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 = 'P2V7' 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 = 'P2V7' 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 NI6R201712010047Engine · vibrationDURING CRUISE FLIGHT, THE CREW EXPERIENCED BANGING, VIBRATIONS, AND A LOW OIL PRESSURE LIGHT ON NR 1 RADIAL ENGINE. THE CREW FOLLOWED EMERGENCY PROCEDURES, SHUT DOWN THE ENGINE, DECLARED AN IFE, DIVERTED TO THE NEAREST SUITABLE AIRPORT, AND PERFORMED AN UNEVESDR NI6R201608270037B-Nut · crackedNR 2 RADIAL ENGINE HYDRAULIC PUMP PRESSURE LINE INTERNAL TO THE FUSELAGE BEGAN LEAKING IN FLIGHT. UPON IDENTIFICATION OF THE LEAK, THE NR 2 ENGINE WAS SHUTDOWN AND AN IFE WAS DECLARED. LANDING WAS UNEVENTFUL. UPON INVESTIGATION OF THE LEAK, IT WAS DISCOVERESDR NI6R201608130036Engine · malfunctionedNR 1 RADIAL ENGINE BEGAN BANGING DURING CLIMB. ENGINE WAS SHUTDOWN, RETARDANT LOAD WAS JETTISONED, AND UNEVENTFUL LANDING PERFORMED.SDR NI6R201506220027Rudder Pedal · brokenDURING LT TURN ON CLIMB OUT, THE CAPTAIN'S RUDDER PEDALS JAMED WITH THE LT SIDE FORWARD AND THE RT SIDE AFT. WHILE PUSHING TRYING TO FREE THEM THEY BROKE LOOSE AND BOTH SIDES WENT ALL THE WAY DOWN. THE CAPTAIN WAS ABLE TO DETERMINE THAT THE PEDAL FORE/AFT ADJSDR NI6R201408040015Hydraulic System · malfunctionedDURING CRUISE FLIGHT, EXPERIENCED MAIN HYDRAULIC SYSTEM PRESSURE LOSS. HYDRAULIC QUANTITY REMAINED AT NORMAL. AN EMERGENCY WAS DECLARED AND INITIATED EMERGENCY CHECKLIST ITEMS. HYDRAULIC SYSTEM WAS PLACED INTO BYPASS AND SYSTEM PRESSURE RETURNED TO NORMAL. SDR NI6R20121105009Skin · crackedDURING PRE-FLIGHT, CREW RELEASED THE FLIGHT CONTROL LOCK AND FOUND THE CONTROL COLUMN WOULD NOT FULLY TRAVEL TO NOSE DOWN POSITION. ON INSPECTION, MX FOUND THE LEFT ELEVATOR FORWARD RIB SKIN BETWEEN ELEVATOR STATIONS 65.5 AND 117.5 HAD CRACKED AND FAILED. RSDR NI6R20120814006Skin · crackedFOUND WING SKIN AT THE ATTACHING FASTENERS AT THE RT LOWER FWD SPAR CAP RUNNING FOR APPROX 20 INCHES TO HAVE WORKED LOOSE. SKIN CAN BE PUSHED UP AND DOWN APPROX .020. UPON REMOVAL OF THE LEADING EDGE AND NACELLE PANEL, A FOUR INCH CRACK IN THE WING SKIN, DISSDR 2012FA0000564Skin · looseFOUND WING SKIN AT THE ATTACHING FASTENERS AT THE RT LOWER FWD SPAR CAP RUNNING FOR APPROX 20" TO HAVE WORKED LOOSE. SKIN CAN BE PUSHED UP AND DOWN APPROX .020". UPON REMOVAL OF THE L/E AND NACELLE PANEL, A 4" CRACK IN THE WING SKIN WAS DISCOVERED RUNNING AFSDR 2010FA0000518Arm · broken((NI6R)) FOUND THAT AT FULL AILERON DEFLECTION AND DESCENT SPOILERS DEPLOYED, WHEN ROLLING AILERONS OUT OF FULL TRAVEL BINDING OCCURED BETWEEN PN 428409 AND PN 428414, CAUSING FAILURE OF PN'S 428409 AND 428410. THIS RENDERS THE ROLL AND DESCENT SPOILERS INOPESDR 2010FA0000517Spoiler Sys · broken((NI6R)) FOUND THAT AT FULL AILERON DEFLECTION AND DESCENT SPOILERS DEPLOYED, WHEN ROLLING AILERONS OUT OF FULL TRAVEL BINDING OCCURRED BETWEEN P/N 428409 AND P/N 428414, CAUSING FAILURE OF PN'S 428409 AND 428410. THIS RENDERS THE ROLL AND DESCENT SPOILERS INSDR 2010FA0000086Window · separatedPILOTS OVERHEAD HATCH WINDOW SEPARATED FROM THE FRAME SHORTLY AFTER TAKEOFF. THE PLEXIGLASS WINDOW IS MOUNTED BY USE OF A FIBERGLASS LAMINATE. THE FIBERGLASS LAMINATE IS WHAT FAILED CAUSING THE SEPARATION. THE WINDOW RIPPED OFF THE COMM 1 ANTENNAE AND DENTED TSDR 18069Structure · crackedTHE CRACK/CORROSION IS LOCATED ON THE AFT VERTICAL SIDE OF STRINGER (HAT SECTION) NR 18. IT IS LOCATED IN THE LEFT HAND OUTER WING AT WING STATION 284. THE CRACK/CORROSION IS 1.25 INCH LONG AND RUNS SPAN WISE. THE CORROSION WAS REMOVED COMPLETELY AT .024 OFSDR 2003FA0001277Skin · crackedCRACKS EMANATING FROM THE LT AND RT MLG FORWARD LOWER CUTOUTS IN THE CENTER WING SKIN. CRACKS RUN FORWARD FROM THE IB CORNERS TO THE FIRST AND SECOND RIVETS. CRACKS DO NOT CONTINUE TO THE EDGE OF THE SKIN. LOCATIONS OF THE CUTOUTS ARE JUST INBOARD OF THE NASDR 2003F00653Skin · crackedCRACKS EMANATING FROM THE LT AND RT MLG FORWARD LOWER CUTOUTS IN THE CENTER WING SKIN. CRACKS RUN FORWARD FROM THE IB CORNERS TO THE FIRST AND SECOND RIVETS. CRACKS DO NOT CONTINUE TO THE EDGE OF THE SKIN. LOCATIONS OF THE CUTOUTS ARE JUST INBOARD OF THE NASDR 2003FA0001250Skin · crackedCRACKS EMANATING FROM THE LT AND RT MLG FORWARD LOWER CUT-OUTS IN THE CENTER WING SKIN. CRACKS RUN FORWARD FROM THE INBOARD CORNERS TO THE FIRST AND SECOND RIVETS. CRACKS DO NOT CONTINUE TO THE EDGE OF SKIN. LOCATIONS OF THE CUTOUTS ARE JUST INBOARD OF THE NSDR 2003FA0001249Skin · crackedCRACKS EMANATING FROM THE LT AND RT MLG FORWARD LOWER CUT-OUTS IN THE CENTER WING SKIN. CRACKS RUN FORWARD FROM THE INBOARD CORNERS TO THE FIRST AND SECOND RIVETS. CRACKS DO NOT CONTINUE TO THE EDGE OF SKIN. LOCATIONS OF THE CUTOUTS ARE JUST INBOARD OF THE NSDR 2003FA0000041Spar Cap · corrodedFUEL INTERCONNECT ACCESS PANEL CUT OUT DOUBLER IS CRACKED AT LT AND RT PANEL NUMBERS 53L AND 53R. LT AND RT UPPER CENTER WING BOX BEAM COVERS HAVE MODERATE TO MILD CORROSION ON THE UPPER HAT SECTIONS AND THE SKIN BETWEEN WING STATIONS 84.5 TO 192 LT AND RT. SDR 2003FA0000040Doubler · corrodedFUEL INTERCONNECT ACCESS PANEL CUT OUT DOUBLER IS CRACKED AT LT AND RT PANEL NUMBERS 53L AND 53R. LT AND RT UPPER CENTER WING BOX BEAM COVERS HAVE MODERATE TO MILD CORROSION ON THE UPPER HAT SECTIONS AND THE SKIN BETWEEN WING STATIONS 84.5 TO 192 LT AND RT. SDR 16214Structure · crackedIN THE WHEEL WELL AREA OF THE P2V-7 THERE ARE 2 FUEL CELL INTERCONNECT ACCESS PANELS. THE FURTHEST INBOARD PANELS ON EACH SIDE ARE PANEL 53L AND 53R. PANEL 53L, THERE IS A CRACK LOCATED AT THE INBOARD FORWARD CORNER, RUNNING FROM THE RADIUS OF THE DOUBLER CUSDR 2002FA0001045Doubler · crackedDOUBLER FAILURE DUE TO IMPROPER MANUFACTURE PROCESS. DOUBLER BROKE AT MACHINE RADIUS AND CORNER OF FUEL ACCESS PANEL LOCATED IN LOWER INBOARD WING SKIN AREA. WING SKIN DEVELOPED CRACKS LOCALIZED TO CORNER OF ACCESS PANEL. REMOVED PAINT AND DYE PEN. INSPECTSDR 2002FA0000994Doubler · crackedLOWER WING SKIN ACCESS PANEL DOUBLER CRACKED IN SEVERAL PLACES CWS 90 LEFT SIDE TO CWS 90 RIGHT SIDE. RIGHT WING LOWER SKIN CRACKED AT AN ACCESS PANEL AT CWS 94. (SW)SDR 2002FA0000996Doubler · crackedLOWER WING SKIN ACCESS PANEL DOUBLER CRACKED IN SEVERAL PLACES CWS 90 LEFT SIDE TO CWS 90 RIGHT SIDE. RIGHT WING LOWER SKIN CRACKED AT AN ACCESS PANEL AT CWS 94. (SW)SDR 2002FA0000993Doubler · crackedLOWER WING SKIN ACCESS PANEL CUTOUT DOUBLER CRACKED IN SEVERAL PLACES CWS 90 LEFT SIDE TO CWS 90 RIGHT SIDE. RIGHT WING LOWER SKIN CRACKED AT AN ACCESS PANEL CWS 94. (SW)SDR NTB2001F00000Landing Gear · malfunctionedNOSE LANDING GEAR DID NOT LOCK WHEN EXTENDED. FLIGHT CREW MANUALLY LOCKED AND PINNED GEAR. NORMAL LANDING WAS THEN MADE. POSSIBLE IMPROPER TORQUE OR FATIGUE.SDR 2001F00405Bolt · defectiveNOSE LANDING GEAR DID NOT LOCK WHEN EXTENDED. FLIGHT CREW MANUALLY LOCKED AND PINNED GEAR. NORMAL LANDING WAS THEN MADE. POSSIBLE IMPROPER TORQUE OR FATIGUE. COMPLIANCE INSPECTED AS PER AIRCRAFT SERVICE CHANGE ASC 803.
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