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 engine_model_key = 'CF680A' 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 engine_model_key = 'CF680A' 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 AU000072Bearing · seized(AUS) RT OUTBOARD AILERON POWER CONTROL ACTUATOR INPUT LINK BEARING SEIZED.SDR AU000193Spar · corroded(AUS) RT WING CENTRE SECTION REAR SPAR WEB CORRODED IN THE AREA LOCATED BEHIND THE REAR SPAR BULKHEAD FITTING PNO 145T2521. AREA OF CORROSION APPROXIMATELY 215.9MM (8.5IN) BY 38.1MM (2.5IN) BY2.54MM (0.100IN) DEEP.SDR AU000079Skin · corroded(AUS) RT WING LOWER SKIN PANEL LOCATED AT WS391 CORRODED. AREA OF CORROSION 76.2MM BY 38.1MM (3IN BY 1.5IN). DEPTH OF CORROSION3.556MM (0.140IN).SDR AALA20000148Nozzle Feeder · damagedORD - FLT 180 - DURING FLIGHT, AIRCRAFT YAWED AND CREW NOTED N1 EGT AND N2 WINDING DOWN. SHUTDOWN ENGINE. ATTEMPTED INFLIGHT START NO SUCCESS. DIVERTED AND LANDED ORD WITHOUT INCIDENT. REPLACED DAMAGED FUEL NOZZLE FEEDER MANIFOLDS AT POSITIONS 10:00 O'CLOCSDR AU000066Wire Rope · frayed(AUS) RT AILERON CONTROL CABLE A4B-3 FOUND FRAYED AT WING STATION 531 FAIR LEAD. ALL STRANDS EXCEPT THE HEART STRAND WERE BROKEN. THE ADJACENT WIRE ROPE A4A-3 HAD BROKEN WIRES AND THE ENTIRE LENGTH OF BOTH WIRE ROPE RUNS WAS WORN AT THE FAIR LEAD LOCATIONS.SDR AU000076Wedge · contaminated(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES CORRODED INTERNALLY & CONTAMINATED WITH MOISTURE.SDR AU000053Valve · fractured(AUS) LEFT HYDRAULIC SYSTEM HP FILTER MODULE PRESSURE RELIEF VALVE BODY FAILED AT O- RING GROOVE.SDR AU991091Duct · burst(AUS) RIGHT ENGINE HP AIR DUCT ELBOW RUPTURED.SDR AU991092Bracket · broken(AUS) RIGHT ENGINE BLEED AIR DUCT SUPPORT BRACKET BROKEN. SUSPECT BROKEN BRACKET CAUSED BLEED AIR DUCT TO FAIL. SEE MDR AU991091.SDR AU990844Sensor · out of adjust(AUS) RIGHT ENGINE THRUST REVERSER LOCK PROXIMITY SENSOR OUT OF ADJUSTMENT.SDR AU990681Sensor · faulty(AUS) LEFT ENGINE FAILED TO ACCELERATE ABOVE FLIGHT IDLE. NR 1 COMPRESSOR INLET TEMPERATURE SENSOR CHANGED.SDR AU990702Fcu · faulty(AUS) NR 2 ENGINE MAIN ENGINE CONTROL SUSPECT FAULTY.SDR DL76S991436Gcu · failedDURING CLIMBOUT AT APPROX FL 250 PILOTS NOTICED ODOR IN COCKPIT. THE ODOR BECAME STRONGER, SEVERAL MINUTES LATER THE RT GEN OFF LIGHT ILLUMINATED WITH ASSOCIATED EICAS LIGHTS. THE INTENSITY OF ODOR REQUIRED USE OF COCKPIT OXYGEN MASKS. A/C DIVERTED TO JAX. SDR AU991038Rod · out of adjust(AUS) OUTBOARD SLAT PDU INPUT ROD OUT OF ADJUSTMENT.SDR AU990494Cover · cracked(AUS) RT LATERAL CENTRAL CONTROL ACTUATOR FILTER COVER `O' RING SEAL DISPLACED. LOSS OF CENTER HYDRAULIC SYSTEM FLUID. INVESTIGATION FOUND THAT THE FILTER COVER CONTAINED A CIRCUMFERENTIAL CRACK INTHE THREADED PORTION EXPOSING THE SEAL TO HYDRAULIC PRESSURE SDR AU990471Valve · failed(AUS) RAM AIR TURBINE CHECKOUT MODULE CHECK VALVE FAILED. LOSS OF CENTER HYDRAULIC SYSTEM FLUID.SDR DL767990986Engine · failedIN DESCENT RT ENGINE FAILED, OIL PRESS WENT TO ZERO. REPLACED ENGINE.SDR AU990453Structure · damaged(AUS) AIRCRAFT SUFFERED HAIL DAMAGE TO THE FOLLOWING AREAS: 1. LT INBOARD AND OUTBOARD AILERONS. 2. LT AND RT LEADING EDGE SLAT WEDGES. 3. LT AND RT INBOARD AND OUTBOARD FLAP TRAILING EDGES. 4. NR 10 SPOILER. 5. VERTICAL STABILIZER RT SIDE LEASDR AU990485Structure · damaged(AUS) AIRCRAFT SUFFERED HAIL DAMAGE TO THE FOLLOWING AREAS: 1. LT OUTBOARD AILERON, RT INBOARD AND OUTBOARD AILERONS. 2. LT AND RT ELEVATORS. 3. NR 1, NR 2, NR 3, NR 4, NR 5, NR 7, NR 8, NR 9, NR 10, NR 11, NR 12 LEADING EDGE SLATS. 4. NR 2, NR 3, NR 4SDR AU990293Pin · cracked(AUS) RIGHT INBOARD ENGINE PYLON MID-SPAR FUSE PIN CRACKED. CRACK LENGTH 11 MM (0.433 INCH). FOUND DURING EDDY CURRENT INSPECTION.SDR AU990407Wedge · disbonded(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES DISBONDED AND CORRODED ON THE FOLLOWING SLATS: SLAT NR 1. DISBOND 150 MM BY 40 MM (5.905 INCHES BY 1.574 INCH) AT INBOARD END, 30 MM (1.181 INCH) FORWARD OF TRAILING EDGE. DISBOND 180 MM BY 12 MM (7.086 INCHES BSDR AU990430Wedge · disbonded(AUS) LEADING EDGE SLAT T/E WEDGES DISBONDED IN FOLLOWING AREAS: 1. NR 3 SLAT UPPER SURFACE DISBONDED AT OUTBOARD END 45 MM (1.771 INCH) FROM T/E . AREA OF DISBOND 50 MM BY 45 MM (1.968 INCH BY 1.771 INCH). 2. NR 4 SLAT UPPER SURFACE DISBONDED 1440 MM (SDR AU990064Engine · making metal(AUS) LEFT ENGINE CHIP DETECTOR CONTAMINATED WITH M50 BEARING MATERIAL.SDR AU990063Heat Exchanger · cracked(AUS) LEFT ENGINE FUEL/OIL HEAT EXCHANGER HEADER RADIUS CONTAINED TWO CRACKS. FOUND DURING ULTRASONIC INSPECTION IAW GE6-79-00-2C AND GE SERVICE BULLETIN SB79-023. PART TC: 26,858.SDR AU990146Gear · corroded(AUS) NR 3 OUTBOARD AND NR 4 INBOARD LEADING EDGE SLAT ROTARY ACTUATORS CONTAINED INTERNAL CORROSION ON THE RING GEAR BEARING SURFACES AND THE PLANET GEAR P/N 256T2152. FOUND DURING VISUAL INSPECTION IAW ER B76-27-80-27 (AD/B767/095). PART TC: 51,949.SDR AU990037Wedge · disbonded(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES FOUND WITH DISBONDED AREAS ON A TOTAL OF SEVEN SLATS. FOUND DURING VISUAL AND ULTRASONIC INSPECTIONS IAW BOEING ALERT SB 767-57A0039.SDR AU990036Web · cracked(AUS) LEFT ENGINE PYLON TOP WEB CRACKED AT THE REAR OUTBOARD CORNER OF ONE WEB CUT-OUT. CRACK LENGTH 9.53 MM (0.375 INCH). FOUND DURING EDDY CURRENT INSPECTION.SDR AU981478Apu · failed(AUS) APU FAILED. REAR BEARING HOUSING AND OIL SCAVENGE PUMP FOUND ON THE RAMP. PART TC: 27,149.SDR AU981703Tube · leaking(AUS) ENGINE REMOVED DUE TO HIGH OIL CONSUMPTION. THE COMPRESSOR REAR FRAME WAS DETACHED AND INVESTIGATION FOUND THE SUMP OIL SUPPLY TUBE HAD BEEN WORN THROUGH BY AN ATTACHMENT 'P' CLIP.SDR AU981310Compressor · damaged(AUS) LEFT ENGINE COMPRESSOR STAGE 10 TO STAGE 12 DAMAGED.SDR AU981476Line · damaged(AUS) NOSE LANDING GEAR `DOWN' TITANIUM HYDRAULIC PIPE LOCATED AT FS 625 BETWEEN THE FORWARD CARGO HOLD LEFT SIDEWALL AND THE FUSELAGE SKIN DENTED AND CRACKED. LEAKING HYDRAULIC FLUID MIST IN CABIN. PIPE HAD BEEN DAMAGED DUE TO PREVIOUS MAINTENANCE. PART SDR AU981284Engine · fod(AUS) LEFT ENGINE VIBRATION. N2 VIBRATION INDICATED 5.1 UNITS AT 40 PERCENT N1. INVESTIGATION FOUND THAT THE VIBRATION WAS DUE TO BIRD STRIKE DAMAGE.SDR AU981261Nozzle · cracked(AUS) ENGINE HIGH PRESSURE TURBINE STAGE TWO NOZZLE SEGMENTS (2OFF) SEVERELY CRACKED.SDR AU981453Nozzle · cracked(AUS) HIGH PRESSURE TURBINE STAGE TWO NOZZLE SEGMENTS (3 OFF) CRACKED.SDR AU981222Slat · delaminated(AUS) NR 1 AND NR 3 LEADING EDGE SLAT TRAILING EDGES DELAMINATING.SDR AU981170Seat Belt · faulty(AUS) PASSENGER SEAT BELTS LOCATED AT 19D, 23E, 30C, 32E, 33E AND 34C AS WELL AS THE FIRST OFFICER'S SEAT BELT HAD MISSING ID LABELS. FOUND DURING INSPECTION IAW ER Z1-25-00-10J (AD/RES/29).SDR AU981152Slat · delaminated(AUS) NR 2 LEADING EDGE SLAT TRAILING EDGE WEDGE DELAMINATED IN FOUR AREAS. FOUND DURING INSPECTION IAW AD/B767/73.SDR AU981049Actuator · failed(AUS) LEFT ELEVATOR POWER CONTROL ACTUATOR LEAKING FROM CHECK VALVE END CAP. LOSS OF RT HYDRAULIC SYSTEM FLUID. INVESTIGATION FOUND THE CHECK VALVE INNER AND BACKUP `O' RING SEALS MISSING FROM THREE CHECK VALVE END CAPS. PERSONNEL/MAINTENANCE ERROR. PART TC:SDR AU981210Fitting · cracked(AUS) LEFT WING DEFLECTION CONTROL SUPPORT FITTING LOWER ATTACHMENT LUG FRACTURED THROUGH THE BEARING HOUSING. FITTING IS LOCATED AT WS 906.20. PART TC: 41,421.SDR AU981208Fitting · corroded(AUS) RIGHT PYLON CONTAINED EXFOLIATION CORROSION ON THE UPPER SURFACES OF THE UPPER WEB OF THE TORQUE BOX ADJACENT TO THE UPPER LINK ATTACHMENT BEAM EITHER SIDE OF AND RUNNING UNDER THE FORWARD UPPER STRUT FITTING. CORROSION HAD PENETRATED THROUGH THE WEB WISDR AU981209Fitting · corroded(AUS) LEFT PYLON CONTAINED EXFOLIATION CORROSION ON THE UPPER SURFACES OF THE UPPER WEB OF THE TORQUE BOX ADJACENT TO THE UPPER LINK ATTACHMENT BEAM OUTBOARD OF AND RUNNING UNDER THE STRUT FITTING. CORROSION HAD PENETRATED TO A DEPTH OF 1.778 MM (0.070 INCH) SDR CA980519014Engine · leaking(CAN) DURING FLIGHT ECAM INDICATION SHOWED LOW OIL QUANTITY ON NR 1 ENGINE. THRUST REVERSERS REDUCED AND AIRCRAFT DIVERTED. SEVERE OIL LEAK FOUND ON AFT CENTER SECTION OF THE ENGINE. ENGINE REPLACED AND SENT FOR INVESTIGATION. INITIAL TEST COULD NOT DUPLICSDR AU980787Collar · cracked(AUS) LEFT INBOARD FLAP INBOARD TORQUE TUBE COLLAR CRACKED AND TORQUE TUBE HEAVILY CORRODED. RIGHT SIDE FLAP COLLARS AND TORQUE TUBE ALSO CORRODED. PART TOTAL CYCLES: 39,633.SDR AU980821Pin · cracked(AUS) LT ENGINE MID SPAR INBOARD FUSE PIN INNER BORE CONTAINED TWO LONGITUDINAL CRACKS. TOTAL CRACK LENGTH 8.89 MM (0.35 INCHES). FOUND DURING EDDY CURRENT INSPECTION IAW ER B76-54-40-4I.SDR AU980612Nozzle · cracked(AUS) NR 1 ENGINE FUEL NOZZLE ELBOW CRACKED AND LEAKING FUEL. THE NOZZLE WAS LOCATED AT APPROXIMATELY THE 1 O'CLOCK POSITION. THE ELBOW WAS IDENTIFIED AS AN OLD TYPE CAST ELBOW WHICH HAD BEEN FOUND TO BE PRONE TO POROSITY.SDR AU980063Skin · damaged(AUS) FUSELAGE SKIN AND STRINGER 31R LOCATED AT STN 485 DAMAGED BY FORK LIFT DURING LOADING OF FORWARD CARGO HOLD.SDR AU971644Actuator · failed(AUS) LH MAIN LANDING GEAR LEFT HAND DRAG BRACE ACTUATOR PISTON ROD SHEARED IN THREADED AREA.SDR 97FDEA00828Compressor · stalledNR 1 ENG CLIMBING THROUGH FL230 NR 1 ENGINE HAD VIBRATION AND COMPRESSOR STALLS. ANY POWER SETTINGS ABOVE IDLE WOULD CAUSE COMPRESSOR STALLS. EGT READING 720 DEG, LANDED WITH PWR AT IDLE.SDR 97FDEA00744Compressor · stalled97-0203, DURING CLIMB-OUT THROUGH FL 180 A LOUD BANG WAS HEARD, AND THE A/C BEGAN TO SHUTTER. THE MAIN DECK SMOKE DETECTION CAME ON, ENGINE WAS SHUTDOWN. EMERGENCY RETURN TO MEMPHIS, OVERWEIGHT LANDING.SDR 97FDEA00660Compressor Line · looseAT APPROX 10,000 FT IN CLIMB, THE LEFT FUEL FLOW STARTED FLUCTUATING. FUEL PRESSURE FLUCTUATED FROM 130 TO 115 PSI, FF FLUCTUATED BETWEEN 6000 AND 14000 AND NR 1 N2 SHOWED A 3 PERCENT SURGE. RESECURED AND SAFTIED COMPRESSOR DISCHARGE LINE. C/W ADJUST TEST O
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