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 = 'CF680A2' 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 = 'CF680A2' 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 IXXA20260809001Stringer · crackedSTRINGER 25L CRACKED AT FUSELAGE BS 676.SDR ABXA20260404148Warning Message · illuminatedDURING TAXI OUT, LEFT ENGINE OIL PRESS ILLUMINATED. A/C RETURNED TO GATE. (BTB) MAINTENANCE DEFERRED IAW ABX-79-33-1-1. A/C RETURNED TO SERVICE.SDR ABXA20251030282Oil System · lowDURING TAXI, RIGHT ENGINE OIL QUANTITY INDICATION INOP. A/C RETURNED TO BLOCKS (BTB). DEFERRED RT ENGINE OIL QTY. INDICATION IAW MEL 79-31-1-1. MBCB 11/02/2025. REPETITIVE INSPECTION REQUIRED BEFORE EACH FLIGHT. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20250929241Bleed Valve · warning messageON T/O ROLL, (R ENG BLEED VAL) CAUTION MSG APPEARED. ABORTED TAKE-OFF AT 68 KNTS AND RETURNED TO GATE (BTB) AND MTX GROUNDED A/C .MTX DEFERRED RH ENGINE BLEED IAW MEL ABX - 36-11-2-1. AND RETURNED A/C TO SERVICE.SDR ABXA2025521098Actuator · malfunctionedSTATUS MSG: "R HYD SYS MAINT" DISPLAYED IN CRUISE. RH HYD PRESSURE AT 1620 AT CRUISE. NOTICED RT ENGINE OIL PRESSURE INDICATED RED, AND MAINT FAULT OF RT IDG, AND R HYD PRIM PUMP CAUTION MESSAGE. AIR TURN BACK TO CVG. (ATB) REMOVED AND REPLACED RH ACMP IAWSDR ABXA20241207244Oil System · lowAFTER BLOCK OUT, ON ENGINE STARTS & ENGINES RUNNING 8 MINUTES (APPROX) LEFT ENGINE QUANTITY 11, RIGHT ENGINE 14, CONTACTED MAINTENANCE & TOLD TO RETURN TO GATE FOR SERVICING. MAINTENANCE GROUNDED THE AIRCRAFT. MAINTENANCE SERVICED LEFT ENGINE OIL IAW 767-AMM 1SDR IXXA20241107001Pad · chafed#1 ENG OTBD T/R UPPER V BAND TAB CHAFFING IN THE FAN CASE AT THE 12:00 POSITION (SDR IXXA20240915064Engine · faultedWHILE CLIMBING THROUGH 31,000 FEET CREW REPORTED A LOUD BANG SUSPECT FROM RH ENGINE FOLLOWED BY A VIBRATION, RISE IN EGT AND LOSS OF ENGINE POWER. FOLLOWING ATI QUICK REFERENCE HANDBOOK COMPLIANCE, THE CREW SECURED RIGHT ENGINE, DECLARED AN EMERGENCY LANDING WSDR IXXA202301276013Engine · faultedRIGHT ENGINE OIL FILTER EICAS MESSAGE DISPLAYED DURING CLIMB OUT FROM DEPARTURE STATION KRIV. PER ATI-QUICK REFERENCE HANDBOOK, CREW ELECTED TO SHUT DOWN RT ENGINE. AIR TURN BACK WITH EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUSDR ABXA2023013016Regulator Valve · defectiveLEFT ENGINE BLEED OFF, 0 DUCT PRESSURE DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED LEFT HPSOV IAW B767 AMM 36-11-07 . OPS AND BITE CHECK GOOD. ACCOMPLISHED BLEED SHIFT CHECK IAW B767 AMM 36-11-00, CHECKS GSDR IXXA20230126013None · noneRIGHT ENGINE OIL FILTER EICAS MESSAGE DISPLAYED DURING CLIMB OUT FROM DEPARTURE STATION KRIV. PER ATI-QUICK REFERENCE HANDBOOK, CREW ELECTED TO SHUT DOWN RIGHT ENGINE. AIR TURN BACK WITH EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRESDR ABXA20221222156Electronic Unit · failedON TAXI OUT N1 ON RT ENG FAILED. INDICATED ZERO. STBY ALSO, ALL OTHER INDICATIONS NORMAL. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REPLACED RT. EEC OPS CHECK GOOD IAW 73-21-07. AIRCRAFT RETURNED TO SERVICESDR ABXA20221117126Controller · failedLT ENG BLEED OFF EICAS MSG DISPLAYED AFTER BOTH ENGINES WERE STARTED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE R&R'D LH HIGH PRESSURE CONTROLLER IAW B767 AMM 36-11-08.0 SYSTEM OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR IXXA20221101143Pump · damagedDESCENT THRU FL190, OIL PSI RT ENGINE DECREASING. ENG NEAR IDLE & SHUTDOWN BEFORE OIL WENT TO 0. SINGLE ENG APPR & LDG PROCEDURES COMPLIED WITH. DECLARED EMERGENCY. OIL PSI AT 6 PSI AT SHUTDOWN & #2 ENG WINDMILLED APROX 7 MIN. LANDING UNEVENTFUL. ACFT RFSDR ABXA2022091191Mec · faultedAFTER ENGINE START, RIGHT ENGINE SURGE AND EGT NOT GOING OVER 500. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED MAIN ENGINE CONTROL (MEC) IAW AMM 73-21-01 . REF. FIM TASK 73-11-FT 812,811 PERFORMED ENGINE RUNS IAW AMM 71SDR 2022F00265None · noneDURING RT ENG START, NO N2; NO START VALVE; NO ROTATION VERIFIED ON GRIND. AIRCRAFT BTB AND GROUNDED BY MAINTENANCE. MAINTENANCE RE-SECURED CANNON PLUG ON START VALVE IAW B767 AMM 20-60-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR IXXA2022050301None · cracked#1 ENGINE I/B CORE COWL UPPER LOUVER EXHAUST ON AFT FLANGE CRACKEDSDR IXXA2022041502Seal Bracket · crackedFAN COWL SEAL RETAINER BRACKET CRACKEDSDR ABXA20210913091Warning Message · false activationRT. ENG FUEL VALVE EICAS MSG APPEARS DURING ENGINE START. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS CHECK OF FUEL CONDITION MOTOR IAW B767 AMM 76-11-00 OPS CHECK NORMAL A/C REMAINS ETOPS 180. AICRAFT RETURNED TO SERVICE.SDR ABXA2021830-28081Controller · faultyLH ENG BLEED VALVE EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE.R&R LH HIGH PRESSURE CONTROLLER IAW AMM 36-11-08 LEAK & BITE CHECK GOOD. AICRAFT RELEASED FOR FLIGHT.SDR ABXA2021430029Bleed Valve · intermittentAFTER ENGINE START EICAS MSG "L ENG BLEED VAL" AND L DISCRETE LIGHT " BLEED" ILLUMINATED.AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED DEFERRAL PROCEDURES IAW MEL FOR LEFT HIGH PRESSURE SHUT OFF REGULATING VALVE. AIRCRAFT RELEASED BSDR ABXA20200803217Actuator · failedRT ENGINE WOULD NOT START, AIRCRAFT BACK TO BLOCK AND AIRCRAFT GROUNDED. TROUBLESHOT, PER B767 FIM 76-11-FT803 VERIFIED 28 VDC ON PIN 8, GROUND ON PIN 7. REMOVED AND REPLACED RIGHT ENGINE FUEL CONDITION MOTOR ACTUATOR, IAW AMM 76-11-04. REMOVED AND REPLACEDSDR ABXA20200803213Warning Message · false activationLT FUEL VALVE EICAS DURING START NO FUEL FLOW. AIRCRAFT BACK TO BLOCK AND GROUNDED. TROUBLESHOT BOTH LT ENGINE SPAR VALVE & ENGINE VALVE NO DEFECTS NOTED. PERFORMED GROUND IDLE ENGINE IDLE RUN, IAW B767 AMM 71-00-00, NO DEFECTS NOTED ENGINE. OPERATES NORMSDR ABXA20200803198Warning Message · false activationRT REV ISOLATION VALVE EICAS MESSAGE AFTER ENGINE START. AIRCRAFT RETURNED TO GATE, AIRCRAFT WAS GROUNDED. MAINTENANCE INVESTIGATED PROBLEM. OPERATIONAL CHECK OF RT REVERSER GOOD, IAW AMM 78-31-00. REV CYCLED 3X TIMES WITH NO MESSAGES. AIRCRAFT RELEASED FSDR ABXA20200803181Warning Light · illuminatedLEFT REVERSER ISOLATION VALVE LIGHT AND EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED. REVERSER WAS DEFERRED AND A/C RELEASED FOR FLIGHT.SDR ABXA202005153061Guide Vane · damaged#1 ENGINE 12 OCLOCK POSITION EXIT GUIDE VANE FAIRING DAMAGED. AIRCRAFT WAS GROUNDED.SDR ABXA201912106177Eec · malfunctionedTHE RIGHT ENGINE DID NOT REACH CLIMB POWER AT HIGH ALTITUDE (FL260) WITH THE ELECTRONIC ENGINE CONTROL ON. THE ENGINE ONLY PRODUCED 105% WITH THE THRUST LEVER FULL FORWARD. THRUST LEVERS WERE SPLIT OVER 1.5 INCHES. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDSDR HALA20181009483Sleeve · tornETOPS SIGNIFICANT SYSTEM - FOUND SEVERAL OGV SLEEVES TORN AT 4 O CLOCK POSITION ON NR 2 ENGINE. REPLACED OGV SLEEVES AT POSITIONS 33, 35, 36, 37, 38, 39, 32 PER TASK CARD E105-C60012-PERM ITEM 1.SDR HALA2018100900483Sleeve · tornETOPS SIGNIFICANT SYSTEM - FOUND SEVERAL OGV SLEEVES TORN AT 4 O CLOCK POSITION ON NR 2 ENGINE. REPLACED OGV SLEEVES AT POSITIONS 33, 35, 36, 37, 38, 39, 32 PER TASK CARD E105-C60012-PERM ITEM 1.SDR DALA201806200001Mount · damagedDURING ACCOMPLISHMENT OF REPAIR 3-2 PER DAL CMM 310T1020-3 ATA 71-21-11, AFTER REMOVAL OF ALL DAMAGE BEARING LUG INDEX 14 WAS FOUND TO MEASURE 0.714 INCH, WHICH IS 0.021 INCH BELOW THE MINIMUM DIMENSION GIVEN IN FIGURE 601, SHEET 2. ADDITIONALLY, ATTACH LUG INSDR HALA2018062000289Mec · malfunctionedRIGHT ENGINE DID NOT REDUCE TO IDLE ON INITIAL DESCENT, FL370 - 11,000, CORRECTED ITSELF FOR FINAL DESCENT N1 53.0 & N2 80.9, FF 1.2. REMOVED & REPLACED THE RT ENGINE MEC IAW AMM 73-21-01-404-032-G00, UP TO STOP 2E(14)(C) COMPLETED UP TO STEPS 2F(9). COMPSDR HALA2018062000290Mec · malfunctionedIDENTICAL RT ENGINE IDLE POWER PROBLEM AS PREVIOUS FLIGHT 23 BUT WITH EEC OFF THRUST LEVER IDLE N1 42.7, N2 79.1, FF 1.3. REMOVED & REPLACED THE RT ENGINE MEC IAW AMM 73-21-01-404-032-G00 UP TO STOP 2E(14)(C). COMPLETED UP TO STEPS 2F(9). COMPLETED 73-21-01-4SDR HALA2018060400274Engine · malfunctionedRIGHT ENGINE PARAMETERS HIGH DURING DECENT AND LANDING, N1 32.0 (L), N2 65.1 (L), N1 48 (R), N2 79.4 (R), > 18000. SUSPECT LEFT ENGINE WENT TO GROUND IDLE ON APPROACH. BITE OF EEC MONITOR SHOWS NO FUALTS. REPLACED RELAYS K433 RT ENG AND K434 L ENG. PERFOSDR HALA2018060400273Sensor · malfunctionedDURING DECENT, AT IDLE POWER. THE RIGHT ENGINE INDICATION WAS 47% N1, THE LEFT ENGINE WAS 33% N1. AUTO THROTTLE OFF, RIGHT ENGINE HAD AT HIGH FLIGHT IDLE. TROUBLESHOT IAW FIM 73-21-00-815-817-G00, REMOVED AND REPLACED THE LEFT ENGINE CIT SENSOR IAW AMM 73-21-SDR HALA2018060400272Engine · malfunctionedDURING DESCENT, THE RIGHT ENGINE STAYED AT 41% N1 AND LEFT AT30 % N1, EQUALIZE AT 10000 FEET. TROUBLESHOT IAW FIM 71.01 F/T 804 EEC BITE WITH NO FAULT. PERFORMED PSEU BITE NO FAULT NOTED. PER TASK 71-00-00-735-001-G00 PERFORMED TEST 3, GROUND TEST FOR IDLE PSDR HALA2017052200239Engine · power lossLEFT THRUST LEVER REQUIRED MANUAL ADJUSTMENT TO OBTAIN TAKEOFF THRUST AT FULL FORWARD STOP. EGT, N1, FUEL FLOWS MATCHED. THREE INCH THRUST LEVER SPLIT FROM FM 1 THR HLD INDICATED AT 100 KTS. LEFT ENGINE ACCELERATION ON TAKEOFF SLOW. LEFT ENGINE RESPONSE ASDR HALA2018051600228Filter · contaminatedRIGHT ENGINE FUEL FILTER EICAS MESSAGE ILLUMINATED INTERMITTENTLY THROUGHOUT FLIGHT. REMAINED FOR LAST 2 HOURS OF FLIGHT. REPLACED THE FUEL FILTER, FOUND DEBRIS ON THE FILTER ELEMENT IAW AMM 73-11-08. ACCOMPLISHED A NR 2 ENGINE RUN UP TEST, NR 3, OPS & LEASDR 9JLA201801269691Fuel Control · defectiveDURING THE LANDING PHASE, THE FLIGHT CREW REPORTED THAT THE RT ENGINE COMPUTER INDICATED A FAIL ANNUNCIATION. INVESTIGATED AND DETERMINED THAT THE RT ENGINE FUEL CONTROL UNIT HAD FAILED. THE FUEL CONTROL UNIT WAS REPLACED. OPS AND LEAK CHECKED SATISFACTORY.SDR PCSA2018102525Engine · vibrationLEFT ENGINE SHUTDOWN IN FLIGHT DUE TO VIBRATION.SDR PCSA20171024001Connector · contaminatedLEFT ENGINE SHUTDOWN IN FLIGHT DUE TO A VIBRATION. ACCOMPLISHED FIM 71-05 FT 814, NO METAL PARTICLES FOUND IN THE INLET OR EXHAUST AREAS, NO COMTAMINATION FOUND ON THE MASTER CHIP DETECTOR. ACCOMPLISHED LT ENGINE BORESCOPE INSPECTION OF THE LPC, HPC, HPT BLSDR PCSA2017053101Fire Warning · false activationTHE LEFT ENGINE FIRE WARNING, THE ENGINE WAS SHUTDOWN IAW THE ENGINE SECURING CHECKLIST. THE FIRE WARNING EXTINGUISHED AFTER THE DISCHARGE OF THE SECOND FIRE BOTTLE. THE OIL PRESSURE WAS NORMAL. THE ENGINE WINDMILLED FOR APPROXIMATELY 28 MINUTES.SDR HALA2017012600017Blade · bentRIGHT ENGINE FAN BLADE DAMAGED, THE TIP IS BENT AND APPEARS TO BE HITTING RUB STRIP. THE RUB STRIP FOUND DAMAGED AND A BIG PIECE AT 6:00 MISSING. RT ENG FAN BLADE REMOVED AND BLENDED AS REQUIRED. READY FOR INSTALL. THE ACOUSTIC LINEAR WAS REPAIRED.SDR HALA2017010200571Liner · damagedETOPS, NR 2 ENG ABRAIDABLE LINER DAMAGED AT 6'OCLOCK POSITION. REPAIRED PER E105-594240-PERM AND AMM 72-33-04.SDR ABXA20161106170Engine · power lossON FINAL APPROACH, THERE WAS A COMPRESSOR STALL AND LOSS OF THRUST FROM THE LEFT ENGINE. ON THE GROUND, THE EGT INCREASED TO 700 DEGREES AFTER ROLLOUT AND THE ENGINE WAS SHUT DOWN. THE AIRPLANE WAS GROUNDED AND A MAXIMUM POWER ASSURANCE TEST WAS PERFORMED IAW SDR ABXA20161023151Engine · malfunctionedLEFT ENGINE LOST POWER ON FINAL APPROACH. EGT WAS 690 DEGREES CELSIUS. AFTER LANDING, ENGINE WOULD NOT PRODUCE THRUST. THE AIRPLANE WAS REMOVED FROM SERVICE AND A VISUAL INSPECTION OF THE LEFT ENGINE INLET AND EXHAUST WAS PERFORMED. NO DISCREPANCIES WERE FOUNDSDR HALA2016062800258Unknown · unknownETOPS SIGNIFICANT SYS. ON TAKEOFF LEFT ENGINE MAX THRUST 103 PERCENT UNABLE TO INCREASE ABOVE 103 PERCENT .29 DEGREES-C AERO DATA REDUCED TARGET 104.1, MAX 107.3. T/S IAW FIM 73-21, FT 811. PERFORMED TESTS AMM 71-00-00 GROUND TESTS 3, 4 CHECKED INLET PROBESSDR IXXA2016041300099Hose · blownEICAS MESSAGE "C HYD QTY", LOSS OF ALL QTY LEADING TO C HYD FAILURE. FOUND HOSE BLOWN.SDR HALA2016031200077Pump · malfunctionedLT FWD FUEL PUMP EICAS MESSAGE ACCOMPLISHED QRH, CONTINUE NORMAL OPERATION, FUEL 6 OF THE QRH. CHECKED CONNECTOR ON BOOST PUMP, NO SHORTS BETWEEN PHASES AND NO SHORTS TO GROUND. CHECKED WIRING BACK TO ACFT, NO SHORTS BETWEEN PHASES & NO SHORTS TO GROUND. RASDR PCSA2015061701Engine · power lossTAKEOFF CANCELLED AT 70 KNOTS DUE TO POWER LOSS RT ENG. PRIOR TO POWER LOSS, ENG PARAMETERS LOOKED NORMAL.SDR HALA2015040400051Wire · brokenEICAS MESSAGE, BLEED VALVE AND OVERHEAD PANEL LT ENGINE. BLEED LIGHT ILLUMINATED DURING CRUISE AT FLT 340, PRIOR TO ETOPS AIRSPACE ATB. REPAIRED BROKEN WIRE AT PRSOV VALVE TERMINAL 1, IAW STANDARD PRACTICE 12-00. RAN ENGINE AND OPS CHECKED IAW AMM 36-11-09.
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