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 GLBA2013091300310Skin · crackedDURING A SCHEDULED INSPECTION, FOUND THE LT LOWER BELLY SKIN AT FS 288 CRACKED, 1.75" IN LENGTH. REPAIRED IAW EO 13-1900-53-059. MAJOR REPAIR.SDR V0DR20130912001Pin · crackedMLG CAME IN FOR OVERHAUL. DURING DISASSEMBLY UPPER TORQUE KNEE PIN WAS VISUALLY INSPECTED. FOUND WHAT APPEARED TO BE A CRACK. ON FUTHER INSPECTION, CRACK CONFIRMED. CRACK RUNS FROM A GREASE GROOVE ON THE PIN, ALONG THE LENGTH OF THE PIN FOR APPROXIMATELYSDR GLBA2013091100308Skin · damagedDURING A SCHEDULED INSPECTION, FOUND BELLY SKIN AND FASTENER DAMAGED AT FS 468.25 BETWEEN STRINGERS 13 - 14L. REPAIRED IAW EO 13-1900-53-058.SDR GLBA2013090900307Wire · damagedPILOT REPORTED THAT THE RT FIRE LOOP AND TEE HANDLE ANNUNCIATORS FLICKERED DURING CLIMB OUT. MAINTENANCE TROUBLESHOT SYSTEM, NO FAULTS FOUND MEGGED WIRE W16A22 FROM J410 T. HRU S16 SWITCH TO PIN 3 OF P157 AND FOUND SHORT TO GROUND. R & R SWITCH S16 IAW AIM 1SDR GLBA2013090900306Fire Loop · chafedSIG EVENT - PILOT REPORTED THAT THE RT FIREWALL FUEL VALVE T-HANDLE FLICKERED ON AND OFF IN FLIGHT. MX TESTED FIRE LOOP ON RT SIDE, TESTED NORMAL. INSPECTED FWD AND AFT LOOP FOUND CHAFE ON TOP SIDE OF FWD LOOP. R & R LOOP IAW BMM 26-10-01. OPS CHECK GOOD ATSDR GLBA2013090300303Actuator · failedPILOT REPORTED THAT WHEN SELECTING THE GEAR DOWN, HAD NO LT MAIN INDICATION AND GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED, LANDING GEAR RELAY CIRCUIT BREAKER WAS TRIPPED, RAN CHECKLIST, MANUALLY PUMPED GEAR DOWN UNTILL HANDLE WAS FIRM, PROCEDED TO LAND, LT GSDR CA130823006Support · cracked(CAN) DURING INSPECTION OF THE RT ELEVATOR, A CRACK LINE IN THE PAINT ALONG A HORIZONTAL PLANE ABOVE THE LOWER LUG, WAS DISCOVERED. UPON FURTHER REMOVAL OF THE PAINT, IT WAS CONFIRMED THROUGH VISUAL MEANS, THAT THERE WAS DEFINITELY A CRACK. THE PART WAS THEN SDR ERAA201308260057Wire · failedON RETURN FLIGHT, TOP EFIS SCREEN, PILOTS SIDE FLICKERED AND CO-PILOTS RMI FLAGGED. AFTER SEVERAL MINUTES CO-PILOTS RMI FLAG BEGAN TO TWITCH AND DISPLAY SPIN. SHORTLY AFTER THAT ALL 4 EFIS DISPLAYS BEGAN TO BLINK TO BLACK WITH WHITE COMPASS CARD AND RED FLASDR GLBA2013082200299Door · failedMX REPORTED THAT THE 4C EMERGENCY DOOR COULDN'T BE OPENED FROM THE INSIDE. R & R EMERGENCY EXIT IAW MM 52-20-00.SDR GLBA2013082300302Handle · unsecurePILOT REPORTED THAT THE OUTSIDE HANDLE ON OVERWING EXIT 4C DOES NOT STAY SECURE IN FLIGHT. MX RESECURED THE OUTSIDE DOOR HANDLE. OPS CHECK GOOD REF BMM 52-20-00-201. LATER THAT DAY MX REEXAMINED DURING SCHEDULED MX, NOTING THAT EMERGENCY EXIT 4C EXTERIOR HANDSDR GLBA2013082300301Handle · unsecurePILOT REPORTED THE 4C OUTER HANDLE ON THE OVERWING EXIT IS POPPED. MX SECURED THE EMERGENCY EXIT OUTER HANDLE. OPS CHECKED GOOD REF BMM 52-20-00-201.SDR GLBA2013082200300Skin · corrodedDURING A SCHEDULED INSPECTION, FOUND BELLY SKIN CORROSION AT FS 213.25, STRINGER 15R. REPAIRED IAW EO 13-1900-53-057. MAJOR REPAIR.SDR GLBA2013082100295Skin · damagedDURING A SCHEDULED INSPECTION, FOUND BELLY SKIN CHAFED, FWD OF FS 370.25 BETWEEN STRINGER 15--16L. REPAIRED IAW EO 13-1900-53-056.SDR GLBA2013082100298Skin · damagedDURING A SCHEDULED INSPECTION, FOUND STRINGER 15L FLANGE DAMAGED AT 2 LOCATIONS FROM THE VENT BLOWER BRACKET, CHAFED AT FS 368.25 AND 370.25, CHAFED HALF WAY THROUGH STRINGER FLANGE. REPAIRED IAW EO 13-1900-53-056. MAJOR REPAIR.SDR GLBA2013082100297Skin · damagedDURING A SCHEDULED INSPECTION, FOUND STRINGER 16 CHAFED AT FOUR LOCATIONS FROM THE VENT BLOWER DUCT HARDWARE-SCREWS, DAMAGE AT TOP OF STRINGER BETWEEN BS 370.25 AND 378.25. REPAIRED IAW. EO 13-1900-53-056. MAJOR REPAIR.SDR GLBA2013082100296Skin · damagedDURING A SCHEDULED INSPECTION, FOUND BELLY SKIN AT FS 368.25 - 370.25 HAS TWO HOLES WORN THRU SKIN, HOLES NEXT TO STRINGER 15L, FWD AREA, HOLE J SHAPED IS .85" IN LENGTH, AFT WORN AREA HOLE IS .3" IN LENGTH. REPAIRED AREA IAW EO 13-1900-53-056. MAJOR REPAIR.SDR GLBA2013081600294Skin · crackedDURING A SCHEDULED INSPECTION FOUND THE RT FUSELAGE BELLY SKIN CRACKED AT JUNCTION WITH WING SPAR AT FS 288, FWD SIDE OF WING SPAR, .9" IN LENGTH. REPAIRED IAW EO 13-1900-53-055.SDR 29GA2013081695633Warning Horn · false activationLANDING GEAR HORN SOUNDS WITH FLAPS AT 17 DEGREES. PERFORMED LANDING GEAR OPS CHECKED, COULD NOT DUPLICATE, NO DEFECTS NOTED.SDR 29GA2013081695332Warning Horn · false activationLANDING GEAR HORN SOUNDS WITH FLAPS AT 17 DEGREES. PERFORMED LANDING GEAR OPS CHECK COULD NOT DUPLICATE, NO DEFECTS NOTED.SDR GLBA2013081300293Spar Cap · chafedDURING A SCHEDULED INSP, FOUND CHAFING ON THE AFT SPAR LOWER CAP AT WS 85.50, APPROX .002 DEEP WITH A SMALL NICK IN THE CENTER OF THE CHAFE, NO OTHER DAMAGE IS NOTED, WIDTH OF THE DAMAGE IS 1.125". REPAIRED IAW EO 13-1900-57-015.SDR CA140418003Blade · broken(CAN) CREW ABORTED TAKEOFF AFTER FAILURE OF THE LT ENGINE ON THE TAKEOFF ROLL. POST INSPECTION BY MAINTENANCE REVEALED A POWER TURBINE BLADE FAILURE. ENGINE WAS REMOVED AND SENT TO REPAIR FACILITY FOR EVALUATION. INSPECTION AT REPAIR FACILITY REVEALED FIRSTSDR GLBA2013080200289Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE COCKPIT RT SIDEWALL FRAME AT FS 107 AT UPPER FASTENER, .5" IN LENGTH. REPAIRED IAW EO 13-1900-53-053.SDR GLBA2013080200288Longeron · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE COCKPIT RT SIDEWALL LONGERON AT FS 107, .5" IN LENGTH. REPAIRED IAW EO 13-1900-53-054.SDR GLBA2013073000287Stringer · damagedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE STRINGER ON THE VERTICAL STAB, LT SIDE AT CSS-68 AND 29.75 PERCENT CHORD, HOLE APPROX .5" IN DIAMETER. REPAIRED IAW EO 13-1900-55-019.SDR GLBA2013073000286Rib · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT INBD WING INBD RIB AT BL-29 AFT SIDE BY SPAR, .75 INCHE IN LENGTH. REPAIRED IAW EO 13-1900-57-014.SDR GLBA2013073000284Angle · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE A/S DOOR ANGLE AT FS 150.60 AT BOTH UPPER SNUBBER MOUNT NUTPLATES, TWO INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-051.SDR GLBA2013073000283Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND THREE CRACKS IN THE FUSELAGE FRAME AT BS 183.5, BETWEEN S2-3R AND SECOND CRACK FOUND FIVE INCHES OTBD, AND THIRD CRACK ON OTHER SIDE OF FASTENER, 1.125 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-050.SDR GLBA2013072600280Valve · inoperativePILOT REPORTED ON GEAR EXTENSION, INTRANSIT LIGHT ILLUMINATED MOMENTARILY, THEN GEAR HANDLE CIRCUIT BREAKER TRIPPED, LOST ALL GEAR INDICATIONS, FOLLOWED CHECKLIST, EXTENDED GEAR MANUALLY, THREE GREEN OBSERVED, LANDED WITHOUT FURTHER INCIDENT, EMERGENCY DECLARSDR GLBA2013072900282Circuit Breaker · trippedPILOT REPORTED THAT THE LANDING GEAR CIRCUIT BREAKER TRIPPED IN FLT, PERFORMED MANUAL EXTENTION. COULD NOT DUPLICATE.SDR GLBA2013072900281Landing Gear · failedPILOT REPORTED THAT DURING AN OPS CHECK, FLIGHT TO TEST THE GEAR, THE GEAR FAILED TO EXTEND, 2 AMP CIRCUIT BREAKER TRIPS AT HANDLE, PUMPED GEAR DOWN MANUALLY. OPS CHECK FLIGHT UNSATISFACTORY.SDR CA130724009Line · chafed(CAN) HYDRAULIC FLUID FOUND ON GROUND UNDER LT WING. REMOVED ACCESS PANEL AND FOUND HYDRAULIC LINE CHAFED THROUGH FROM ADJACENT DRAIN LINE CLAMP RUBBING AGAINST IT.SDR GLBA2013072500280Relay · failedDURING CRUISE, LOWERED LANDING GEAR HANDLE, HEARD NOTHING, INTRANSIT LIGHT WAS ON THEN WENT OUT AFTER 60 SECONDS, NOTICED LANDING GEAR HANDLE CIRCUIT BREAKER TRIPPED, RAN CHECKLIST, NO CHANGE, PUMPED GEAR DOWN, & DIVERTED. MX REPLACED THE LANDING GEAR HANDLE,SDR 29GA2013072300001Actuator · inoperativeAFTER TAKEOFF THE GEAR HANDLE RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTED. RAN QRH AND PROBLEM PERSISTED. F/O NOTED THAT THE RT MAIN GEAR DID NOT APPEAR TO BE FULLY RETRACTED. RETURNED TO DEPARTURE, GEAR FULLY EXTENDED FOR LANDING AND INDICATED 3 GRESDR GLBA2013072000278Unknown · odorPILOT REPORTED THAT THERE WAS AN ODOR COMING FROM THE ENVIRO SYSTEM. MX INSPECTED BOTH ENGS, NO OIL OR FUEL LEAKS INSPECTED, ENVIROMENTAL SYS, NO DEFECTS NOTED.SDR GLBA2013071900277Unknown · odorPILOT REPORTED THAT THERE WAS AN IRRITATING ODOR COMING FROM THE ENVIROMENTAL SYSTEM WITH THE BLOWERS ON. MX STARTED LT AND RT ENGINES AND RAN WITH BLOWERS AND VCM ON, ODOR DISAPATED AFTER 20 MIN, NO FURTHER DISCREPANCY NOTED.SDR GLBA2013072200276Unknown · odorPILOT REPORTED AN IRRIATING ODOR COMING FROM THE ENVIROMENTAL SYS WITH THE BLOWERS OFF. MX R & R THE EPA CAN CHECK VALVE AND LOWER FUEL TUBE, LEAK AND OPS CHECKED GOOD.SDR GLBA2013071800274Skin · leakingDURING A SCHEDULED ROUTINE INSPECTION, FOUND A PREVIOUS REPAIR LEAKING FUEL ON THE LT OTBD WING L/E AT WS 192.51 TO 198. REPAIRED IAW EO 13-1900-57-013.SDR GLBA2013071800275Unknown · odorPILOT REPORTED THAT WHILE RUNNING ACFT, AN ODOR WAS COMING FROM THE BLOWERS. MX INSPECTED, THE VENT BLOWERS AND ASSOCIATED SYSTEMS, NO DEFECTS, ALL CHECKED GOOD.SDR 29GA93532071613Valve · intermittentLEFT AND RIGHT MAIN GEAR DID NOT RETRACT AFTER TAKEOFF. NOSE GEAR RETRACTED RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED AND J HOOK INDICATED THAT THE PLANE WAS ON THE GROUND. LANDING GEAR RELAY CB POPPED AFTER 20 SECONDS QRH WAS RUN AND CB RESET AND GEAR RECYSDR 29GA2013071500001Cam Lock · inoperativeAFT CAM LOCKS WOULD NOT ROTATE ON AIRSTAIR DOOR. REPLACED LOWER AFT AIRSTAIR DOOR CABLE AND RIGGED, OPS CHECKED GOOD.SDR GLBA2013071200715Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE AFT FUSELAGE FRAME AT BS 509.5 AND STRINGER 3L IN THE FLANGE BEND RADIUS, 1.25" IN LENGTH. REPAIRED IAW EO 13-1900-53-048.SDR GLBA2013071200714Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT FWD SPAR CAP ANGLE ON THE VERTICAL STAB AT SECOND FASTENER FROM THE TOP, .375" IN LENGTH. REPAIRED IAW EO 13-1900-55-018.SDR GLBA2013071200713Rib · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT WING INBD RIB (JUNCTION WITH WING SPAR), RIB FLANGE AND DOUBLE, .75" IN LENGTH. REPAIRED IAW EO 13-1900-57-012.SDR GLBA2013071100712Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE RT FRAME AT FS 451 AND STRINGER 10R IN THE BEND RADIUS, 1.3" IN LENGTH. REPAIRED IAW EO 13-1900-53-049.SDR 29GA201307120001Powerpack · inoperativeLANDING GEAR RELAY CIRCUIT BREAKER TRIPPED AFTER TAKEOFF, WOULD NOT RESET. LANDING GEAR FAILED TO EXTEND NORMALLY USED ALTERNATE GEAR EXTENSION PROCEDURE. REPLACED HYDRAULIC POWERPACK, MOTOR AND PCB. OPS CHECKED GOOD.SDR 29GA94232070513AActuator · intermittentNOSE WHEEL GREEN ANNUNCIATOR LIGHT HAS ABOUT A 1 TO 2 SECOND DELAY WHEN GEAR HANDLE IS PLACED IN THE DOWN POSITION. REPLACED NOSE GEAR ACTUATOR OPS CHECKED GOOD.SDR ERAA201307080049Spar Web · chafedRIGHT WING REAR SPAR HAS DEEP CHAFE SPOT CAUSED BY SPLIT FLAP SWITCH WIRE WS120.98 AND WS121.73. REPAIRED (BLENDED)CHAFING RT WING AFT SPAR WEB, WS 120 IAW FIELD REPAIR FR-CO-100695.SDR ERAA201307080048Indicator · stuckLEFT TORQUE INDICATOR STUCK. R & R LT TORQUE INDICATOR, CALIBRATED INDICATOR IAW B1900D, MM 77-10-00. OPS CHECKED GOOD. OK FOR SERVICE.SDR GLBA2013070500269Blower · odorPILOT REPORTED A FOUL ODOR EMINATING FROM THE ENVIROMENTAL SYS WITH A NOTIABLE VIBRATION IN THE BACK OF THE ACFT. MX CLEANED THE ENVIRO VENT BLOWER AND SECURED THE PANEL, OPS CHECKED GOOD, NO ODOR NOTED.SDR CA130703004Engine · making metal(CAN) DURING FLIGHT, NG STARTED TO DETERIORATE, SLOW UN-COMMANDED DECELERATION. WHILE THE FUEL FLOW, WF AND TEMPERATURE, ITT, STARTED TO CLIMB. A COMMANDED FLIGHT SHUTDOWN WAS PERFORMED AFTER THE ENGINE TEMPERATURE REACHED 1027 OC WITH NG AT APPROXIMATELY 45 P
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