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 = '1900D' 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 = '1900D' 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 29GA2013021395557Spar Cap · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT WING MAIN SPAR UPPER CAP AT WS 124 CORRODED. BLENDED CORROSION AND PERFORMED NDT INSPECTION, NO CORROSION OR CRACKS NOTED.SDR 29GA2012110795557Spar · corrodedREPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT WING MAIN SPAR UPPER CAP HAS CORROSION.SDR 29GA2012110795555Angle · corrodedREPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED VERTICAL SPAR RIGHT ANGLE BELOW UPPER RUDDER ATTACH BRACKET HAS CORROSION.SDR 29GA93532110312Generator · faultyFLIGHT:4067 CLE/DUJ PILOT REPORTED GEAR HORN CLICKS INSTEAD OF SOUNDING. REPLACED 605 TONE GENERATOR, OPERATIONAL CHECK GOOD.SDR GLBA2012110100101Skin · dentedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A DENT IN THE RT FUSELAGE LOCATED BETWEEN STRINGERS 10R AND 11R AT FS 228.25 AND 243.25 IN A AREA OF 6" BY 4.6", WITH A DEPTH OF .15". REPAIRED IAW EO 12-1900-53-063. MAJOR REPAIRSDR GLBA2012110100102Tab · damagedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 6 AREAS OF SCALLOPING ON THE T/E IN THE TRIM TAB CUTOUT AREA OF A LT ELEVATOR. REPAIRED IAW EO 12-1900-27-003. MAJOR REPAIR.SDR GLBA2012110100100Stringer · corrodedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CORROSION AT STRINGER 15R BETWEEN 228.25 AND 243.25. REPAIRED IAW EO 11-1900-53-064. MAJOR REPAIR.SDR GLBA2012103100099Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CORROSION ON THE BELLY AT FS 228 BETWEEN STRINGERS 16 AND 15L, .75" BY .75, AND A CRACK IN THE AREA, .5" IN LENGTH. REPAIRED IAW EO 11-1900-53-065. MAJOR REPAIR.SDR GLBA2012103100098Stringer · corrodedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CORROSION ON THE STRINGER BETWEEN FS 228.25 AND 243.25. REPAIRED IAW EO 11-1900-53-062. MAJOR REPAIR.SDR GLBA2012103000095Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT UPPER 2ND FASTENER HOLE, CRACK RADIATES UPWARD AND DOWNWARD AT THE OB EDGE OF FASTENER HOLE, .2 ICHES IN LENGTH. REPAIRED IAW EO 12-1900-55-052. MAJOR REPAIRSDR GLBA2012103000094Spar · misrepaired- DURING A SCHEDULED ROUTINE INSP FOUND THAT THE HORIZONTAL STAB FWD SPAR WEB MISREPAIRED. REPAIRED IAW EO 12-1900-55-053. MAJOR REPAIRSDR GLBA2012103000097Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB RT FWD SPAR CAP ANGLE AT THE UPPER FASTENER HOLE AT VSS 84.10, 20 PERCENT, CRACK RADIATES DOWNWARD & OTBD FROM FASTENER HOLE, .15 INCHES IN LENGTH. REPAIRED IAW EO 12-1900-55-054. MAJOSDR GLBA2012102900092Structure · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 451 AND STRINGER 10R IN THE BEND RADIUS PROTRUDING UPWARD, .5" IN LENGTH. REPAIRED IAW EO 12-190 0-53-059.SDR GLBA2012102900091Structure · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND CRACK AT A PREVIOUS REPAIR AT FS 163.97 AND STRINGER 9AR FRAME PROTRUDING OUT OF A STOP DRILL, .25" IN LENGTH. REPAIRED IAW EO 12-1900-53-060.SDR GLBA2012103000096Oil System · leakingPILOT REPORTED THAT THE OIL PRESSURE ON NR 1 ENGINE DROPPED TO 50 PSI REDUCED POWER TO IDLE OIL PRESSURE CONTINUED TO DROP TO 40 PSI LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED SHUT ENGINE DOWN OBSERVED OIL PRESSURE AT 20 PSI JUST PRIOR TO ENGINE SHUTDOWN. MAINTSDR GLBA2012102900093Light · inoperativePILOT REPORT THAT THE INSTRUMENT EMERGENCY LIGHT IS INOPERATIVE. MX OPS CHECKED GOOD.SDR V0DR2012003Bearing · brokenPROPELLER ASSEMBLY HC-E4A-3J CAME IN FOR O/H. UPON DISASSEMBLY NR 4 BLADE LOWER RETENTION BEARING WAS FOUND TO BE CRACKED. THE BEARING PART # IS D-7745B.SDR GLBA2012102400087Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE VERTICAL STAB RT FWD SPAR CAP ANGLE FROM UPPER FASTENER HOLE TO UPPER EDGE OF ANGLE, .5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-050. MAJOR REPAIR.SDR CA121024005Boot · burned(CAN) AFTER LANDING THE GROUND HANDLERS WERE MOVING THE ACFT AND NOTICED THAT THE DEICE BOOT ON 1 OF THE PROPELLER BLADES HAD A 1" BURNED HOLE AT THE BLADE ROOT. MAINTENANCE WAS NOTIFIED, ACFT WAS SNAGGED AND PARTS WERE ORDERED. PROP HAS ONLY 52.0 HRS SINCE ITSDR GLBA2012102200086Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON FRAME AT FS 183.25 AND STRINGER 1, DOWNWARD TO THE EDGE OF THE FRAME, 2.75" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-057. MAJOR REPAIR.SDR GLBA2012102200085Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION FOUND CORROSION ON THE BELLY SKIN AT FS 243 BETWEEN STRINGERS 16 & 15R, VISIBLE CORROSION IS APPROX 1 BY 1 INCH. REPAIRED IAW EO 11-1900-53-055. MAJOR REPAIR.SDR GLBA2012102200084Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CORROSION ON THE BELLY SKIN AT FS 213, LOWER FUSELAGE. REPAIRED IAW EO 11-1900-53-056. MAJOR REPAIR.SDR GLBA2012102200083Web · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE AFT HORIZONTAL STAB WEB AT THE 2 O'CLOCK POSITION, .125" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-049. MAJOR REPAIR.SDR GLBA2012101900081Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE VERTICAL STAB LT SPAR CAP ANGLE AT 20 PERCENT, STARTING AT TOP FASTENER AT FSS 84.18 MOVING DOWN TO THIRD FASTENER AT FSS 84.16, 1.75" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-048.SDR 29GA93755101712Channel · crackedDURING SCHEDULED INSPECTION FCD 55-09-19-02 FOUND CRACK IN HAT SECTION OF VERTICAL STABILIZER AREA C.SDR GLBA2012101800080Warning Light · illuminatedPILOT REPORTED THAT THE CARGO DOOR CAME OPEN IN FLIGHT, LANDED SAFELY. MAINTENANCE REPLACED ALL PARTS AND FRAMES REQ IAW SRM, OPS CHECKED FLIGHT SAT.SDR GLBA2012101500078Connector · unsecurePILOT REPORTED THAT WHILE EXTENDING THE GEAR, LANDING GEAR HAD NO GREEN LIGHTS, MANUALLY EXTENDED GEAR, STILL NO GREEN INDICATION, DECLARED AN EMERGENCY AND LANDED WITH NO INCIDENT. MX RESEATED THE DOWNLOAD/SAFETY SWITCH CONNECTOR PLUG, OPS CK GOOD.SDR GLBA2012100800077Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON FRAME AT FS 163.97 AT STRINGER 9R CUTOUT, .5" IN LENGTH. REPAIRED IAW EO 12-1900-53-053. MAJOR REPAIR.SDR V0DR2012002Knob · crackedPITCH CHANGE KNOB WAS REMOVED FROM SERVICE, BECAUSE VISUAL INSPECTION REVEALED CRACKS COMING FROM PINGED MARKS FOR WASHER RETENTION.SDR GLBA2012100500076Structure · damagedBIRD STRIKE ON LT OTBD WING FROM WS 192.74 TO APPROX 201.74, APPROX .5" IN DEPTH. REPAIRED IAW EO 12-1900-57-011. MAJOR REPAIRSDR GLBA2012100400075Spar · damagedDURING A SCHEDULED ROUTINE INSPECTION MX REQURESTED TO PRECAUTIONARY REPLACEMENT OF THE HSS 0.00 HORIZONTAL STABILIZER AFT SPAR WEB. REPAIRED IAW EO 12-1900-55-047. MAJOR REPAIRSDR CA121005007Vane · damaged(CAN) ICE VANE ASSY FOUND HANGING IN INTAKE OF COWLING ON LT ENGINE DURING A PREFLIGHT INSPECTION. UPON REMOVAL, VANE WAS FOUND TO BE CRACKED ALONG WITH BOTH MOUNTING BRACKETS.SDR 29GA95732100212Actuator · malfunctionedFLIGHT: 4016 FPO/FLL NOSE GEAR INDICATOR DID NOT ILLUMINATE MANUALLY PUMPED GEAR AND LANDED, INDICATOR ILLUMINATED ON TAXI INTO GATE. REPLACED NOSE LANDING GEAR ACTUATOR OPERATIONAL CHECK GOOD.SDR GLBA2012100200074Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FRAME AT FS 150.6 BETWEEN STRINGERS 2R AND 3R, 1" IN LENGTH. REPAIRED IAW EO 12-1900-53-051. MAJOR REPAIR.SDR GLBA2012100200073Pressure Blkhd · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS IN THE LT FWD PRESSURE BULKHEAD INBD EDGE ABOVE INBD RIVET ROW AT STATION 84.00, 1.3" IN LENGTH. REPAIRED IAW EO 12-1900-53-082. MAJOR REPAIR.SDR GLBA2012100100070Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS ON THE HORIZONTAL STAB AFT SPAR WEB AT RELIEF HOLE AT HSS 00.0, .5 INCHES IN LENGTH. REPAIRED IAW EO 11-1900-55-045.SDR GLBA2012100100069Spar · crackedDURING A SCHEDULED ROUTINE INSP FOUND FOUR CRACKS ON THE HORIZONTAL STAB FWD SPAR WEB AT HSS 00.00, 2" IN LENGTH TOTAL. REPAIRED IAW EO 11-1900-55-046.SDR 29GA94228093012Fuel Cap · missingFLIGHT 4031 FLL/FLL AFTER TAKEOFF RIGHT FUEL CAP LOST FLIGHT. INSTALLED FUEL CAP ON RIGHT WING.SDR 29GA95732092912Downlock Switch · defectiveFLIGHT:4021 TCB/FLL DURING APPROACH NOSE WHEEL GEAR GREEN INDICATOR DOWN LIGHT DID NOT ILLUMINATE ON EXTENSION BULB TESTED OK. REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH AND ANNUNCIATOR PCB OPERATIONAL CHECK NORMAL.SDR GLBA2012100100072Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT VSS 84.10 AT 20 PERCENT. 1.5 INCHES IN LENGTH. REPAIRED IAW EO 11-1900-55-043.SDR GLBA2012100100071Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS ON THE VERTICAL STAB RT FWD SPAR CAP ANGLE AT VSS 84.10 AT 20 PERCENT CHORD, CRACKED FROM FIRST RIVET HOLE AND SECOND CRACK IS FROM SECOND RIVET HOLE, AND THIRD CRACK AT THIRD RIVET HOLE, AND FOURTH CRASDR ERAA201209250064Uplock Switch · defectiveDEPART ANC, NORMAL GEAR RETRACT/EXTEND, GEAR UNSAFE LIGHT IN CRUISE, RECYCLED GEAR, NORMAL, UNSAFE GEAR LIGHT AGAIN. AIR RETURN PER ANCHORAGE MAINTENANCE/DISPATCH. REMOVED AND REPLACED NLG UPLOCK SWITCH AND RIGGED IAW B1900D MM CHAPTER 32-60-00, PERFORMED OPSDR GLBA2012092400068Cam · out of adjustPILOT REPORTED THAT THE AIRSTAIR DOOR IS DIFFICULT TO OPEN. MX ADJUSTED 2 AFT LOWER CAM'S IAW BMM 52-10-00, OPS CK GOOD.SDR 29GA95732092412Downlock Switch · dirtyFLIGHT: 4012 TPA/FLL NOSE GEAR GREEN LIGHT DID NOT COME ON LEFT AND RIGHT MAIN GEAR LIGHTS NORMAL. CLEANED NOSE GEAR DOWNLOCK SWITCH, OPERATIONAL CHECK NORMAL.SDR GLBA2012092400067Angle · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS ON THE LT FWD SPAR CAP ANGLE ON THE VERTICAL STAB COMING DOWN TO THE FIRST FASTENER, .375" IN LENGTH, AND A SECOND CRACK NEXT TO THE SECOND FASTENER FROM THE TOP, .5" IN LENGTH. REPAIRED IAW FR-CO-02532,SDR GLBA2012092400066Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK ON THE RT FWD SPAR CAP ANGLE ON THE VERTICAL STAB COMING DOWN TO THE FIRST FASTENER, .375" IN LENGTH. REPAIRED IAW FR-CO-02532 REV 1, STEP 1. MAJOR REPAIR.SDR CA130128011Governor · malfunctioned(CAN) ABORTED TAKEOFF DUE UN-COMMANDED AFX. FOLLOWING SETTING FULL POWER, THE LT TORQUE WAS NOTED BY BOTH PILOTS TO RISE TO 5000FT/LBS, IN LESS THAN 1 SECOND, AT APPROXIMATELY 50 KTS. THE CAPTAIN (FP) CALLED ABORT AND RETARDED THE POWER LEVERS. THE ACFT WAS SDR GLBA2012092000065Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE AT THE VERT STAB AT VSS 84.10 AND THE 20 PERCENT AT THE SECOND FASTENER, CRACK RADIATES DOWNWARD FROM FASTENER, .375" IN LENGTH. REPAIRED IAW FR-CO-02530, REV 1, STEP 1. MAJOSDR GLBA2012091800063Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS ON THE VERTICAL STAB LT FWD SPAR CAP ANGLE, (1) RADIATES UPWARD FROM THE UPPER FASTENER TO THE EDGE OF THE SPAR CAP ANGLE, RADIATES DOWNWARD FROM THE SECOND FASTENER, VSS 84.10 AT 20 PERCENT CHORD, .875" SDR GLBA2012091800062Longeron · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE RT SIDEWALL FRAME LONGERON AT FS 107, 1 INCH IN THE BEND RADIUS OF THE INBD FLANGE AND AT THE UPPER (2) FASTENER HOLES, RT LONGERON CRACKED 2.7" FROM THE INBD FLANGE EDGE RADIATING UP AND OTBD TO
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