# Service difficulty reports: N933VJ, cancelled Jul 17, 2003 A list on [N933VJ, cancelled Jul 17, 2003](https://openairdocs.org/deregistered/N933VJ-2003-07-17.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAD99049](https://openairdocs.org/sdr/USAAD99049.md): Coalescer · out of position · Apr 1, 1999 · N933VJ · Doug DC931 · Humidity Control System > ATL-PIT - FLT 1558 - AFTER TAKEOFF THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. AFTER LANDING THE CAPTAIN TALKED FURTHER WITH THE FLIGHT ATTENDANTS AND FOUND THEY WERE NOT SURE IF THERE WAS - [SDR USAAD99027](https://openairdocs.org/sdr/USAAD99027.md): Battery · discharged · Feb 15, 1999 · N933VJ · Doug DC931 · Emergency Lighting > IND - THE FORWARD ENTRY DOOR, SERVICE DOOR, AND TAILCONE SLIDE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD ENTRY DOOR, SERVICE DOOR, AND TAILCONE SLIDE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD99011](https://openairdocs.org/sdr/USAAD99011.md): Hose · ruptured · Jan 18, 1999 · N933VJ · Doug DC931 · Humidity Control System > EWR-PIT - FLT 537 - DURING CLIMB-OUT, THE FLIGHT ATTENDANT NOTIFIED THE FLIGHT CREW OF A LOUD BANG AND THE SOUND OF AIR RUSHING. THE CAPTAIN NOTICED THERE WAS ONLY A 4 PSI CABIN PRESSURE DIFFERENTIAL AND THE CABIN ALTITUDE WAS CLIMBING AT 1100 FT PER MIN. TH - [SDR USAA990001](https://openairdocs.org/sdr/USAA990001.md): Pan · cracked · Jan 7, 1999 · N933VJ · Doug DC931 · Service Doors > PIT - DURING C-CHECK, FOUND 1 INCH CRACK IN FORWARD SERVICE DOOR PAN AFT SIDE AT HORIZONTAL BEAM END NR 6. INSTALLED PAN SPLICE (-39) PER SRM 52-05 FIG 27. (M) - [SDR USAA990000](https://openairdocs.org/sdr/USAA990000.md): Pan · cracked · Jan 7, 1999 · N933VJ · Doug DC931 · Service Doors > PIT - DURING C-4 CHECK, FOUND 1.5 INCH LONG CRACK IN SERVICE DOOR PAN AT NR 6 HORIZONTAL BEAM AFT END. SPLICED IN NEW PAN SECTION PER SRM 52-05 FIG 27 VIEW T-T. (M) - [SDR USAAD98205](https://openairdocs.org/sdr/USAAD98205.md): Seal · damaged · Nov 16, 1998 · N933VJ · Doug DC931 · Passenger/Crew Doors > PIT-PWM - FLT 1274 - AFTER TAKEOFF A NOISE WAS HEARD AT THE FORWARD MAIN ENTRY DOOR. THE NOISE STOPPED AND THEN STARTED AGAIN. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE ENVIRONMENTAL SEAL DAMAGED AND HANGING OUT O - [SDR USAA980411](https://openairdocs.org/sdr/USAA980411.md): Skin · cracked · Sep 18, 1998 · N933VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - DURING RON, FOUND CRACKS RANGING FROM.125 INCH TO.75 INCH ON SKIN AT LT SIDE STATION 1132 BETWEEN LONGERONS 15L/16L. CRACKS AT 4 FASTENER HOLES RT SIDE STATION 1143 BETWEEN LONGERONS 12R/159 CRACKS AT 10 FASTENER HOLES. CLASSIFIED A MINOR REPAIR. CU - [SDR USAAD98047](https://openairdocs.org/sdr/USAAD98047.md): Windshield · cracked · Mar 20, 1998 · N933VJ · Doug DC931 · Flight Compartment Windows > PIT - FLT 1237 - THE CAPTAINS OUTER WINDSHIELD PANE CRACKED DURING CRUISE ABOUT 20 MINUTES AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE CAPTAINS WINDSHIELD. (M) - [SDR USAAD98030](https://openairdocs.org/sdr/USAAD98030.md): Power Supply · inoperative · Feb 19, 1998 · N933VJ · Doug DC931 · Emergency Lighting > ROC - THE AFT CABIN CEILING MOUNTED EMERGENCY LIGHTS WERE INTERMITTENT. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M) - [SDR USAA970377](https://openairdocs.org/sdr/USAA970377.md): Longeron · cracked · Dec 18, 1997 · N933VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - DURING C-3 CHECK, FOUND 1 INCH CRACK STATION 1109 BETWEEN 3-4 RT LONGERONS. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 27 (10 INCHES BY 7 INCHES). (M) - [SDR USAAD97065](https://openairdocs.org/sdr/USAAD97065.md): Battery Pack · discharged · Apr 3, 1997 · N933VJ · Doug DC931 · Emergency Lighting > SAV - FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M) - [SDR USAA960777](https://openairdocs.org/sdr/USAA960777.md): Angle · corroded · Dec 6, 1996 · N933VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-1, C-2 CHECK, FOUND SKIN BULGE AT CUSP ANGLE AT STATION 996, LONGERON 18R. SPLICED IN NEW SECTION OF CUSP ANGLE PER SRM 53-05 FIG 25. CORROSION TASK NR C50-53300, CORROSION LEVEL 1. (M) - [SDR USAAD96110](https://openairdocs.org/sdr/USAAD96110.md): Door · not latched · Jul 26, 1996 · N933VJ · Doug DC931 · Electrical/Electronic Compartment Doors > FLT NR 7003 - BNA-BOS - AFTER TAKEOFF, GOT VIBRATION FROM NOSE AREA. RETURNED TO FIELD. CLOSED E/E COMPT DOOR. (M) - [SDR USAAD96019A](https://openairdocs.org/sdr/USAAD96019A.md): Press Amplifier · failed · Feb 4, 1996 · N933VJ · Doug DC931 · Cabin Pressure Control System > LGA - FL 8002 - CREW REPORTED, THAT THE AIRCRAFT WOULD NOT PRESSURIZE ABOVE 10,000 FEET. FLIGHT DIVERTED TO LGA AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE AMPLIFIER. (M) - [SDR USAAD96019](https://openairdocs.org/sdr/USAAD96019.md): Pressurization · malfunctioned · Feb 4, 1996 · N933VJ · Doug DC931 · Cabin Pressure Control System > LGA - FLT 8002 - CREW REPORTED, THAT THE AIRCRAFT WOULD NOT PRESSURIZE ABOVE 10,000 FT. FLIGHT DIVERTED TO LGA AND LANDED WITH NO FURTHER INCIDENT. (M) - [SDR USAA950851](https://openairdocs.org/sdr/USAA950851.md): Angle · cracked · Jul 26, 1995 · N933VJ · Doug DC931 · Vertical Stabilizer > PIT - DURING C-1 CHECK INSPECTION, FOUND.5 INCH CRACK IN VERTICAL STAB ATTACH ANGLE VERTICAL LEG AFT END LEFT SIDE. INSTALLED DOUBLER REPAIR 14 INCHES IN LENGTH PER SRM 53-05 FIG 23A. (M) - [SDR USAA950540](https://openairdocs.org/sdr/USAA950540.md): Oil Tank Assy · leaking · May 30, 1995 · N933VJ · Doug DC931 · Engine Oil Storage (Airframe Furnished) > DAY - FLT NR 0152 - FLIGHT DIVERTED TO DAY DUE TO THE NR 2 ENGINE OIL PRESSURE DECREASING. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE OIL TANK DUE TO LEAKAGE. LEAK CHECKED GOOD. (M) - [SDR USAA950237](https://openairdocs.org/sdr/USAA950237.md): Control Cable · frozen · Mar 9, 1995 · N933VJ · Doug DC931 · Landing Gear Retraction/Extension System > DTW - FLT 1698 - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. CREW RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE FOUND LANDING GEAR CONTROL CABLE IN THE RIGHT WHEEL WELL FROZEN. THE OBSTRUCTION WAS CLEANED. AIRCRAFT OKAY FOR SERVICE. (X) - [SDR USAA950042](https://openairdocs.org/sdr/USAA950042.md): Schader Vlv · leaking · Jan 25, 1995 · N933VJ · Doug DC931 · Nose/Tail Landing Gear Strut/Axle > SWF - FLT 1522 - ON TAKEOFF, THE NLG WOULD NOT RETRACT. FLIGHT RETURNED TO SWF. MAINTENANCE FOUND THE NLG STRUT FLAT, AND SERVICED THE STRUT WITH NITROGEN. THE SCHRADER VALVE WAS REPLACED. LEAK CHECKED GOOD. (W) ## 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 = 'N933VJ' AND deregistration_id = 'N933VJ-2003-07-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N933VJ-2003-07-17/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.