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 = '212' 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 = '212' 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 AU001329Nozzle · burned(AUS) NR 1 ENGINE CONTINUOUS HIGH TEMPERATURE. STRIP INSPECTION FOUNDTHE FOLLOWING DEFECTS: HOLE BURNT IN INLET GUIDE VANE. FIRST STAGE NOZZLE BURNED AND PIECE MISSING . T5 HARNESS THERMOCOUPLE END BURNED OFF. POWER TURBINE VANE RING CRACKEDBETWEEN ADJACENT BLSDR AU001268Inlet Guide Vane · damaged(AUS) NR 1 ENGINE EXPERIENCED CONTINUOUS HIGH TEMPERATURES. INVESTIGATION FOUND THE FOLLOWING DEFECTS: HOLE BURNED IN INLET GUIDE VANE. FIRST STAGE NOZZLE BURNED WITH A PIECE MISSING. T5 HARNESS THERMOCOUPLE END BURNED OFF. POWER TURBINE VANE RING CRACKED BETWSDR CA001205024Bearing · seized(CAN) TOP BEARING SEIZED ON CARGO HOOK CAUSING SUPPORT TO CRACK AT BOLT HOLES, SEVERE STRESS ON MOUNTING BOLTS AND BUSHING CAUSING ABNORMAL WEAR OF MOUNTING BUSHING. (X)SDR AU001110Line · fractured(AUS) ENGINE P3 LINE FRACTURED AT THE FLANGE WHERE THE LINE IS SWAGED TO THE FILTER BOWL. (X)SDR AU001072Filter · contaminated(AUS) NR 2 ENGINE P3 FILTER PARTIALLY BLOCKED. AIRCRAFT IS OPERATING IN EAST TIMOR. (X)SDR CA001130003Transmission · making metal(CAN) APPROXIMATELY 1.3 HR INTO FLT MAIN TRANSMISSION WARNING LIGHT ILLUMINATED. A/C WAS APPROXIMATELY. 3 MINS AWAY FROM AN ON ROUTE AIRPORT; THE PILOT ELECTED TO LAND AT AIRPORT & HAVE MAINTENANCE ENGINEER INVESTIGATE PROBLEM. AME PULLED MAGNETIC CHIP DETECTOSDR 20001019SH032Bearing · failedDURING MAINTENANCE CHECKS, WHITE M/R BLADE TRUNNION BEARING GREASE WAS FOUND TO BE DARKER THAN RED BLADE. GRAY/RED IN COLOR. REMOVED AND REPLACED M/R TRUNNION BEARINGS WITH NEW BEARINGS. WHILE BLADE BEARING SHOWS SIGNS OF ADVANCED BRINNELLING. SUBMITTER STSDR CA001103021Solenoid Valve · leaking(CAN) WHILE THE FUEL SUMPS WERE BEING DRAINED IN PREPARATION FOR FLIGHT, IT WAS NOTED THAT THE LEFT FUEL SUMP WAS LEAKING. THE SUMP SOLENOID WAS RECYCLED AND FUEL LEAK STOPPED. WITH SIMPLEX SPRAY SYS INST FUEL DRAIN SOLENOID IS INACCESSIBLE. TH E SOLENOID DRSDR CA000925029Mount · cracked(CAN) IN THE PROCESS OF CHANGING WEAK TRANSMISSION LORD MOUNTS, FOUND A CRACKED LIFT LINK (FITTING) MOUNT. THE RIGHT FORWARD EAR WAS CRACKED. THE FITTING IS ON THE TRANSMISSION. THE DAMPERS WERE WEAK ALSO. (X)SDR CA000901018Fitting · cracked(CAN) WEB OF FITTING COMPLETELY CRACK THROUGH AND 1/8 CRACK PROPAGATING OUTBOARD. BOTH CRACKS START AT LOWER INBOARD HI-LOK HOLE.SDR AU000904Panel · cracked(AUS) MAIN BEAM PANEL CRACKED AT STA 166. CRACK LENGTH 100 MM (4 INCHES). FOUND DURING INSPECTION AND REPLACEMENT OF CRACKED MAIN BEAM CAP IAW BHT TB 212-88-106. (X)SDR CA000824009Main Rotor · cracked(CAN) WHILE WASHING THE M/R BLADES THE WASHER ON THE UNDERSIDE OF M/R BLADE A-1567 THAT THE SOAP BUBBLED AS PUSHED UP ON THE BLADE. FURTHER INVESTIGATION FOUND A CRACK RUNNING CHORDWISE FROM THE AFT EDGE OF THE SPAR TO ABOUT 4 INCHES FORWARD OF THE TRAILING ESDR 20000804SH004Pump · brokenNR 2 ENGINE SHUT DOWN IN-FLIGHT. PILOT MADE NORMAL LANDING. INVESTIGATED PROBLEM. PULL FUEL PUMP OFF. FOUND INTERNAL SPLINES OF PUMP GROUND OFF. SPLINES MISSING DUE TO ABNORMAL WEAR ON SPLINES. INSTALLED NEW PUMP. GROUND RAN ENGINE. ENGINE FUNCTIONED PSDR CA000731025Pivot · wrong part(CAN) PARTS NOT TO MANUFACTURERS SPECIFICATIONS I.E. BOGUS.ADDITION TO MULTIPLE REPORT PREVIOUSLY RE THE SAME PROBLEM. MELT DOWN.SDR CA000801005Oil Cooler · leaking(CAN) WHILE IN CRUISE FLIGHT THE C BOX OIL PRESSURE LIGHT ILLUMINATED. THE PILOT THEN LOOKED AT THE PRESSURE GAUGE AND SAW IT FLUCTUATING. THE HELICOPTER WAS LANDED WITHOUT INCIDENT. UPON GROUND RUN THE AME NOTICED OIL STREAMING FROM THE OIL COOLER.SDR CA000801007Line · leaking(CAN) UPON LANDING THE ENGINEER NOTICED OIL ON THE BELLY OF THE AIRCRAFT. UPON INVESTIGATION HE FOUND A PIN HOLE IN THE OIL LINE.SDR 20001019SH031Bearing · failedDURING A POST-FLIGHT INSPECTION, DARK BLACK GREASE WAS FOUND ON THE M/R TRUNNION. REMOVED AND DISASSEMBLED M/R TRUNNION. ONE TRUNNION BEARING HAD TOTALLY FAILED. INNER AND OUTER RACES WERE BROKEN. (X)SDR CA001205004Blade · delaminated(CAN) TAIL ROTOR BLADE DELAMINATION FOUND BETWEEN THE SKIN AND THE TIP BLOCK THAT WAS BEYOND LIMITS. TAILROTOR ASSEMBLY REPLACED.SDR GJQR0000272Indicator · brokenINDICATOR BUTTON WAS EXTREMELY DIFFICULT TO RESET AND WAS BROKE OFF WHEN ATTEMPTING TO PUSH IN. (X)SDR CA000427004Beam · cracked(CAN) DURING PRE-FLIGHT, THE LEFT HAND BEAM CAP ON THE TAILBOOM PYLON WAS FOUND CRACKED (.080 INCH). NOTE: THIS CRACK WAS FOUND IN THE SAME PLACE AS DESCRIBED IN FAA AD 99-18-02 APPLICABLE TO BELL 205 SERIES.SDR CA000719003Fastener · corroded(CAN) EXCESSIVE DISSIMILAR METAL CORROSION CAUSED BY SHEET METAL CLECOS BEING LEFT IN SINCE MANUFACTURE. THEY WERE LOCATED IN THE LEFT-HAND DOOR POST ON BULKHEAD STATION 63.27. NOTE: THIS AREA IS NOT ACCESSIBLE UNLESS THE SKIN IS REMOVED. IT WAS FOUND DURINSDR CA000427003Tube · loose(CAN) DURING INSPECTION, THE RIGHT CYCLIC SERVO INPUT LEVER WAS FOUND IN AN AFT OF CENTER ORIENTATION. SUBSEQUENT OBSERVATION REVEALED BOTH CYCLIC BOOST TUBES HAD LOOSE CLEVIS ASSEMBLIES AT LOWER END. THIS CAUSED THE SERVO TO ROTATE IN ANY POSITION AND INTERSDR CA000404002Pump · failed(CAN) FUEL PUMP SHAFT WAS ROUGH TO TURN. SENT FOR EVALUATION.SDR LS1R066573Indicator · stuckGAUGE IS STICKING.SDR 20000502SH015Air Filter · debondedDURING ROUTINE MAINTENANCE, BOTH END CAPS ON BOTH FILTERS DEBONDED. (X)SDR CA000316001Nut · fractured(CAN) AFTER M/R BLADE STRIKE, A CONDITIONAL INSPECTION WAS CARRIED OUT. BOTH ACORN NUTS WERE CONFIRMED FRACTURED BY NDT. ACORN NUTS SENT OUT FOR ANALYSIS.SDR LS1R066571Strap · tornSTRAP IS TORN. (RUBBER COMING APART).SDR LS1R066570Strap · tornSTRAP IS TORN. (RUBBER COMING APART).SDR LS1R066569Damper · wornDAMPER IS WORN EXCESSIVELY.SDR LS1R066568Damper · wornDAMPER IS WORN EXCESSIVELY.SDR LS1R066560Annunciator · inoperativeANNUNCIATOR IS INOPERATIVE.SDR CA001013003Elt · failed(CAN) ELT WAS TESTED AS PER THE 100 HOUR INSPECTION SCHEDULED AND UNIT WOULD NOT ACTIVATE AFTER BEING SHAKEN OR WHEN THE MASTER SWITCH WAS TURNED TO THE ON POSITION. UNIT REPLACED.SDR LS1R066439Bolt · wornBOLT ASSY WORN EXCESSIVELY.SDR LS1R066438Pin · wornBLADE PIN WORN EXCESSIVELY.SDR LS1R066435Bolt · wornBOLT WORN EXCESSIVELY.SDR LS1R066434Bolt · wornBOLT WORN EXCESSIVELY.SDR CA000224021Gcu · wrong part(CAN) UNAPPROVED COMPONENTS SUCH AS CAPACITORS, RESISTORS, DIODES.SDR CA000518007Planetary Gear · chipped(CAN) METAL FOUND ON THE PLANETARY CHIP DETECTOR (.040 INCH - .060 INCH). TRANSMISSION WAS REMOVED SHORT OFF AND SENT FOR REPAIR.SDR CA000215026Floorboard · corroded(CAN) FLOOR HONEYCOMB CORRODED IN PANELS DIRECTLY UNDER THE DOWN RING ASSY AND TIE DOWN STUD. CORROSION IS ONLY APPARENT VISUALLY ON BOTTOM SIDE OF PANELS WHEN FILLER ASSY P/N 205-031-257-074 IS REMOVED.SDR CA000215028Bearing Cover · chafed(CAN) DURING INSPECTION, THE SWASHPLATE BEARING COVER (P/N 204-011-428-003) WAS FOUND CHAFED THROUGH APPROX 330 DEGREES OF ITS CIRCUMFERENCE. THE CHAFING WAS CAUSED BY THE SEAL JUST BELOW THE BEARING COVER AS IT WAS RIDING HIGHER IN ONE SPOT WHICH CAUSED IT TOSDR AGQA065683Bearing · scoredINNER RACE IS SCORED.SDR AGQA065682Bearing · damagedBEARING IS DAMAGED.SDR AGQA065681Bearing · damagedBEARING IS DAMAGED.SDR AGQA065680Bearing · scratchedINNER RACE IS SCRATCHED.SDR CA000322002Pivot · damaged(CAN) THE SHAFT PIVOT ASSY CONTAINS PARTS THAT DO NOT CONFORM TO MFG''S SPECS. BUS BAR ASSY AND INSULATORS SHOW SIGNS OF MELTING. THIS ASSY CARRIES MAIN LAMP POWER AND HIGH AMPS. THERE IS A POSSIBILITY OF AN ELECTRICAL SHORT AND SUBSEQUENT SAFETY CONCERNS.SDR CA000530010Fuel Line · delaminated(CAN) WHEN REPLACING FLEXIBLE LINES INSIDE THE FUEL CELL, IT WAS NOTED THAT THE BOTTOM OF THE FUEL CELL WAS SPONGY. IT WAS THEN DESCOVERED THAT LAYERS OF RUBBER WERE BREAKING DOWN AND SEPARATING.SDR AGQA065568Strobe · intermittentSTROBE ASSY IS INTERMITTENT.SDR AGQA065567Control Unit · failedCONTROL UNIT WOULD NOT MATCH TORQUES TORQUE SPLITSDR AGQA065566Warining Box · failedNR 2 ENGINE OUT LIGHT INTERMITTENTLY.SDR AGQA065564Warining Box · failedWARNING BOX IS INOPERATIVE. NR 2 ENGINE LIGHT STAYS ON.
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