N495AJ, cancelled Mar 9, 2019
Service difficulty reports · 72
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 = 'N495AJ' AND deregistration_id = 'N495AJ-2019-03-09' 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 = 'N495AJ' AND deregistration_id = 'N495AJ-2019-03-09' 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 PCSA2016120701Sensor · defectiveDURING LANDING GEAR RETRACTION THE LT MLG RED LIGHT REMAINED ILLUMINATED. PERFORMED SUPPLEMENTAL PROCEDURESSDR PCSA2016070501Engine · fireEXCESSIVE VIBRATION FROM NR 3 ENGINE ON TAKEOFF ROLL. TOWER REPORTED SPARKS AND FLAMES FROM NR 3 ENGINE TAIL PIPE.SDR PCSA2015050801Hydraulic Line · looseHYDRAULIC SYS A FAILURE. DECLARED AN EMER. FOUND NR 1 ENG HYD PUMP PRESS LINE LOOSE IN NR 1 ENG PYLON. THE LINE WAS SECURED, THE HYD SYS SERVICED, ENG OPERATED, FLIGHT CONTROLS CYCLED & LEAK CHECKS PERFORMED IAW THE AMM.SDR PCSA2015050601Bolt · missingNOSE LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. REPLACED THE NOSE GEAR SENSOR ACTUATOR ARM BUSHING & BOLT. PERFORMED A LG OPERATIONAL CHECK IAW THE AMM.SDR SPUY201502180027Skin · crackedLT WING UPPER SKIN L/E CRACKED 1.5", WS 410.0.SDR SPUY201502180026Floorbeam · crackedMAIN CARGO COMPARTMENT FLOORBEAM CRACKED 3", BS 1183, RBR 24.5 NEAR WL 263.SDR SPUY201502130025Skin · crackedLEFT WING UPPER SKIN L/E CRACKED .3125" FROM WS 574.0 TO WS 601.5.SDR SPUY201502130024Skin · crackedLEFT WING UPPER SKIN L/E CRACKED .3125" FROM WS 574.0 TO WS 601.5.SDR SPUY2015021300024Skin · crackedENTRY DOORS, SERVICE DOOR SKIN LOWER PART CRACKED 2".SDR SPUY201502130023Skin · corrodedUPPER FUSELAGE SKIN CORRODED AT BS 1380.5.SDR SPUY201502130022Skin · crackedLEFT WING UPPER SKIN L/E CRACKED FROM WS 410.0 - 436.5.SDR SPUY201502130021Skin · crackedLEFT WING UPPER SKIN L/E CRACKED WS 464.0 - 491.5.SDR SPUY201502130020Skin · crackedLEFT WING UPPER SKIN L/E CRACKED "WS 546.5 - WS 574.0".SDR SPUY201502130019Spar · corrodedLEFT WING REAR SPAR UPPER FITTING SHOWS CORROSION FROM WS 627.0 TO WS 656.5 WBL 492.5, REF N/R 02747.SDR PCSA2014041501Flow Multiplier · seizedSMOKE & FIRE RT WW. EXTINGUISHER DEPLOYED TO PUT OUT FIRE FROM THE FLOW MULTIPLIER INLET. BURNED COMPONENTS REMOVED. REPLACEMENT IN WORK.SDR PCSA2014012001Unknown · vibrationVIBRATION FELT IN NR 1 POWER & FUEL LEVERS. VIBRATION REDUCED WHEN POWER REDUCED, ENG SHUT DOWN. WIND MILLED FOR 45 MINUTES WITH 30-35 PSI OIL PRESS.SDR PCSA2013082201Controller · failedOUT OF 11,000 FT, PRESSURIZATION IN AUTO MODE FAILED. RAN CHECK LISTS, CALLED COMPANY, STARTED GETTING CONTROL IN MANUAL MODE. MX REPLACED THE PRESSURIZATION CONTROLLER AND THE SYS CHECKED NORMAL IAW THE AMM.SDR PCSA2013081501Fire Warning · false indicationOUT OF FL 180, ENGINE NR 1 FIRE DETECTION LIGHT ILLUMINATED. RAN CHECKLIST, FAULT LIGHT EXTINGUISHED. MX CHECKED THE SYS IAW THE AMM, NO DISCREPANCIES NOTED. A VISUAL INSPECTION OF THE NR 1 FIRE LOOP WAS ACCOMPLISHED, NO DISCREPANCIES WERE FOUND. THE SYS ADSDR PCSA2013050601Bushing · missingAT FL 250 LOWER CARGO AFT COMPARTMENT FIRE WARNING ILLUMINATED AND REMAINED ON UNTIL SHORT FINAL INTO NAS. MAINTENANCE REMOVED CARGO FROM AFT COMPARTMENT. INSPECTED CARGO AND COMPARTMENT NO EVIDENCE OF FIRE/SMOKE NOTED. ACCOMPLISHED SMOKE DETECTION TEST IAWSDR PCSA2013020801Shutoff Valve · malfunctionedAFTER START, ENGINE NR 2 SHUTDOWN. MAINTENANCE REPLACED THE NR 2 ENGINE FUEL SHUTOFF VALVE PER THE B727 AMM.SDR SPUY20120907048Window Frame · corrodedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT - WINDOW FRAME SHOWS CORROSION (BS 720C - 720D, S-1213L) REF N/R 1411.SDR SPUY20120907047Skin · corrodedDURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER LOWER SKIN CORRODED AT STAB STA 152 REF N/R 1369.SDR SPUY20120907046Floorbeam · corrodedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPARTMENT, FLOORBEAM UPPER HORIZONTAL CHORD SHOWS CORROSION AT BS 870 RBL 3 REF N/R 1357.SDR SPUY20120907045Beam · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT - VERTICAL BEAM FWD FLANGE HAS A 1.5 INCH APPROX CRACK AT BS 1183 LBL 22 WL 222.20 REF N/R 1327.SDR SPUY20120905044Skin · corrodedDURING ROUTINE C CHECK INSPECTION, UPPER RUDDER LEFT SIDE SKIN SHOWS CORROSION STA 230 REF N/R 1397.SDR SPUY20120905043Fitting · corrodedDURING ROUTINE C CHECK INSPECTION: NOSE LANDING GEAR - FITTING SHOWS CORROSION AT BS 351 REF N/R 1395.SDR SPUY20120820042Frame · corrodedDURING ROUTINE C CHECK INSPECTION, LOWER NOSE COMPT - FRAME WEB CORRODED AT BS 351.2 LBL 9 RBL 18 REF NR 1292.SDR SPUY20120820041Spar · corrodedDURING ROUTINE C CHECK INSPECTION, WING CENTER SECTION REAR SPAR WEB CORRODED AT STA 870 LBL 30 REF NR 1099.SDR SPUY20120820039Spar · corrodedDURING ROUTINE C CHECK INSPECTION, LEFT WING LOWER REAR SPAR CORRODED AT WBL 90 REF NR 0582.SDR SPUY20120820038Frame · crackedDURING ROUTINE C CHECK INSPECTION, AIR CONDITIONING DISTRIBUTION BAY - FRAME HAS A 1 INCH CRACK AT BS 740 STRINGER 20 – 21L REF NR 0442.SDR SPUY20120820037Skin · crackedDURING ROUTINE C CHECK INSPECTION, RIGHT WING L/E SLAT NR 6 INTERNAL SKIN CRACKED 1 INCH AT SLAT STA 1674.0 REF NR 0379.SDR SPUY20120820036Skin · crackedDURING ROUTINE C CHECK INSPECTION, LEFT WING SLAT NR 3 LWR SKIN CRACKED 5/16 INCH APPROX AT SLAT STA 135.0 REF NR 0170.SDR SPUY20120820035Stiffener · corrodedDURING ROUTINE C CHECK INSPECTION, RIGHT WING FRONT SPAR AREA - STIFFENER CORRODED AT FS 232.0 REF NR 0133.SDR SPUY20120820034Frame · deformedDURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT- FRAME DEFORMED BS 580 STR 25L REF NR 0798.SDR SPUY20120820033Frame · deformedDURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT FRAME DEFORMED BS 560 STR 25L REF NR 0797.SDR SPUY20120820032Frame · deformedDURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT FRAME DEFORMED, BS 540 STR 24L REF NR 0796.SDR SPUY20120820031Torque Box · corrodedDURING ROUTINE C CHECK INSPECTION, VERTICAL FIN - TORQUE BOX INBOARD CHORD LEFT CORRODED STA 1342 FIN STA 0 AND FWD REAR SPAR CHORD REF NR 0642.SDR SPUY20120820030Shim · corrodedDURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER TRAILING EDGE UPPER BEAM SHIM CORRODED STAB STA 62 REF NR 0641.SDR SPUY20120820029Skin · corrodedDURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER REAR SPAR AND SKIN LOWER CHORD SHOWS CORROSION STAB STA 152 REF NR 0640.SDR SPUY20120820028Beam · wornDURING ROUTINE C CHECK INSPECTION, LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER BEAM WORN STAB STA 54 REF NR 0639.SDR SPUY20120820027Beam · corrodedDURING ROUTINE C CHECK INSPECTION, LEFT HORIZONTAL TRAILING EDGE BEAM SHOWS CORROSION STAB STA 128 REF NR 0638.SDR SPUY20120820026Spar · corrodedDURING ROUTINE C CHECK INSPECTION, RIGHT HORZ STAB - REAR SPAR AND SKIN LOWER CHORD CORRODED STAB STA 180 REF NR 0637.SDR SPUY20120820025Skin · nickedDURING ROUTINE C CHECK INSPECTION, RIGHT WING OUTBOARD AILERON UPPER SURFACE SHOWS NICKS BETWEEN STA WBL 492.5 AND 602.5 REF NR 0127.SDR PCSA20110301Engine · flamed outCREW LOG ITEM "ENGINE NR 3 SURGED 3 TIMES (EPR N1 & N2). ON THIRD SURGE ENGINE 3 FLAMED OUT (EPR DROP FOLLOWED BY N1 AND EGT). RESTARTED ENGINE AND INDICATIONS NORMAL FOR REMAINDER OF FLIGHT. ENGINE WINDMILLED FOR 10 MINS." MAINTENANCE INSPECTED THE ENGINESDR PCSA2010122101Clamp · looseNUMBER 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. MAINTENANCE RETORQED THE BLEED AIR HEAT EXCHANGER CLAMP, PERFORMED A LEAK AND OPERATIONAL CHECK ON AN ENGINE RUN-UP.SDR PCSA2010083001Tube · leakingNUMBER 1 ENGINE OIL QUANTITY STEADILY DECREASED DURING FLIGHT. ALSO OIL TEMP EXCESSIVE. ONLY DROPPED DURING POWER BACK. MAINTENANCE FOUND THE NUMBER 6 BEARING OUTER TUBE ON NUMBER 1 ENGINE LEAKING. THE TUBE PART NUMBER 793651 WAS REPLACED AND THE AIRCRAFT SDR PCSA2010072201Battery · dischargedPASSING THROUGH 3000 FT THE LOWER AFT CARGO FIRE ALARM SOUNDED. UPON LANDING MAINTENANCE PERFORMED OPS CHECK OF THE LOWER CARGO COMPT SMOKE DETECTION SYSTEM. FOUND NORMAL PER SECRURAPLANE CMM. NO FREIGHT IN AFT CARGO COMPT. PERFORMED VISUAL INSPECTION OF CSDR PCSA2009060401Flange · corrodedCORROSION FOUND ON RT MAIN WHEEL WELL OTBD AFT FLANGE AT STA 930 RBL 72 ABOVE MANUAL EXTENSION TORQUE TUBE. REMOVED SUPPORT FITTING FOR ACCESS. REMOVED CORROSION IAW SRM 51-30-2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW EO SIE-AJ-N495AJ-05-09 REV 1R. REPLACSDR PCSA2008120301Blade · brokenAMERIJET FLIGHT SXM - SJU NUMBER ONE ENGINE VIBRATION FOLLOWED BY HIGH FUEL FLOW. PERFORMED A PRECAUTIONARY SHUTDOWN. MAINTENANCE DISCOVERED A BROKEN C2 BLADE AND COMPRESSOR DAMAGE.SDR 2008032701Turbine Blades · failedFLT 433 MIA-BLA - CREW REPORTED, LOSS POWER ON NUMBER NR 3 ENGINE ON TAKEOFF. THE CAPTAIN REJECTED TAKEOFF ROLL AT APPROXIMATELY 10 KNOTS. AIRCRAFT RETURNED BACK TO AMERIJET LINE MAINTENANCE FACILITY WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MULTIPLE TURB
Back to N495AJ, cancelled Mar 9, 2019