N912VJ, cancelled Feb 7, 2005
Service difficulty reports · 27
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 = 'N912VJ' AND deregistration_id = 'N912VJ-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.
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 = 'N912VJ' AND deregistration_id = 'N912VJ-2005-02-07' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAAD00115Light · inoperativeIND - THE SERVICE DOOR EVACUATION SLIDE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE BETWEEN THE LIGHT ASSEMBLY AND THE SWITCH. (M)SDR USAAD00037Power Supply · failedIND - THE RIGHT NACELLE SCAN LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FOR THE RIGHT NACELLE SCAN LIGHT. (M)SDR USAAD99071Light · dischargedPHL - THE GALLEY SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE GALLEY SERVICE DOOR EMERGENCY LIGHT ASSEMBLY. (X)SDR USAA990352Frme · crackedPIT - DURING C-6 CHECK, FOUND 2 INCH CRACK IN BELLFRAME AT STATION 1074 LONGERON 14R. INSTALLED A REPAIR DOUBLER PER SRM 53-03 FIG 30. (M)SDR USAA990351Frame · crackedPIT - DURING C-6 CHECK, FOUND TWO 1 INCH CRACKS IN BELLFRAME STATION 1076 LONGERON 14L. STOP DRILLED CRACKS AND INSTALLED A DOUBLER PER EA 51889. (M)SDR USAAD98128Valve Pulley · blockedPIT - FLT 972 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE GEAR WAS CYCLED TWICE, BUT WOULD NOT RETRACT. THE FLIGHT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPOSITIONED A TEMPORARY HYDRAULIC LINE IN THE RIGHT WHEEL WELL THSDR USAAD97123Control Handle · jammedPIT - FLT 1266 - AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE PRESSURIZATION CONTROL HANDLE JAMMED AND FREED IT. (X)SDR USAAD97112Downlock Switch · failedATL/CLT - FLT 703 - ON FINAL INTO CLT, DID NOT RECEIVE NOSE DOWN AND LOCKED INDICATION. RECYCLED GEAR, NO CHANGE. VERIFIED DOWN AND LOCKED THROUGH VIEW PORT. REPLACED DOWNLOCK SWITCH. (X)SDR USAA970173Angle · gougedPIT - DURING Q1 CHECK, FOUND GOUGES AT LEFT LAV STA 984 CUST ANGLE. REPAIRED PER EA 46857 SRM 53-05 FIG 25. INSTALLED ANGLE AND STRAP. (X)SDR USAA970172Bulkhead · chafedPIT - DURING Q1 CHECK, FOUND CHAFE .50 INCH LONG BY .016 INCH DEEP AFT SIDE OF REAR PRESSURE BULKHEAD JUST FWD AND ABOVE THE 'X' FEED VALVE. INSTALLED DOUBLERS PER EA 46859. (X)SDR USAA970171Belt Frame · chafedPIT - DURING Q1 CHECK, FOUND DEEP CHAFE IN BELT FRAME AT STA 332 ABOVE LONGERON 30. INSTALLED SPLICE BETWEEN LONGERON 28L AND LONGERON 26R PER SRM 53-03 FIG 2A. (X)SDR USAA970170Bulkhead · gougePIT - DURING Q1 CHECK, FOUND .010 INCH DEEP GOUGE ON THE AFT PRESS BULKHEAD FWD FACE BEHIND THE RIGHT THRUST REVERSER PULLEY. INSTALLED DOUBLER PER EA 46791. (X)SDR USAA970169Bulkhead · gougePIT - DURING Q1 CHECK, FOUND .018 INCH GOUGE ON THE AFT PRESS BULKHEAD FWD FACE BEHIND THE LEFT THRUST REVERSER PULLEY SECTOR. INSTALLED DOUBLER PER EA 46791. (X)SDR USAA970168Cusp Membrane · crackedPIT - DURING Q1 CHECK, FOUND CRACK IN CUSP MEMBRANE RIGHT SIDE STA 945 TO STA 965. REPLACED CUSP MEMBRANE WITH MANUFACTURED ONE PER EA 46691. (X)SDR USAA970167Cusp Membrane · crackedPIT - DURING Q1 CHECK, FOUND CRACK IN CUSP MEMBRANE AT RT SIDE STA 589. REPLACED MEMBRANE WITH MANUFACTURED ONE PER EA 46691. (X)SDR USAA970166Skin · crackedPIT - DURING Q1 CHECK, FOUND CRACK IN RIVET HOLE AT STA 719 SKIN CLIP RT SIDE OF LONGERON 1R. INSTALLED DOUBLER 6.50 INCHES BY 4.50 INCHES PER SRO 9530129. (X)SDR USAA970165Longeron · crackedPIT - DURING Q-1 CHECK, FOUND CRACK IN LONGERON 17L AT STA 945. SPLICED IN NEW SECTION OF LONGERON BETWEEN STA 929 AND STA 970 PER 543-02 FIG 2. (X)SDR USAA970164Longeron · crackedPIT - DURING Q-1 CHECK, FOUND 2 CRACKS .25 INCH LONG AT STA 389 AND STA 408, LONGERON 17R. SPLICED IN NEW SECTION OF LONGERON BETWEEN STA 389 AND STA 415, LONGERON 17R PER SRM 53-02 FIG 2. (X)SDR USAA970044Skin · crackedPIT - DURING B-CHECK, FOUND 1.5 INCH CRACK IN VETICAL SKIN PANEL AT LEFT SIDE, VERTICAL STABILIZER SKIN, BENEATH DRAG ANGLE. REPAIRED DOUBLER .032 TITANIUM PER EA 46218. (M)SDR USAA970043Angle · crackedPIT - DURING B-CHECK, FOUND .75 INCH CRACK AT LEFT VERTICAL STABILIZER DRAG, DORSAL FIN, ANGLE JUST AFT OF STATION 1076. REPAIRED FOR MFG DRWG ANGLE AND DOUBLERS PE EA 46217. (M)SDR USAAD97008Press Controller · failedFLT 536 - PIT-SYR - AIRCRAFT DID NOT PRESSURIZE AFTER TAKEOFF. RETURNED TO FIELD. MEL'D PRIMARY PRESS CONTROL. REPLACED NR 2 PRESS CONTROLLER 1/12/97. (M)SDR USAAD97002Switch · failedFLT 1146 - ATL-PIT - LEFT ENGINE OIL QTY STARTED A STEADY DECREASE 15 MINUTES AFTER TAKEOFF. DIVERTED TO TYS. OIL PRESSURE STARTED TO OSCILLATE RAPIDLY ONE MINUTE BEFORE LANDING, SO THE ENGINE WAS SHUT DOWN. FOUND LEFT ENGINE OIL PRESSURE SWITCH FAILED. RESDR USAAD96184Latch · wornFLT 1035 - CLT-SAV - ON GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ON. RETURNED TO CLT. FOUND LEFT MAIN STRIKER WORN ON DOOR LATCH MECHANISM. REPLACED DOOR LATCH ASSEMBLY. (M)SDR USAAD96112Battery Pack · dischargedFORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK. (M)SDR USAAD96069Battery Pack · dischargedLEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE EMERGENCY LIGHT BATTERY PACK. (X)SDR USAAD96066Battery Pack · dischargedLEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE EMERGENCY LIGHT BATTERY PACK. (X)SDR USAA960260Angle · crackedPIT - DURING C-3 CHECK INSPECTION, FOUND 1.5 INCH CRACK IN LEFT DORSAL FIN DRAG ANGLE AT STATION 1126. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-05 PG 506. (M)
Back to N912VJ, cancelled Feb 7, 2005