# Service difficulty reports: N2310, cancelled Mar 17, 2006 A list on [N2310, cancelled Mar 17, 2006](https://openairdocs.org/deregistered/N2310-2006-03-17.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DL733050035](https://openairdocs.org/sdr/DL733050035.md): Outflow Valve · contaminated · Jan 15, 2005 · N2310 · Boeing 737347 · Pressure Regulator/Outflow Valve > AIRCRAFT FAILED TO PRESSURIZE. FOUND PRESSURE RELIEF VALVE STUCK OPEN. - [SDR DL733030478](https://openairdocs.org/sdr/DL733030478.md): Fitting · corroded · May 19, 2003 · N2310 · Boeing 737347 · Fuselage, Landing Gear Attach Fittings > 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 CORROSION. A REPAIR BUSHING WAS INSTALLED IN THE BORE AND A WASHER INSTALLED TO FILL THE SPOTFACE. - [SDR DL733030434](https://openairdocs.org/sdr/DL733030434.md): Skin · dented · May 7, 2003 · N2310 · Boeing 737347 · Fuselage Main, Plate/Skin > 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 AND TRIPLER PER ER/A 384851-14. - [SDR DL733030408](https://openairdocs.org/sdr/DL733030408.md): Frame · cracked · May 1, 2003 · N2310 · Boeing 737347 · Fuselage Main, Frame > FUSELAGE / COCKPIT FLOOR STRUCTURE / CRACKED WEB AND INTERCOSTAL / STA 178, WL 207, RBL 28, THE INTERCOSTAL OUTBOARD STRUCTURE AND HORIZONTAL WEB WERE FOUND CRACKED. BOTH ARE LOCATED IMMEDIATELY AFT OF THE STA 178 BULKHEAD. THE CRACK WAS TRIMMED OUT OF THE ST - [SDR DL733020892](https://openairdocs.org/sdr/DL733020892.md): Smoke Detector · faulty · Jul 30, 2002 · N2310 · Boeing 737347 · Smoke Detection > 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 CHIME. FOUND AFT RT DETECTOR INOP. REPLACED DETECTOR, OPS CHECKS GOOD. - [SDR DL733020877](https://openairdocs.org/sdr/DL733020877.md): Engine · overtemp · Jul 27, 2002 · N2310 · Boeing 737347 · Engine (Turbine/Turboprop) > 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 SECONDS. N1 INDICATES AT ABOUT 96.6. PULLED BACK THROTTLES, RED LIGHT EXTINGUISHED. REMOVED AND REP - [SDR DL733020874](https://openairdocs.org/sdr/DL733020874.md): Transmitter · malfunctioned · Jul 26, 2002 · N2310 · Boeing 737347 · Trailing Flap Position Indicating System > 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 KIAS. REPLACED RIGHT T/E FLAP POSITION TRANSMITTER, OPS NORMAL. - [SDR DL733010703](https://openairdocs.org/sdr/DL733010703.md): Skin · cracked · May 1, 2001 · N2310 · Boeing 737347 · Fuselage Main, Plate/Skin > 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 REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 380703-14, REV - [SDR DL733001662](https://openairdocs.org/sdr/DL733001662.md): Battery · inoperative · Aug 29, 2000 · N2310 · Boeing 737347 · Emergency Lighting > 1L DOOR AND 1R EXIT SIGN EMERGENCY LIGHT INOP. REPLACED BATTERY. - [SDR DL733001622](https://openairdocs.org/sdr/DL733001622.md): Wire · failed · Aug 21, 2000 · N2310 · Boeing 737347 · Electrical Power System Wiring > 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 SIMULTANEOUSLY. F/A IN AFT NOTED SPARKS IN CEILING. CRACK IN CEILING ON CAPT SIDE WHERE AISLE MEETS GALL - [SDR DL733001552](https://openairdocs.org/sdr/DL733001552.md): Attach Fitting · corroded · Aug 12, 2000 · N2310 · Boeing 737347 · Nacelle/Pylon, Attach Fittings > 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 OVERSIZED BY.10 INCHES TO REMOVE THE CORROSION, A 15-5 STEEL BUSHING INSTALLED, AND A NEW SPHERICAL BEARIN - [SDR DL733001134](https://openairdocs.org/sdr/DL733001134.md): Actuator · failed · Jun 10, 2000 · N2310 · Boeing 737347 · Autopilot System > 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 SHOWED NO ABNORMAL INDICATIONS. NO TURBULENCE IN AREA. A/C IN CLEAN CONFIG. A AUTOPILOT ENGAGED AT - [SDR DL733000984](https://openairdocs.org/sdr/DL733000984.md): Valve · open · May 18, 2000 · N2310 · Boeing 737347 · Engine Start Valves/Controls > START VALVE CAME OPEN DURING TAXI ON NUMBER 2 ENGINE. STARTER DESTROYED. REPLACED STARTER AND START VALVE. - [SDR DL733981470](https://openairdocs.org/sdr/DL733981470.md): Skin · cracked · Jul 12, 1998 · N2310 · Boeing 737347 · Fuselage Main, Plate/Skin > 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 ROUTED OUT AND REPAIRED WITH AN EXTERNAL STEEL REPAIR DOUBLER AND AN ALUMINUM REPAIR TRIPLER. THE RE - [SDR DL733970502](https://openairdocs.org/sdr/DL733970502.md): Brakes · failed · Mar 18, 1997 · N2310 · Boeing 737347 · Landing Gear Brake System > 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.md): Hyd Hose · ruptures · Jan 1, 1997 · N2310 · Boeing 737347 · Hydraulic System, Main > 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.md): Skin · dented · Jul 21, 1995 · N2310 · Boeing 737347 · Fuselage Main, Plate/Skin > 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 DAMAGED SECTION WILL BE CUT OUT AND AN EXTERNAL REPAIR DOUBLER WILL BE INSTALLED. - [SDR DL733953126](https://openairdocs.org/sdr/DL733953126.md): Skin · worn · Jul 12, 1995 · N2310 · Boeing 737347 · Nacelle/Pylon, Plate/Skin > 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.md): Angle · cracked · Jul 10, 1995 · N2310 · Boeing 737347 · Fuselage Miscellaneous Structure > 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.md): Apu Door · damaged · Jan 10, 1995 · N2310 · Boeing 737347 · Auxiliary Power Unit (APU) Doors > DURING LETTER CHECK, FOUND LOWER APU SHROUD RUBBING ON THE APU DOOR CAUSING DAMAGE WHICH REQUIRED REPAIRS PER SRM 52-40-01 FIG 204. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N2310' AND deregistration_id = 'N2310-2006-03-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N2310-2006-03-17/reports --- 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.