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 aircraft_model_key = 'G1159B' 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 aircraft_model_key = 'G1159B' 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 N382006F00004Downlock Switch · damagedGEAR LIGHT NOSE GEAR FAILED TO ILLUMINATE WITH GEAR EXTENSION UNTIL 150 KTS. PINNED LANDING GEAR , ISSUED SPECIAL FLIGHT PERMIT FOR AC RETURN. JACKED AC AND INSPECTED NOSE GEAR, DISCOVERED LOCKING CLIP ON NOSE GEAR DOWN/LOCKED SWITCH POPPED OUT OF DETENT-SECSDR N382005F00004Starter · meltedLT ENGINE WILL NOT START; NO START VALVE OR IGNITION LIGHT WHEN STARTER BUTTON PRESSED. A REPLACEMENT STARTER WAS INSTALLED AND THE AIRCRAFT WAS FLOWN BACK TO ITS HOME BASE. (K)SDR 2005FA0000967Attach Fitting · corrodedIAW MM TO COMPLY WITH THE 24 MONTH NDT REQUIREMENTS UNDER THE ULTRASONIC PART OF THE INSPECTION CORROSION WAS FOUND ON BOTH THE LT AND RT WING ATTACHMENT FITTINGS AT FS 452, BL33, LT AND RT. TECH OPS REQUIRES COMPLIANCE WITH ASC FOR A 3 PIECE FITTING PLATE. SDR 2005FA0000489Rivet · looseUPON X-RAY INSPECTION OF AIRCRAFT FOR A 4000 LANDING INSPECTION, FOUND SEVERAL WORKING RIVETS AROUND CABIN WINDOWS AS INDICATED. LT NR 3 WINDOW; ONE (1) WORKING RIVET, LT NR 4 WINDOW; FOUR (4) WORKING RIVETS, LT NR 5 WINDOW, ONE (1) WORKING RIVET, RT NR 3 WINSDR 2005FA0000105Probe · brokenNR 2 STICK SHAKER AND PUSHER ACTIVATED IN FLIGHT. ENROUTE, CREW ENCOUNTERED ABOVE MENTIONED ISSUE. CREW DIVERTED, DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. MAINTENANCE DEPARTMENT WAS NOTIFIED IMMEDIATELY. REMOVED AND REPLACED NR AOA PROBE, PN ON SLZ9SDR N382005F00000Door Frame · crackedDURING AC 4000 LANDING INSPECTION, FOUND APPROX 1INCH CRACK AT THE UPPER FORWARD RADIUS OF DOOR FRAME. STOP DRILLED CRACK AND REPAIRED WITH AN OVERLAY DOUBLER IAW THE SRM. OVERLAY INSTALLED WET WITH PRC 1440. (K)SDR 2005FA0000003Door Frame · crackedDURING AIRCRAFT 4000 LANDING INSPECTION, FOUND APPROX A 1 INCH CRACK AT THE UPPER FORWARD RADIUS OF DOOR FRAME. STOP DRILLED CRACK AND REPAIRED WITH AN OVERLAY DOUBLER IAW THE SRM. OVERLAY INSTALLED (WET) WITH PRC 1440. (K)SDR N3B2004F00000Tire · blownLT MAIN GEAR TIRE BLEW OUT ON TAKEOFF. DAMAGE TO LT WING, LT GEAR HARNESS, BRAKE LINES, AND A DENT IN THE LT LOWER ENGINE COWL.SDR JGV2004F00001Pitot Line · brokenORIGINAL PITOT/STATIC TUBING AND PLASTIC FITTINGS BRITTLE AND EASILY BROKEN. MOVING TUBING OR EVEN WIRE BUNDLES TOUCHING TUBING CAUSES LEAKS. THIS IS DUE TO ITS OLD AGE. IT NEEDS TO BE REPLACED WITH A NEWER, MORE FLEXIBLE TUBING.SDR CA030507005Bolt · broken(CAN) ENGINE IS AT RRC FOR REPAIR DUE TO HIGH VIBRATION ON WING. VIBRATION ON THE REAR PICK UP WAS CONFIRMED ON A TEST BED RUN AT RRC. DURING THE STRIP OF THE TURBINE SECTION IT WAS NOTED THAT 2 OF BOLTS HAVE RELEASE THEMSELVES FROM THE LP TURBINE INNER SEAL SDR N382003F00000Actuator · crackedLEAKING ACTUATOR OR LINE CAUSED EXCESSIVE LESS OF COMBINED HYDRAULIC FLUID. FOUND THE END CAP CRACKED APPROXIMATELY .3333 OF THE CAP CIRCUMFERENCE.SDR O2G2003F00003Harness · intermittentRT WING HEAVY CONDITION CAUSED BY FUEL IMBALANCE. ON CLIMB OUT, FUEL MIGRATED TO WING TIPS MAKING IMBALANCE SEEM MORE THAN IT WAS. BOTH FUEL TANKS OPENED, INSPECTED ALL PROBES, CONNECTORS, AND WIRING. REPLACED ANY CONNECTORS THAT COULD HAVE HAD CORROSION STSDR 2002FA0000964Fitting · scoredCOMBINED HYDRAULIC SYSTEM INDICATED LOW QUANITY PRESSURE 330PSI TEE FITTING SCORED ON HYD LINE.SDR BTV2001F00000Bracket · fracturedDURING A ROUTINE SCHEDULED INSPECTION, A MECHANIC NOTED THE RUDDER GUST LOCK HOOK SUPPORTING STRUCTURE WAS FRACTURED. FURTHER INVESTIGATION FOUND THREE PIECES THAT MAKE UP THE 1159C20509 ASSEMBLY (2 EA 115920509-13 ANGLES AND 1 EA 1159C20509-35 ANGLE) WERE FRSDR MQGR20013601Attach Fitting · corrodedDURING RECOMMENDED INSPECTION OF WINGLET ATTACH HARDWARE FOR CORROSION, FOUND CORROSION IN THE WINGLET TO WING ATTACHMENT FITTING. IT APPEARS THIS CORROSION IS THE RESULT OF IMPROPER SEALING OF THE ATTACHMENT HARDWARE SINCE WATER WAS FOUND TRAPPED IN THE ONLYSDR 20010205CW019Bearing · brokenNOTICED INBOARD ROLLER BEARING ON LEFT FLAP TRACK, B, WAS MISSING THE OUTER CASING AND BEARING...ONLY STUD REMAINED, CAUSE IS UNKNOWN. RECOMMEND THAT ROLLER BEARINGS ARE VISUALLY INSP AT EACH PRE-FLIGHT INSPECTION AND MOVED WITH FINGERS TO CHECK FOR BINDING. NSDR 20001227SH015Beam · corrodedLEFT WING REAR BEAM HAD CORROSION UNDERNEATH AILERON. (X)SDR 20000907SH009Flange · failedFLANGE ON INBOARD SIDE OF HEAT EXCHANGER FAILED AND DUCT BECAME DISCONNECTED. HEAT EXCHANGER IS BEING SENT TO GULFSTREAM FOR ENGINEERING ANALYSIS. (X)SDR 2000ZZZX380Rivet · missingDURING AN EXTERNAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER, FOUND TWO RIVET HEADS FROM LOWER RT SKIN TO BE MISSING. REMAINING RIVET STEMS/SHANKS FOUND, ALSO PREVIOUSLY PAINTED OVER WHEN AIRCRAFT WAS PAINTED. UPON REPLACING THESE RIVETS WITH NEW SOLID SDR 99ZZZX4623Plank · corrodedDURING NDT OF WING CLOTHESPIN FITTINGS, FOUND CORROSION ON TOP OF UPPER AFT WING PLANK. CORROSION MAY BE DUE TO HARSH AREA THAT IT IS SUBJECTED TO.SDR 98ZZZM772Transducer · malfunctionedLOST CABIN PRESSURIZATION CONTROL AT 37,000 FT, WENT TO MANUAL AND COULD NOT CONTROL. MADE EMERGENCY DESCENT TO 10,000 FT. REPLACED PRESSURIZATION SYSTEM TRANSDUCER, S/N 94-630, WITH REPAIRED UNIT P/N 2100136-1-10, S/N 12-946. PERFORMED CABIN PRESSURIZATIONSDR 98ZZZX1631Seal · torn'LOST PRESSURIZATION AT FL 390. COULD NOT CONTROL CABIN. MADE EMERGENCY DESCENT AND RETURNED TO PONTIAC'. REPLACED CABIN DOOR SEAL AND DOOR SEAL CHECK VALVE. GROUND TEST AND FLIGHT TEST OF PRESSURIZATION SYSTEM NORMAL.SDR 98ZZZX798Bolts · corrodedREMOVED LEFT WING WINGLET ATTACHMENT BOLTS AND SLEEVES TO REMOVE WINGLET FOR ACCESS. FOUND ALL SIX BOLTS EXCESSIVELY CORRODED. THERE IS NO REQUIRED INSPECTION IN CHAPTER 5 FOR THESE BOLTS. THERE IS ALSO NO REMOVAL OR INSTALLATION INSTRUCTIONS FOR WINGLET INSDR 98ZZZX797Bolts · corrodedREMOVED LEFT WING WINGLET ATTACHMENT BOLTS AND SLEEVES TO REMOVE WINGLET FOR ACCESS. FOUND ALL SIX BOLTS EXCESSIVELY CORRODED. THERE IS NO REQUIRED INSPECTION IN CHAPTER 5 FOR THESE BOLTS. THERE IS ALSO NO REMOVAL OR INSTALLATION INSTRUCTIONS FOR WINGLET INSDR 98ZZZX796Bolts · corrodedREMOVED LEFT WING WINGLET ATTACHMENT BOLTS AND SLEEVES TO REMOVE WINGLET FOR ACCESS. FOUND ALL SIX BOLTS EXCESSIVELY CORRODED. THERE IS NO REQUIRED INSPECTION IN CHAPTER 5 FOR THESE BOLTS. THERE IS ALSO NO REMOVAL OR INSTALLATION INSTRUCTIONS FOR WINGLET INSDR 98ZZZM728Actuator · bindingFLAPS WOULD NOT DEPLOY IN FLIGHT, NORMAL OR EMERGENCY, UPON APPROACH TO TEB. RETURNED TO PTK AND LANDED. REPLACED LEFT WING INBOARD FLAP ACTUATOR P/N 1159SCC211-7, S/N 36-1174, WITH OVERHAULED UNIT P/N 1159SCC211-15, S/N 76-117. CHECKED FLAP SYSTEM RIGGING SDR 98ZZZX325Igniter · failedIGNITER UNIT OVERHAULED 11 MONTHS, 138 HOURS, 66 CYCLES AGO. FAILED OPS INSPECTION WITH DISCHARGE ONLY EVERY 5-6 SECONDS. SHOULD BE APPROXIMATELY 1 SECOND.SDR 98ZZZX319Generator · wornBLACK SOOT ON COWLING. CHECKED GENERATOR BRUSHES AND FOUND UNDER ONE-QUARTER LIFE REMAINING.SDR 96ZZZX5073Alternator · failedLEFT AC GENERATOR SUSPECT FAILED. DROPPED OFF LINE IN-FLIGHT. TVI FROM .5 TO 2.0 IPS. NOTED DEBRIS AROUND MOUNTING FLANGE UPON INSPECTION. REPLACED ALTERNATOR. THIS IS THE 3RD AC GENERATOR FAILURE WITH A REAL LOW TSO IN THE LAST 6 MONTHS, BEARINGS FAILED.SDR EW7A379WWindshield · crackedPILOT NOTICED INTERIM WINDOW HEATING WIRES GLOWING AND OVERHEATING. APPROXIMATELY 10 SECONDS AFTER TURNING HEAT OFF, THE OUTER GLASS PANE CRACKED FROM SHOCK COOLING.SDR 96ZZZM670Skin · debondedRIGHT LOWER AFT PYLON SKIN DELAMINATED BEYOND MANUFACTURE'S ACCEPTABLE LIMITS.SDR 96ZZZM671Doubler · corrodedON FS 580 PRESSURE BULKHEAD COMM SCAN INSPECTION, CORROSION WAS DETECTED BETWEEN THE SKIN AND LONGERON NR 24 ON THE RIGHT SIDE OF AIRFRAME AT LOCATION NR 59 BETWEEN LAYERS NR 10 THROUGH 15. SKIN WAS REMOVED TO REPAIR PROBLEM AND A HOLE WAS DETECTED IN STRAP (SDR 96ZZZX803Bulb · burning endAEROSPACE LIGHTING AD'S HAVE BEEN ISSUED, BUT THIS HAS NOT CORRECTED THE PROBLEM. FLUORESCENT BULB ENDS ARE STILL BURNING OFF. SUBMITTER SUGGESTS POSSIBLE CABIN FIRE COULD RESULT.SDR 97ZZZX3069Fitting · corrodedDURING PROCESS OF REMOVING RT THRUST STRUT FOR NDT, DISCOVERED SEVERE INTERGRANULAR CORROSION AT AFT/UPPER THRUST STRUT/FUSELAGE ATTACH FITITNG, PN 1159BM20518-XX. BRACKET IS LOCATED IN PYLON. AREA AFFECTED SURROUNDS STRUT ATTACH BOLT/BUSH BRACKET LOCATION,
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