N598AJ, cancelled Feb 1, 2019
Service difficulty reports · 64
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 = 'N598AJ' AND deregistration_id = 'N598AJ-2019-02-01' 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 = 'N598AJ' AND deregistration_id = 'N598AJ-2019-02-01' 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 PCSA2014122201Engine · making metalENGINE NR 3 HAD A COMPRESSOR STALL & A FLAMEOUT AT FL320. METAL FOUND IN TAIL PIPE.SDR 3FMR20140903001Skin · corrodedDURING ACCOMPLISHMENT OF AD 85-24-02, CORROSION WAS FOUND IN LOWER SKIN BS 870, RBL 3 - 8, WATERLINE 160.8.SDR 3FMR20140903006Skin · corrodedDURING ACCOMPLISHMENT OF AD 82-24-02, CORROSION WAS FOUND IN THE LT AIR CONDITIONING PLENUM AREA ON THE LOWER SURFACE SKIN AT BS 826 - 848 AT LBL 32, W/L 160.8. FOUND TO BE OUT OF SRM LIMITS. REPAIRED IAW DWG AMJ-N598AJ - 04/ 14.SDR 3FMR20140903004Structure · corrodedDURING ACCOMPLISHMENT OF AD 2005-05-19, CORROSION WAS FOUND ON THE LT FRONT SPAR LOWER ANGLE AT WS 383 - 465. FOUND TO BE OUT OF SRM LIMITS. REPAIRED.SDR 3FMR20140903005Spar Cap · corrodedCORROSION WAS FOUND ON THE RT HORIZONTAL STABILIZER. CORROSION IS LOCATED AT HORIZONTAL STAB STATION 78.13. FOUND TO BE OUT OF MFG SRM LIMITS. REPAIRED IAW DWG 55-14215-1A.SDR 3FMR20140903003Skin · corrodedRIGHT WING LOWER SKIN WAS FOUND CORRODED AROUND FRONT SPAR ATTACH FASTENERS LOCATED AT WING STA 509 - 519. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS. REPAIRED IAW DWG AMJN598AJ 3/14.SDR 3FMR20140903002Spar · corrodedDURING ACCOMPLISHMENT OF AD 2005-05-19, CORROSION WAS FOUND ON THE RIGHT HAND WING, FRONT SPAR, LOWER CHORD AT WING STATION 509 TO 519. CORROSION WAS FOUND OUTSIDE OF MANUFACTURER SRM LIMITATIONS. A DESIGNATED ENGINEERING REPRESENTATIVE REPAIR HAS BEEN SOUGHT.SDR PCSA2013092501Duct · rupturedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. FOUND DUCT RUPTUREDSDR PCSA2013051001Fuel Control · faultyENGINER 2 FLAMEOUT AT CRUISE. ALL PARAMETERS NORMAL. ENG WINDMILL FOR ABOUT 15 MIN. 20 PSI OIL PRESS. THE NR 2 ENGINE OIL FILTER WAS CHECKED, FOUND NORMAL, THE NR 2 FUEL PUMP AND FUEL CONTROL UNIT REPLACED AND TESTED PER THE B727 AMM AND THE AIRCRAFT RETURNSDR PCSA2012072101Connector · damagedENGINE NR 2 FIRE WARNING BELL AND LIGHT ACTUATED IN FLIGHT.SDR PCSA2012072001Connector · defectiveNR 2 ENGINE FIRE WARNING SOUNDED INTERMITTENTLY IN FLIGHT.SDR SPUY20120628024Support · corrodedAFTER REMOVAL OF LT MLG FWG TRUNNION SUPPORT FITTING FOUND INBD SUPPORT ASSY RUSTED.SDR SPUY20120628023Support · corrodedAFTER REMOVAL OF RT MLG FWD TRUNNION SUPPORT FITTING FOUND INBD SUPPORT ASSY RUSTED.SDR SPUY20120627022Support · corrodedRT WING REAR SPAR AREA. REAR SUPPORT TO FLAP TRACK NR 5 SHOWS CORROSION AT WS 224.50 (FWD PART).SDR SPUY20120627021Support · corrodedLEFT WING REAR SPAR AREA. REAR SPAR SUPPORT TO FLAP TRACK NR 4 SHOWS CORROSION AT WS 224.50. (FWD PART)SDR SPUY20120620020Trunnion · corrodedRT WING MLG FORWARD TRUNNION ATTCH FITTING INBD FLANGE SHOWS CORROSION.SDR SPUY20120620019Trunnion · corrodedLEFT WING MLG FOWARD TRUNNION ATTACH FITTING INBD FLANGE SHOWS CORROSION.SDR SPUY20120620018Frame · deformedMAIN CARGO BAY FRAME DEFORMED, BS 380.SDR SPUY20120620017Floorbeam · corrodedMAIN CARGO BAY AFT UPPER FLANGE OF FLOORBEAM SHOWS CORROSION RBL 10 BS 950.SDR SPUY20120620016Floorbeam · corrodedMAIN CARGO BAY FLOORBEAM UPPER FLANGE SHOWS CORROSION BS 1070 BETWEEN LBL 45" AND LBL 62.5.SDR SPUY20120620015Cargo Track · corrodedCARGO TRACK SHOWS CORROSION BS 1010, LBL 62.5.SDR SPUY20120620014Cargo Track · corrodedCARGO TRACK SHOWS CORROSION BS 950 LBL 24.5.SDR SPUY20120620013Cargo Track · corrodedCARGO TRACK UPPER AND LOWER LT FLANGE SHOWS CORROSION BETWEEN BS 950C AND BS 950D, RBL 24.5.SDR SPUY20120620012Cargo Track · corrodedCARGO TRACK LOWER PART BOTH FLANGES SHOW CORROSION BS 1130, RBL 24.5.SDR SPUY20120620011Cargo Track · corrodedCARGO TRACK RT FLANGE SHOWS CORROSION BETWEEN BS 950C AND BS 950F LBL 24.5.SDR SPUY20120620010Cargo Track · corrodedCARGO TRACK SHOWS CORROSION UPPER LBL 62.5 BS 445.000, BS 485.000 AND BS 502.00.SDR SPUY20120620009Beam · corrodedMAIN CARGO BAY BEAM FWD LOWER FLANGE SHOWS POINTS OF CORROSION AT STA 890, RBL 35".SDR SPUY20120620008Beam · corrodedMAIN CARGO BAY BEAM FWD LOWER FLANGE SHOWS CORROSION AT STA 900 RBL 45"SDR SPUY20120620007Floorbeam · corrodedMAIN CARGO BAY FLOORBEAM LOWER FLANGE SHOWS CORROSION STA 890, LBL 30".SDR SPUY20120620006Cargo Track · corrodedNR 1 CARGO TRACK LOWER PART CORRODED AT BS 950, LBL 62.5.SDR SPUY20120620005Skin · corrodedCENTER SECTION LOWER SKIN SHOWS CORROSION STA 804-5 - STA 825.95, LBL25.SDR SPUY20120620004Spar · corrodedLT WING FRONT SPAR LOWER CHORD SHOWS CORROSION BETWEEN WS 304.0 AND WS 320.5SDR SPUY20120620003Frame · deformedFWD CARGO BAY FRAME DEFORMED BS 560, STRINGER 24L TO 25L.SDR SPUY20120620001Frame · crackedFWD CARGO BAY FRAME CRACKED .5" BS 580, STRINGER 23L TO 25L.SDR SPUY20120620002Frame · deformedFWD CARGO BAY FRAME DEFORMED BS 520, S22-26L.SDR PCSA2011012201Actuator · leakingDURING CLIMBOUT, LOST HYDRAULIC SYSTEM "A" QUANTITY AND PRESSURE. T/S FOUND LEAKING NR 5 KRUEGER FLAP ACTUATOR. REMOVED AND REPLACED ACTUATOR AND OPS AND LEAK CHECK GOOD.SDR PCSA10420071Compressor · damagedFLIGHT 743 DURING THE TAKEOFF ROLL FROM MIA THE CREW EXPERIENCED A VIBRATION ON THE NUMBER 3 ENGINE, THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED BACK TO THE GATE WITHOUT ANY FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 3 ENGINE AND FOUND THE C-2 COMPRSDR PCSA111706SUPOil Filter · bypassingFLIGHT 858 DEPARTED MAR AND DURING THE CLIMB THE CREW REPORTED THE NR 1 ENGINE LOW OIL FILTER BYPASS LIGHT ILLUMINATED, THE CREW ACCOMPLISHED COMPANY ALTERNATE PROCEDURES, THE NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY. THE AIRCRAFT RETURNED TO MAR WITHOUT SDR PCSA7140601Actuator · corrodedTHE NOSE LANDING GEAR MANUAL EXTENSION INBOARD & OUTBOARD SHAFT SEGMENTS WERE FOUND TO HAVE CORROSION, THE DRAG BRACE PIN & FITTING & THE TRANSFER CYLINDER WERE FOUND TO HAVE CORROSION. THE NOSE LANDING GEAR DEFECTIVE COMPONENTS WERE REMOVED AND REPLACED IAW SDR PCSA6130601Compressor · stalledFLIGHT 721 PREPARED TO TAKEOFF FROM MIA; THE CREW REPORTED NR 2 ENGINE COMPRESSOR STALLING AS POWER WAS APPLIED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE BLOCK. AMERIJET MAINTENANCE ACCOMPLISHED AN ENGINE RUN ON NR 2 ENGINE AND WAS ABLE TO DUSDR PCSA05190601Handle · damagedFLIGHT 741 DEPARTED MIA THE CREW REPORTED DURING CLIMB ON GEAR RETRACTION THE LEFT GEAR DOOR AMBER LIGHT CAME ON, AMERIJET PROCEDURES WERE FOLLOWED AND THE AIRCRAFT RETURNED BACK TO MIA WITHOUT ANY FURTHER INCIDENT. MIA MAINTENANCE TROUBLESHOT THE GEAR LIGHT SDR PCSA03030601Switch · false indicationFLIGHT 859 DEPARTED MIA THE CREW REPORTED DURING CLIMB THE NUMBER 3 LEADING EDGE FLAP IN TRANSIT LIGHT STAYED ON AFTER THE FLAPS WERE RETRACTED ON THE FLIGHT ENGINEERS FLAP PANEL LIGHT, AND THE FORWARD PANEL LIGHT. THE AIRCRAFT RETURNED BACK TO MIA AND LANDEDSDR PCSA01310601Nut · looseKMIA-MDSD FLIGHT 871 - CREW REPORTED APPROXIMATELY 20 MINUTES INTO CRUISE, NR 1 ENGINE EGT, N1 AND N2 RAPIDLY APPROACHED THEIR LIMITS. ENGINE NR 1 WAS SHUTDOWN PER AOM. ENGINE WINDMILLED FOR 50 MINUTES AND ENGINE OIL PRESSURE AT 25 PSI DURING WINDMILLING. A/CSDR PCSA12070502Adc · failedFLIGHT 8216 DURING TAKEOFF FROM CUR CREW REPORTED CAPTAIN'S AIRSPEED INDICATION SHOWED NO AIRSPEED INDICATION, THE F/O'S AIRSPEED INDICATOR WAS SHOWING 80 KNOTS, CREW ABORTED THE TAKEOFF AND RETURNED TO THE BLOCK WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUSDR PCSA11250501Fuel Heater · failedAT TOP OF DESCENT NR 2 ENGINE OIL TEMP BEGAN TO RISE, NR 2 FUEL HEAT VALVE WAS STUCK OPEN. NR 2 ENGINE FUEL HEAT VALVE WAS CYCLED, BUT WOULD NOT CLOSE, OIL TEMP WENT INTO RED 175 DEG, COULD NOT BE DECREASED, OIL PRESSURE NORMAL. DURING NORMAL ATTEMPT TO SHUTSDR PCSA11030501Engine · vibrationWHILE IN CRUISE, CREW REPORTED VIBRATION ON THE CENTER CONSOLE, WHEN NR 1 ENGINE THROTTLE WAS PULLED BACK VIBRATION SEEMS TO DIMINISH. AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED ALL 3 ENGINES, INTAKES, AND EXHAUST, NO DAMAGE FSDR PCSA7060501Adc · false indicationON TAKEOFF ROLL, CAPT AIRSPEED INDICATOR WENT TO 300 KNOTS AT AROUND 60 KNOTS INDICATED. CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS. NO FURTHER INCIDENT REPORTED. MAINTENANCE INSPECTED AIRSPEED INDICATION AND FOUND SYSTEM ENCOUNTERED A GLICK FROM NR 1 AIR SDR PCSA04270501Proximity Switch · out of adjustFLIGHT 881 DEPARTED MIA DURING CLIMBOUT CREW REPORTED AMBER LEADING EDGE FLAP INTRANSIT LIGHT REMAINED ILLUMINATED ON CAPTAINS FWD PANEL, CREW VERIFIED INDICATION ON FLIGHT ENGINEERS PANEL NR 3 LEADING EDGE FLAP INTRANSIT LIGHT ON. AIRCRAFT RETURNED BACK TO MSDR PCSA04260501Outflow Valve · intermittentFLIGHT 710 MID-MIA, DURING CLIMBOUT CREW REPORTED PRESSURIZATION OUTFLOW VALVE WOULD NOT CLOSE IN ANY MODE IN FLIGHT ON DEPARTURE FROM MID. AIRCRAFT RETURNED BACK TO MID WITH NO FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED A PRESSURIZATION CONTROL SYSTEM TEST SDR PCSA05041401Housing · strippedFLT 8414 ON APPROACH TO MIA CREW REPORTED NR 1 ENGINE LOST OIL, ENG. NR 1 WAS SHUTDOWN AS A PRECAUTION. A/C LANDED AT INTENDED DESTINATION WITHOUT FURTHER INCIDENT. MX INSPECTION OF THE NR 1 ENGINE FOUND OIL FILTER & GEARBOX CHIP DETECTORS HAD NO METAL, INSPEC
Back to N598AJ, cancelled Feb 1, 2019