/DL733953114), Jul 10, 1995: ANGLE. CRACKED. FLOOR SUPPORT ANGLE CRACKED ABOVE STR 27L AT STA 807. REMOVED DAMAGED SECTION OF ANGLE, MADE REPAIR PARTS, AND INSTALLED PER SRM 53-00 -53, FIG 201. - [SDR DL733950141](https://openairdocs.org/sdr/DL733950141), Jan 10, 1995: APU DOOR. DAMAGED. DURING LETTER CHECK, FOUND LOWER APU SHROUD RUBBING ON THE APU DOOR CAUSING DAMAGE WHICH REQUIRED REPAIRS PER SRM 52-40-01 FIG 204. ## FAA accident and incident reports (3) 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 19970630020659I](https://openairdocs.org/incident/19970630020659I), Jun 30, 1997: Boeing 737347 (N2310), Kansas City, MO. High oil temperature. Diverted. Shut down NR1 engine. Ground wire for oil temp gauge broken from stud. - [Incident 19960423045239I](https://openairdocs.org/incident/19960423045239I), Apr 23, 1996: Boeing 737347 (N2310), Salt Lake City, UT. Narrative: aircraft landed at 1300 MDT. Company later reported tread loss on one tire. No further incident. Maintenance found no. 4 main tire threw cap and… - [Incident 19930623024519I](https://openairdocs.org/incident/19930623024519I), Jun 23, 1993: Boeing 737347 (N2310), Kansas City, MO, Minor damage. NR1 and NR2 main tires blew on landing rollout. Stopped on taxiway. Passengers deplaned via portable stairs. ## Other aircraft with N2310 - [Cancelled 1971-08-27](https://openairdocs.org/deregistered/N2310-1971-08-27): Spencer-Bensen B-8M, S/N 366-6274, built 1968. Owner: [Spencer Jr Ernest O](https://openairdocs.org/faa-owner/SPENCER%20JR%20ERNEST%20O), [Jackson, MS](https://openairdocs.org/faa-place/MS/Jackson) - [Cancelled 1934-07-25](https://openairdocs.org/deregistered/N2310-1934-07-25): Curtiss Aeroplane & Motor CURTISS JN-4D, S/N 1072 SUB. Owner: [Coleman Fred](https://openairdocs.org/faa-owner/COLEMAN%20FRED), [Iola, KS](https://openairdocs.org/faa-place/KS/Iola) --- 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.