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 = 'C90' 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 = 'C90' 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 CA011127006Skin · cracked(CAN) ON A RECENT ROUTINE INSPECTION ON LJ886 A CRACK WAS FOUND ON THE LT UPPER WING SKIN AT STA 175 AND WL 81 SEEN FROM THE UNDERSIDE IN THE WHEELWELL. THE AFT NACELLE FAIRING WAS REMOVED AND ANOTHER CRACK WAS FOUND AT STA 182 AND WL70.THE AFT NACELLE FAIRINSDR VG42001F00001Skin · crackedTHE LEFT ELEVATOR LOWER SKIN AT THE OUTBOARD HINGE POINT HAD TWO CRACKS EXTENDING FROM THE HINGE CUTOUT AREA ACROSS SPAR CAP.SDR 2001F00069Connector · corrodedNO FUEL TRANSFER LIGHT WOULD STAY ILLUMINATED EVEN IF FUEL WAS BEING TRANSFERRED. THIS WAS AN INTERMITTENT PROBLEM AND WAS NOT ABLE TO BE SOLVED UNTIL THE PROBLEM OCCURRED WHEN A MECHANIC COULD TROUBLESHOOT THE SYSTEM. AT TIMES THE NO FUEL TRANSFER LAMP WOULSDR CA010622006Control Cable · failed(CAN) ELEVATOR TRIM WOULD NOT FUNCTION AT TOP CLIMB. ELECTRIC TRIM MOTOR APPEARED TO FUNCTION NORMALLY BUT NO TRIM CONTROL MOVEMENT AVAILABLE. MANUAL TRIM DID NOT ACTUATE CONTROL SERVICE. MANUAL TRIM WHEEL WOULD ONLY FREE WHEEL, NO TRIM CONTROL AVAILABLE. AIRCSDR CTU2002F00001Link · missingREMOVED AND REPLACED THE NOSE LANDING GEAR RETRACT DUPLEX CHAIN IN THE NOSE. THE TECH INSTALLED THE CONNECTING LINK PN 13137825CL INSPECTOR FOLLOWED UP AND NOTICED THAT THE CONNECTING LINK WAS MISSING THE TWO CENTER PLATES. WHEN THE TECH WAS ASKED ABOUT THESDR SAILJ1052Torque Tube · crackedAIRCRAFT CAME INTO MAINTENANCE FOR SCHEDULED TBO OF THE LANDING GEAR MOTOR. THE MOTOR IS ATTACHED TO THE LANDING GEAR GEARBOX WHICH IS ALSO ATTACHED TO THE FAILED TORQUE TUBE. INSPECTION SHOWED NO EVIDENCE OF CORROSION. FAILURE AREA IS LOCATED AT AND AROUND THSDR 20001127SH013Bracket · damagedWHILE RE-INSTALLING THE RIGHT ELEVATOR, THE MECHANIC NOTICED THE BOLT THAT HOLDS THE ELEVATOR OUTBOARD BRACKET TO THE HORIZONTAL BEARING BRACKET PN 50-620001-69 WAS SLOPPY. AFTER REMOVING BOLT, FOUND IT SEVERELY WORN AND BRACKET 50-61000-546 HAD SEVERELY ELONSDR CA001110003Pump · failed(CAN) FUEL PUMP FAILED. (X)SDR 20001026SH012Skin · crackedON 5-15-00, LEFT AILERON SKIN FOUND CRACKED AT OUTBOARD AFT EDGE UNDERSIDE. UPON FURTHER INSPECTION, FOUND THE SKIN TO BE VERY BRITTLE. ON 9-10-00, FOUND RIGHT AILERON SKIN CRACKED AT SKIN LAP AFT OF CENTER ATTACH POINT BOTH UPPER AND LOWER. SKIN FOUND TO BSDR AU000702Exciter · failed(AUS) LEFT ENGINE IGNITION EXCITER FAILED. INVESTIGATION ALSO FOUND THAT AN ATTACHMENT POINT HAD FAILED. (X)SDR 20001025SH004Gasket · splitGASKET SPLITTING AND FUEL LEAKING FROM NACELLE INTO ENGINE EXHAUST PATH. (X)SDR 2002FA0000178Strap · defectiveDEFECT IN SK SPAR STRAP SYSTEM.SDR 20000601SH020Gusset · crackedRIGHT LOWER OUTBOARD WING HAD CRACK IN DOUBLER AT FORWARD ATTACH POINT AND GUSSET CRACKED AT APPROX BS 160.00 AND WS 110.11. TWO CRACKS IN WING SKIN RIGHT WING 4 INCHES BEHIND FORWARD SPAR JUST AFT OF FORWARD WING BOLT ON TOP SIDE OF WING. TWO CRACKS IN WINGSDR 20000504SH009Torque Link · mismarkedREF: RAYTHEON SB 32-3116. SOME TORQUE KNEES IDENTIFIED AS MLG P/N''S 50-810032-12 AND 50-810295-25 WERE MACHINED TO BE NOSE GEAR COMPONENTS. IF INSTALLED, THESE TORQUE KNEES WILL ALLOW MAIN GEAR TO OVER EXTEND AND DAMAGE FORWARD PORTION OF WHEELWELL UPON RSDR 20000615SH010Tube · brokenWHILE APPLYING POWER FOR TAKEOFF, THE LEFT ENGINE WOULD NOT RESPOND. INSPECTED AND FOUND THE PY LINE CRACKED AT THE FUEL CONTROL UNIT. (X)SDR 2000ZZZX370Fcu · defectiveSERIAL NUMBERS ARE THE UNITS THAT REPLACED THE DEFECTIVE UNITS. S/N 72779. SHAFT IN ENGINE FUEL CONTROL SHEARED CAUSING ENGINE TO SHUT DOWN.SDR 2000ZZZX369Pump · defectiveSERIAL NUMBERS ARE THE UNITS THAT REPLACED THE DEFECTIVE UNITS. S/N 7848. SHAFT IN ENGINE FUEL CONTORL SHEARED CAUSING ENGINE TO SHUT DOWN.SDR CA991103020Hinge · cracked(CAN) AT INSPECTION IT WAS NOTICED THAT THE DOOR HINGE WAS CRACKED AT A FEW LOCATIONS ON THE DOOR SIDE OF THE HINGE. THE HINGE WAS REPLACED ON BOTH SIDES C/W NEW HINGE PIN.SDR 99ZZZX3509Skin · crackedON THE LOWER SURFACE OF THE WING AT FORWARD WING BOLT ATTACH POINT, A CRACK IN THE WING SKIN BOTH FORWARD AND AFT OF THE ATTACH FITTING WAS FOUND DURING A ROUTINE INSPECTION. THE CRACK ON THE FORWARD SIDE STARTED AT THE FUEL CELL DRAIN NIPPLE CUT-OUT AND EXTESDR 99ZZZX3064Warning Light · illuminatedRIGHT ENGINE CHIP DETECTOR LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT WAS EN ROUTE TO PICK UP PASSENGERS. AIRCRAFT RETURNED TO HOME BASE. DOM REMOVED CHIP DETECTOR AND FOUND TINY SLIVERS OF METAL ACROSS CONTACTS. SPECIAL OIL SAMPLE TAKEN AND SENT TO LAB. OSDR 99ZZZX1964Harness · chafedAIRCRAFT WAS ON A LOCAL TRAINING FLIGHT. IMMEDIATELY AFTER TAKEOFF, PILOT TRAINEE REPORTED NO RESPONSE TO ELEVATOR INPUTS. ACFT APPROX 200 FEET AGL AND AIRSPEED WAS 120 KNOTS. INSTRUCTOR PILOT ASSUMED COMMAND AND MADE AN IMMEDIATE LANDING USING ELEVATOR TRISDR AU990748Blade · failed(AUS) LEFT ENGINE FAILED. INVESTIGATION FOUND FAILURE OF ONE COMPRESSOR TURBINE BLADE DUE TO FATIGUE. DAMAGE CAUSED TO THE OTHER BLADES.SDR AU990419Turbine · damaged(AUS) LEFT ENGINE FAILED WITH AN EXPLOSIVE SOUND AND SPARKS FROM THE EXHAUST. INITIAL INVESTIGATION REVEALED EXTENSIVE DAMAGE TO THE POWER SECTION.SDR CA990412003Fcu · failed(CAN) DURING CRUISE, THE NR 2 ENGINE BEGAN TO SURGE AND RUN ROUGH, THE T5 AND TORQUE BEGAN TO FLUCTUATE AND THE PILOT HAD NO CONTROL OF POWER. THE ENGINE WAS SHUT DOWN AND AN UNEVENTFUL LANDING WAS CARRIED OUT. POST-FLIGHT INSPECTION FOUND THE FUEL CONTROL USDR 20000426SH001Clevis Pin · failedDURING FLIGHT INTO AQW, PASSENGERS AND CREW HEARD A LOUG BANG AND THE PRESSURIZATION BEGAN TO DESCEND QUICKLY. LANDING WAS MADE WITHOUT INCIDENT. INSPECTION REVEALED THE CLEVIS PIN THAT IS THE PIVOT FOR THE UPPER CABIN DOOR LATCH HOOK HAD BROKEN. RAYTHEON HSDR CA990308003Guard · chafed(CAN) RUDDER AUTOPILOT SERVO CAPSTAN CABLE GUARD ASSEMBLIES FOUND DAMAGED. ONE CABLE GUARD CUT IN HALF AND THE OTHER CUT THROUGH MORE THAN 50 PERCENT BY THE RUDDER TRIM AUTOPILOT SERVO CABLE. INVESTIGATION REVEALED THAT THE INCORRECT CAPSTAN ASSEMBLY HAD BEESDR 99ZZZX1463Knee · failedAIRCRAFT LANDED AT TTN. ON TOUCH-DOWN, AIRCRAFT PULLED TO RIGHT AND TRAVELED OFF RUNWAY WITHOUT FURTHER INCIDENT. ON INVESTIGATION, FOUND RIGHT LANDING GEAR UPPER TORQUE KNEE FAILED WHICH ALLOWED LOWER LANDING GEAR (PISTON ASSY) TO TURN SIDEWAYS.SDR 99ZZZX1171Window · brokenNR 1 LEFT PASSENGER WINDOW BROKE AND BLEW OUT. POLORIZER STAYED IN PLACE.SDR 99ZZZX944Wire · chafedNR 1 ENGINE LOST OIL PRESSURE INDICATION. WIRE ON TRANSMITTER AT CANON PLUG FOUND CHAFED UNDER ADEL CLAMP.SDR AU981661Wing Tip · lightning strike(AUS) DURING CRUISE, LIGHTNING DISCHARGED ONTO THE LEFT HAND WING TIP. INVESTIGATION FOUND DAMAGE WAS LIMITED TO THE OUTBOARD WING TIP PLASTIC FAIRING AND MINOR TRAILING EDGE DAMAGE AT THE EXIT POINT LOCATED ON THE LEFT HAND WING TRAILING EDGE APPROXIMATELY 3SDR 98ZZZX4688Roller · damagedDURING GEAR RETRACTION IT WAS NOTED THE RT MLG DOORS DID NOT CLOSE. UPON FURTHER INVESTIGATION, FOUND THE GEAR DOOR ROLLER ASSEMBLY HAD BEEN BROKEN OFF CAUSING THE GEAR DOORS TO STAY OPEN. REPLACED PART AND HAD NO FURTHER PROBLEMS. SUBMITTER SUGGESTED CLOSESDR AU981551Control Cable · broken(AUS) ELEVATOR TRIM CABLE BROKEN AT TRIM DRUM.SDR CA981123005Wire · broken(CAN) ON SELECTING LANDING GEAR DOWN, THE LEFT MAIN GEAR FAILED TO INDICATE DOWN AND LOCKED. GEAR CYCLED SEVERAL TIMES WITH NO CHANGE. A TOWER FLY-BY SHOWED GEAR APPEARED TO BE DOWN AND LOCKED. SAFE LANDING CARRIED OUT WITH NR 1 ENGINE SHUTDOWN. MAINTENANCSDR AU981520Servo · sticking(AUS) AUTOPILOT SERVO STICKING. UNCOMMANDED ELEVATOR PITCH DOWN RESULTED IN SEVERE DAMAGE TO THE NLG WHEN THE AIRCRAFT IMPACTED THE GROUND DURING LANDING.SDR 98ZZZX4576B-Nut · crackedFUEL TRANSFER TUBE B-NUTS FOUND CRACKED.SDR 98ZZZX4186Bracket · crackedWHILE PERFORMING PRE-BUY INSPECTION, ELEVATOR PULLEY BRACKET WAS INSPECTED PER MSB 2150, R1. BRACKET FOUND CRACKED. SB 2150-R1 STATES IF ANY CRACKS ARE FOUND KIT 90-4098-1S, WHICH IS AN IMPROVED HEAVIER BRACKET, IS TO BE INSTALLED.SDR 98ZZZX3804Finger · looseDURING ROUTINE INSPECTION, FOUND SHOULDER SEPARATED FROM SCREEN. THIS CONDITION COULD LEAD TO POSSIBLE INJESTION OF SCREEN.SDR 99ZZZX64Exciter · misinstalledUNIT RECEIVED AS OVERHAULED UNIT AND WAS INSTALLED ON RT ENGINE OF C-90 KING AIR. UNIT FAILED AFTER ONE START. FAULTY SOLDERING ON EXTERIOR OF CASE. TAGS ON THE EXTERIOR OF THE UNIT DRAW A QUESTION AS TO ITS ORIGIN AND SERVICEABILITY.SDR 99ZZZX1369Ignition Exciter · failedUNIT RECEIVED AS OVERHAULED UNIT AND INSTALLED ON RT ENGINE OF C-90 KINGAIR. UNIT FAILED AFTER ONE START. FROM APPEARANCE OF EXTERIOR OF EXCITER, IT MAKES YOU WONDER WHAT THE INTERIOR LOOKS LIKE. FAULTY, SLOPPY OF SOLDERING ON EXTEIROR OF CASE. TAGS ON THESDR 98ZZZX3056Blower Motor · failedDURING CRUISE FLIGHT, SMOKE FILLED THE COCKPIT AND CABIN. A SAFE LANDING WAS MADE. THE PILOT REPORTED THE ORIGIN OF THE SMOKE TO BE AT HIS FEET. THE FLOOR WAS PULLED UP AND IT WAS CLEAR THE BLOWER MOTOR HAD SEVERELY OVERHEATED. THE BLOWER ASSY WAS REMOVED SDR AU980979Switch · lack of lube(AUS) RIGHT MAIN LANDING GEAR DOWNLOCK MICROSWITCH STIFF DUE TO LACK OF LUBRICATION.SDR 98ZZZX1870Connector · failedWIRES BROKE INSIDE CABLE AT FACE OF HARD EPOXY POTTING COMPOUND. CONNECTOR HAD NO STRAIN RELIEF. BOTH SYSTEMS HAD SIMILAR FAILURE. CABLES WERE REPAIRED BY CUTTING OFF CONNECTORS AND POTTED AREA OF CABLES, RETERMINATING SHIELDS, AND INSTALLING NEW CONNECTORSSDR 98ZZZX1369Skin · crackedDURING PHASE 1 AND 2 INSPECTIONS FOUND 2 CRACKS APPROXIMATELY 1 INCH LONG EMANATING FROM LT HORIZONTAL STABILIZER INBOARD LEADING EDGE RIVETS.SDR 98ZZZX906Wire · splitALL FOUR CABLE LEADS COMING FROM STARTER/GENERATOR ON LEFT SIDE, P/N'S P10C4, P10A4, K2D4, K2F4, SHIELDING IS SPLITTING ALL ALONG THE LENGTH OF WIRE EXPOSING BARE CABLE WHICH COULD RESULT IN ARCING. REF: CHAPTER 24 DC GENERATION OF WIRING MANUAL.SDR 98ZZZX183Retract Chain · failedNLG AFT RETRACT CHAIN MASTER LINK FAILED. ALL PIECES OF MASTER LINK FOUND AND IN SERVICEABLE CONDITION. RECOMMEND INSTALLATION OF NEW STYLE PRESS FIT LINK, PN 131378-25-2-CL, TO PREVENT RECURRENCE.SDR CA970612005Hub · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. CUSTOMER OPTED FOR EARLY AD 96-18-14 COMPLIANCE. PROPELLER HUB WAS FOUND CORRODED, HUB REPLACED WITH HUB S/N BUA 19988.SDR CA970609025Hub · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. HUB FOUND CORRODED. NEW HUB S/N BUA 19986 INSTALLED AND EARLY COMPLIANCE WITH FAA AD 96-18-14 CARRIED OUT.SDR AU970736Circuit Breaker · intermittent(AUS) LANDING GEAR MOTOR 50AMP CIRCUIT BREAKER INTERMITTENTSDR 97ZZZX4284Outflow Valve · failedAFTER TAKEOFF, CABIN PRESSURIZATION STARTED TO PRESSURIZE TO 6,000 FEET CLIMB UNTIL THE SAFETY VALVE OPENED, THE CABIN WENT TO A 6,000 FOOT DESCENT. THE CABIN CONTINUED TO OSCILLATE IN THIS MANNER UNTIL PILOT DUMPED THE CABIN AND CONTINUED UNPRESSURIZED. ON TSDR CA970430003Wheel Half · cracked(CAN) HALF OF THE WHEEL ASSY OF THE LEFT HAND MAIN LANDING GEAR WHEEL BROKE DURING TAKEOFF. A TUBE IN THE TUBELESS TIRE PREVENTED AIR FROM ESCAPING THROUGH THE CRACK THAT HAD DEVELOPED. AIRCRAFT WAS IMPORTED AND THE SUBMITTER SPECULATES THE PREVIOUS OWNER C
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