N919VJ, cancelled Jan 30, 2003

Service difficulty reports · 18

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 = 'N919VJ' AND deregistration_id = 'N919VJ-2003-01-30'
  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 USAAD01041Battery · dischargedPIT - FOUND THE COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Feb 28, 2001 · N919VJ · Doug DC931 · Emergency LightingSDR USAAD00061Battery · dischargedIND - THE SERVICE DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Apr 24, 2000 · N919VJ · Doug DC931 · Emergency LightingSDR USAA991012Skin · crackedPIT - DURING RON FOUND 3 CRACKS 2.5 INCH BY 1 INCH LONG AT STATION 58.750 LT, LONGERON 18/19. INSTALLED DOUBLER AND FILLER PER SRM 53-01 FIG 2 SHEET 3, PAGE 9. (M)Aug 24, 1999 · N919VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA990222Support · corrodedPIT - DURING Q-1 CHECK, FOUND RIGHT LAV CENTER FLOOR SUPPORT CORRODED AND CRACKED .75 INCH AT STATION 965. CORROSION LEVEL 1, CORROSION TASK NR C58-5330. CLEANED CORROSION, TREATED AND PRIMED PER SRM. MANUFACTURED NEW FLOOR SUPPORT TAB FROM 7075-T6.040 PER Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990201Jamb · damagedPIT - DURING Q-1 CHECK, FOUND SMALL HOLE IN AFT CARGO DOOR JAMB WEB JUST ABOVE 29 RIGHT. REMOVED DAMAGED SECTION OF WEB, MANUFACTURED NEW WEB PIECE FROM C/C 109-5712. MADE SPLICES FROM 7075-T6 .050 INCH AND INSTALLED PER EA NR 51599. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990200Frame · crackedPIT - DURING Q-1 CHECK, FOUND .5 INCH LENGTH BY .21875 INCH WIDE BY .019 INCH DEEP CHAFE IN FRAME NR 1059 LONGERON 15L. INSTALLED DOUBLER PER SRM 53-01, FIG 2 SHEET 4 AND EA 51616. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Main, FrameSDR USAA990199Cusp · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN CUSP MEMBRANE LEFT BETWEEN STATION NR 935 AND 945. FABRICATED CUSP MEMBRANE AND INSTALLED PER EA 51628. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990198Bracket · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK ON TAIL INTERIOR ON VERTICAL ATTACH BRACKET FOR 'Y' DUT STATION 1087 BELOW 5R. REPLACED DEFECTIVE PART WITH IDENTICAL PART NUMBER. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990197Frame · chafedPIT - DURING Q-1 CHECK, FOUND CHAF .372 INCH BY .196 INCH WIDE BY .029 INCH DEEP AT FRAME 1019 BELOW LONGERON 13R. CUT OUT DAMAGE AREA OF FRAME AND SPLICED IN A NEW SECTION OF FRAME AND SPLICED IN A NEW SECTION OF FRAME PER SRM 53-03 FIG 4. (M0Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Main, FrameSDR USAA990196Cusp · crackedPIT - DURING Q-1 CHECK, FOUND CRACKS 1.75 AND 3.5 INCH LEFT SIDE OF CABIN STATION 598 CUSP MEMBRANE. CUT OUT AND INSTALLED NEW SECTION PER EA 51628. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990195Intercostal · crackedPIT - DURING Q-1 CHECK, FUOND 1.25 INCH CRACK IN INTERCOSTAL BETWEEN CABIN FLOORBEAMS NR 965-980, C/L OF A/C UPPER FLANGE. INSTALLED DOUBLER MANUFACTURED FROM 7075T6 .032 INCH PER SRM 53-01, FIG 2. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990194Strap · corrodedPIT - DURING Q-1 CHECK, FOUND CORROSION ON CARGO TIE DOWN STRAP .75 INCH DIAMETER BY .008 DEEP AT LEFT SIDE BETWEEN STATION 897-925 ON STRAP. CORROSION LEVEL 1, CORROSION TASK NR C57-53300. SPLICED IN NEW PART MANUFACTURED SPLICE ANGLES AND INSTALLED PER DRAMar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990193Support · corrodedPIT - DURING Q-1 CHECK, FOUND 41.5 INCH LONG, LEVEL 1 CORROSION AT ENTRANCE FLOOR SUPPORT 39 EXTRUSION, LIGHT CORROSION FULL LENGTH. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. REPLACED SUPPORT WITH MODIFIED PART NR 992348429. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990192Support · corrodedPIT - DURING Q-1 CHECK, FUOND 4.5 INCH LONG, LEVEL 1 CORROSION AT ENTRANCE FLOOR SUPPORT 23 EXTRUSION, LIGHT CORROSION FULL LENGTH. CORROSION LEVEL 1, CORROSION TASK NR C46-533013. REPLACED SUPPORT WITH MODIFIED PART NR S265247912000. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAAD98127Battery · dischargedPIT - THE FLOOR LEVEL EMERGENCY LIGHTS ROW 16 THROUGH ROW 21 AND THE CEILING EMERGENCY LIGHTS ROW 9 THROUGH ROW 12 WERE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN BUTT SPLICE FOR THE FLOOR LEVEL EMERGENCY LIGHTS AND REPLACED FLOOR LEVEL AND CEILING EMERGENCY Jul 20, 1998 · N919VJ · Doug DC931 · Emergency LightingSDR USAAD98056Slide · inoperativePIT - AFT ESCAPE SLIDE FAILED TO DEPLOY DURING OPERATIONAL TEST. MAINTENANCE REPLACED THE SLDIE ASSEMBLY. TWO ADDITIONAL OPERATIONAL TESTS WERE SCHEDULED. (M)Mar 9, 1998 · N919VJ · Doug DC931 · Escape SlideSDR USAAD97230Apu · smokingCMH - FL 818 - AFTER T/O THE CREW NOTICED THE SMELL OF BURNED OIL IN THE COCKPIT. THE FLT ATTENDANTS NOTICED SMOKE IN THE CABIN AND BOTH LAVATORY SMOKE DETECTORS WENT OFF. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MX INSPECTED BOTH LEFDec 4, 1997 · N919VJ · Doug DC931 · APU Core EngineSDR USAAD95005Retract Mech · malfunctionedCLT - FLT 880 - AFTER RETRACTING GEAR, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON. THE CAPTAIN DECIDED TO RETURN TO CLT. THE FLT LANDED WITHOUT FURTHER INCIDENT. RECYCLED LEFT MAIN GEAR THROUGH 5 CYCLES ON GROUND. GEAR INDICATION NORMAL. AIRCRAFT OK FOR Oct 21, 1995 · N919VJ · Doug DC931 · Landing Gear Retraction/Extension System
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