N970VJ, cancelled Feb 7, 2005

Service difficulty reports · 23

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N970VJ' AND deregistration_id = 'N970VJ-2005-02-07'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR USAAD00070Light · inoperativeDTW - THE AFT OVERHEAD SECTION OF EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPAIRED THE WIRING TO THE EMERGENCY LIGHTS. (X)May 12, 2000 · N970VJ · Doug DC931 · Emergency LightingSDR USAAD00073Slide · dischargedDAY - THERE WAS NO PRESSURE IN THE TAILCONE EMERGENCY EVACUATION SLIDE ASSEMBLY. MAINTENANCE REPLACED THE TAILCONE EMERGENCY EVACUATION SLIDE ASSEMBLY. (X)May 11, 2000 · N970VJ · Doug DC931 · Escape SlideSDR USAAD00069Battery · dischargedIND - THE LEFT AND RIGHT EMERGENCY NACELLE LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)May 10, 2000 · N970VJ · Doug DC931 · Emergency LightingSDR USAA000358Skin · crackedPIT - FOUND CRACK .25 INCH LONG, AFT LOWER CORNER OF SERVICE DOOR. INSTALLED DOUBLERS PER SRO 09530172. (M)Mar 3, 2000 · N970VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA000359Spar · crackedPIT - FOUND CRACK 1.125 INCH LONG AT STATION 164 LEFT WING AFT SPAR LOWER OUTBOARD FLAP HINGE. REPAIR DOUBLER INSTALLED PER EO 5788D348. (M)Mar 3, 2000 · N970VJ · Doug DC931 · Wing SparSDR USAA000360Skin · crackedPIT - FOUND TWO CRACKS, .1875 INCH AND .375 INCH LONG, FORWARD UPPER CORNER OF SERVICE DOOR SKIN. INSTALLED DOUBLERS PER SRO 09530172. (M)Mar 3, 2000 · N970VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAADD99118Link · failedPIT-BNA - FLT 223 - ON GEAR RETRACTION AFTER TAKEOFF THE AIRCRAFT DEVELOPED A SEVERE VIBRATION IN THE NOSE GEAR AREA. THE VIBRATION INCREASED IN PROPORTION TO AIRSPEED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THEAug 21, 1999 · N970VJ · Doug DC931 · Landing Gear Door Retract SectionSDR USAAD99088Battery · dischargedIND - THE MAIN ENTRANCE DOOR SLIDE EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE MAIN ENTRANCE DOOR SLIDE EMERGENCY LIGHT BATTERY. (X)Jul 3, 1999 · N970VJ · Doug DC931 · Emergency LightingSDR USAA990389Structure · damagedPIT - DURING UNSCHEDULED MAINTENANCE, PILOT REPORT ENGINE FAILURE, DETROIT FOUND 22 INCH BY 8 INCH SECTION OF LT UPPER PYLON SKIN (SKIN, WEB PANEL AND ANGLES) TORN AT STATION 1038, DETECTED IN FLIGHT, PASSENGERS HEARD LOUD NOISE. INSTALLED DOUBLER OVER CUT OUApr 18, 1999 · N970VJ · Doug DC931 · Nacelle/Pylon StructureSDR USAAD99057Engine · failedDTW - PILOT RECORDED IN LOG BOOK THAT THE CABIN CREW HEARD A LOUD NOISE FROM THE LEFT SIDE OF THE AIRCRAFT. NO IRREGULARITIES WERE REPORTED FOR ENGINE READINGS. MAINTENANCE FOUND PARTS OF THE COWLING SKIN BLOW OUT NEAR THE 12 O'CLOCK POSITION. A 3 FT BY 6 IApr 16, 1999 · N970VJ · Doug DC931 · Engine (Turbine/Turboprop)SDR USAAD99044Retract Mech · iced upBUF-LGA - FLT 1731 - AFTER TAKEOFF AND LANDING GEAR RETRACTION THE LEFT GEAR INDICATED UNSAFE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEARS COVERED WITH ICE SLUSH. ALL THREE LANDING GEAR WERE DEICED AND OMar 10, 1999 · N970VJ · Doug DC931 · Landing Gear Retraction/Extension SystemSDR USAAD98219Battery · dischargedPHL - THE FIRST CLASS SECTION FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FIRST CLASS FLOOR EMERGENCY LIGHT BATTERY. (M)Dec 19, 1998 · N970VJ · Doug DC931 · Emergency LightingSDR USAAD98216Engine · failedLGA-CMH - FLT 1833 - DURING CRUISE, THE RIGHT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. THE CREW FOLLOWED THE ABNORMAL PROCEDURES BUT THE LIGHT REMAINED ON. THE OIL TEMPERATURE WAS RISING AND THE OIL QUANTITY DECREASING. THE ENGINE WAS SHUT DOWN AND THE ADec 16, 1998 · N970VJ · Doug DC931 · Engine (Turbine/Turboprop)SDR USAAD98202Tire · failedBOS-PIT - FLT 828 - ON ROTATION, THE NR 3 MAIN TIRE BLEW OUT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 3 MAIN TIRE AND WHEEL ASSEMBLY, RIGHT SHIMMY DAMPER, RIGHT LANDING GEAR SPRAY DEFLECTOR, NR 3 BRAKE LINENov 11, 1998 · N970VJ · Doug DC931 · TireSDR USAAD98196Retract Mech · failedDAY-PHL - FLT 648 - AFTER TAKEOFF AND GEAR RETRACTION THERE WAS EXCESSIVE VIBRATION FROM THE NOSE GEAR AREA. THE LANDING GEAR WAS CYCLED BUT DID NOT HELP. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SECURED THE RIGHT NOSE LANNov 2, 1998 · N970VJ · Doug DC931 · Landing Gear Door Retract SectionSDR USAAD98043Control Panel · failedIND - FLT 1120 - AFTER ROTATION WHILE CLIMBING OUT OF IND EN ROUTE TO PHL, CREW HAD TOTAL RADIO FAILURE. CREW WAS ABLE TO GET THE NR 3 RADIO TO PICK UP DELTA FLIGHT IN THE AREA AND ALTITUDE AND ROUTING INSTRUCTIONS WERE PASSED ALONG. FLIGHT DIVERTED TO PIT WMar 17, 1998 · N970VJ · Doug DC931 · Audio Integrating SystemSDR USAAD97146Screws · looseYYZ - 1806 - UPON APPROACH TO YYZ, CREW COULD NOT MOVE FLAPS BEYOND 0 DEGREES. CREW PERFORMED AN ABORTED APPROACH. SLATS OPERATED NORMALLY. CREW PERFORMED A NO FLAP LANDING AT YYZ WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THAT THE TWO SCREWS IN THE FLAP Aug 29, 1997 · N970VJ · Doug DC931 · Trailing Edge Flap Control SystemSDR USAA970075Skin · crackedPIT - DURING Q2 CHECK, FOUND NR 1 ADF ANTENNA HAS 4 HOLES WITH 1.125 INCH CRACK ON SKIN AND LONGERON. REPAIRED 4 FREEZE PLUGS INSTALLED PER EA NR 46195A. (M)Feb 26, 1997 · N970VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR 97ZZZM460Longeron · crackedPIT - DURING Q2 CHECK, FOUND NR 1 ADF ANTENNA HAS 4 HOLES WITH 1.125 INCH CRACK ON SKIN AND LONGERON. REPAIRED 4 FREEZE PLUGS INSTALLED PER EA NR 46195A. REF USAA970075.Feb 26, 1997 · N970VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAAD96032Line · crimpedPIT - FL 441 - AFTER TAKEOFF FROM PIT AND REACHING 6000 FEET, CREW COULD NOT PRESSURIZE THE AIRCRAFT. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND A CRIMPED SENSE LINE TO THE PRESSURE CONTROLLER. LINE WAS REPLACED AND REPOSIMar 25, 1996 · N970VJ · Doug DC931 · Cabin Pressure Control SystemSDR USAA960351Door Frame · crackedPIT - DURING C-6 CHECK INSPECTION, FOUND THREE .5 INCH CRACKS IN SKIN 7TH, 8TH AND 13TH RIVITS ABOVE STOP TOP FORWARD CORNER FORWARD CARGO DOR FRAME EDDY CURRENT INSPECTION. INSTALLED DOUBLER REPAIR PER USAIR EA NR 32409 AND SRO 09530117. (M)Mar 23, 1996 · N970VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA960350Longeron · crackedPIT - DURING C-6 CHECK INSPECTION, FOUND TWO .25 INCH CRACKS IN LONGERON 16R FRAME 427 AND LONGERON 17R FRAME 408, 427 EDDY CURRENT INSPECTION. INSTALLED NEW SECTIONS OF LONGERON 16R AND 17R PER SRM 53-02 FIG 2 AND USAIR EA NR 32408. (M)Mar 23, 1996 · N970VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA950365Control Cable · failedPIT - FLT NR 1206 - UPON GEAR RETRACTION, FLIGHT EXPERIENCED A LOUD NOISE AS THE NOSE GEAR WAS RETRACTED. CREW EXTENDED THE LANDING GEAR AND RETRACTED AGAIN AND RECEIVED AN UNSAFE NOSE GEAR LIGHT. FLIGHT RETURNED TO PIT. MAINTENANCE REPLACED THE LEFT NOSE GApr 8, 1995 · N970VJ · Doug DC931 · Landing Gear Door Retract Section
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