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 AMW082983BCBattery · false indicationWHILE IN FLT, THE BATTERY CHARGE ANNUN ILLUMINATED. CREW PROCEEDED TO DESTINATION, LANDED SAFELY WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. REMOVED AND REPLACESDR BSAASDR0703Circuit Board · malfunctionedWHEN GEAR HANDLE WAS SELECTED DOWN DURING APPROACH, THE GEAR DIDN'T EXTEND, THE RED UNSAFE LIGHT CAME ON, AND THE GREEN GEAR DOWN LIGHTS STAYED OFF. CREW FOUND THE 2 AMP CONTROL CB POPPED. GEAR HANDLE WAS PUT BACK UP, THE CB WAS RESET, AND THE CB POPPED AGAISDR CA070305004Windshield · failed(CAN) CO-PILOTS WINDSHIELD SHATTERED IN CRUISE. AIRCRAFT DESCENDED IAW ABNORMAL OCCURRENCE CHECKLIST AND BROUGHT CABIN DIFF DOWN TO BELOW 2PSI. AIRCRAFT DESCENDED TO 11000 FT LOWERED CABIN ALTITUDE AT 500 FPM TO 11000FT. PUT CABIN INTO DUMP MODE AND CONTINUSDR NSVA20070051Connector · corrodedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. CLEARED CORROSION FROM A10881 CONNECTOR, PINS 5/9 P NR ZONE 521, OPS CK GOOD IAW 32-60-05.SDR AMW070228004Skin Panel · cracked4 INCH LONG CRACK NEAR BASE OF NR 2 COMM ANTENNA, IN FUSELAGE SKIN. REPAIRED BY INSTALLING EXTERNAL DOUBLER IAW AERODESIGN ENGINEERING REPORT NR 6586-1 AND BSRM 51-40-02. LT PN 129-430065-1, PANEL ASSY-LT BONDED.SDR GUUA94771022607ATube · chafedDURING INSP DISCOVERED ENGINE TRUSS TUBE PN 129-910032-101 HAD CHAFING DAMAGE AT 2.50 INCHES AFT OF FIRE SEAL FLANGE ON INBD SIDE. PERFORMED ENGINE TRUSS REPAIR TO CHAFED AREA, IAW FAA APPROVED DATA.SDR GUUA02260701Truss · chafedAT SCHEDULED ROUTINE MAINTENANCE DISCOVERED ENGINE TRUSS TUBE PN 129-910032-101 CHAFING DAMAGE AT 2.5 INCHES AFT OF FIRE SEAL FLANGE ON IB SIDE. PERFORMED TRUSS REPAIR TO CHAFFED AREA IAW APPROVED DATA CONTAINED IN THE DWG NR 070226,DERT 510305-CE.SDR AMW070206033Spar Cap · corrodedBIO-CORROSION ON RT SPAR CAP FLANGE AT WS124. REPAIRED IAW AERODESIGN ENGINEERING REPORT NR6556-1.SDR GLBA20060919Skin · misrepairedUPON ROUTINE INSPECTIONS MAINTENANCE FOUND THAT A REPAIR MUST CONFORM WITH SRM TECHNICAL DATA SPECIFICATIONS AT FS 126 TO FS 131.3 STRINGER 3R TO APPROXIMATELY 3 INCHES IB OF STRINGER 2R ABOVE PILOTS WINDSHIELD. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 17SDR GLBA20060918Stringer · crackedUPON ROUTINE INSPECTIONS, MAINTENANCE FOUND A STRINGER RELIEF HOLE CRACKED AT FS 177.3 RT STRINGER 9AL. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 177.3 RT STRINGER 9AL RELIEF HOLE IAW SRM 51-70 AND TC 8.2.1.SDR GLBA20060917Stringer · crackedUPON ROUTINE INSPECTIONS MAINTENANCE FOUND A STRINGER RELIEF HOLE CRACKED AT FS 163.9 RT STRINGER 9AL. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 163.9 RT STRINGER 9AL RELIEF HOLE IAW SRM 51-70 AND TC 8.2.1.SDR GLBA20060911Skin · crackedUPON ROUTINE INSPECTION MAINTENANCE FOUND THE BELLY SKIN CRACKED AT APPROXIMATELY F.S. 298.0, B.L. 27.0. MAINTENANCE REPAIRED BELLY SKIN AT APPROXIMATELY F.S.298.0 B.L. 27.0 PER BEECH SRM 51-70. RII INSPECTION COMPLIED WITH PER TC 8.2.1.SDR GUUA02190701Truss · chafedAT SCHEDULED ROUTINE MAINTENANCE DISCOVERED ENGINE TRUSS TUBE PN 129-910032-101 CHAFING DAMAGE AT 2.5 INCHES AFT OF FIRE SEAL FLANGE ON IB SIDE. PERFORMED TRUSS REPAIR TO CHAFFED AREA IAW APPROVED DATA CONTAINED IN THE MFG AIRLINER SERIES STRUCTURAL REPAIR MASDR GLBA20060910Skin · corrodedMAJOR REPAIR - UPON ROUTINE MAINTENANCE, EVIDENCE OF CORROSION WAS FOUND ON THE BELLY OF THE AIRCRAFT AT APPROXIMATELY FS 228.25, 1.5 INCHES ON RT SIDE OF STRINGER 16. MAINTENANCE REPAIRED THE BELLY SKIN FROM APPROXIMATELY F.S. 228.25 ON RIGHT HAND SIDE OF STRSDR GLBA20060913Skin · delaminatedMAJOR REPAIR - UPON ROUTINE INSPECTION MAINTENANCE FOUND A DELAMINATION ON THE AIRSTAIR DOOR SKIN BELOW THE EXTERIOR DOOR HANDLE. MAINTENANCE REPAIRED AIRSTAIR DOOR SKIN IAW BEECH 1900D SRM 52-10. RII COMPLIED WITH PER TC 8.2.1.SDR GLBA20060914Shimmy Dampener · missingUPON PRE-FLIGHT INSPECTION, PILOT REPORT OF SHIMMY DAMPENER DAMAGE/MISSING AND SUSPECTED DAMAGE TO STRUCTURE IN SURROUNDING AREA WAS ALSO REPORTED. MAINTENANCE REMOVED AND REPLACED THE SHIMMY DAMPER IAW B1900D MM 32-20. MAINENANCE REMOVED AND REPLACED STEERINSDR GLBA20060907Skin · crackedUPON ROUTINE INSPECTION- MAINTENANCE FOUND A CRACK APPROXIMATELY 7.750 INCHES LONG AT APPROXIMATELY FS 352, APPROXIMATELY 27.5 INCHES LT OF THE BELLY CENTERLINE. MAINTENANCE REPAIRED THE AFFECTED AREA IAW SRM 51-70 FROM FS 298 TO 305.75. PATCH DIMENSION 14 INCSDR GLBA20060908Skin · crackedUPON ROUTINE INSPECTION MAINT FOUND A CRACK AT A RIVET .2500 INCH LONG ON THE RT LOWER BELLY AREA AT FS 288. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS288 IAW SRM 53-90 AND TC 8.2.1. REPAIR DIMENSIONS 7 INCHES BY 6 INCHES.SDR GLBA20060909Skin · crackedUPON ROUTINE INSPECTION MAINTENANCE FOUND A 6 INCH CRACK 27.5 INCHES RT OF THE BELLY CENTERLINE FROM FS 303.75 TO FS 309.75.MAINTENANCE REPAIRED THE 6 INCH CRACK 27.5 INCHES RT OF THE BELLY CENTERLINE FROM FS 303.75 TO 309.75 IAW SRM 51-70 AND TC 8.2.1. REPASDR GLBA20060912Angle · crackedUPON ROUTINE INSPECTION MAINTENANCE FOUND AN AIRSTAIR DOOR ENTRANCE ANGLE CRACKED AT FS 150.6 AND RT STRINGER 9AL. MAINTENANCE AIRSTAIR DOOR ENTRANCE ANGLE IAW BEECH 1900D SRM 53-90. RII INSPECTION COMPLIED WITH PER TC 8.2.1.SDR GLBA2006910Skin · corrodedUPON ROUTINE MAINTENANCE, EVIDENCE OF CORROSION WAS FOUND ON THE BELLY OF THE AIRCRAFT AT APPROXIMATELY FS 228.25, 1.5 INCHES ON RT SIDE OF STRINGER 16.SDR AMW070219056Spar · crackedHORIZONTAL STAB MAIN SPAR CENTER WEB (4 EA) 0.5 INCH LONG CRACKS EXTENDED OUT FROM DEICE TUBE HOLE. FABRICATED/INSTALLED WEB PATCH.SDR GLBA20060906Skin · crackedUPON ROUTINE INSPECTION, MAINTENANCE DISCOVERED A 3.25 INCH LONG CRACK 27.5 INCHES LT OF BELLY CENTERLINE AT APPROXIMATELY STA. F.S. 352. MAINTENANCE REPAIRED THE CRACK IN THE FUSELAGE IAW SRM 51-70 FROM F.S. 351 TO F.S. 354.25. REPAIR DIMENSIONS 7.25 INCHES BSDR GUUA02170702Motor · failedAFTER TAKEOFF LANDING GEAR CIRCUIT BREAKER POPPED GEAR UNSAFE LIGHT ILLUMINATED NOSE GEAR RETRACTED BUT BOTH MAIN GEARS STAYED DOWN. CONTINUED, MANUALLY EXTENDED NOSE GEAR LANDED WITHOUT INCIDENT. REPLACED THE LANDING GEAR DC MOTOR OPERATIONAL CHECK NORMAL.SDR AMW082683Link · wornAFTER TAKEOFF, FLAPS STUCK AT 17 DEGREES. THE CAPTAIN RETURNED TO FIELD AND DECLARED AN EMERGENCY. ACFT LANDED AND FLAPS RETRACTED TO ZERO WITH NO FURTHER INCIDENT. REMOVED AND REPLACED RT FLAP SAFETY SWITCH LINKS AND BUSHINGS. OPS CK NORMAL.SDR GLBA20060903Window · crackedABORTED TAKEOFF, AIRCRAFT FLIGHT 5133, UPON ADVANCEMENT OF THROTTLE LEVERS A NEW CRACK APPEARED ON THE FIRST OFFICERS WINDOW. APPROXIMATELY 12 INCHES IN LENGTH. OUTER PANE ONLY. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDOW IAW MM 56-10. OPERATIOSDR AMW082669BCBattery · false indicationWHILE IN FLT, THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED. CREW PROCEEDED TO DESTINATION, LANDED SAFELY WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. REPLACED BATTSDR AMW082671Actuator · false indicationON APPROACH TO LANDING THE NOSE GEAR INDICATOR D/N SHOW GEAR DOWN AND LOCKED. CREW PERFORMED EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. A FLY-BY OF THE TOWER CONFIRMED GEAR WAS DOWN. THE INTRANSIT LIGHT IN THE GEAR HANDLE WAS ALSO OUT. SO CREW LANDED SSDR AMW082646Dpu · will not armAFTER T/O, THE FOS FEES COMPARE (PUSH TO RESET) BUTTON ILLUMINATED AND WOULD NOT RESET. AC RETURNED TO FIELD WITH NO OTHER INCIDENT. REMOVED AND REPLACED NR1 DPU, INSPECTED WIRING, OPS NORMAL.SDR GLBA20060902Unknown · odorUNSCHEDULED LANDING DURING TRAINING, GLA FLIGHT 41. PILOTS REPORTED THAT THE AIRCRAFT HAD JUST BEEN FUELED AND AFTER TAKEOFF A STRONG FUEL ODOR WAS PRESENT. MAINTENANCE INSPECTED THE WINGS AND FUSELAGE FOR LEAKS, AIRED OUT CABIN AND PERFORMED ENVIRONMENTAL CHESDR AMW061222025ADoor Frame · crackedAIRSTAIR DOOR FRAME ANGLE CRACKED. REPAIRED IAW REPORT 6512-1.SDR AWM061222025BRib · corrodedBIO CORROSION RT WING RIB AT WS124. REPAIRED IAW REPORT AERODESIGN REPORT 6497-1.SDR AMW082600Switch · dirtyAFTER T/O, FLAPS STUCK AT 17 DEGREES. CREW CALLED IT IN AND TOWER DECLARED EMERGENCY. EMERGENCY WAS THEN IMMEDIATELY TERMINATED A/C FLEW ITS ROUTE, ARRIVED ON TIME, NO FURTHER INCIDENT. (DIRECTED BY FAA TO ENTER AS AN SDR, INITIALLY ENTERED AS AN MIS) CLEASDR NSVA20070036Shutoff Valve · inoperativeFOUND LT ENGINE FIREWALL SHUTOFF VALVE IS INOP. REMOVED AND REPLACED LT ENGINE FIREWALL SHUTOFF VALVE PN/OFF/ON 118-389005-1, SN/OFF 9307076 SN/ON9031512, OPS CHECK GOOD.SDR GLBA20060893Skin · crackedDURING ROUTINE MAINTENANCE, A CRACK WAS FOUND ON THE RT SIDE OF THE FUSELAGE AT FUSELAGE STATION 545.5 AND RIVETS PROTRUDING DOWN THE 3 INCH CRACK AT WATERLINE 112. MX REMOVED DAMAGED AREA APPROXIAMTELY 6.25 INCH LONG BY 5.25 INCHES WIDE AT FUSELAGE STATION 5SDR GLBA20060892Skin · crackedDURING ROUTINE MAINTENANCE 6 INCH CRACK FOUND IN BELLY SKIN 27.5 INCH, RT OF BELLY CENTER LINE AT STATION 298 TO STATION 304. MX REPAIRED CRACK ON BELLY SKIN IAW SRM 51-70. REPAIR DIMENSIONS OF 15.75 INCH X 6 INCH. INSERT 12 INCH X 4.5 INCH. RII COMPLIED WISDR 20060893Skin · crackedDURING ROUTINE MAINTENANCE, A CRACK WAS FOUND ON THE RT SIDE OF THE FUSELAGE AT FUSELAGE STATION 545.5 AND RIVETS PROTRUDING DOWN THE 3 INCH CRACK AT WATERLINE 112. MX REMOVED DAMAGED AREA APPROXIAMTELY 6.25 INCHES LONG BY 5.25 INCHES WIDE AT FUSELAGE STATIONSDR 20060892Skin · crackedDURING ROUTINE MAINTENANCE 6 INCH CRACK FOUND IN BELLY SKIN 27.5 INCH RT OF BELLY CENTER LINE AT STATION 298 TO STATION 304. MX REPAIRED CRACK ON BELLY SKIN IAW SRM 51-70. REPAIR DIMENSIONS OF 15.75 INCHES X 6 INCHES. INSERT 12 INCHES X 4.5 INCHES. RII COMPLSDR NSVA20070034Selector Valve · malfunctionedFOUND LANDING GEAR CIRCUIT BREAKER POPPED ON GEAR RETRACTION, UPON EXTENSION BREAKER POPPED AGAIN BEFORE NOSE SHOWED DOWN AND LOCKED. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE PN ON/OFF 101-388008-3, SN ON 1886, SN OFF 1825 IAW B-1900MM CHAPTER 32-30-0SDR GUUA94753020507ASkin · crackedDURING SCHEDULED ROUTINE MX DISCOVERED AFT LOWER FUSELAGE SKIN AT AFT COMM ANTENNA FS 400 HAD CRACK. STOP DRILLED CRACK FABRICATED AND INSTALLED AN EXTERNAL REINFORCEMENT DOUBLER REPAIR.SDR GLBA20060890Skin · damagedRT WING SKIN TRAILING EDGE RIVETS LOOSE AND RIVET HOLES ELONGATED AT TRAILING EDGE BETWEEN WS 124.6 TO WS 136.6.SDR AMWA82479BCBattery · dischargedBATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR THE DISCREPANCY. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS.SDR GUUA02050702Skin · crackedAT SCHEDULED INSPECTION, DISCOVERED ONE CRACK AT AFT COMM ANTENNA (FS400) CRACK 3.0 INCHES RUNNING LONGITUDINALLY FORWARD FROM FS 400. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURALREPAIR MANUAL 51-70-06.SDR CA070514020Bearing · damaged(CAN) THE ENGINE EXHIBITED FLAMES FROM THE EXHAUST IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A DAMAGED (NR 2) BEARING. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514020)SDR CA070314014Compressor · seized(CAN) FLAMES WERE SEEN EXITING THE ENGINE EXHAUST AND THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED COMPRESSOR SEIZURE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070314014)SDR NSVA20070024Fire Loop · malfunctionedWHEN TESTING THE LT FIRE LOOP THE LEFT T HANDLE ILLUMINATED AND THE ANN DID NOT ILLUMINATE. REPOSITIONED LT FIRE LOOP NEAR LT EXHAUST STACK, INSPECTED FWD DIRE SEAL CONNECTIONS AND AFT GROUND, NDN, INSPECTED CONNECTIONS AT AMP NG AND PERFORMED ALL OPS CHECKS,SDR AMWA82406Bolt · missingUPON TAXI, CREW STATED AIRCRAFT WAS SHAKING AND RETURNED TO GATE. RT MAIN LANDING GEAR TORQUE KNEES FOUND TO HAVE PIVOT BOLT MISSING. CAUSE UNKNOWN. SUBSEQUENT INSPECTION OF RT MAIN GEAR SATISFACTORY. REPLACED UPPER AND LOWER TORQUE LINKS AND HARDWARE. AIRCRSDR CA070212010Bearing · destroyed(CAN) WHEN THE AIRCRAFT LANDED ALL OF PASSENGERS WERE UNLOADED FOR REFUELING. THE CAPTAIN OF THE AIRCRAFT WALKED AROUND THE RT SIDE OF THE AIRCRAFT TO TALK TO THE FUELER AND NOTICED THAT THE RT MAIN GEAR ONLY HAD ONE MAIN WHEEL ASSEMBLY ATTACHED. HE IMMEDIATSDR GLBA20060889Angle · crackedRT WING TO FUSELAGE CLOSING ANGLE CRACKED AT FS 288.0. CRACK 1.750 INCHES IN LENGTH.SDR GUUA01310701Bearing · failedFLIGHT: 9179 FLL/EYW AFTER LANDING IN EYW FELT SOME VIBRATION LOST NOSE WHEEL. REPLACED NOSE GEAR ASSEMBLY AND NOSE WHEEL ASSEMBLY.
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