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 = '35A' 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 = '35A' 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 BSY2001F00020Downlock Switch · failed(CMH)(MIR) HAD NO NOSE GEAR DOWN LIGHT. REMOVED AND REPLACED DOWN AND LOCK SWITCH. OPS CHECKS GOOD.SDR JIK2001F00000Bearing · failedENGINE INFLIGHT SHUTDOWN AS A RESULT OF TOWER SHAFT FRACTURE. FRACTURE CAUSED BY THRUST BEARING FAILURE. BEARING FAILURE MADE AND THE TOTAL TIME NOT YET DETERMINED.SDR IJLA20011106Bolt · backed outNR 2 ENGINE OIL LOSS AND OIL PRESSURE LOSS. BOLT THAT HOLDS KEEPER FOR OIL TUBE TO OIL COOLER BACKED OUT AND ALLOWED OIL TO LEAK. ENGINE WAS SHUT DOWN IN CRUISE FLIGHT AND LANDED AS SOON AS PRACTICAL. BOLT HAS NO SAFETY OR SELF LOCKING DEVICE. REPAIRED ANDSDR GMA2001F00000Wire · brokenIN SERVICE FLEXING OF WIRE BUNDLE CAUSED THE SHIELDING AND A WIRE TO BREAK AT THE AIRFRAME-TO-WIRE BUNDLE CLAMP. SERVICE LOOP DID NOT APPEAR TO BE OF SUFFICIENT SIZE TO ALLOW THE NEEDED FLEXING OF THE WIRE BUNDLE. FORCE SENSOR DID NOT FUNCTION.SDR GMA2001F00001Wire · brokenIN SERVICE OF WIRE BUNDLE CAUSED THE SHIELDING TO BREAK, AND A WIRE TO BREAK AT THE AIRFRAME-TO-WIRE BUNDLE CLAMP. SERVICE LOOP DID NOT APPEAR TO BE OF SUFFICIENT SIZE TO ALLOW FOR THE NEEDED FLEXING OF THE WIRE BUNDLE. FORCE SENSOR DID NOT FUNCTION.SDR IMJ2001F00000Drive Shaft · disengagedON LANDING THE NR 1 THRUST REVERSER WOULD NOT STOW. THE FLEXIBLE DRIVESHAFT (OUTBOARD) BECAME DISENGAGED FROM THE AIR MOTOR DRIVE ASSEMBLY. WITH ONLY ONE SIDE DRIVING THE THRUST REVERSER, THE MECHANISM COCKED AND BOUND UP. ALTHOUGH THIS PROBLEM MAY HAVE RESSDR AUS20011062Line · chafed(AUS) LT ENGINE FIRE. DAMAGE TO COWLING. FIRE DAMAGE EVIDENT IN AREA OF STARTER MOTOR. INVESTIGATION FOUND THAT ELECTRICAL ARCING FROM A CHAFED WIRE TO A P' CLAMP HAD BURNT A SMALL HOLE APPROXIMATELY 1MM (0.039IN) IN DIAMETER IN THE ENGINE FUEL FEED LINE CAUSISDR BSY2001F00015Transmitter · faultyRIGHT ENGINE OIL PRESSURE RUNNING HIGH, OIL TEMPERATURE, RED LINE AT FLIGHT LEVEL 37,000. FOUND OIL PRESSURE TRANSMITTER 12 PSI HIGH, REMOVED AND REPLACED OIL PRESSURE TRANSMITTER OIL PRESSURE, CHECKS GOOD. COULD NOT DUPLICATE OIL TEMPERATURE PROBLEM.SDR 0017Shutoff Valve · leakingAT CRUISE ALT 43,000 FT PILOT NOTICE CABIN ALT WARNING LIGHT ILLUMINATED. THE PILOT INITIATED A DESCENT TO 27,000 FT PRESSURIZATION STARTED WORKING NORMAL. FLT CONTINUED AT 35,000 FT & WORKED NORMAL REST OF FLT. AFTER TROUBLESHOOTING SYS THE WINDSHIELD DEICE SSDR IRG2001F00001Computer · faultySPOILERON CAU LIGHT. LIGHT COMES ON DURING TEST AND WILL NOT RESET. REPLACED FAULTY SPOILERON COMPUTER AND ADJUSTED FOLLOW-UP ON RIGHT SPOILER.SDR BSY2001F00012Hydraulic Line · leaking(CMH) LOST HYDRAULIC PRESSURE COMING INTO AIRPORT, BLEW GEAR DOWN LANDED OK. REPAIRED HYDRAULIC LINE. NOSE WHEEL WELL, SERVICED RES. CHANGED BOTH PUMPS AS PRECAUTIONARY MEASURES, OPS CHECK GOOD.SDR BSY2001F00013Engine · leaking(ATL) IN ROUTE FROM (BNA) TO (ATL) LOST OIL PRESSURE, RIGHT ENGINE. SHUT ENGINE DOWN LANDED AT (ATL). HAD GARRETT FROM AUGUSTA LOOK AT ENGINE, HAS MAJOR OIL LEAK. REMOVED ENGINE FOR REPAIR AT AUGUSTA.SDR MXI2001F00000Valve · defectiveOIL PRESSURE GAUGE INDICATES IN THE RED ZONE (HIGH) AT TAKE OFF POWER. OIL PRESSURE FOLLOWS THE POWER LEVER.SDR BSY2001F00009Battery · overheatedRIGHT MAIN SHIP BATTERIES GOT HOT TURNING ON 160 DEGREE LIGHT AND INDICATION READ HIGH. REMOVED LOANER BATTERIES AND REPLACED WITH SERVICEABLE SET. OPS CHECK OK.SDR BSY2001F00008Battery · overheatedRIGHT MAIN SHIP BATTERY GOT HOT TURNING ON 160 DEGREE LIGHT AND INDICATION READ HIGH. REMOVED LOANER BATTERIES AND REPLACED WITH SERVICEABLE SET. OPS CHECK, OK.SDR BSY2001F00007Light · inoperativeHAD NO LEFT MAIN GEAR DOWN AND LOCK INTO AIRPORT. REMOVED AND REPLACED BULB OPS OK.SDR WIB2001F00000Shutoff Valve · leakingMAINTENANCE PERSONNEL DETECTED BLEED AIR LEAK IN TAILCONE DURING GROUND OPERATION. TRACED SOURCE TO CENTER MATING SURFACES OF WINDSHIELD ANTI-ICE SHUTOFF VALVE. REPLACED VALVE WITH OVERHAULED UNIT. PROBABLE CAUSE: BLOWN GASKET IN VALVE.SDR KKFA62201N72CTire · failedLEFT MAIN GEAR TIRES BLEW ON LANDING ROLL OUT. REPLACED TIRES WITH SERVICEABLE UNITS. TIRES SHIPPED TO MFG FOR ANALYSIS, THE FOLLOWING IS THEIR CONCLUSION BASED ON INSPECTION AND OBSERVATION FROM MFG REPORT NR NA010707: SUBMITTER STATES, PROBABLE CAUSE OF THSDR DIN2001F00000Check Valve · mislocatedCHECK VALVES ON LEFT SIDE, RIGHT SIDE OF CABIN INSTALLED WITH HINGE NOT AT 12 OCLOCK POSITION. RIGHT VALVE AT 5 OCLOCK, LEFT VALVE AT 2 OCLOCK. FACTORY ORIGINAL TORQUE SEAL WITH INSPECTORS STAMP ON IT HAD NEVER BEEN BROKEN. VALVES REMOVED AND INSPECTED AND SDR MJ12001F00000Flapper Valve · defectiveFLAPPER VALVE SEAL PN S-461 FOR LEFT AND RIGHT WING TIP TANKS WERE INSTALLED IAW SB 35/36-28-10 ON 02/19/01 AIRCRAFT HOURS 8,167.3 CUSTOMER ARRIVED AT OUR FACILITY ON 06/04/2001 AIRCRAFT HOURS 8306.9 WITH REPORTED DISCREPANCY AS FOLLOW: INVESTIGATE TIP TANK SDR 2001F00064Engine · flamed outRIGHT ENGINE FLAMED OUT DURING DESCENT, RESTART UNSUCCESSFUL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED FUEL FILTERS, SUMPS, ENGINE FUEL PRESSURES. PERFORMED ENGINE GROUND PERFORMANCE RUN ALL WITH NO DEFECTS NOTED. AIRCRAFT RELEASED FOR TEST FLSDR AOQA201CLight · inoperativeUPON LANDING GEAR EXTENSION, DURING FINAL APPROACH, RIGHT MAIN GEAR GREEN DOWN AND LOCK LIGHT DID NOT ILLUMINATE. PERFORMED LIGHT TEST AND CONFIRMED LIGHT INOPERATIVE. REPLACED BULBS IN LANDING GEAR CONTROL PANEL. JACKED AIRCRAFT AND PERFORMED LANDING GEAR SDR 2001F00070Door Frame · crackedDURING ROUTINE INSPECTION FORWARD DOOR JAMB WAS FOUND CRACKS THE WIDTH OF THE DOOR JAMB IN LINE WITH THE HINGE SEAM. FURTHER DISASSEMBLY FOUND ADDITIONAL CRACKS ON THE FORMED STEP RISER, DIRECTLY BELOW THE DOOR JAMB BETWEEN THE JAMB AND THE DOOR SKIN.SDR IRG2001F00000Relay · failedRUDDER TRIM INOPERATIVE. IN FLIGHT, REPLACED FAULTY RELAY(K1) IN E504 TRIM RELAY PANEL. OPPS CHECK GOOD.SDR DEL2001F00001Valve · inoperativeAT APPROX VR WHEN THE WHEELS LEFT GROUND, NOTICED SIGNIFICANTLY HIGHER LEVEL OF WIND NOISE. CONTINUED TO FLY THE AC UNTIL WE WERE AT A SAFE ALTITUDE. LOOKED IN BACK OF AC AND NOTICED SOME FAINT SMOKE, SO WE TOOK OUT OUR SMOKE GOGGLES AND HAD THEM STAND BY ASSDR DEL2001F00000Switch · inoperativeAT APPROX VR WHEN THE WHEELS LEFT GROUND, NOTICED SIGNIFICANTLY HIGHER LEVEL OF WIND NOISE. CONTINUED TO FLY THE AC UNTIL WE WERE AT A SAFE ALTITUDE. LOOKED IN BACK OF AC AND NOTICED SOME FAINT SMOKE, SO WE TOOK OUT OUR SMOKE GOGGLES AND HAD THEM STANDING BSDR 20010430CW011Module · defectiveDURING A PREFLIGHT, NR 1 ALTIMETER C/B TRIPPED AND WOULD NOT RESET. AFTER TROUBLESHOOTING FOUND SDC MODULE DEFECTIVE WITH MOISTURE. THE TRIP WAS MOVET TO A LR55-119. REPLACED SDC MODULE, REPAIRED AVIONIC BOY SEDL. TESTED D/C FOUND OK.SDR 20010501CW012Engine · malfunctionedLEFT ENGINE CAUSING SMOKE IN CABIN. TROUBLE SHOT ENGINE TO NR 4 AND NR 5 CARBON SEALS. REMOVED AND REPLACED ENGINE.SDR 20010501CW011Selector Switch · inoperativeLANDING GEAR WOULD NOT RETRACT. COULD NOT DUPLICATE ON GROUND. CHANGED GEAR SELECTOR SWITCH AND JUNCTION BLOCK FOR PRECAUTIONARY MEASURES, OPS CHECKED GOOD.SDR 20010501CW010Block · inoperativeLANDING GEAR WOULD NOT RETRACT. COULD NOT DUPLICATE ON GROUND. CHANGED GEAR SELECTOR SWITCH AND JUNCTION BLOCK FOR PRECAUTIONARY MEASURES, OPS CHECKED GOOD.SDR 20010416CW019Tire · delaminatedTREAD COMPLETELY SEPARATED FROM TIRE CAUSING DAMAGE TO WHEEL AND GEAR DOOR ASSEMBLIES. INCIDENT OCCURED AT TAKE OFF FROM DEPLOYED LOCATION, CREW HEARD AN UNUSUAL NOISE. ALL PARAMETERS NORMAL AND RECOVERED. AIRCRAFT LANDED AND TIRE DID NOT DEFLATE. ASSUME SDR 2002FA0000264Solenoid · intermittentSPOILER OPERATION INTERMITTENT. MAINIFOLD ASSEMBLY HAS TWO SOLENOIDS, APPEARS THAT ONE MAY BE STICKING OR HAVE AN ELECTRICAL PROBLEM.SDR DBCR122D0213Control Unit · failedNR1 ENGINE WOULD NOT START.1-DID TROUBLESHOOT TO FAILED IGNITION CONTROL UNIT. 2-REPLACED UNIT PN 3070378-2 SN452505 OFF, SN0002180160783-OPS CHECK OKSDR CA010118002Fuel Control · bypassing(CAN) DURING DESCENT, RIGHT ENGINE FLAME OUT, SINGLE ENGINE APPROACH AND LANDING IN CYQB, NO DAMAGE TO AIRCRAFT, PASSENGERS UNHURT(5).1. CREW NOTICED RT FUEL PRESSURE RED ANNUNCIATOR, SWITCH BOOST PUMP ON LIGHT OUT BUT ENGINE BEGAN SPOOL DOWN. 2. ENGINE FLAMESDR CIEA0010Mount · crackedDURING COMPLIANCE OF RECURRING AD 87-02-06 EFFECTIVE 2-6-87, WHILE PERFORMING VISUAL INSPECTION AS REQUIRED BY PAR A (1) OF THE AD, A SUSPECTED CRACK WAS NOTED IN THE UPPER FORWARD RADIUS OF THE MOUNT. THE CRACK WAS CONFIRMED BY MAGNETIC PARTICLE INSPECTION ASDR 20010122CW006Fire Loop · shortedMRR / BDL. RIGHT ENGINE FIRE LIGHT CAME ON. CREW SHUT DOWN ENGINE AND FIRED BOTH BOTTLES. FOUND AFT FIRE LOOP INSIDE ENGINE, WAS SHORTED. REMOVED AND REPLACED FIRE LOOP. OPS CKS GOOD, REPLACED BOTH ENGINE FIRE BOTTLES.SDR 20010122CW005Downlock Switch · failedMIR / CMH. HAD NO RIGHT GEAR DOWN AND LOCK LIGHT, BLEW GEAR DOWN, LANDED OK. REMOVED AND REPLACED DOWN AND LOCK SWITCH. OPS CHECKED GOOD.SDR 20010208CW003Servo · inoperativeDURING TAXI OUT FOR TAKE OFF AT ERI, NOSE STEERING BECAME INOPERATIVE. FOUND NOSE STEERING SERVO MOTOR INOPERATIVE.SDR CA010108020Seal · contaminated(CAN) PILOT REPORTED OF FROZEN AILERONS AT CRUISE ALTITUDE. AIRCRAFT RETURNED TO BASE. DURING DESCENT PILOT WAS ABLE TO REGAIN CONTROL. INVESTIGATION FOUND EXCESIVE AMOUNT OF WATER IN AILERON BRUSH SEALS. BRUSH SEALS CLEANED, DRIED AND RE-LUBRICTED PER M.M. 27SDR 20010321CW003Carbon Seal · wornAPPROX 5 MIN AFTER DEPARTURE, WHILE CONDUCTING AFTER TAKE OFF CHECK LIST, THE FO NOTICED THE NR 1 OIL PRESSURE, HIGH 80 PSI EVERYTHING ELSE WAS NORMAL. NOTICED ODOR OF HOT OIL, RETARDED NR 1 POWER LEVEL, OK PRESSURE FOLLOWED SO DID THE ODOR. OPTED FOR PRECASDR 20010208CW008Control Valve · inoperativeCREW REPORTED SMOKE IN CABIN DURING FLIGHT. REMOVED AND REPLACED TEMPERATURE CONTROLLER AND H VALVE. OPS CHECKED OKSDR ERYA682D5O-Ring · leakingCOMPLETE HYDRAULICS FAILURE DUE TO LEFT MAIN GEAR ACTUATOR O-RING FAILING.SDR 20010301CW003Bearing · failedWHILE ENROUTE RIGHT ENGINE FAILED DURING CLIMB AT ABOUT 30,000 FT. TURBINE RPM DROPPED TO ZERO. LANDING MADE WITHOUT INCIDENT. UPON INITIAL INSPECTION NOTED FAN SPINS FREELY BUT TURBINE WILL NOT ROTATE. ENGINE WAS REMOVED AND SENT FOR REPAIR OF NR2 SPOOL LSDR 20010123SG001Engine · failedWHILE EN ROUTE TO CEDAR RAPIDS, IOWA FROM JVY RIGHT ENGINE FAILED DURING CLIMB AT ABOUT 30,000 FEET. TURBINE RPM DROPPED TO ZERO. LANDING MADE AT IND WITHOUT INCIDENT. UPON INITIAL INSPECTION NOTED FANS SPINS FREELY BUT TURBINE WILL NOT ROTATE. (M)SDR 20001120SH031Motor · damagedCREW NOTICED SMOKE IN CABIN AFTER TAKEOFF AND RETURNED TO AIRPORT. MOTOR INSIDE BLOWER ASSY WAS FOUND HEAT AND SMOKE DAMAGED. (X)SDR 20001113SH003Tire · failedDURING TAKEOFF ROLL, BOTH LEFT MAIN GEAR TIRES FAILED CAUSING DAMAGE TO BOTH LEFT MAIN WHEELS, BRAKES, AND OUTBOARD GEAR DOOR. BOTH TIRES WERE SHREDDED TO THE POINT THAT MADE ANY INSPECTION OF THE TIRES IMPOSSIBLE. (X)SDR CA001026017Switch · failed(CAN) FAULTY PILOT TRIM SWITCH CAUSED VERTICAL VOLTAGE BLEEDING WHICH PREVENTED PROPER HORIZONTAL STAB TRIMMING WITH AUTOPILOT ENGAGED. THE SET SCREW HOLDING THE SWITCH IN PLACE HAD BROKEN THROUGH THE SIDE OF THE SWITCH ALLOWING THE BROKEN PIECES INSIDE THE SWSDR ERYA682D1Regulator Valve · failedHYDRAULIC FAILURE.SDR 20001030SH010Connector · dirtyDAL - RT ENGINE OIL TEMPERATURE SHOT UP TO RED LINE. SHUT DOWN ENGINE AND NOTIFIED DAL TOWER AND RETURNED. SUBLET GULFSTREAM IN DAL CLEANED AND TIGHTED OIL TEMPERATURE SENSOR CANON PLUG. COULD NOT DUPLICATE PROBLEM. (X)SDR 20001016SH011Wheel · failedTHIS PART WAS JUST OUT OF OVERHAUL. IT WAS THE FIRST LANDING AFTER INSTALLATION. THE WHEEL HALF FAILED AT BEAD HALF AND ABOUT ONE-THIRD OF THE WHEEL HALF BROKE OFF. AT THE MID-POINT OF THE BREAK, THE MATERIAL HAD A POLISHED LOOK AND APPEARED IT HAD BEEN WOR
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