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 ABXA20260916410Engine · fluctuatesDURING TAKEOFF FROM MIA, RT ENG STARTED TO ROLL BACK 2-3 PER N1. AFTER TAKEOFF FLUCUATED BETWEEN 2-3 TO 6-8%. BY 500FT IT WAS BOUNCING BETWEEN 95% & 68%. UPON THRUST REVERSER APPLICATION R ENGINE WAS 8% LOWER. CREW DECLARED EMERGENCY (EDC) AND PERFORMED AIR TUSDR ABXA20260608251Actuator · defectiveDURING ENGINE START, "L ENG FUEL VAL" EICAS MSG AND DISCRETE LIGHT ON ABOVE FUEL CONTROL SWITCHES. REMOVED AND REPLACED THE LEFT ENGINE CONDITION CONTROL ACTUATOR, REF ABX B767 AMM 76-11-04. ALL FUNCTIONS AND INDICATIONS NORMAL. AIRCRAFT "NO ETOPS". A/C RETURNSDR ABXA20260117015Circuit Breaker · faultedON PUSHBACK, ALL T/O SPEEDS DUMPED AND UNABLE TO SET ANY T/O PWR SETTING ON TMC OR SET A TEMPERATURE A/C RETURNED TO THE GATE AND MTX GROUNDED A/C .MTX RESET CIRCUIT BREAKER IAW B767 AMM 20-60-01. OPS CHECK GOOD. NO FAULT NOTED AT THIS TIME. ACFT REMAINS CASDR ABXA20250922235Elec Connector · defectiveON TAKE OFF, LT ENGINE EGT FLUCTUATED. AIRCRAFT ABORTED TAKE OFF AND RETURNED TO BLOCKS. (BTB). MAINTENANCE C/W HIGH ENERGY STOP INSPECTION IAW AMM 05-51-14. NO DISCREPANCIES NOTED AT THIS TIME. REMOVED AND REPLACED D4208P AND D4208J (PYLON CONNECTORS), D9SDR ABXA20250813175Manifold · crackedON TAXI R ENG HAD VIBRATIONS FROM 2.8 TO 3.3. WHEN ADDING TAXI THRUST VIBRATION INDICTIONS UP NTO 4.9 AND STARTED BEING VARIABLE- VIBRATION FELT IN AIRFRAME. AIRCRAFT RETURNED TO BLOCKS. (BTB). PERFORMED D.V.I OF RT ENG & FOUND UPPER & LOWER LPT COOLING AIR SDR ABXA20250512094Compressor · stalledDURING CLIMB, LT ENG COMPRESSOR STALL AT APPROX FL 310 WITH CLIMB AND THRUST. STOPPED WHEN APPROX BELOW 93% N1. NO EICAS EXCEEDANCES. NO FURTHER STALLS IN CRUISE OR DESCENT. CONDUCTED STALL INSPECTION PER AMM 72-00-00/601, THEN CONDUCTED T/S PER FIM 71-05 FT SDR IXXA2024032600002Frame Angle · crackedREPAIR, MAIN FRAME INNER CHORD TRANSITION RADIUS. STA 883.5 RBL 89SDR IXXA2024032001Skin Panel · delaminatedR/H VERTICAL STAB HAS AREA DELAMINATED ON SKIN PANELSDR ABXA20221026297Engine · hung startHUNG START AFTER STARTER CUTOUT. EGT CONTINUED TO RISE TWD THE LIMIT. N2 AND N1 NORMAL WITH NO INCREASE IN SPEED WITH THE INCREASING EGT. FOLLOWED QRH PROCEDURE FOR THE ABORTED START AND ELECTED TO RETURN TO BLOCK. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCESDR IXXA20220820126Mec · failedDESCENDING FROM 11,500 TO 7000 FT, LEFT ENGINE OIL PRESSURE FOLLOWED BY LEFT ENGINE BLEED OFF EICAS MESSAGE. OIL PRESSURE WAS INDICATING 8 PSI EVENTUALLY GOING TO 0 WITH N1 AT 20%. NO VIBRATION OR INDICATION OF FIRE. #1 ENGINE FLAMEOUT AND ALL INDICATIONS ROLSDR IXXA2022060102Rub Strip · crackedRUB STRIP CRACKEDSDR IXXA2022050402Thrust Reverser · crackedTHRUST REVERSER TRAILING EDGE CRACKEDSDR IXXA2022060306Web · cracked#2 OB CORE COWL INNER WEB CRACKEDSDR IXXA2022060811Cowling · cracked#1 ENGINE OB CORE COWL CRACKED AT LOWER CORNER OF VENT PANELSDR ABXA20211012100None · noneON TAKE OFF ROLL RIGHT REV (AMBER) LIGHT ILLUMINATED. ABORTED TAKE OFF AND RETURNED TO BLOCK. AIRCRAFT GROUNDED BY MAINTENANCE. RIGHT REVERSER WAS DEFERRED IAW ABX MEL 78-31-1A. AIRCRAFT RETURNED TO SERVICE.SDR ABXA202109021086Start Valve · uncontrollableRH ENGINE START VALVE UNCOMMANDED POSITION DURING START, ABORTED START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED # 2 ENG. START VALVE PER AMM 80-11-02. OPS CK GOOD. AIRCRAFT RELEASED FOR FLIGHT.SDR ABXA2021830083Start Valve · bindingLH ENGINE START VALVE FAILED TO OPEN. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. FOUND L/H ENGINE START VALVE BINDING DURING MANUAL OPERATION. REMOVED OLD, THEN INSTALLED NEW L/H START CONTROL VALVE PER AMM 80-11-02. AICRAFT RELEASED FOR FLIGHT.SDR ABXA2021829080Starter · faultedLEFT ENGINE FAILED TO START, N2 NEVER GOT ABOVE 8.7 DUCT PRESSURE WAS NORMAL. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED THE #1 ENGINE STARTER IAW B767 AMM 80-11-0. AIRCRAFT RELEASED FOR FLIGHT.SDR ABXA2021529055Starter · failedRH ENGINE STARTER FAILED ON ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. STARTER WAS REPLACED IAW AMM 80-11-01 AND AIRCRAFT WAS RELEASED FOR FLIGHT.SDR ABXA2021523053Starter · faultyRH ENG WOULD NOT START. WILLNOT GET ANY ROTATION ,WHEN, "GND " IS SELECTED, AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. ENGINE STARTER WAS REMOVED AND REPLACED IAW AMM 80-11. AIRCRAFT RELEASED FOR FLIGHT.SDR ABXA202143023Shutoff Valve · stuckRT ENG BLEED OFF LIGHT ON WITH ALSO THE RT PACK OFF LIGHT ON DURING TAXI. AIRCRAFT LINED UP FOR TAKE OFF AND RT ENG. BLEED LIGHT DID NOT EXTINGUISH DURING ENGINE ACCELERATION. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE GROUNDED AIRCRAFT. REMOVESDR ABXA2021131006Engine · reads highAFTER ENGINE START LEFT ENGINE WAS IDLING HIGHER THAN RIGHT ENGINE, ITEM WAS CREW DEFERRABLE. THE DEFERRAL REQUIRED MORE FUEL TO BE ADDED FOR FLIGHT. AIRCRAFT BACK TO BLOCKS, GROUNDED BY MAINTENANCE UNTIL DEFERRAL WAS COMPLETE AND FUEL WAS ADDED.SDR ABXA20200803185Igniter · failedNO START ON RIGHT ENGINE WITH NR 1 IGNITER, HAD TO PULL BACK TO GATE FOR TRAFFIC. AIRCRAFT GROUNDED. REMOVED AND REPLACED RIGHT ENGINE NR 1 IGNITOR PLUG, IAW AMM 74-21-02. RAN ENGINE IAW AMM 71-00-00 TABLE 501 TEST 3. ENGINE OPERATION CHECK GOOD. DI CLEARSDR UIEA2020090841951Igniter Box · malfunctionedRT ENGINE NR 1 IGNITION INOPERABLE (IGNITION SYSTEM, EXCEPT ER OPERATIONS (NOTIFY DISPATCH ) R-60. TRANSFERRED TO MDDR 133851 IAW MEL 74-00-01B,CAT C,NO MAINTENANCE ACTIONS, PLACARD INSTALLED. R & R RT ENGINE NR 1, IGNITION EXCITOR BOX IAW B767 AMM 74-11-01.SDR ABXA20200803154Pump · failedLEFT ENGINE HAD NO FUEL FLOW ON START. AIRCRAFT WAS GROUNDED.SDR UIEA2020012310103Engine · vibrationHEARD SEVERAL BANGS AND FELT THE AIRFRAME SHUDDER EACH TIME FOLLOWED BY ABNORMAL ENGINE INDICATIONS ON RIGHT ENGINE, WHICH RESULTED IN THE ENGINE SHUTTING DOWN IN FLIGHT. NR 2 ENG REMOVED & REPLACED IAW WORK CARD A-71-999-03-01.SDR ABXA20190717126Transducer · faultyDURING TAKEOFF, NEITHER ENGINE REACHED TAKEOFF N1 SPEED (109.7). THE RIGHT ENGINE N1 INDICATED 108.8 AND THE RIGHT EGT INDICATED 925 CELSIUS. THE LEFT ENGINE N1 INDICATED 107.9. THE CREW ABORTED THE TAKEOFF AT 125 KIAS. THE AIRPLANE WAS REMOVED FROM SERVICE (GSDR UIEA2019021543218Fuel Filter · warning messageDURING CLIMB POWER EICAS MSG "L ENG FUEL FILTER" DISPLAYED (<P>ACCOMPLISHED FIM 73-11 F/T 804 BLOCKS 1 AND 21. REMOVED AND REPLACED LH ENG FUEL FILTER I.A.W. AMM 73-11-02, FILTER CONTAMINANTS NOT FOUND. PERFORMED GROUND ENG RUN I.A.W AMM 71-00-00, NO LEAKS NOTSDR UIEA2018110902556Engine · unknownDURING TAKEOFF, RIGHT ENGINE THRUST 94.2 N1, AUTOTHROTTLE SET 92.2 N1, AND REQUIRED A MANUAL ADJUSTMENT TO SET REQUIRED THRUST, LEFT ENGINE NORMAL, DISCONNECTED CDP SENSE LINE AND EXAMINED FOR BLOCKAGE AND LEAKAGE WITH NO NO DEFECTS NOTED, INSTALLED CDP SSDR ABXA20180828096Engine · making metalON CLIMB OUT AT APPROXIMATELY FLIGHT LEVEL 190, THE CREW HEARD A BOOM AND SMELLED A STRONG SMOKE ODOR. AT THE SAME TIME, THE AIRPLANE YAWED AND SHUTTERED. THE RIGHT ENGINE HAD HIGH EGT (1100 DEG) AND N2 INDICATION (113.1). THE RIGHT ENGINE WAS SHUT DOWN AND THSDR ABXA20180821095Engine · failedIN THE BEGINNING OF THE TAKEOFF ROLL WITH THRUST SELECTED, THE RIGHT ENGINE DID NOT RESPOND TO THROTTLE ADVANCEMENT & THE TAKEOFF WAS REJECTED. THEN DURING THE SECOND TAKEOFF ROLL WITH THE AUTO THROTTLE SELECTED OFF, THE RIGHT ENGINE FAILED TO ACCELERATE, CAUSSDR UIEA2018031000358Cable · not reportedVBV FLEX CABLE FAILED RIG TEST ON THE NR 2 ENGINE. REMOVED AND REPLACED VBV FLEX CABLE, RIGGED VBV AND VSV SYSTEM, FUNCTIONAL CHECK GOOD.SDR ABXA20170102144Mec · malfunctionedLEFT ENGINE FLAME OUT (SHUTDOWN) OCCURRED WHILE DESCENDING THROUGH APPROXIMATELY 18,000 FEET. THE ENGINE WOULD NOT RESTART IN FLIGHT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE LEFT ENGINE'S MAIN ENGINE CONTROL (MEC), COMPRESSOR INLET TEMPERATURESDR UIEA2017120302342Filter · warning messageINTERMITTENT RIGHT ENGINE FUEL FILT EICAS MESSAGE AT HIGH THRUST SETTINGS (<P>ACCOMPLISHED FIM 73-11 F/T 804. FOUND CONTAMINATION ON FILTER ELEMENT (NO METAL) REMOVED AND REPLACED FILTER ELEMENT IAW AMM 73-11-02. PERFORMED OPS OF DIFFERENTIAL PRESSURE SWITCH ISDR ABXA20171201142Stator Vane · out of adjustTHE RIGHT ENGINE HAD COMPRESSOR STALLS DURING CLIMB BETWEEN FL340 AND FL350. THE THROTTLE WAS RETARDED 10% AND THE COMPRESSOR STALLS STOPPED. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE RIGHT ENGINE'S VARIABLE STATOR VANE SYSTEM WAS INSPECTED AND SDR ABXA20171127141Sensor · malfunctionedPASSING THROUGH FLIGHT LEVEL 230, THE RIGHT ENGINE EXPERIENCED COMPRESSOR STALLS. THE CREW COULD NOT RESTORE NORMAL ENGINE OPERATION VIA THE QUICK REFERENCE HANDBOOK PROCEDURES. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE RIGHT ENGINE'S MAIN ENGINE CONTROL SDR ABXA20171124140Stator Vane · out of adjustDURING CLIMB THROUGH FLIGHT LEVEL 200, THREE LOUD BANGS OCCURRED THAT JOLTED THE AIRCRAFT. THE AIRPLANE SEEMED TO YAW EACH TIME. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE LEFT ENGINE'S VARIABLE STATOR VANE SYSTSDR ABXA20171122139Compressor · stalledRIGHT ENGINE HAD A COMPRESSOR STALL. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE FAULT ISOLATION MANUAL DIAGRAM 71-05, FAULT TREE 808 WAS ACCOMPLISHED. ALL FINDINGS WERE WITHIN LIMITS. THE CAUSE OF THE COMPRESSOR STALL IS UNKNOWN.SDR UIEA2017093001907Engine · odorSTRONG ELECTRICAL ODOR DETECTED WHIILE CLIMBING THROUGH FL 320 AND UNTIL A RETURN LANDING, THE ODOR DISSIPATED AT 4000 FT, NO SMOKE OR OTHER ABNORMALLY OBSERVED. REMOVED AND REPLACED THE NR 2 ENGINE IAW 71-00-00, PERFORMED REQUIRED TEST 1, 3, 4, 7, AND 12.SDR UIEA2017092201787Pressure Switch · no testNR 2 ENGINE FUEL FILTER BYPASS DIFFERENTIAL PRESSURE SWITCH FAILED A FUNCTIONAL CHECK. REMOVED AND REPLACED THE NR 2 ENGINE FUEL FILTER BYPASS DIFFERENTIAL PRESSURE SWITCH, OPS CHECKED GOOD IAW AMM 73-34-01 AND AMM 71-00-00.SDR UIEA2017092201780Shutoff Valve · no testNR 1 ENGINE PRSOV FAILED A FUNCTIONAL CHECK. REMOVED AND REPLACED THE PRSOV. OPS CHECKED GOOD IAW AMM 36-11-09.SDR UIEA2017092201774Cable Assy · malfunctionedNR 2 ENGINE SLOW TO SPOOL. REMOVED AND REPLACED THE NR 2 ENGINE VSV FEED BACK CABLE ASSY, OPS CHECKED GOOD AND ACCELERATION NORMAL IAW AMM 75-31-03, AND AMM 71-00-00.SDR UIEA2017073001383Warning Message · false activationRIGHT ENGINE BLEED VALVE CAUTION DESCENDING OUT OF FL 390. ACCOMPLISHED FIM 36-11 FT 954. NO DEFECTS NOTED TO SENSE, MUSCLE OR LINES. NO DEFECTS TO WIRING OR CONNECTORS PERFORMED HPSOV OPS CHECK IAW AMM 36-11-07, OPS CHECKED NORMAL. GROUND RUN ENGINE, RT ENGSDR IXXA20170513999Engine · making metalFLIGHT ATN3706 EN ROUTE FROM DEPARTURE STATION KABE TO DESTINATION STATION KONT EICAS MESSAGE DISPLAYED "R OIL FILTER". AS DIRECTED BY QRH, THE RIGHT ENGINE WAS SHUTDOWN. NOTIFIED ATC, DECLARED EMERGENCY. DIVERSION TO KILN. LANDED WITHOUT FURTHER INCIDENT. AIRSDR UIEA2017042900677Solenoid · failedRIGHT ENGINE EEC OFF EICAS AND OFF LIGHT ILLUMINATED ON POWER TRANSFER DURING ENGINE START. RESET AND OPS NORMAL FOR FULL FLIGHT, COMPLIED WITH FIM 73-21 FT 805 AND FIM 71-01FT 804 REMOVED AND REPLACED THE RT ENGINE PMC IAW AMM 73-21-02, NO HELP, RE INSTALLSDR UIEA2017040900531Line · looseDURING TAKE OFF AT 80 KTS, THE RT ENGINE ROLLED BACK TO 96.8 N1, UNABLE TO PUSH BACK TO MATCH, LT ENGINE AT 100.4. ACCOMPLISHED EEC BITE IAW FIM 71-01, 804, NO FAULTS NOTED. FOUND LOOSE CBT LINE ON MEC. RAN ENGINE TO POWER IAW AMM 71-01-00, ALL INDICATIONSDR UIEA2017022000218Inlet · corrodedNR 2 ENGINE INLET LOWER TWO BOLT HOLES HAVE CORROSION. FREEZE PLUGS FABRICATED AND INSTALLED IAW SRM 51-20-07, PARA B, FIG 5 & FIG C, AND PARA 3B AND RDR PMO-TLS-17-007-14B.SDR ABXA20170114002Bolt · missingLEFT ENGINE FLAME OUT (SHUT DOWN) OCCURRED WHILE DESCENDING THROUGH APPROXIMATELY 10,000 FEET. THE QUICK REFERENCE HANDBOOK’S ENGINE FAILURE AND ENGINE IN FLIGHT START CHECK LIST WAS COMPLETED. THE ENGINE RESTART WAS SUCCESSFUL. THE AIRPLANE WAS REMOVED FROMSDR UIEA2016092000763Engine · power lossRTO ON TAKEOFF RT ENGINE DID NOT PRODUCE TAKEOFF THRUST, RTO BELOW 80 KNOTS. COMPLIED WITH GROUND TEST NR 4 VERIFIED BOTH ENGINE MAKE T/O POWER 108.6 NO THROTTLE SPLIT ELECTRONIC ENGINE CONTROL OFF REF AMM 71-00-00. TRANSFERED TO MDDR 70393 IAW MEL 73-21-01SDR IXXA20160420019Skin · corrodedTHE FOLLOWING WORK WAS ACCOMPLISHED DURING VISIT BY MX & ENGINEERING SERVICES. FUSELAGE SKIN, PN 146T3531-3, CORRODED AT STATION 1414, STRINGER 35R INBD OF AFT DRAIN MAST AT SKIN LAP. THE FUSELAGE SKIN WAS REPAIRED IAW SRM 53-00-01 REPAIR 12 FIGURE 201 & 469
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