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 = '400A' 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 = '400A' 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 DJFA2007119Strut · overservicedON LANDING CREW REPORTED LOSS OF BRAKING BELOW 40 KTS. ADDITIONALLY THE TR AND SPEEDBRAKES FAILED TO DEPLOY. MAINTENANCE DISCOVERED THE MAIN STRUTS WERE OVERSERVICED WITH N2 AND WERE NOT ACTUATING THE SQUAT SWITCH. STRUTS WERE PROPERLY SERVICED AND ALL OPERSDR DJFA2007118Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED SDR DXTA200702549Downlock Switch · malfunctionedON FINAL APPROACH THE RT MAIN GEAR (GREEN) LIGHT FAILED TO ILLUMINATE. ACCESSED CONNECTOR P272 IN RT WW. OHMED OUT DOWN LOCK SWITCH FOUND 2 OHMS RESISTANCE THROUGH CLOSED CONTACTS OF SWITCH, REMOVED SWITCH AND INSTALLED NEW CUSTOMER SUPPLIED SWITCH. REINSTALSDR DJFA2007117Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER INBOARD RIB AND BRACKET ASSEMBLIES, BOTH THE RIGHT AND LEFT INBOARD ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTISDR DXTA200702532Landing Gear · malfunctionedAFTER TAKEOFF, GEAR RETRACTED BUT IN TRANSIT RED LIGHT IN HANDLE DIDN'T GO OUT. TOWER REPORTED AT LEAST BOTH MAIN GEAR DOORS WERE OPEN. 11-01-07 JACKED AIRCRAFT, PERFORMED 5 GEAR SWINGS. NO DEFECTS NOTED. INSPECTED ALL GEAR UPLOCK HOOKS, SWITCHES AND RIGSDR DJFA2007116Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED SDR DJFA2007127Skin · corrodedDURING A SCHEDULED MAINTENANCE INSPECTION, TECHNICIANS FOUND MODERATE CORROSION ON BOTH HORIZONTAL STABILIZER LEADING EDGES. CORROSION WAS BEYOND REPAIRABLE LIMITS. BOTH LEADING EDGES WERE REPLACED.SDR DJFA2007115Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RT AND LT IB ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREASDR 2007FA0000914Fitting · looseWHILE PERFORMING AN A-D INSPECTION FOUND 8 LOOSE RIVETS IN THE FORWARD RIVET LINE OF THE ATTACHMENT PIVOT FITTING PN 45A21183-11 ON THE BOTTOM OF THE HORIZONTAL STABILIZER. IT IS SUSPECTED THAT THE LOOSE RIVETS WERE CAUSED BY FATIGUE AND AGE. RECOMMEND INSPESDR DJFA2007114Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED SDR 2007FA0000912Window · crackedWHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND NR 2 (COPILOT) SIDE WINDOW CRACKED USING THE PRISM INSPECTION METHOD. THE D-INSPECTION REQUIRES THAT BOTH WINDSHIELD RETAINERS OR USING OPTICAL PRISM INSPECTION METHOD. THE IS NO STATEMENT IN THE AIRCRAFT MM SDR 2007FA0000895Unknown · unknownAC EXPERIENCED A FLAP ASYMMETRIC LIGHT IN FLIGHT. THE CREW DID NOT TRY TO PUT THE FLAPS DOWN AND DIVERTED FOR A NO FLAP LANDING. CRITICAL CARE MAINTENANCE DROVE DOWN TO REPAIR THE AIRCRAFT. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM AFTER SEVERAL ATTEMPTS.SDR DJFA2007113Unknown · odorCREW NOTED AN "ACRID ODOR" FROM THE LAV AREA. AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE LAV AREA AND FOUND NO DISCREPANCIES. MAINTENANCE PERFORMED AN ENGINE RUN WITH NO DEFECTS NOTED.SDR DJFA2007110Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RIGHT AND LEFT INBOARD ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OSDR 2007FA0000910Door · crackedFOUND DURING INSPECTION. NOSE GEAR FOLLOW UP DOOR, P/N 45A31615-21 ON BRACKETS PN 45A31613-9, 45A31613-7 AND 45A31616-3 AT ATTACHING RIVET HAS CRACKS GOING FORWARD TO AFT THOUGH THE FIRST RIVET ALONG THE RIVET ROW. RELATIVE WIND PUSHING AFT ON THE DOOR WHILE SDR 2007FA0000911Structure · crackedFOUND DURING INSPECTION. NOSE GEAR FOLLOW UP DOOR PN 45A31615-21 ON BRACKETS PN 45A31613-9 AND 45A31613-7 AT ATTACHING RIVET HAS CRACKS GOING FORWARD TO AFT THROUGH THE FIRST RIVET ALONG THE RIVET ROW. RELATIVE WIND PUSHING AFT ON THE DOOR WHILE GEAR IS EXTESDR DJFA2007109Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RT AND LT IB ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREASDR DXTA200702482Engine · power lossON TAKEOFF FROM SAN T/O POWER COMPUTED AS 99 PERCENT N1. WITH THRUST LEVERS FIREWALLED, LT ENGINE N1 AT 99 PERCENT, RT ENGINE N1 AT 97.8 PERCENT. CONDITIONS AT SAN: SEA LEVEL, 22DEG C WIND 250 AT 7KNTS. 29.95.SDR DXTA200702481Downlock Switch · malfunctionedDID NOT GET A RT LANDING GEAR GREEN DOWN AND LOCKED INDICATION UPON GEAR EXTENTION. 09-28-07 REMOVED FAULTY RT MAIN GEAR DOWN AND LOCKED SWITCH AND INSTALLED NEW SWITCH IAW HAWKER 400XP MM CHAP. 32-10-00. AND TEMP REV 32-1. OPS CHECK GOOD. FOR DETAILS REF SDR DXTA200702479Handle · malfunctionedRT MLG LIGHT OUT & RED GEAR HANDLE ILLUMINATED DURING APPROACH. STAYS ON WHILE ON GROUND. CHECKED RT MLG UPLOCK SWITCH, RT MLG DOWNLOCK SWITCH & RT MLG DOOR CLOSE SWITCH, NO DISCREPANCIES NOTED. VISUALLY NOTED RT MLG NOT LOCKED. JACKED RT WING. PUSHED LOCKSDR 2007FA0000834Structure · damagedWHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND 8 SHEARED RIVETS IN THE FORWARD RIVET LINE OF THE ATTACHMENT PIVOT FITTING PN 45A21183-11 ON THE BOTTOM OF THE HORIZONTAL STABILIZER. IT IS SUSPECTED THAT THE MISSING RIVETS FAILED FROM FATIGUE. RECOMMEND INSSDR 2007FA0000833Structure · damagedWHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND 6 SHEARED RIVETS AND 2 LOOSE RIVETS IN THE FORWARD RIVET LINE OF THE ATTACHMENT PIVOT FITTING PN 45A21183-11 ON THE BOTTOM OF THE HORIZONTAL STABILIZER. IT IS SUSPECTED THAT THE MISSING RIVETS FAILED FROM FATISDR 2007FA0000832Window · crackedWHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND COPILOT COCKPIT SIDE WINDOW CRACKED USING THE PRISM INSPECTION METHOD. THE D-INSPECTION REQUIRES THAT BOTH WINDSHIELDS BE INSPECTED BY REMOVING THE WINDSHIELD RETAINERS OR USING OPTICAL PRISM INSPECTION METHODSDR 2007FA0000831Air Duct · crackedWHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND THE LEFT AFT FUSELAGE BLEED AIR LINE BELLOWS BLOWN APART PN 45A63517-073 AND THE RT AFT FUSELAGE BLEED AIR LINE BELLOWS BRAIDING FRAYING PN 45A63517-075. WHEN THE LT BLEED AIR LINE BLEW APART IT CRACKED A FUSESDR 2007FA0000830Cover · corrodedWHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND SPOILER MIXER ASSEMBLY BOX COVER NOT SEALED. REMOVED COVER AND FOUND CORROSION ON ACTUATOR AND MIXER ASSEMBLY. RECOMMEND THAT THE SPOILER MIXER AREA BE INSPECTED THOROUGHLY THE BOX COVER REMOVED. INSTALLED TSDR 2007FA0000909Door · crackedFOUND DURING INSPECTION. NOSE GEAR FOLLOW UP DOOR PN 45A31615-21 ON BRACKETS, PN 45A31613-9 AND 45A31613-7 AT ATTACHING RIVET HAS CRACKS GOING FORWARD TO AFT THROUGH THE FIRST RIVET ALONG THE RIVET ROW. RELATIVE WIND PUSHING AFT ON THE DOOR WHILE GEAR IS EXTSDR DXTA200702468Downlock Switch · failedDID NOT GET A RT LANDING GEAR GREEN DOWN NR LOCKED INDICATION UPON GEAR EXTENTION. 09-27-07 RESEATED LANDING GEAR DOWN LIGHT CLUSTER SOCKET, NO DEFECTS NOTED, INSPECTED RT MLG DOWNLOCK SWITCH FOR SAFETY AND SECURITY, JACKED ACFT IAW 400A MM 32-00-00, OPS SDR DJFA2007108Unknown · odorDURING FLIGHT CREW NOTED A BURNING ODOR FROM THE COPILOTS AIR VENT. AIRCRAFT LANDED SAFELY AT ITS DESTINATION. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. NO BURNING ODOR WAS NOTED.SDR DXTA200702458Anti-Skid Sys · inoperativeANTI SKID INOP ON LANDING IN SDF (HARD PEDALS AND WHEEL BRAKES LOCKING). RAN & TAXIED AIRCRAFT TO PERFORM OPERATIONAL CHECK AND TO VERIFY SQUAWK. COULD NOT DUPLICATE SQUAWK AFTER SEVERAL ATTEMPTS W/ SWITCH IN EACH POSITION. SYSTEM OPERATES NORMALLY. PERFORMESDR DXTA200702451Engine · power lossTARGET TAKEOFF POWER COMPUTED AS 99.0 PERCENT N1. CONDITIONS SEA LEVEL 22 DEG C. POWER AT 0 KNOTS 97.5 PERCENT N1. POWER AT 80 KNOTS 98.0 PERCENT N1 TAKEOFF ABORTED. PERFORMED ENGINES GROUND CHECKS I.A.W HAWKER 400XP MAINT MANUAL 71-00-00, FIG 206. FOUND THASDR DXTA200702448Adapter · failedRDR BST FAIL LIGHT FLASHED INTERMITTENTLY DURING TAKEOFF, THEN CAME ON STEADY 1 MIN AFTER TAKEOFF. 09-27-07 INTERROGATED AVIONICS STATUS ON THE MFD & FOUND NO CODES FOR RUDDER BOOST FAIL MESSAGE. PER THE RUDDER BOOST T/S CHART INTERROGATED THE LRU FAULT SDR DJFA2007107Inlet · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A CRACK ON THE RT ENGINE INLET AT THE 12 O'CLOCK POSITION THAT EXTENDED FWD AND AFT OF THE SCREW TRANSECTING THE SCREW HOLE. MAINTENANCE REPLACED THE INLET.SDR DJFA2007104Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLSDR DJFA2007105Inlet · crackedDURING A SCHEDULED MAINTENANCE EVENT MAINTENANCE FOUND A CRACK ON THE RT ENGINE INLET RING AT THE 7 O’CLOCK POSITION. THE CRACK TRANSECTED THE SCREW HOLE FROM THE AFT EDGE OF THE RING. 10-9-07 MAINTENANCE REPLACE THE INLET ASSEMBLY.SDR DJFA2007103Coalescer Bag · dirtyDURING CRUISE, PAX REPORTED AN ODOR OF BURNING RUBBER IN THE CABIN. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE COALESCER SOCK DIRTY AND REPLACED IT.SDR CA071003022Turbine Blades · damaged(CAN) THE ENGINE FLAMED OUT IN FLIGHT AND AN ATTEMPTED RELIGHT WAS UNSUCCESSFUL. SUBSEQUENT INSPECTION REVEALED DAMAGED POWER TURBINE BLADES. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071003022)SDR DJFA2007096Engine · failedDURING CLIMB 34,000 TO 40,000 HEARD A LOUD BANG & NOTICED LT ENGINE SPOOLING DOWN. DECLARED AN EMERGENCY & DIVERTED. RESTART ATTEMPT FAILED. 1 ENGINE LANDING NORMAL, NO PROBLEMS. MX FOUND SEVERE DAMAGE IN AFT PORTION OF ENGINE INCLUDING DAMAGED TURBINE BLASDR DXTA200702408Switch · looseON APPROACH TO FTY THE LEFT MAIN LANDING GEAR LIGHT WOULD NOT ILLUMINATE. WE RECYCLED THE GEAR TWO TIMES, AND ALSO VERIFIED THE LIGHT BULB WORKED WITH THE IND LIGHTS TEST. WE ALSO USED THE ALTERNATE GEAR EXTENSION PROCEDURE AND THE LIGHT WOULD NOT ILLUMIATE. SDR DXTA200702407Unknown · unknownDURING DESCENT WHEN SPEED BRAKES WERE EXTENDED, THE AIRPLANE ROLLED TO THE RT. WHEN THE SPEED BRAKES WERE EXTENDED IN LEVEL FLIGHT, NO ROLL CHANGES WERE NOTED. C/W SPEED BRAKE SYSTEMS, OPS CHECKS. CHECKED RIGGING & CABLE TENSIONS ALL CHECKS GOOD. IAW 400XP SDR DJFA2007093Uplock Switch · inoperativeON APPROACH, CREW REPORTED GEAR UNSAFE LIGHT IN CONJUNCTION WITH DOWN AND LOCKED INDICATION. CREW USED EMEREGENCY GEAR EXTENSION PROCEDURE AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG UPLOCK SWITCH INOPERATIVE. THE SWITCH WAS REPLACED.SDR DJFA2007091Downlock Switch · inoperativeON LANDING, CREW REPORTED NO GEAR DOWN AND LOCKED INDICATION FOR THE LT MLG. BULB TEST SHOWED THE BULB TO BE FUNCTIONAL. MAINTENANCE FOUND THE LT MLG DOWN LOCK SW INOPERATIVE. THE SWITCH WAS REPLACED.SDR DJFA2007092Line · misinstalledON CLIMB OUT, CREW REPORTED VERY HOT AIR COMING FROM THE AIR VENTS. CABIN TEMP WAS UNCONTROLLABLE AND REACHED 120 DEG F. AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE DISCOVERED COCKPIT TEMP CONTROL VALVE LINE SWAPPED WITH CABIN TEMP CONTROL LINE. LINESSDR DXTA200702392Valve · stickingON LANDING AND ROLLOUT WHILE BRAKING LT, BRAKE DID NOT OPERATE FROM 3-4 SECONDS THEN GRABS AND PULLS LT SHARPLY. CONFIRMED DISCREPANCY, FOUND POWERBRAKE VALVE STICKING. GAINED ACCESS TO VALVE. REMOVED VALVE AND INSTALLED AN OVERHAULED VALVE. BLED SYSTEM, PESDR DJFA2007090Line · failedDURING PREFLIGHT, CREW NOTED HYDRAULIC FLUID AT THE LT TR AREA. MAINTENANCE FOUND THE HYDRAULIC LINE FOR THE TR ACTUATOR STOW PRESSURE TO HAVE BURST. THE LINE WAS REPLACEDSDR DJFA2007089Line · looseON LANDING CREW REPORTED HYD LOW LEVEL LIGHT WITH 0 QTY INDICATED. BRAKES FAILED AND EMERGENCY BRAKING WAS USED. MAINTENANCE FOUND A LOOSE HYDRAULIC LINE AT THE PYLON. THE LINE WAS TIGHTENEDSDR DJFA2007088Coalescer Bag · dirtyON LANDING, CREW REPORTED SMOKE IN THE COCKPIT. SMOKE APPEARED TO BE COMING FROM THE WEMACS; AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE COALESCER SOCK DIRTY. THE SOCK WAS REPLACED.SDR DJFA2007086Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RT AND LT IB ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREASDR DJFA2007087Unknown · odorON DECENT, CREW NOTED A BURNING ODOR IN THE CABIN. CREW WAS UNABLE TO ISOLATE THE PROBLEM. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. PROBLEM HAS NOT REPEATED.SDR DJFA2007085Idler Link · brokenON POST FLIGHT, CREW NOTICED THE RT TR FAIRING DAMAGED. MAINTENANCE FOUND THE DRIVER LINK BROKEN. THE IDLER LINK CRACKED IN TWO PLACES 180 DEG APPART AT THE BEARING WHERE THE ARM IS CONNECTED TO THE TR DOOR CAUSING THE ARM TO SEPARATE FROM THE BEARING. MAINSDR DXTA200702375Brake · weakRT SEAT BRAKES FADE EXCESSIVELY AFTER DEPRESSING PEDALS. LT SEAT BRAKES ARE GOOD. REMOVED COPILOT RH MASTER CYLINDER, P/N 45AS38401-012, SN 2807. INSTALLED A NEW MASTER CYLINDER PN 45AS38401-012, SN 3274. WORK PERFORMED IAW HS-400XP MM CHAPTER 32-40-00.
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