N395AJ, cancelled Mar 9, 2019
Service difficulty reports · 70
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 = 'N395AJ' AND deregistration_id = 'N395AJ-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 = 'N395AJ' AND deregistration_id = 'N395AJ-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 PCSA2017120801Warning Light · illuminated#1 ENGINE SHUTDOWN (BY CREW)DUE TO OIL PRESSURE LIGHT ILLUMINATED.SDR SPUY201605060006Beam · corrodedLEFT HORIZONTAL STABILIZER T/E LOWER BEAM SHOWS CORROSION AT SEVERAL LOCATIONS.SDR SPUY201605060005Splice · corrodedWING TO BODY SPLICE PLATE ATTACH, UNDER WING TO BODY WITH CORROSION BS 870, WLB 70.5 LT REF N/R 0337.SDR SPUY201605060004Frame · corrodedWING CENTER FRONT SPAR LOWER CHORD, CENTER WING WITH CORROSION BS 740.00 LT LBL 20,SDR SPUY201605060003Plate · corrodedSPLICE PLATE ATTACHMENT UNDER WING TO BODY SHOW CORROSION AT BS 870, WLB 70.5.SDR PCSA2015011202Warning Light · illuminatedLEFT GEAR UNSAFE LIGHT.SDR PCSA2015011201Warning Light · illuminatedLEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED.SDR PCSA2014060501Compressor · stalledAT 3500’ NR 3 ENG COMPRESSOR STALL. RETARDED THRUST, SLOWLY INCREASED THRUST, COMPRESSOR STALLED AGAIN. THRUST AT IDLE, RETURNED TO MIAMI.SDR PCSA2014012201Flex Hose · rupturedLOSS OF B SYS HYD FLUID IN FLIGHT. DECLARED EMERGENCY & RETURNED TO MIA.SDR SPUY201302020026Spar · corrodedDURING ROUTINE C-CHECK INSPECTION, LT WING FRONT SPAR LOWER CHORD SHOWS CORROSION WS 383.5.SDR SPUY201302020025Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, CARGO BAY UPPER INNER SKIN SHOWS CORROSION BS 740, STRINGER 1 LT.SDR SPUY201302020024Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, CARGO COMPARTMENT INNER UPPER SKIN SHOWS CORROSION BS 740, S1R.SDR SPUY201302020023Stiffener · corrodedDURING ROUTINE C-CHECK INSPECTION, LT WING FRONT SPAR STIFFENER SHOWS CORROSION, WS 224.5.SDR SPUY201302020022Stiffener · corrodedDURING ROUTINE C-CHECK INSPECTION, LT WING FRONT SPAR STIFFENER CORRODED, WS 198.SDR SPUY201302020021Stiffener · corrodedDURING ROUTINE C-CHECK INSPECTION, RT WING FRONT SPAR STIFFENER SHOWS CORROSION, WS 212.SDR SPUY201302020020Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, LT WING NR 2 SLAT SKIN SHOWS CORROSION, WS 656.5, REF N/R 0440.SDR SPUY201302020019Fitting · corrodedDURING ROUTINE C-CHECK INSPECTION, RT WING L/E FLAP FITTING CORRODED, WS 198.0, WS 224.5 REF N/R 0393.SDR SPUY201302020018Fitting · corrodedDURING ROUTINE C-CHECK INSPECTION, RT WING L/E FLAP FITTING CORRODED WS 188.0, REF NR 0392.SDR SPUY201302020017Angle · corrodedDURING ROUTINE C-CHECK INSPECTION, RT WING L/E FLAP HOUSING ANGLE CORRODED, WS 171.5, WS 198.0.SDR SPUY201302020016Angle · corrodedDURING ROUTINE C-CHECK INSPECTION, RT WING FRONT SPAR ANGLE CORRODED WS 198.0, REF N/R.SDR SPUY201302020015Stiffener · corrodedDURING ROUTINE C-CHECK INSPECTION, RT WING FRONT SPAR STIFFENER SHOWS CORROSION WS 251.0.SDR SPUY201302020014Stiffener · corrodedDURING ROUTINE C-CHECK INSPECTION, RT WING FRONT SPAR STIFFENER SHOWS CORROSION WS 222.0.SDR SPUY201302020013Intercostal · corrodedDURING ROUTINE C-CHECK INSPECTION, RT MLG INTERIOR UPPER PART INTERCOSTAL SHOWS CORROSION FS 920.SDR SPUY201302020012Frame · corrodedDURING ROUTINE C-CHECK INSPECTION, CARGO COMPARTMENT. FRAME SHOWS CORROSION AT STA 1168 NEAR STRINGER S16R.SDR SPUY201302020011Structure · crackedDURING ROUTINE C-CHECK INSPECTION, LT WING LOWER CHORD (NEAR MLG SUPPORT BEAM) CRACKED 4 WS 244.5, REF N/R 0305.SDR SPUY201302020010Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, LOWER HALF FUSELAGE. RT UPPER AFT FUSELAGE SKIN SHOWS CORROSION FROM BS 1343 TO BS 1376.SDR SPUY201302020009Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, LT WING UPPER SKIN NEAR REAR SPAR SHOWS CORROSION WS 601.5, REF NR 0258.SDR SPUY201302020008Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, LT WING UPPER SKIN T/E NEAR OTBD AILERON CORRODED WBL 492.0, REF NR 0257.SDR SPUY201302020007Flap Track · corrodedDURING ROUTINE C-CHECK INSPECTION, LT WING LOWER SURFACE INBD FLAP TRACK COUPLING SHOWS CORROSION WS 304.0, REF N/R 0250.SDR SPUY201302020006Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, LT WING LOWER SURFACE SHOWS CORROSION WS 491.5 REF NR 0249.SDR SPUY201302020005Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, RT WING UPPER SKIN L/E SHOWS CORROSION L/E STA 130.7, REF NR 0183.SDR PCSA2012082403Seat Track · corrodedSEAT TRACK AT STA 360 TO 480 LBL 45.5 CORRODED.SDR PCSA2012082402Seat Track · corrodedSEAT TRACK AT STA 950 TO 950C LBL 24.7 CORRODED.SDR PCSA2012082401Seat Track · corrodedSEAT TRACK AT STA 689 CORRODED.SDR PCSA2012050301Splice · crackedFOUND 1.5 INCH CRACK AT STA 481 BETWEEN 13R AND 14R ON THE BUTT SPLICE.SDR PCSA2011011801Fire Detector · unsecureNR 1 STRUT OVERHEAT LIGHT ILLUMINATES WITH NR 1 ENGINE BLEED AIR VALVE CLOSED. MECH FOUND FIRE DETECTOR UNIT UN-SECURED. RE-RACKED AND SECURED FIRE DETECTOR UNIT, OPS CHECK GOOD.SDR PCSA2010120101Warning Light · illuminatedNR1 STRUT OVERHEAT LIGHT ILLUMINATED AT 33,000 FT. CLOSED NR 1 POWER LEVER AND LIGHT EXTINGUISHED. MX OPENED NR 1 PYLON, PRESSURIZED PNEUMATIC SYS CHECK FOR LEAKS, NONE NOTED IAW AMM 36-00-00. PERFORMED ENGINE RUN-UP AT PART POWER AND TAKEOFF. NO DEFECT NOTESDR PCSA2010110501Warning System · activatedNR 1 STRUT OVERHEAT LIGHT ILLUMINATED DURING CRUISE WITH ENGINE ANTI-ICE ON. WHEN THE ANTI-ICE WAS TURNED OFF THE LIGHT WENT OUT.SDR PCSA201010210Warning Light · illuminatedLOG ITEM LEFT ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. REDUCED THRUST LEVER PER PROCEDURE. LIGHT EXTINGUISHED AFTER APPROX 30 SECONDS. RETURNED TO MIA. MAINTENANCE REMOVED THE PYLON PANELS. PERFORMED LEAK CHECK. NO LEAKS NOTED. PERFORMED ENGINE RUN-UP ASDR PCSA2010011301Fire Warning · malfunctionedAFTER GEAR RETRACTION RECEIVED APU FIRE WARNING. FOLLOWED AMJ PRECEDURES. MAINTENANCE ACCOMPLISHED AN APU INSPECTION. NO SIGNS OF FIRE NOTICED. OPERATIONAL AND FUNCTION CHECKS WERE PERFORMED PER THE AMM ALL OK. THE APU FIRE BOTTLE WAS REPLACED.SDR PCSA2009051801Sensor · out of positionNR1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT. SHUTDOWN NR1 ENGINE AND RETURNED TO DEPARTURE. WINDMILLING 15 MINUTES, OIL PRESSURE WITHIN LIMITS. MX FOUND NR 1 STRUT SENSING ELEMENT OUT OF POSITION. THE ELEMENT WAS REPOSITIONED AND A PNEUMATIC LEAK CHECK WAS SDR PCSA2008093001Actuator · leakingLOST A HYDR SYS AFTER FLAP RETRACTION DEPARTING. ON APPROACH TO POS NR 7 L/E SLAT FAILED TO EXTEND. LANDING GEARS WERE EXTENDED MANUALLY, THE AC LANDED SAFELY AND WAS TOWED FROM THE RUNWAY. MAINT DISCOVERED THE NR 7 L/E ACTUATOR BODY HAD FAILED CAUSING A LOSSDR PCSA818200701Engine · malfunctionedFLIGHT 861 DEPARTED SJU AND DURING THE TOP OF THE CLIMB THE CREW REPORTED THE NUMBER 1 ENGINE OIL PRESSURE DROPPED TO ZERO, THE NUMBER 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT CONTINUED TO MIA AND LANDED WITHOUT INCIDENT. THE NUMBER 1 ENGINE WAS REMOVED AND REPSDR PCSA7090601Fuel Tank · leakingDURING THE MAINTENANCE WALK AROUND INSPECTION, A FUEL LEAK WAS DISCOVERED AT THE REAR SPAR OF THE NR 2 FUEL TANK (WING BOX CENTER SECTION). FURTHER INSPECTION REVELED CORROSION BEYOND LIMITS IN THE NR 2 FUEL TANK AT THE REAR SPAR. REPAIR WEB DOUBLER AND STIFSDR PCSA033006Engine · damagedFLIGHT 848 AFTER PUSHBACK FROM PAP, THE CREW REPORTED WHEN POWER WAS ADDED THE NUMBER ONE ENGINE EXPERIENCED A VIBRATION. THE AIRCRAFT RETURNED TO THE GATE WITHOUT ANY FURTHER INCIDENT. FURTHER INSPECTION OF THE NUMBER ONE ENGINE INLET FOUND THE C-1 BLADES HSDR PCSA708051Module · malfunctionedON DEPARTURE, CREW REPORTED STALL WARNING STICK SHAKER CAME ON AT ROTATION. CREW DUMPED FUEL, RETURNED AND LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUBLESHOT STALL WARNING SYSTEM. OPERATIONAL CHECK NORMAL IAW B-727 MM CH 34-18-01, UNABLE TO DUPLICATSDR PCSA6210501Oil System · leakingDURING CRUISE NR 3 ENGINE OIL TEMP WAS BETWEEN 125 & 130 DEG FOR 15 MINUTES. PERFORMED ALT PROCEDURES, RETARDED THROTTLE, DIDN'T HELP. SHUTDOWN NR 3 ENGINE, ENGINE WINDMILLED FOR 45 MIN. OIL PRESSURE STAYED ABOVE 25 PSI. DIVERTED & LANDED AT SJU. MX INSPESDR PCSA0518051Cover · leakingDURING CLIMB CREW REPORTED LOSS OF HYDRAULIC (A) SYSTEM. AIRCRAFT WAS DIVERTED AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND FEEL COMPUTER FILTER COVER LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED FEEL COMPUTER FILTER CAP AND O-RING IAW MM CH 20-10SDR COOSDR030158Skin · corrodedLT WING, LOWER SKIN, LOWER SURFACE, ACCESS DOOR CUTOUT CORRODED. (K)SDR COOSDR030159Frame · corrodedRT MAIN GEAR WHEEL WELL, STA 950 WL 201, FORGING FRAME, HORIZONTAL FLANGE, LOWER SURFACES CORRODED.
Back to N395AJ, cancelled Mar 9, 2019