# Service difficulty reports: N9347, cancelled Nov 19, 2013 A list on [N9347, cancelled Nov 19, 2013](https://openairdocs.org/deregistered/N9347-2013-11-19.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 0203069951](https://openairdocs.org/sdr/0203069951.md): Door · cracked · Aug 12, 2002 · N9347 · Doug DC932 · Cargo/Baggage Doors > During HCK in DHN, crack damage was found on the lower forward cargo door inner and outer flange. Repaired per EA 99-191322. - [SDR 0203059951](https://openairdocs.org/sdr/0203059951.md): Bulkhead · cracked · Aug 8, 2002 · N9347 · Doug DC932 · Fuselage Main, Structure > During HCK in DHN, the aft pressure bulkhead web was found cracked under Z=63.5 stiffener approx. 10" outboard of the ventral door jamb. Repaired per EA 99-191325. - [SDR 0201909951](https://openairdocs.org/sdr/0201909951.md): Duct · damaged · Jun 5, 2002 · N9347 · Doug DC932 · Leading Edge Slat Control System > UPON SLAT EXTENSION, THE SLAT DISAGREEMENT ANNUNCIATOR LIGHT ILLUMINATED AND THE AIRCRAFT ROLLED. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED IN MSP WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT -T- DUCT OUTER TOP FORWARD POSITION DAMAGED FR - [SDR 0201919951](https://openairdocs.org/sdr/0201919951.md): Door · damaged · May 25, 2002 · N9347 · Doug DC932 · Leading Edge Devices > DURING APPROACH FOR LANDING WHEN SLATS EXTENDED, THE AIRCRAFT ROLLED TO THE LEFT. THE SLAT DISAGREEMENT LIGHT WAS ON AND THE SLATS RETRACTED LIGHT WAS OUT. CREW CYCLED THE SLAT EXTENSION PROCEDURES AND THE SLATS AGREED AND NO TENDENCY TO ROLL. ALL INDICATIO - [SDR 9905399951](https://openairdocs.org/sdr/9905399951.md): Battery · discharged · Dec 20, 1999 · N9347 · Doug DC932 · Emergency Lighting > DURING PERIODIC CHECK, FOUND FORWARD CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY. OPERATIONAL CHECK NORMAL. - [SDR 9904409951](https://openairdocs.org/sdr/9904409951.md): Battery Pack · discharged · Oct 21, 1999 · N9347 · Doug DC932 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT ESCAPE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9901609951](https://openairdocs.org/sdr/9901609951.md): Wire · loose · Apr 16, 1999 · N9347 · Doug DC932 · Light System Wiring > DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS IN TAILCONE AND LIGHT ABOVE TAILCONE RELEASE HANDLE INOPERATIVE. MAINTENANCE FOUND BAD CONNECTION AT BROWN DISARM WIRE AT SPLICE NEAR POWER SUPPLY. REPLACED WIRE. OPERATIONAL CHECK NORMAL. - [SDR 9809919951](https://openairdocs.org/sdr/9809919951.md): Prox Sensor · broken · Aug 16, 1998 · N9347 · Doug DC932 · Landing Gear Position and Warning > NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW RECYCLED GEAR TWICE WITH SAME RESULTS. EMERGENCY GEAR EXTENSION PRODUCERS WERE UTILIZED AND AIRCRAFT LANDED WITHOUT INCIDENT. RED EMERGENCY WAS DECLARED BY THE CAPTAIN. MAINTENANCE FOUND - [SDR 9807679951](https://openairdocs.org/sdr/9807679951.md): Battery Pack · discharged · Apr 28, 1998 · N9347 · Doug DC932 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9802019951](https://openairdocs.org/sdr/9802019951.md): Bulb · burned out · Feb 1, 1998 · N9347 · Doug DC932 · Landing Gear Position and Warning > LEFT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW ABORTED APPROACH AND NORMAL INDICATIONS WERE ACHIEVED DURING GO-AROUND. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RELAMPED LEFT MAIN LANDING GEAR GREEN DOWNLOCK LIGHT, OPER - [SDR 9724389951](https://openairdocs.org/sdr/9724389951.md): Batteries · discharged · Dec 28, 1997 · N9347 · Doug DC932 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9718569951](https://openairdocs.org/sdr/9718569951.md): Battery Pack · discharged · Oct 1, 1997 · N9347 · Doug DC932 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS BETWEEN ROWS 8, 9, AND 10 INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9714159951](https://openairdocs.org/sdr/9714159951.md): Csd · malfunctioned · Jul 24, 1997 · N9347 · Doug DC932 · Alternator-Generator Drive > AFTER TAKEOFF FROM DFW, LEFT CSD OIL PRESSURE ANNUNCIATOR CAME ON AND OIL TEMP PEGGED OFF SCALE. VOLTS INDICATED NORMAL BUT FREQUENCY READ VERY HIGH. CSD WOULD NOT DISCONNECT. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN PROCEDURE. AIRCRAFT RETURNED TO DFW AND - [SDR 9624739951](https://openairdocs.org/sdr/9624739951.md): Switch Pack · failed · Nov 14, 1996 · N9347 · Doug DC932 · Landing Gear Position and Warning > UPON RAISING GEAR AFTER TAKEOFF, GEAR WARNING HORN SOUNDED CONTINUOUSLY. RECYCLED GEAR SEVERAL TIMES, BOTH CLEAN AND FLAPS 15. CYCLED THROTTLES UP AND PUSHED HORN OFF BUTTON, HORN CEASED. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE CHA - [SDR 9614739951](https://openairdocs.org/sdr/9614739951.md): Switch · failed · Nov 14, 1996 · N9347 · Doug DC932 · Landing Gear Position and Warning > UPON RAISING GEAR AFTER TAKEOFF, GEAR WARNING HORN SOUNDED CONTINUOUSLY. RECYCLED GEAR SEVERAL TIMES, BOTH CLEAN AND FLAPS 15. CYCLED THROTTLES UP AND PUSHED HORN OFF BUTTON, HORN CEASED. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE CHA - [SDR 9624249951](https://openairdocs.org/sdr/9624249951.md): Frame · corroded · Nov 6, 1996 · N9347 · Doug DC932 · Fuselage Main, Frame > DURING H-CHECK, FOUND CORROSION ON THE FS 218 FRAME LOWER CHORD AT LONGERON 30. REPAIRED FRAME (P/N S 2777930-5) PER EA 99-109580. - [SDR 9624239951](https://openairdocs.org/sdr/9624239951.md): Skin · corroded · Nov 5, 1996 · N9347 · Doug DC932 · Fuselage Main, Plate/Skin > DURING H-CHECK, FOUND CORROSION ON THE FUSELGE SKIN AND FINGER DOUBLER AT FS 510 FROM LONGERON 29L TO 29R. REPAIRED SKIN (P/N 5911412-191, -55). - [SDR 9624229951](https://openairdocs.org/sdr/9624229951.md): Longeron · corroded · Nov 5, 1996 · N9347 · Doug DC932 · Fuselage Main, Longeron/Stringer > DURING H-CHECK, FOUND CORROSION AT LONGERONS 29L AND 29R AT FS 579. REPAIRED LONGERONS (P/N 3920596-1) PER EA 99-120176, 99-120174. - [SDR 9624209951](https://openairdocs.org/sdr/9624209951.md): Fitting · corroded · Oct 31, 1996 · N9347 · Doug DC932 · Nacelle/Pylon Structure > DURING H-CHECK, FOUND CORROSION ON THE NR 2 PYLON LOWER FORWARD SURFACE BEAVER TAIL FITTING AND LOWER SPAR CHORD. REPLACED FITTING AND REMOVED SPAR CORROSION PER EA 99-120169. - [SDR 9624189951](https://openairdocs.org/sdr/9624189951.md): Frame · corroded · Oct 29, 1996 · N9347 · Doug DC932 · Fuselage Main, Frame > DURING H-CHECK, FOUND CORROSION ON THE FS 756 BULKHEAD FRAME T-CHORD AT LONGERON 29L. REPAIRED FRAME (P/N 9958212-3) PER EA 99-109572. - [SDR 9624169951](https://openairdocs.org/sdr/9624169951.md): Skin · delaminated · Oct 28, 1996 · N9347 · Doug DC932 · Trailing Edge Flaps > DURING H-CHECK, FOUND DELAMINATION IN THE LEFT WING FLAP TRAILING EDGE UPPER SKIN AT XFLS 187-235. REPAIRED SKIN (P/N 9957578-503) PER EA 99-120171. - [SDR 9622939951](https://openairdocs.org/sdr/9622939951.md): Fitting · corroded · Oct 26, 1996 · N9347 · Doug DC932 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND CORROSION ON BOTH THE LEFT AND RIGHT OUTBOARD BATHTUB FITTINGS IN THE MAIN LANDING GEAR WHEELWELLS. REPLACED FITTINGS PER SRM 51-01, PAR.1C. - [SDR 9622259951](https://openairdocs.org/sdr/9622259951.md): Fitting · corroded · Oct 17, 1996 · N9347 · Doug DC932 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND CORROSION ON THE LEFT WHEEL WELL ATTACH FITTING FS 690 AT THE KEEL SKIN. REPLACED FITTING PER SRM 53-01 FIG 1. - [SDR 9620949951](https://openairdocs.org/sdr/9620949951.md): Lights · inoperative · Sep 29, 1996 · N9347 · Doug DC932 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND ALL OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BOTH BATTERY PACKS AND POWER SUPPLIES, OPERATIONAL CHECK NORMAL. - [SDR 9619509951](https://openairdocs.org/sdr/9619509951.md): Ind Switch · malfunctioned · Sep 7, 1996 · N9347 · Doug DC932 · Landing Gear Position and Warning > DURING APPROACH INTO MSP, NOSE LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. MAINTENANCE REPLACED NOSE LANDING GEAR INDICATION SWITCH AND RELAMPED INDICATOR. OPERATIONAL CHE - [SDR 9606279951](https://openairdocs.org/sdr/9606279951.md): Battery Pack · discharged · Mar 18, 1996 · N9347 · Doug DC932 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT ENGINE NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9604889951](https://openairdocs.org/sdr/9604889951.md): Uplock Latch · binding · Feb 28, 1996 · N9347 · Doug DC932 · Landing Gear Retraction/Extension System > DURING CLIMBOUT, RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FREED MOVEMENT TO RIGHT MAIN GEAR UPLOCK LATCH. OPERATIONAL CHECK NORMAL, AIRCRAFT RETURNED TO SERVICE. - [SDR 9521129952](https://openairdocs.org/sdr/9521129952.md): Generator · failed · Dec 18, 1995 · N9347 · Doug DC932 · AC Generator-Alternator > DURING CRUISE, THE RIGHT AC BUS, RIGHT GENERATOR, AND DC BUS OFF LIGHTS ILLUMINATED. THE RIGHT DC BUS WAS RESTORED BY DC BUS CROSSTIE. AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED RIGHT CONSTANT SPEED DRIVE, GENERATOR CONTROL PANEL, AND E - [SDR 9513409951](https://openairdocs.org/sdr/9513409951.md): Rmi Compass · malfunctioned · Aug 27, 1995 · N9347 · Doug DC932 · Visual Omnirange (VOR) System > LOSS OF NR 2 COMPASS INDICATOR OCCURRED DURING INITIAL SPOOL UP ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED NR 2 RMI. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. - [SDR 9510679951](https://openairdocs.org/sdr/9510679951.md): Fuel Control · reqd service · Jul 4, 1995 · N9347 · Doug DC932 · Fuel Control/Turbine Engines > NR 1 ENGINE EPR FLUCTUATED WHILE ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AT 70 KTS, FLIGHT RETURNED TO THE GATE. MAINTENANCE DRAINED THE F.C.U. MOISTURE TRAP AND RAN THE ENGINE. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. - [SDR 9510019951](https://openairdocs.org/sdr/9510019951.md): Thermostat · leaking · Jun 21, 1995 · N9347 · Doug DC932 · Pneumatic Indicating System > TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF AT 60 KNOTS AND RETURNED TO GATE. FOUND SMALL AIR LEAK AT THERMOSTAT, TIGHTENED THERMOSTAT. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. - [SDR 9506569951](https://openairdocs.org/sdr/9506569951.md): Vent Valve · malfunctioned · Apr 21, 1995 · N9347 · Doug DC932 · Aircraft Fuel Distribution System > FUEL BEGAN LEAKING FROM RIGHT WING TANK EN ROUTE PVD-DTW. LEAK WAS APPROXIMATELY 1600 LBS IN ONE HOUR. FLIGHT DIVERTED TO BUF AND LANDED WITHOUT INCIDENT. REPLACED CLIMB VENT VALVE IN LEFT MAIN FUEL TANK. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR 9502609951](https://openairdocs.org/sdr/9502609951.md): Cable · frayed · Feb 12, 1995 · N9347 · Doug DC932 · Aerodynamic Fairings > DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ALSO, FOUND THE TAILCONE CABLE FRAYED BETWEEN THE RIGHT SIDE LATCHES AT THE LOWER PULLEY. REPLACED THE CABLE AND RERIGGED THE TAILCONE. - [SDR 9502269951](https://openairdocs.org/sdr/9502269951.md): Skin · oil canned · Feb 9, 1995 · N9347 · Doug DC932 · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, FOUND OIL CANNING IN THE FUSELAGE SKIN FS 1056 - 1080 BETWEEN LONGERONS 17R - 18R. REPAIRED PER EA 99-096893. - [SDR 9502219951](https://openairdocs.org/sdr/9502219951.md): Longeron · cracked · Feb 7, 1995 · N9347 · Doug DC932 · Fuselage Main, Longeron/Stringer > DURING PERIODIC CHECK, FOUND CRACKS IN LONGERON 17R AT FS 389 AND FS 408 AND IN LONGERON 17L AT FS 435. REPAIRED ALL THREE LOCATIONS PER EA 99-096899. - [SDR 9502159951](https://openairdocs.org/sdr/9502159951.md): Skin · oil canned · Feb 4, 1995 · N9347 · Doug DC932 · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, FOUND OIL CANNING IN FUSELAGE SKIN BETWEEN LOWER LEFT PYLON ATTACH ANGLE AND LONGERON 17L AT FS 1002 AND BETWEEN LONGERONS 17L - 18L AT FS 1015. REPAIRED BOTH PER EA 99-096893. ## 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 = 'N9347' AND deregistration_id = 'N9347-2013-11-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N9347-2013-11-19/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.