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 AMW1061111008Rib · corrodedCORROSION RT WING LEADING EDGE RIB LOWER FLANGE, AT WS 124.588. REPAIRED IAW REPORT 6452-1 REV. 1R.SDR BSAASDR0624Warning Switch · wornDURING CRUISE AT FL180, THE CARGO DOOR WARNING LIGHT CAME ON. CREW FOLLOWED CHECKLIST AND REQUESTED LOWER ALTITUDE. THE LIGHT WENT OUT, AND CREW LANDED WITHOUT INCIDENT. THE LIGHT WAS DEFERRED PER MEL. THE SWITCH WAS FOUND AT LIMITS OF ADJUSTMENT. THE MICSDR AMWA081219Safety Switch · malfunctionedAIRCRAFT WAS ON A FERRT FLIGHT FROM CHS TO CLT FOR MAINTENANCE. ON APPROACH, WHEN GEAR WAS EXTENDED FOR LANDING, NOSE GEAR DIDNT SHOW DOWN AND LOCKED. THE CREW THEN TRIED TO CYCLE THE GEAR A COUPLE TIMES AND ANNUNCIATOR STILL SHOWED NOSE GEAR AS IN TRANSIT. THSDR BSAASDR0623Switch Actuator · wornDURING CRUISE FLIGHT AT FL180 THE CARGO DOOR WARNING LIGHT CAME ON. CREW FOLLOWED EMERGENCY CHECKLIST PROCEDURES AND STARTED DESCENT. THE LIGHT WENT OUT AT 500 FT AGL. CREW LANDED WITH NO FURTHER INCIDENT. THE DOOR WARNING SWITCH ACTUATOR FOR THE LOCK WAS SDR NSVA200600223Wire · brokenRT FUEL PRESSURE LIGHT NOT ILLUMINATING WHEN T-HANDLE IS PULLED AND STANDBY PUMP IS ON. REPAIRED BROKEN WIRE ON DIODE CR3/CR4 IAW BE1900 WDM 76-21-01, OPS CHECK GOOD.SDR GUUA12050602Wire Harness · chafedFLIGHT: 9255, AFTER TAKEOFF SMOKE IN THE COCKPIT COMING FROM ADF. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. SECURED AND PROTECTED CHAFING WIRE BUNDLE BEHIND ADF CONTROL HEAD ADF ALSO REPLACED ADF CIRCUIT BREAKER OPERATIONAL CHECK NORMAL.SDR GUUA12050603Bleed Valve · malfunctionedFLIGHT: 9165, DURING FLIGHT LT ITT INDICATED ABOVE 900 DEGREES SHUTDOWN ENGINE IN FLIGHT ALL OTHER PARAMETERS NORMAL. COMPLETED RESTART ALL OPERATIONS RESUMED NORMAL. MAINTENANCE FERRY. PERFORMED ITT SYSTEM CHECK,TORQUE CALIBRATION CHECK AND PRECOOLER CHECK RSDR GUUA12040601Hose · rupturedFLIGHT: 5402 DURING APPROACH LANDING GEAR UNSAFE LIGHT APPEARED WITH A POPPED CIRCUIT BREAKER MANUALLY EXTENDED LANDED GEAR. LANDED WITHOUT INCIDENT. REPLACED RETRACTING ACTUATOR HOSE ASSEMBLY LANDING GEAR OPERATIONAL CHECK NORMAL.SDR AM1061127044DSpar · crackedDURING INSPECTION, MAINTENANCE FOUND A CRACK IN THE RT REAR SPAR WEB NEAR WS 117.50. REPAIRS DONE IAW MFG FIELD REPAIR, FR-CO-01407 REV.2.SDR AM1061127044CSpar Cap · crackedDURING INSPECTION MAINTENANCE FOUND A CRACK IN THE RT REAR SPAR, LOWER CAP AT APPROXIMATELY WS 117.50. MAINTENANCE REPAIRED THE CRACK IAW MFG FIELD REPAIR FR-CO-01405 REV. 3.SDR AM1061127044BSpar Cap · nickedDURING INSPECTION, MAINTENANCE FOUND A SMALL NICK IN THE LT REAR SPAR LOWER CAP AFT FLANGE. REPAIRED IAW MFG FIELD REPAIR FR-CO-01466.SDR AM1061127044ASpar Cap · damagedDURING INSPECTION, MAINTENANCE FOUND DAMAGED AND MISSING RIVETS ON LT WING LOWER AFT SPAR CAP. MAINTENANCE THEN REPAIRED THE AREA IAW MFG FIELD REPAIR FR-CO-01456.SDR NSVA200600219Wire · burnedLT ENG AUTOFEATHER DID NOT ARM ON DEPARTURE. PERFORMED AUTOFEATHER OPS CHECKS IAW BEECH 340 1900 AMM 61-21-00. OPS CHECKS NO GOOD. RT AFX REPEATER LIGHT NOT ILLUMINATING AND RT CWP RT AUTOFEATHER LIGHT NOT ILLUMINATING. DURING TROUBLESHOOTING FOUND PCB A14SDR AMWA081062Actuator · inoperativeDURING TAXI OUT, THE NOSE WHEEL STEERING FAILED MANUAL CASTER MODE, SINCE CAPT. KNEW THAT CONDITION WAS DEFERRABLE HE CONTINUED ON TO THE NEXT STATION. AFTER ARRIVING, DURING WALK AROUND INSPECTION HE DETECTED THE FAILURE OF THE ACUATOR. PROCEDURE 32-4 WAS PERSDR NSVA200600216Unknown · unknownRIGHT TORQUE FLUCTUATES 50LBS AND PROPS DO NOT SINK. PERFORMED OPERATIONAL CHECK OF ENGINE IAW BMM 76-10-00 AND PROP SYNC SYSTEM IAW COLGAN CARD 61-22-01. ALL SYSTEMS CHECK GOOD.SDR CA061127002Unknown · unknown(CAN) AIRCRAFT DEPARTED, DURING CLIMB THE LANDING GEAR RED UNSAFE LIGHT ILLUMINATED. GEAR WAS CYCLED AND LIGHT WOULD NOT EXTINGUISH. GEAR WAS SELECTED DOWN AND (3) GREEN ILLUMINATED WITH NO RED HANDLE. CREW ELECTED TO RETURN TO MAINTENANCE. MAINTENANCE INSPECSDR S2YA06010Drag Angle · brokenDURING INSPECTION OF THE LANDING GEAR, MAINTENANCE DISCOVERED THE RIGHT MAIN LANDING GEAR DRAG BRACE ARM WAS BROKEN. THIS PART IS A TRIANGLE SHAPED PART THAT CONNECTS THE DRAG BRACE TO THE ACTUATOR. THE ARM HAD ONE OF THE TWO LUGS THAT CONNECT IT TO THE LANDSDR AMWA80870Landing Gear · malfunctionedUPON GEAR EXTENTION FOR LANDING IN DFW, THE CREW NOTED LT MAIN LANDING GEAR ANNUNCIATOR DID NOT SHOW GEAR DOWN AND LOCKED. CREW THEN COMPLIED WITH EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. LANDED SAFELY WITHOUT FURTHER INCIDENT.SDR AMWA80797Annunciator · inoperativeUPON GEAR EXTENSION FOR LANDING INTO PIT, CREW NOTED NOSE GEAR ANNUNCIATOR DID NOT SHOW GEAR DOWN AND LOCKED. CREW C/W EMERGENCY CHECKLIST AND DECLAIRED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY INTO PIT WITH NO FURTHER INCIDENTS. MAINTENANCE WAS CALLED AND REMSDR AMWA224834Unknown · leakingRT WING LEADING EDGE FUEL LEAK: REPAIRED IAW MFG AIRCRAFT ENGINEERING REPORT NR 6449-1 REV. 1R.SDR SJ3R021444Bearing · brokenBLADE POSITION 4, S/N 1091 THRUST BEARING BROKEN. DAMAGE TO PROPELLER HUB BLADE SOCKET NR 4 IS BEYOND REPAIRABLE LIMITS. MFG SB 287 HAS NOT BEEN PERFORMED ON THIS PROPELLER.SDR GUUA11170601Skin · corrodedAT SCHEDULED INSPECTION DISCOVERED LT FUSELAGE SKIN DAMAGE DUE TO CORROSION. LOCATED AT F.S.363.250 STRINGER 13L CUT OUT SECTION OF CORRODED SKIN 2.0 IN X 5.0 IN FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER IAW STRUCTURAL REPAIR MANUAL 51-70-06.SDR AM1060904005CSpar · corrodedBIOCORROSION ON LT WING MAIN SPAR FWD AND AFT SPAR CAP FLANGES. REPAIRED IAW MFG REPAIR FR-CO-01425.SDR AM1060904005BSpar Cap · corrodedCORROSION ON WING MAIN SPAR CAP LOWER CAP BETWEEN WS114 AND WS124. MAINTENANCE REPAIRED IAW MFG REPAIR FR-CO-1426.SDR GUUA11150602Handle · malfunctionedFLIGHT: 5402 FLL/FLL AFTER TAKEOFF LANDING GEAR DID NOT RETRACT ON FIRST ATTEMPT RECYCLED HANDLE THEN THE GEAR RETRACTED. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR HANDLE SWITCH ASSEMBLY. LANDING GEAR OPERATIONAL, CHECK NORMAL. TEST FLIGSDR GUUA11150601Landing Gear · malfunctionedFLIGHT: 9220 PBI/TPA AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. DIVERTED AND LANDED WITHOUT INCIDENT. LANDING GEAR OPERATIONAL CHECK NORMAL COULD NOT DUPLICATE.SDR GUUA11110601Annunciator · malfunctionedFLIGHT: 9128 VPS/TPA, DURING TAKEOFF LT DISCHARGE LIGHT ANNUNCIATED CONTINUED TO TPA, LANDED WITHOUT INCIDENT. INSPECTED DISCHARGE SYSTEM AND OPERATIONAL CHECK NO DEFECT NOTED.SDR AMW1061104009Rivet · shearedFOUND SHEARED RIVETS ON LT WING AFT SPAR, FORWARD + AFT FLANGE AT W.S. 115.5 AND STRETCHED RIVETS ON BOTH FORWARD AND AFT FLANGE FROM WS 115 TO 123.5. FOUND DURING SERVICE BULLETIN: 57-3815. RIVETS REMOVED, EDDY CURRENT PERFORMED. HOLES REAMED AND LOCK FASTENSDR AMW1061019035Seat Track · wornSEAT TRACK WORN AND GOUGED. REPAIR COMPLIED WITH IAW MFG FR-CO-00532, FR-CO-00216, FR-CO-01271, FR-CO-1303, FR-CO-01365.SDR 2006FA0001140Fire Loop · malfunctionedON 10/4/2006, AFTER DEPARTING, APPROXIMATELY 30 MINUTES INTO THE FIRST LEG OF THE DAYS TRIP, THE PILOT REPORTED GETTING A RT ENGINE FIRE INDICATION. FOLLOWING PROCEDURE, THE PILOT PULLED THE T-HANDLE AND BLEW THE FIRE BOTTLE, SHUTTING DOWN THE ENGINE. THE PISDR NSVA200600197Connector · looseLEFT FIRE LOOP TEST INOP. INSTEAD OF THE LEFT FIRE LIGHT ILLUMINATING, THE T HANDLE ILLUMINATES. FOUND LT ENGINE FIRE LOOP CONNECTION LOOSE AT FIREWALL CONNECTOR TIGHTENED CONNECTION AND RESEALED IAW MM 26-10-01. TEST OF FIRE LOOP, OPS CK GOOD.SDR GUUA110601Warning Light · false activationFLIGHT: 9128 VPS/TPA DURING TAKEOFF LT DISCHARGE LIGHT ANNUNCIATED CONTINUED TO TPA LANDED WITHOUT INCIDENT. INSPECTED DISCHARGE SYSTEM AND OPERATIONAL CHECK NO DEFECT NOTED.SDR NSVA200600196Engine · power lossPARTIAL POWER ON NR 2 ENGINE DURING TAKEOFF. TRQ COULD NOT EXCEED 2500 LBS REGARDLESS OF POSITION. TAKEOFF ABORTED. ADJUSTED LOST MOTION LINK REF 76-10-00. RUN UP OPS CHECK NORMAL.SDR CA061113001Engine · malfunctioned(CAN) .5 HRS AFTER A SCHEDULED REPLACEMENT OF THE NR 3 AND NR 4 BEARING ASSY AND THE NR 1 AND NR 2 POWER TURBINE DISC`S DUE TO CYCLE LIFE LIMIT BEING REACHED, THE ENGINE LOST OIL PRESSURE AND WAS SHUTDOWN AND AIRCRAFT RETURNED TO DEPARTURE FIELD WITHOUT FURTHESDR CA061106017Transducer · malfunctioned(CAN) ON CLIMB NR 2 ENGINE DISPLAYED OIL PRESSURE FLUCTUATIONS FROM 120 TO 60 PSI. NO LOW OIL PRESSURE LIGHTS ILLUMINATED AND NO TORQUE FLUCUATIONS. THEY ELECTED TO RETURN TO AIRPORT. MAINTENANCE REPLACED THE R/H OIL PRESSURE TRANSDUCER AND AIRCRAFT WAS TESTEDSDR CA061106016Switch · failed(CAN) AFTER TWO MISSED APPROACHES, THE FLAPS WOULD NOT RETRACT FROM 17 DEGREES. AIRCRAFT DIVERTED, ON THE GROUND THE FLAP ASYMETRICAL OVERRIDE SWITCH WAS USED AND FLAPS RETRACTED. THE FLAPS WHERE THEN DEFERRED UNTIL MAINTENANCE INPECTED SYSTEM AND FOUND FAULTYSDR AMWA80555Warning System · false activationCABIN DOOR ANNUN ILLUMINATED IN FLIGHT AIRCRAFT DIVERTED TO DDC LANDED SAFELY WITH NO FUTHER INCIDENT. MAINTENANCE CAME AND COULD NOT DUPLICATE THE DISCREPANCY AFTER SEVERAL OPERATIONAL CHECKS. COMPANY RESEARCH SHOWS NO HISTORY FOR THIS DISCREPANCY FOR THIS AISDR NSVA200600193Panel · looseRT EMERGENCY INNER DOOR PANEL COMING LOOSE ON BOTTOM. SECURED INNER DOOR PANEL IAW 52-20-00.SDR GUUA11020601Landing Gear · maladjustmentFLIGHT:9199 EYW/MCO/DURING APPROACH, LANDING GEARS DID NOT EXTEND, MANUAL GEAR EXTENSION EXECUTED. MAINTENANCE FERRY TO FLL. INSPECTED LANDING GEAR SYSTEM REPLACED HYDRAULIC PUMP MOTOR AND CIRCUIT BREAKER. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHESDR NSVA200600195Handle · no testRT FIRE DETECTOR SYSTEM FIRE PULL HANDLE DOES NOT ILLUMINATE DURING TEST. EXERCISED PULL HANDLE NUMEROUS TIMES. OPS CHECK NORMAL IAW 26-10-01-101.SDR GLBA20060866Spar · crackedHORIZONTAL STABLIZER, MAIN SPAR WEB CRACKED.SDR AM1060904005DSkin · puncturedHOLE RT SIDE OF FUSELAGE (FS 143.0) NEAR STRINGER 11R REPAIRED IAW MM REPAIR FR-CO-01424. CAUSE OF HOLE UNKNOWN. DISCOVERED DURING ABC STRUCTURAL INSPECTION.SDR GLBA20060864Stringer · crackedSTRINGER 10R CRACKED AT FS 451.00 APPROXIMATELY .5 INCH.SDR GLBA20060863Frame · crackedFRAME CRACKED AT STRINGER 10R FS 451.00, APPROXIMATELY .7500 INCH.SDR GLBA20060865Skin · corrodedBELLY SKIN CORROSION ON STRINGERS 15L AND 14L FROM APPROXIMATELY FS 243.25 TO 250.75.SDR BSAASDR0622Spar Cap · crackedDURING INITIAL INSPECTION FOR SB57-3815, A CRACK WAS FOUND IN THE LEFT WING REAR SPAR CAP AFT FLANGE AT THE SUSPECT RIVET HOLE AT WS 115. THE CRACK STOPPED AT THE RADIUS OF THE VERITCAL LEG OF THE AFT SPAR WEB.SDR NSVA200600188Roller · failedFLAPS FAILED TO EXTEND ON APPROACH. REMOVED AND REPLACED LT FLAP ROLLER IAW 27-50-06, OPS CHECK GOOD, PN OFF/ON 101-521057-7.SDR NSVA200600184Governor · malfunctionedLEFT TORQUE INDICATOR INNACURATE WHEN CHANGING POWER. REMOVED AND REPLACED LEFT PROP GOV PN 8210-410 IAW 61-20-02, OPS CHECK GOOD.SDR BSAASDR0621Spar Cap · corrodedLEVEL 3 PITTING CORROSION WAS FOUND INITIALLY AROUND THE QUICK DRAIN IN THE 3RD INTERIOR SKIN DOUBLER. THIS CORROSION STARTED FROM THE UNTREATED EDGE OF THE QUICK DRAIN FITTING HOLE IN THE WING SKIN, AND PROGRESSED IN ALONG THE BOND LINE BETWEEN THE SKINS. WSDR AMWA080299Valve · malfunctionedON LANDING THE LT BRAKE PEDAL BLED OFF PRESSURE. THE AIRCRAFT MADE IT TO THE GATE SAFELY WITH NO FURTHER INCIDENT. THE AIRCRAFT WAS THEN FERRIED SO MAINTENANCE COULD ATTEND TO THE PROBLEM. MAINTENANCE THEN REMOVED AND REPLACED THE LT MLG BRAKE LINE, REFLARED
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