N982VJ

Service difficulty reports not matched to an aircraft · 38

They name N982VJ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N982VJ' AND registry_match IS NULL
  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 USAAD00039Battery · dischargedIND - THE RIGHT EXTERIOR EMERGENCY LIGHTS WERE INOPERATIVE, AFT CARGO CEILING. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Mar 7, 2000 · N982VJ · Doug DC931 · Emergency LightingSDR 2000ZZZX355Frame · crackedPIT - DURING A CHECK, FOUND 3 INCH CRACK IN TAIL CONE ATTACH FRAME RT SIDE AT RUDDER ACTUATOR ATTACH POINT. CUT OUT DAMAGE. SPLICED IN SECTION PER DOUGLAS DRAWING 9911843. (X)Dec 29, 1999 · N982VJ · Doug DC931 · Fuselage Main, FrameSDR USAA991217Jamb · crackedPIT - DURING RON, FUOND 1.5 INCH CRACK ON SKIN AND DOUBLER AT FORWARD PASS ENTRANCE DOOR JAMB UPPER FORWARD CORNER. INSTALLED DOUBLERS PER SRM 53-05 FIG 26. (M)Oct 29, 1999 · N982VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAAD99101Battery · dischargedIND - THE AFT OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT OVERWING EMERGENCY EXIT LIGHT BATTERIES. (M)Jul 24, 1999 · N982VJ · Doug DC931 · Emergency LightingSDR USAAD99083Battery · dischargedDAY - THE LEFT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE LEFT NACELLE EMERGENCY LIGHT. (X)Jun 21, 1999 · N982VJ · Doug DC931 · Emergency LightingSDR USAAD99048Retract Mech · malfunctionedDAY-PHL - FLT 648 - AFTER TAKEOFF AND UPON RETRACTING, THE LANDING GEAR THERE WAS A VIBRATION COMING FROM THE NOSE GEAR AREA. THE CAPTAIN DECIDED TO RETURN TO THE FIELD. THE VIBRATION CONTINUED UNTIL THE NOSE GEAR WAS EXTENDED AT ABOUT 180 KTS WHEN THE VIBRAMar 26, 1999 · N982VJ · Doug DC931 · Landing Gear Door Retract SectionSDR USAAD99032Battery Charger · failedIND - THE AFT SECTION OF THE FLOOR TRACK EMERGENCY LIGHTS WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT FLOOR TRACK EMERGENCY LIGHT BATTERY CHARGER. (M)Feb 28, 1999 · N982VJ · Doug DC931 · Emergency LightingSDR USAAD98050Retract Mech · malfunctionedIND - FLT 942 - AFTER TAKEOFF AND THE LANDING GEAR RETRACTED, THE FLIGHT CREW EXPERIENCED SEVERE VIBRATION FROM THE NOSE GEAR AREA. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT NOSE GEAR DOOR OPEN. THE NOSE GEARMar 23, 1998 · N982VJ · Doug DC931 · Landing Gear Door Retract SectionSDR USAAD98009Bungee Cylinder · failedPIT - FLT 1777 - DURING CLIMB-OUT THROUGH 11,000 FT, THE RIGHT GEAR AND GEAR DOOR UNSAFE LIGHT ILLUMINATED. ABNORMAL PROCEDURES WERE FOLLOWED AND THE AIRCRAFT RETURNED TO THE FIELD. UPON GEAR EXTENSION ALL THREE GEAR INDICATED DOWN AND LOCKED AND THE AIRCRAFJan 18, 1998 · N982VJ · Doug DC931 · Landing Gear Retraction/Extension SystemSDR USAAD97222Battery · dischargedROC - FOUND AFT SECTION OF EMERGENCY LIGHTING SYSTEM INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND REPAIRED BROKEN WIRES. (M)Nov 29, 1997 · N982VJ · Doug DC931 · Emergency LightingSDR USAAD97199Battery · dischargedPHL - EMERGENCY COCKPIT OVERHEAD LIGHT DOES NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK. (M)Nov 15, 1997 · N982VJ · Doug DC931 · Emergency LightingSDR USAAD97171Battery · dischargedIND - FOUND LEFT ENGINE INLET EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)Sep 27, 1997 · N982VJ · Doug DC931 · Emergency LightingSDR USAAD97120Electrical Power · lostPIT/MHT - FLT 1180 - AFTER TAKEOFF, RT ENGINE GEN OFF LIGHT AND CROSS-TIE LOCK OUT. LOST PRESSURIZATION. RT ENGINE SHUT DOWN DUE TO PERCEIVED LOSS OF OIL PRESSURE AND OIL QUANTITY. RESTARTED ENGINE AFTER 10 MINUTES. RETURNED TO PIT. RAN RT ENGINE, VOLTS AJul 12, 1997 · N982VJ · Doug DC931 · AC Power Distribution SystemSDR USAAD96092Door Target · out of adjustFLT 8560 - PIT-MCO - ON CLIMB, GEAR DOOR OPEN LIGHT ILLUMINATED. DIVERTED TO CLT. ADJUSTED RIGHT GEAR DOOR TARGET. PERFORMED GEAR SWING, CHECKED GOOD. (M)Jun 29, 1996 · N982VJ · Doug DC931 · Landing Gear Position and WarningSDR USAAD96010Relay · failedPIT - ON GEAR EXTENSION CREW RECEIVED THREE UNSAFE GEAR INDICATIONS. CREW CYCLED THE GEAR AND RECEIVED THREE SAFE INDICATIONS. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE R2-28 LANDING GEAR LEVER RELAY, AND SWUNG THE GEAR. (M)Jan 23, 1996 · N982VJ · Doug DC931 · Landing Gear SelectorSDR USAA950893Frame · corrodedPIT - DURING Q-3/CX-2 INSPECTION, FOUND LEVEL 2 CORROSION AT BELTFRAME 20 INCHES BY 2 INCHES BETWEEN LONGERON 27L AND 27R AT STATION 980 (CORROSION TASK REF C51-53300). CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM 53-03 PG 4A FIG 2A. (M)Jul 10, 1995 · N982VJ · Doug DC931 · Fuselage Main, FrameSDR USAA950885Keel Beam · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND 2 INCH CRACK RT SIDE OF KEEL BEAM RIB. INSTALLED ANGLE DOUBLER REPAIRS PER SRM 53-03 FIG 12. (M)Jul 10, 1995 · N982VJ · Doug DC931 · Fuselage Main, KeelSDR USAA950884Clips · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 3 INCH CRACKS IN SKIN CLIPS AT STATION 637 LONGERON 26L AND STATION 658 LONGERON 25L. INSTALLED ANGLE DOUBLERS PER SRM 53-03 PAGE 51. (M)Jul 10, 1995 · N982VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950883Angle · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 2 INCH CRACKS IN ATTACH ANGLES INNER VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLES LEFT AND RT AT STATION 1076. REPAIRED ATTACH ANGLES PER SRM 53-05 FIG 90 AND USAIR EO 5388X223. (M)Jul 10, 1995 · N982VJ · Doug DC931 · Vertical StabilizerSDR 95ZZZM496Angle · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 2 INCH CRACKS IN ATTACH ANGLES INNER VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLES LEFT AND RT AT STATION 1076. REPAIRED ATTACH ANGLES PER SRM 53-05 FIG 90 AND USAIR EO 5388X223. REF USAA950883.Jul 10, 1995 · N982VJ · Doug DC931 · Vertical StabilizerSDR USAA950879Track · wornPIT - DURING Q-3/CX-2 INSPECTION, FOUND 20 INCH BY 20 INCH FIRST OFFICERS FORWARD AND AFT INBOARD AND OUTBOARD SEAT TRACK WORN STATION 110-140. INSTALLED DOUBLER REPAIRS PER DOUGLAS DRAWING 995-7855. (M)Jun 23, 1995 · N982VJ · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR USAA950878Track · wornPIT - DURING Q-3/CX-2 INSPECTION, FOUND 20 INCH BY 2 INCH WEAR IN PILOTS FORWARD AND AFT INBOARD AND OUTBOARD SEAT TRACK STATION 110-140. INSTALLED DOUBLERS PER DOUGLAS DRAWING 9957855. (M)Jun 23, 1995 · N982VJ · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR USAA950876Skin · puncturePIT - DURING Q-3/CX-2 INSPECTION, FOUND .25 INCH SKIN PUNCTURE STATION 985 AT LONGERON 17 R. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 12B. (M)Jun 23, 1995 · N982VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA950894Frame · corrodedPIT - DURING Q-3/CX-2 INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH RIGHT LAV STATION 980 FLOOR BEAM AROUND SCREW HOLES IN FLOOR BEAM. CUT OUT DAMAGE AND INSTALLED FILLERS AND DOUBLERS PER SRM 53-05 FIG 20D. (M)Jun 22, 1995 · N982VJ · Doug DC931 · Fuselage Main, FrameSDR USAA950892Floor Beam · corrodedPIT - DURING Q-3/CX-2 INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH STATION 980 LEFT LAV INBOARD SCREW HOLE IN FLOOR BEAM. CUT OUT DAMAGED AREA AND INSTALLED FILLERS AND DOUBLER PER SRM 53-10-19. (M)Jun 22, 1995 · N982VJ · Doug DC931 · Fuselage Main, Floor BeamSDR USAA950890Skin · dentedPIT - DURING Q-3/CX-2 INSPECTION, FOUND DENT IN FUSELAGE SKIN 3 INCHES BY 2.5 INCHES BY .187 INCH DEEP AT STATION 996 LONG 18R. INSTALLED .032 INCH TITANIUM DOUBLER PER SRM 53-04 FIG 38. (M)Jun 22, 1995 · N982VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA950886Blkhd Panel · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND STATION 965 BULKHEAD LOWER PORTION 1 INCH CRACK IN PANEL. CUT OUT DAMAGED AREA AND FABRICATED NEW PANEL AND INSTALLED PER SRM 53-03 FIG 19. (M)Jun 22, 1995 · N982VJ · Doug DC931 · Fuselage Main, BulkheadSDR USAA950882Beltframe · chafedPIT - DURING Q-3/CX-2 INSPECTION, FOUND 2 INCH BY 2 INCH CHAFE IN BELTFRAME STATION 1059 AT LONGERON 22R. INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 26. (M)Jun 22, 1995 · N982VJ · Doug DC931 · Fuselage Main, FrameSDR USAA950881Beltframe · chafedPIT - DURING Q-3/CX-2 INSPECTION, FOUND 2 INCH BY 2 INCH CHAFE IN BELTFRAME AT STATION 1076 LONGERON 20R. INSTALLED SPLICE REPAIR PER SRM 53-03 FIG 26 - 3 SPLICE. (M)Jun 22, 1995 · N982VJ · Doug DC931 · Fuselage Main, FrameSDR USAA950880Rib · crackedPIT - DURNIG Q-3/CX-2 INSPECTION, FOUND 1 INCH CRACK AT VERTICAL STABILIZER LEADING EDGE LOWER RT RIB. INSTALLED DOUBLER REPAIR PER SRM 52-01. (M)Jun 22, 1995 · N982VJ · Doug DC931 · Vertical Stabilizer, Spar/RibSDR USAA950877Skin · damagedPIT - DURING Q-3/CX-2 INSPECTION, FOUND 6 INCHES BY 8 INCHES TEMPORARY REPAIR STATION 996 AT LONGERON 17R IN SKIN. REMOVED TEMPORARY REPAIR. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 17. (M)Jun 22, 1995 · N982VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA950875Clip · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 3 INCH CRACKS IN STATION 945 SKIN CLIPS BETWEEN LONGERON 14R AND 15R AND BETWEEN 15R AND 16R. REPLACED SECTION OF SKIN CLIPS PER SRM 51-10-04. (M)Jun 22, 1995 · N982VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950874Clip · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND 3 INCH CRACK AT STATION 945 SKIN CLIP AT LONGERON 45L AND 16. REPLACED SECTION OF SKIN CLIP PER SRM 51-10-04. (M)Jun 22, 1995 · N982VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950891Floor Beam · corrodedPIT - DURING Q-3/CX-2 INSPECTION, FOUND CORROSION 20 INCHES BY 20 INCHES STATION 180-200, FROM RT SIDE WALL SUB FLOOR BEAM. CLEANED CORROSION AND SPLICED IN FILLER AND DOUBLER PER SRM 51-10-2. (M)Jun 21, 1995 · N982VJ · Doug DC931 · Fuselage Main, Floor BeamSDR USAA950889Web · crackedPIT - DURING Q-3/CX-2 INSPECTION, FOUND .75 INCH CRACK IN WEB OF RHS FLAP AT XFS341. INSTALLED .090 INCH FILLER AND .063 INCH 7075T6 DOUBLER PER SRM 57-01 AND USAIR EA 30788. (M)Jun 21, 1995 · N982VJ · Doug DC931 · Leading Edge DevicesSDR USAA950888Skin · chafedPIT - DURING Q-3/CX-2 INSPECTION, FOUND SKIN CHAFE .014 BY .018 INCH DEEP 5 INCHES BY 1 INCH AT STATION 813 AND LONGERON 26L UNDER FILLET PANEL. INSTALLED DOUBLERS PER SRM 53-04 FIG 37. (M)Jun 21, 1995 · N982VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA950887Skin · chafedPIT - DURING Q-3/CX-2 INSPECTION, FOUND SKIN CHAFED .014 INCH DEEP 5 INCHES BY 1 INCH STATION 813 AT LONGERON 26R UNDER FILLET PANEL. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 37. (M)Jun 21, 1995 · N982VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA950205Eel Assembly · inoperativeCLT - THE EMERGENCY LIGHT AT THE PASSENGER ENTRY DOOR IS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (W)Mar 4, 1995 · N982VJ · Doug DC931 · Emergency Lighting
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