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 = '550' 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 = '550' 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 N87SFSwitch · intermittentUPON APPROACH TO DESTINATION AIRPORT THE GEAR WAS SELECTED DOWN. THE PILOT NOTED THAT THE LT GEAR DOWN & LOCKED ANNUNCIATOR WAS NOT ILLUMINATED. THE PILOT RECYCLED THE GEAR BUT THE LIGHT STILL WOULD NOT ILLUMINATE. FOLLOWING PROCEDURES, THE EMERGENCY GEAR ESDR CA070607001Bearing · worn(CAN) AC WAS UNABLE TO LOWER THE RT MAIN LANDING GEAR. THE EMERGENCY EXTENSION PROCEDURE DID NOT INITIALLY RELEASE THE LANDING GEAR UPLOCK. SUBSEQUENT MANIPULATION OF THE SYSTEM RELEASED THE GEAR TO A DOWN AND LOCKED CONDITION AND THE AIRCRAFT MADE A SAFE LANDSDR 2007FA0000512Panel · delaminatedDURING COMPLETION OF MFG PROGRAM PHASE 5 INSPECTION, NOTICEABLE DEPRESSION WAS OBSERVED IN UPPER SURFACE OF LT AND RT WING SKINS IN AREA OF MLG UPLOCK HOOK ASSY ATTACHMENT. DURING COMPLETION OF LANDING GEAR OPERATIONAL CHECK, IT WAS NOTED THAT DEPRESSION ARE SDR 2007FA0000511Panel · delaminatedDURING COMPLETION OF MFG PROGRAM PHASE 5 INSPECTION, NOTICEABLE DEPRESSION WAS OBSERVED IN UPPER SURFACE OF LT AND RT WING SKINS IN AREA OF MLG UPLOCK HOOK ASSY ATTACHMENT. DURING COMPLETION OF LANDING GEAR OPERATIONAL CHECK, IT WAS NOTED THAT DEPRESSION AREASDR CA070530001Gyro · damaged(CAN) DURING THE COMPLETION OF AN UNASSOCIATED SB IT WAS NOTICED THAT THE C-12 GYRO HAD FREED ITSELF OF ITS MOUNTING. UNTIL NOW NO COMPARATOR ANNUNCIATIONS OR COMPASS RELATED SNAGS HAD BEEN REPORTED OR DETECTED. (TC NR 20070530001)SDR 2007FA0000570Frame · damagedFUSELAGE FRAME WEB DAMAGED BY DRILL BIT FROM THE BEND RADIUS OF THE OUTER (SKIN) FLANGE. REPLACEMENT REQUIRED SRM, CHAPTER 53-12-27. PROBABLE CAUSE: INCORRECTLY DRILLED AT AIRCRAFT MFG. (K)SDR 052407N322CSBulb · inoperativeDURING APPROACH WHEN GEAR WAS EXTENDED, THE LT MLG DOWN ANNUNCIATION FAILED TO ILLUMINATE. ABORTED APPROACH AND INITIATED AFM CHECKLIST PROCEDURES. COMPLIED WITH EMERGENCY EXTENSION ACTION BY BLOWING GEAR DOWN AND DECLARING EMERGENCY. AIRCRAFT LANDED WITHOUT SDR B3OR2007138Actuator · bindingFOLLOWING INSTALLATION OF A NEWLY OVERHAULED ELEVATOR TRIM TAB ACTUATOR, PARTIAL BINDING OF THE ACTUATOR OCCURRED. FURTHER INVESTIGATION REVEALED THAT THIS ACTUATOR HAD EXCESSIVELY WORN END BEARINGS ALLOWING LATERAL PLAY IN INTERNAL JACKSCREWS SUFFICIENT TO CSDR B3OR2007131Actuator · bindingA NEWLY OVERHAULED ELEVATOR TRIM TAB ACTUATOR WAS BINDING AND WOULD NOT PROVIDE ADEQUATE DEFLECTION AT THE TRIM TAB ONCE INSTALLED. FURTHER INVESTIGATION REVEALED THAT THIS ACTUATOR HAD EXCESSIVE PLAY AT THE END BEARINGS AND THAT THE PRIMARY SPROCKET PN WAS ISDR 050907N307CS1Bulb · burned outON APPROACH INTO PVD THE RIGHT MAIN LANDING GEAR LIGHT WOULD NOT ILLUMINATE WHITH GEAR SELECTED IN THE DOWN POSITION. THE CREW FOLLOWED THE AFM PROCEDURES DECLARED AN EMERGENCY AND DIVERTED TO BED. THE EMERGENCY GEAR EXTEND PROCEDURE WAS PERFORMED AND THE AIRCSDR 050807N334CS1Bulb · burned outON APPROACH INTO LAS THE LEFT MAIN LANDING GEAR UNLOCK LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION AND INDICATOR LIGHT TEST. THE APPRAOCH WAS ABORTED AND A GO AROUND WAS PERFORMED. THE EMERGENCY GEAR EXTENSION PROCEDURE WAS FOLLOWED AS PER THE CHECLIST AND SDR 42807N303CS1Lamp · inoperativeDURING APPROACH, THE LANDING GEAR WAS SELECTED DOWN. THE USUAL (3) BUMPS WERE HEARD BUT ONLY (2) GREEN LIGHTS ILLUMINATED. THE RT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. THE LANDING GEAR WAS CYCLED WITH THE SAME RESULTS AND INDICATION. THE EMERGENCY SDR CA070425001Actuator · malfunctioned(CAN) AIRCRAFT EXPERIENCED UNSAFE GEAR EXTENSION WHILE DOING CIRCUITS. GEAR SELECTION WAS MADE WHILE IN DOWNWIND TURN AND RT MAIN GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE, (GEAR UNLOCKED) AND (HYD PRESS ON) LIGHTS REMAINED ON. GEAR WAS RECYCLED IN LEVEL SDR CA070419001Wire · chafed(CAN) DURING AN ATTEMPT TO RUN THE AIRCRAFT TO FUNCTION CHECK THE WINDSHIELD ANTI-ICE BLEED AIR (SNAG-NO BLEED AIR TO THE WINDSHIELD FOR ANTI-ICE UNTIL WINDSHIELD ANTI-ICE CB IS PULLED). WHEN THE BATTERY SWITCH WAS TURNED ON THE LT CB PANEL 35 AMP CIRCUIT BREASDR 041507N318CS1Actuator · contaminatedDURING DECENT THROUGH 6000 FT MSL, ELEVATOR TRIM FROZE. BOTH MANUAL AND ELECTRIC OPERATION OF TRIM INOPERATIVE. CREW DECLARED AN EMERGENCY, DIVERTED FROM SCHEDULED DESTINATION. AIRCRAFT LANDED WITHOUT INCIDENT. WATER WAS FOUND IN BOTH MANUFACTURED LT AND RT SDR 040807N338CS1Door Seal · separatedLOUD NOISE FROM CABIN DOOR AT FL370. FOUND DOOR SEAL TO BE THE CAUSE. ALERTED ATC FOR LOWER ALTITUDE. NO PRESSURIZATION PROBLEMS INDICATED, HOWEVER PRESSURIZATION CONTROLLER BEGAN TO FLUCTUATE. CREW DONNED THEIR O2 MASKS, DECLARED AN EMERGENCY DESCENT AND DIVESDR CA070405001Bearing · corroded(CAN) WATER INFILTRATED BETWEEN SLEEVE P/N LA7140 AND BEARING P/N LA7139A CAUSING PIN HOLE CORROSION IN THE BEARING JACKET, ALLOWING WATER TO COME IN CONTACT WITH THE DRIVER LINK P/N 202-0007-3 PIVOT POINT CORRODING IT BEYOND REPAIR. (TC NR 20070405001)SDR 2007FA0000303Actuator · bindingAFTER A PHASE 1-4 INSPECTION THE ELEVATOR TRIM WAS FOUND TO BE BINDING. INSPECTION OF THIS SYSTEM FOUND THAT THE WILKIE BUTTON IN THE BACK OF THE ACTUATOR TRIM JACK SCREWS HAD COME OUT AND WAS BINDING THE TRIM CHAIN AND SPROCKETS. WHEN THE ACTUATORS ARE LUBED SDR 2007FA0000302Actuator · bindingAFTER A PHASE 1-4 INSPECTION THE ELEVATOR TRIM WAS FOUND TO BE BINDING. INSPECTION OF THIS SYSTEM FOUND THAT THE WILKIE BUTTON IN THE BACK OF THE ACTUATOR TRIM JACK SCREWS HAD COME OUT AND WAS BINDING THE TRIM CHAIN AND SPROCKETS. WHEN THE ACTUATORS ARE LUBED SDR CA070409004Window · delaminated(CAN) PILOT`S STORM WINDOW DELAMINATED AT UPPER EDGE, RESULTING IN A CRACK FROM ATTACH HOLE RADIUS TO AFT EDGE. (TC NR 20070409004)SDR CA070329005Buckle · interference(CAN) CONTROL YOKE INTERFERENCE WITH ROTORY SEAT BUCKLES INSPECTED IAW INTERNAL CAMPAIGN NOTICE 010-25-10-011. OPERATION OF EITHER PILOTS AND CO-PILOTS YOKES WITH SEATS FULL FORWARD CONFIRMS THAT INTERFERENCE CAN CAUSE UNLATCHING OF THE SEATBELT ROTARY BUCKLESSDR 2007FA0000262Duct · unknownUPON RECEIVING THE NEW PART P/N 6555030-11 IT WOULD NOT FIT THE ENGINE. THE ORIGINAL DUCT IS 27 .2500 INCH OUTSIDE AND 25.5 INCH INSIDE. THE NEW UNIT IS A FULL .5 INCH SMALLER IN DIAMETER ALL AROUND. THIS IS THE SECOND ISSUE WITH THESE DUCTS THE FIRST WERE MISSDR 2007FA0000261Seal · mismanufacturedWHILE INSTALLING THIS FACTORY NEW SEAL IT WAS NOTED THAT THE SEAL WAS VERY TIGHT GOING AROUND THE DOOR. UPON CABIN PRESS TEST THE SEAL WILL NOT INFLATE DUE TO BEING TO TIGHT. (2) SEAL FROM STOCK WERE TRIED WITH THE SAME AFFECT. THE LAST SEAL WAS INSTALLED ANDSDR 032007N300CS1Switch · malfunctionedAFTER TAKEOFF, THE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. THE LT MAIN GEAR GREEN LIGHT ILLUMINATED ABOUT 10 SECONDS LATER FOLLOWED BY THE RT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BAD SWITCH IN THE RT MAIN LANDING GEAR ACTUATORSDR 031707N319CS1Bulb · inoperativeDURING APPROACH, WHEN GEAR WAS EXTENDED THERE WAS NO GREEN DOWN INDICATION FOR LT MAIN GEAR. ABORTED APPROACH AND CLIMBED TO SAFE ALTITUDE, PERFORMED AFM EMERGENCY CHECK LIST PROCEDURES. LANDING GEAR WAS BLOWN DOWN AND CREW DECLARED EMERGENCY AND LANDED UNEVESDR 2007FA0000256Duct · mismanufacturedDURING INSPECTION MULTIPLE PATCHES WERE FOUND ON EXHAUST DUCT ASSY P/N 6555030-11. A REPLACEMENT WAS ORDERED AND FOUND TO HAVE 2 HOLES MISDRILLED BY 2 DEGREES. MFG WAS CONTACTED AS TO WHAT COULD BE DONE AND AFTER CONFIRMING THAT IN TRUTH 2 HOLES WERE NOT PROPESDR 2007FA0313001Hinge · crackedDESCRIPTION AMENDED TO SAY THAT THE LOWER LUG WAS CRACKED INSTEAD OF THE UPPER LUG.SDR 20582007TJ001Hinge · crackedDURING A DAILY INSPECTION OF THE AIRCRAFT A CRACK WAS FOUND ON THE UPPER LUG OF THE DOOR HINGE. DURING REPLACEMENT OF THE HINGE THE LUG COMPLETELY BROKE IN (2) PEICES.SDR CA070328002Duct · debonded(CAN) COMPANY CAMPAIGN NOTICE 851-21-20-034 WAS CARRIED OUT. INSPECTION FOUND THE CLAMP PORTION OF THE BLEED AIR WELD ASSEMBLY LOOSE. THE WELD ASSEMBLY WAS REPAIRED BY COLD BONDING IAW INSTRUCTIONS RECEIVED FROM MFG CUSTOMER SUPPORT. UNIT RETURNED TO SERVICE. SDR 2007FA0000253Actuator · bindingWHILE REPLACING TRIM ACTUATOR P/N 6565141-2 WITH WHAT MFG SAID WAS AN APPROVED SUB PART P/N 5565450-92. IT WAS FOUND THAT THE LOLLIPOPS (JACK SCREWS) WERE 5.5 INCHES LONG AND THE ORIGINAL LOLLIPOPS ARE 5.75 INCHES LONG. IF YOU LOOK AT THE COMPONENT MANUAL FOSDR 2007H0002Actuator · misoverhauledACTUATOR RODS PROVIDED WITH UNIT WERE TOO SHORT TO MOVE ELEVATOR TABS THE REQUIRED AMOUNT.SDR 2007FA0000220Seat · crackedUPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. CHAIR WAS REPAIRED IAW ST01042WI STRUCTURAL SEAT REPAIR. (K)SDR 2007FA0000176Roll Pin · brokenDURING A PHASE 5 INSPECTION THE FLAPS SEAMED TO BE SLOW AND BINDING. AT CLOSER INSPECTION IT WAS FOUND THAT THE ROLL PIN HAD BROKEN ALLOWING THE SPROCKET TO MOVE FWD. ON THE P/N 5565190-9 BRAZE ASSY-DRIVE THIS CAUSED BINDING AND ALLOWED THE SPROCKET TO EVEN DRSDR 2007FA0000188Seat · crackedUPPER CHAIR BASE ASSY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. CHAIR WAS REPAIRED IAW STC 01042WI STRUCTURAL SEAT REPAIR. (K)SDR 213200744ASSkin · damagedPULLED FASTENERS AND CRACK IN LT WING LOWER SKIN.SDR FCPR20070004Static Port · leakingFOUND RT STATIC PORT P/N CM2933-7 CRACKED DURING LEAK TEST.SDR 020907N300CS1Indication Sys · malfunctionedON FINAL APPROACH, WHEN LANDING GEAR WAS EXTENDED, THE LT MAIN GEAR GREEN DOWN LIGHT FAILED TO ILLUMINATE. CREW ABORTED APPROACH AND CLIMBED TO SAFE ALTITUDE TO ADDRESS SITUATION. AN EMERGENCY WAS DECLARED, CREW FOLLOWED AFM EMERGENCY PROCEDURES AND BLEW GEAR SDR CA070209003Buckle · interference(CAN) WITH A COCKPIT CREW MEMBER STRAPPED INTO THEIR SEAT WITH THE SEAT FULLY FORWARD, INTERFERENCE BETWEEN THE CONTROL COLUMN YOKE AND THE ROTARY SEAT BELT BUCKLE FINS OCCURS WHEN THE CONTROL YOKE IS PULLED FULLY AFT AND ROTATED. THE POSSIBILITY EXISTS THAT TSDR CA070209002Buckle · malfunctioned(CAN) WITH A COCKPIT CREW MEMBER STRAPPED INTO THEIR SEAT WITH THE SEAT FULLY FORWARD, INTERFERENCE BETWEEN THE CONTROL COLUMN YOKE AND THE ROTARY SEAT BELT BUCKLE FINS OCCURS WHEN THE CONTROL YOKE IS PULLED FULLY AFT AND ROTATED. THE POSSIBILITY EXISTS THAT TSDR CA070221005Buckle · malfunctioned(CAN) COMPLIED WITH COMPANY CAMPAIGN NOTICE 010-25-10-011/SAIB NM-06-29. THE CREW SEATBELT ROTARY LATCH CAN BE CONTACTED WITH THE CONTROL YOKE LET DOWN HOLDER WITH THE SEAT FULL FORWARD AND THE YOKE FULL AFT. IT IS POSSIBLE TO UNLATCH THE SEATBELT BY ROTATINGSDR CA070205005Buckle · failed(CAN) REF FAA SPECIAL AIRWORTHINESS INFORMATION BULLETIN NM-06-29 AND MFG CAMPAIGN NOTICE 010-25-10-011 REV 1 FIXED WING AIRCRAFT EQUIPPED WITH ROTARY CREW SEAT BELT BUCKLES. WHEN THE CONTROL COLUMN IS PULLED FULLY AFT THE SEAT BELT BUCKLE CAN BE RELEASED BY SDR CA070124002Solenoid Valve · failed(CAN) STILL IN CRUISE CONFIG PILOTS DECIDED TO SELECT ANTI-ICE IN PREPARATION FOR DECENT TO AIRPORT. AT THIS TIME, A LT ANTI-ICE FAIL LIGHT ILLUMINATED. TROUBLESHOOTING LATER CONFIRMED THAT THE LT ENGINE ANTI-ICE VALVE HAD FAILED. THE VALVE IS POWERED 28VDC SDR CWQR200701Pushrod · mismanufacturedDURING THE REPAIR STATION PRELIMINARY INCOMING PARTS INSPECTION, IT WAS OBSERVED THAT ONE OF THE NEW ELEVATOR PUSHROD CLEVIS ENDS WERE ATTACHED WITH ALUMINUM RIVETS. ANOTHER NEW UNIT AND THE OLD PUSHRODS USED MONEL RIVETS. A CALL TO MFG CONFIRMED THAT MONEL RISDR CA070123004Fan · odor(CAN) ON APPROACH WHEN THE CREW SMELLED SOMETHING BURNING IN THE CABIN. THE CABIN FILLED UP WITH SMOKE AND THE CREW PUT ON THEIR MASKS AND DROPPED THE PASSENGERS MASKS. THEY LANDED WITHOUT DECLARING AN EMERGENCY. AN AME WAS SENT TO AND DETERMINED THAT THE DSDR 012107N338CS1Connector · faultyON APPROACH, CREW NOTICED LT MLG DOWN/LOCK LIGHT OUT. ABORTED APPROACH, CONFIRMED LT MLG WAS PHYSICALLY DOWN. DIVERTED, DECLARED EMERGENCY, FOLLOWED AFM EMERGENCY PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE STAFF FOUND LT DOWN AND LOCK CONNECTOR TO BSDR CA061207001Wire · damaged(CAN) THE FUEL TANKS SHOW EVIDENCE OF LOCALIZED DISCOLORATION AND VARIOUS NICKS ON OUTER JACKETS OF FUEL QUANTITY PROBE WIRING. THERE IS ALSO DISCOLORATION ON THE TERMINALS OF THE VARIOUS FUEL PROBES. THIS DAMAGE IS PROBABLY CAUSED BY IMPROPER USE OF THE TYRAPSDR 2006FA0001127Hinge · corrodedAT INSPECTION THE HINGE WAS FOUND CORRODED AND THE PINS WORN PAST LIMITS. A FACTORY NEW HINGE ASSY WAS ORDERED AND INSTALLED. UPON COMPLETION OF THE WORK THE AIRCRAFT WAS PRESSURIZED AND THE HINGE ASSY WAS FOUND TO BE LEAKING. UPON CLOSER INSPECTION THE SKIN TSDR 2007FA0000142Valve · out of positionAT G; 390 15A, -12 DEGREES CABIN DOOR SEAL DEFLATED NECESSATING AN EMERGENCY DESCENT TO 10,000 FT. AFTER 5-8 MINUTES, DOOR SEAL RE-INFLATED OPERATION WAS NORMAL, CONDITION DID NOT REOCCUR. FOUND DOOR SEAL VALVE WARM AIR TUBE BLAOCKED BY TAPE AND OUT OF POSITSDR 112006N335CS1Bolt · looseDURING FINAL APPROACH, THE PILOT SELECTED GEAR DOWN FOR LANDING. THE ONLY GEAR TO EXTEND WAS THE NOSE GEAR, ALL OTHER INDICATIONS INDICATED AN UNSAFE CONDITION. PILOT NOTIFIED TOWER OF PROBLEM AND DECLARED AN EMERGENCY. THEY WENT THROUGH THE EMERGENCY CHECKSDR CA061114005Guard · cracked(CAN) WHILE COMPLYING WITH COMPANY CAMPAIGN NOTICE CN 851-27-20-035, BOTH ELEVATOR CABLE GAURDS WERE FOUND CRACKED ADJASENT TO THE CLAMPS. THE TUBES WERE FOUND WITH .5 INCH LONGITUDINAL CRACKS. ADDITIONALLY ONE OF THE ATTACH CLAMPS WAS FOUND TO HAVE THE WRONG
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