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 jasc_code = '7603' 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 jasc_code = '7603' 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 N6WA2026081701Control Valve · faultedRT THRUST LEVER WILL NOT ADVANCE ABOVE IDLE WITH ENG RUNNING FOR TAKEOFF. REMOVED AND REPLACED T/R DCV IAW AMM 78-32-01 LEAK AND OPS CHECK GOOD. FAULT PERSISTS. REF LOG PAGE 645688 ITEM 2 FOR CORRECTIVE ACTION.SDR QR9R2026081300001Cable · bindingNEW #1 ENGINE N2 CABLE RECEIVED IS BINDING SITTING IN RESTING POSITION AND GETS WORSE AS CABLE IS BENT INTO SIMILAR SHAPE OF IT BEING INSTALLED ON AIRCRAFT. REPLACED #1 ENGINE N2 CABLE IAW 76-12-00, 4-8.SDR ABXA20260812359Throttle · stiffSTIFF RESISTANCE FELT ON THROTTLE LEVERS. SLOW ACCELERATION AND RESPONSE DURING TAXI. A/C RETURNED TO THE GATE (BTB). MTX ACCOMPLISHED ACCELERATION AND DECELERATION TEST IAW B767 AMM 71-00-00. BOTH ENGINES WITHIN LIMITS. CYCLED THROTTLES MULTIPLE TIMES, NO RESSDR 2026FA0000581Control Cable · bindingLH ENGINE THROTTLE CONTROL STIFF / BINDING.SDR QXEA2026061000135Throttle · malfunctioned"AT FAIL" MASTER CAUTION ON EICAS 8-10 MIN AFTER AIRCRAFT POWER UP . PLACED ON MEL. MEL CLEARED BY VERIFIED FCS 22310020TA(1/2) IN CMC. CND FAULT, REPLACED THROTTLE QUADRANT PER FIM 22-31-00-810-860-A AND AMM 76-11-01-000/400-801-A AS PRECAUTION, OPS CHECKS SDR QXEA2026051200114Throttle · malfunctionedTHROTTLES ARE VERY STIFF & STICKY THROUGHOUT RANGE OF TRAVEL. REMOVED FROM SERVICE. REMOVED AND REPLACED THROTTLE CONTROL QUADRANT IAW AMM 76-11-01-000-801-A, 76-11-01-400-801-A. OPS CHECK GOOD. OPS CHECK GOOD. A/C REMAINS CAT III QUALIFIED, PLACARD READSSDR QXEA2026042700093Throttle · malfunctionedAT FAIL CAUTION EICAS MESSAGE DURING DESCENT. PLACED ON MEL MEL CLEARED BY: FAULT NOT ACTIVE ON STARTUP. FOUND FC 22310019TA(1/2) IN CMC 1X. REPLACED THROTTLE QUADRANT AS PRECAUTIONARY REF AMM 76-11-01-000/400-801-A, OPS CHECK GOOD. AT OPS TEST AMM 22-31-00-71SDR 2026FA0000285Throttle Cable · severedLOSS OF THROTTLE CONTROL IN FLIGHT, DUE TO SEVERED THROTTLE CABLE.SDR QXEA2026040100076Throttle · malfunctionedFLIGHT 2133. REVERSERS ARE DIFFICULT TO INITIATE. DIFFICULTY IS IN THE GATES, NO ABLE TO PULL UP ON THEM DURING THE ROLLOUT. REMOVED FROM SERVICE. REPLACED THROTTLE QUADRANT ASSY PER AMM 76-11-01-000-801-A/-400-801-A. OPS CHECK ALL GOOD. AIRCRAFT REMAINS CAT ISDR WX0A2026022332737Control Unit · intermittent(EMERGENCY DECLARED) (AIRCRAFT NOT GROUNDED) ENG 1 THRUST LEVER DISAGREE ECAM TRANSIENT INITIALLY, STAYED ON AFTER MULTIPLE FAILURES. / PER TSM 76-11-00-810-813-A RMEOVED AND REPLACED CTL UNIT-THROTTLE, ENG 1 (8KS1) PER AMM 76-11-19-000-042A, AND AMM 76-11-19-SDR QXEA2026021100030Throttle · malfunctionedFLIGHT 2460. ON FINAL AT 2000 FT AIRCRAFT WENT INTO GO AROUND MODE UNCOMMANDED. LANDED UNEVENTFULLY. REMOVED FROM SERVICE. REMOVED AND REPLACED THRUST CONTROL QUADRANT WITH NEW PART FROM STOCK IAW AMM 76-11-01-000-801-A, 76-11-01-400-801-A. OPS CHECK GOOD. A/CSDR BAGA2026011900003Throttle · failedAT CRUISE, FL 360, RECEIVED RT THROTTLE FAILED CAUTION MESSAGE. RAN QRH AND DIVERTED TO MEM. REMOVED AND REPLACED THROTTLE QUADRANT. OPS CHKD WAS GOOD. PERFORMED OPS CHECK OF BRAKE SYSTEM, OPS CHKD GOOD.SDR DXTA2026010806475Throttle · faultyLEFT ENGINE THROTTLE LEVER. UPON RUNWAY LINE-UP, FIRST OFFICER ADVANCED THROTTLES, LEFT THROTTLE DID NOT ADVANCE BEYOND THE CONTROL LOCK POSITION. CONTROL LOCK WAS NOT ON, AND NO CAS MESSAGES WERE DISPLAYED. PERFORMED VOLTAGE AND RESIISTANCE CHECKS OF CONTROLSDR P6VA20251204001Throttle · dirtyDURING CRUISE FLIGHT LEFT ENGINE THROTTLE STUCK AT 95% N2 WITH NO ABILITY TO ADJUST. LEFT ENGINE THROTTLE CUTOFF ALSO LOCKED IN ON POSITION. PILOTS WERE ABLE TO FREE THE ENGINE CONTROL AND MANIPULATE POWER AS REQUIRED. UPON INSPECTION OF THE AIRCRAFT AT KMDT ISDR QXEA2025120100358Throttle · malfunctionedFLIGHT 2406. NR 2 TLA STICKY AT LOW POWER, ABOVE IDLE. REV NOT AFFECTED. REMOVED FROM SERVICE. REPLACED TCQ WITH SERVICABLE FROM STOCK IAW AMM 76-11-01-000/400-801-A OPS TEST GOOD VERIFIED FREE AND SMOOTH FULL TRAVEL. A/C REMAINS CAT III QUALIFIED. COCKPIT PLASDR QXEA2025112400356Throttle · malfunctionedPILOT REPORTS "ENG TLA TRIM FAIL" ON EICAS ON A/C POWER UP. REMOVED FROM SERVICE. INTERROGATED CMC, NO FAULTS FOUND. PERFORMED FHDB DOWNLOAD REF. MCN E450009-01 ISSUE 4. PER PROPULSION, SUGGESTS AIOP MODULE & TCQ REPLACEMENT. REF L/P 1116932 FOR REPLACEMENT OFSDR F3LA202511060323Throttle · fodTHIRD WRITE-UP THRUST LEVERS STIFF. REQUIRES SO MUCH FORCE TO COME OUT OF REVERSE THAT LEVERS INADVERTENTLY GO TO CLIMB DETENT. PERFORMED ENGINE THROTTLE CONTROL LEVERS TROUBLESHOOT AND ADJUSTED THE MECHANICAL LINKAGE PER AMM 76-11-00-820-044-A ADJUSTMENT WISDR CALA2025101710220Throttle · obstructedLARGE SPLIT ON THROTTLE TO TRY TO OBTAIN TO THRUST. ENGINE UNAB LE TO MAKE TAKEOFF POWER PERFORMED TEST 13 (TAKE OFF POWER TEST) IAW MM-71-00-00-715-223 ON NR 2. ALL TEST PASSED. PERFORMED TEST 9 (THRUST LEVER /POWER ANGLE TEST) IAW MM-71-00-00-715-170. TEST SDR DALA2025101007392Control Unit · faultedDIV - DIVERTED TO RDU DUE TO AN ENG 2 THROTTLE LEVER DISAGREE MESSAGE. REPLACED THROTTLE CONTROL UNIT PER A320AMM 76-11. OPERATIONAL CHECK GOOD, NO FAULTS.(LP: 7403542)SDR 2025FA0000694Throttle Cable · brokenRIGHT THROTTLE FAILED TO ADVANCE ON TAKEOFF. FOUND BROKEN RIGHT THRUST REVERSER AFT INTERLOCK FEEDBACK CABLE FLEXIBLE CASING ASSEMBLY.SDR 8SMA202509090001Throttle · faultedPILOT REPORTED AN UNCOMMANDED LOSS OF THRUST DURING INITIAL CLIMB AFTER TAKING OFF. AFTER REVIEW WITH PILATUS, P&WC, HONEYWELL AND ENGINEERING DEPARTMENTS, NO FAULTS WHERE FOUND. HOWEVER, THE PILOT REPORTED HE DID NOT MOVE THE PCL AND HE COULD NOT GET MAX POWESDR DXTA2025080104399Throttle · unknownWHILE IN A DESCENT FROM FL 410 TO FL 340 ZERO, WITH THE THRUST LEVERS AT IDLE, THERE WAS A VIBRATION FROM THE RIGHT ENGINE AND THE ENGINE SHUTDOWN R CYAN MESSAGE ILLUMINATED. MOVED THE RIGHT THROTTLE OUT OF IDLE AND THE ENGINE SHUTDOWN R CYAN MESSAGE EXTINGUISDR QXEA2025072400282Throttle · malfunctionedFLIGHT 2171. DURING T/O REACHING 1000/ AGL THE #2 THRUST LEVER DECREASED TO THE POINT THAT THE A/T DISENGAGED. WE ADVANCED THE THRUST LEVER TO T/O POSTION & REENGAGED A/T. NO FURTHER PROBLEMS NOTED. REMOVED FROM SERVICE AND PLACED ON MEL. MEL CLEARED BY REMOVISDR QXEA2025060900251Throttle · malfunctioned'AT FAULT' MSG ON EICAS AFTER AUTOTHROTTLE ENGAGED ON TAKEOFF REMOVED FROM SERVICE. REPLACED TCQ ASSY IAW E175 AMM 76-11-01-000/400-801-A REF W/O 352373 N/R-00008 FOR OTHER WORK PERFORMED OPS CHECK PASSED. ACFT REMAINS CAT III QUALIFIED & COCKPIT PLACARD READSSDR AALA202506048034Lever · out of adjustAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: ON CLIMB BETWEEN FL260 AND FL300 WITH ENGINE ANTI-ICE ON. THE NR 1 ENGINE THRUST LEVER WAS A FULL KNOB FORWARD OF THE NUMBER TWO ENGINE. THEN AFTER A WHILE IT WAS A FULL KNOB BEHIND. THE THRUST LEVERSDR QXEA2025052300226Throttle · faultedTECHNICAL ORDER – PARTS REPLACEMENT – THROTTLE QUADRANT TCQ REPLACEMENT DUE TO FAULT TREND IN AHEADPRO. " A/T FAIL" CAUTION WHEN "A/T" PUSHED ON MAIN PANEL FOR T.O CYCLED A/T DISC SWITCHES ON THROTTLES WHICH CLEARED "A/T FAIL" CAUTION. RESELECTED "A/T" ON MAINSDR QXEA2025051200176Throttle · malfunctionedFLIGHT 2215- IN CRUISE AUTO BRAKE FAIL MASTER CAUTION APPEARED ON CAS FOR APPROXIMATLY 30 SECONDS AND EXTINGUISHED IT DID NOT REAPPEAR. PLACED ON MEL 32-41-02A. MEL CLEARED 5/9 BY INTERROGATED CMC FOUND FAULT CODE 32410003AM REPLACED THRUST CONTROL QUADRANT ASSDR QMLA2025042020050Throttle · faultedDURING CLIMBOUT, AT 8,000 FEET MSL, THERE WAS NO THROTTLE RESPONSE FOR APPROXIMATELY THE LAST 20% OF THROTTLE LEVER TRAVEL. THE THROTTLE OPERATED NORMALLY THROUGH APPROXIMATELY THE FIRST 80% OF TRAVEL BUT TORQUE, TEMP, AND NG% WOULD NOT RESPOND TO ANY THROTTLESDR QXEA2025041600118Control Quadrant · malfunctionedTECHNICAL ORDER – PARTS REPLACEMENT - PRIORITY 2 - THRUST CONTROL QUADRANT REPLACEMENT. REMOVED AND REPLACED THRUST CONTROL QUADRANT IAW E175 AMM TASK 76-11-01-000/400-801-A. OPS TEST GOOD. NFDN.SDR 2025FA0000280Throttle · disconnectedWHILE TAXIING THE AIRCRAFT, THE PILOT EXPERIENCED A COMPLETE LOSS OF ENGINE CONTROL DUE TO A FAILURE OF THE THROTTLE AND MIXTURE ASSEMBLY. SPECIFICALLY, THE THROTTLE AND MIXTURE CONTROLS BECAME DISCONNECTED, RESULTING IN THE PILOT BEING UNABLE TO MANIPULATE ENSDR QXEA2025022400053Throttle · damagedFLIGHT 2060. #1 THOTTLE LEVER IS CRACKED AND PIECES ARE FALLING OFF. REMOVED FROM SERVICE. REMOVED AND REPLACED THRUST CONTROL QUADRANT ASSEMBLY. REF E175 AMM TASK 76-11-01-000/400-801-A. ALL OP'S CHECKS GOOD. A/C REMAINS CAT III. CATAGORY STATUS PLACARD READSSDR QXEA2025021700027Throttle · noneWORK ORDER 348091. THROTTLE QUADRANT REPLACED BY TECHNICAL ORDER DUE TO AHEAD MESSAGES.SDR QXEA2025013100015Throttle · malfunctionedFLIGHT 2358. ON T/O AT FAULT CYAN MSG ON EICAS. MANUALLY MATCHED THROTTLE LH THAT LAGGED RH. SHORTLY AFTER L/O FL250 AT FAIL MASTER CAUTION. BEFORE CALLING VLIST COMPLETE MSG DISAPPEARED. FIVE MINUTES LATER MASTERCAUTION AT FAIL. FLOW MANUAL THRUST LEVERS REMSDR DXTA2024111401140Throttle Control · faultedDURING TAXI OUT AND RUDDER BIAS CHECK NOTICED RIGHT THROTTLE CATCHING AS ITS ADVANCES. FEELS LIKE IT IS BINDING ON ITSELF. CORRECTIVE ACTION; ACCESSED THROTTLE QUADRANT, REMOVED DUST COVER PLATE TO ACCESS FRICTION PLATE MECHANISM. CLEANED THROTTLE FRICTION LEVSDR QXEA2024101000235Lever · malfunctioned#1 ENGINE THRUST LEVER DOES NOT RETURN TO MIN REV POSITION AFTER MAX REV WAS USED WITHOUT MANUALLY MOVING THE #1 LEVER TO MIN REV. REMOVED FROM SERVICE. INTERROGATED CMC, NO FAULTS FOUND. REMOVED AND REPLACED THRUST CONTROL QUADRANT IAW AMM 76-11-01-000-801-A SDR FDEA202410091453Throttle Control · malfunctionedDURING LEFT ENGINE START, WITH THE RIGHT ENGINE SHUTDOWN, BOTH THROTTLES ADVANCED UNCOMMANDED TOWARDS MAX POWER. CREW PULLED BOTH THROTTLES TO FLIGHT IDLE AND APPLIED MAX WHEEL BRAKING. NO STATUS OR MAINTENANCE MSGS RELATED TO THIS OBSERVED FAULT. RAN ALLSDR QXEA2024100400228Throttle · malfunctionedFLIGHT 2160. THRUST REVERSER #1 VERY DIFFICULT TO ENGAGE UPON LANDING DUE TO REVERSER SWITCH NOT RELEASING (UNABLE TO PULL). REMOVED FROM SERVICE. REPLACED TCQ ASSEMBLY IAW E175 AMM 76-11-01-000/400-801-A. OPS TESTS PASSED. INTERROGATED CMC, NO FAULTS. AIRCRAFSDR ANCF20240929019Lever · damagedTHR LEVER NOT SET. RTO RWY O1 THR LEVER NOT SET TO TAKE OFF THRUST, FMA INDICATED MAN FLX, ENG 2 TOOK LONG TIME TO SPOOL UP, ENG THR LEVERS NOT SET THR LEVER NOT SET I.A.W TSM 76-11-00-810-823-A ENGINE THRUST NOT SET AT CORRECT POSITION , ADJUSTMENT OF MECHAANSDR 2024F00199Throttle · faultedAUTOTHROTTLE DOES NOT ARMSDR 2024FA0000558Throttle Arm · brokenPILOT EXPERIENCED SEPARATION OF THE THROTTLE LEVER FROM THE AIRCRAFT THROTTLE QUADRANT DURING RUNUP FOR TAKEOFF. AS FULL POWER WAS SELECTED (LEVER FORWARD), IT SHEARED OFF IN HIS HAND. AIRCRAFT WAS AT FULL POWER, SO WAS ABLE TO BE TAXIED BACK TO CHOCKS AND SHUSDR QMLA2024072920093Spacer · out of limitsTHROTTLE LINKAGE SPACER OUT OF POSITION CAUSED THE PROPELLER TO TRY TO GO INTO BETO RANGE EARLY DURING FINAL APPROACH TO RWY 18R AT KLRD. SPACER WAS LATER ADJUSTED PROPERLY, GROUND ENGINE RUN WAS NORMAL. ACFT RETURNED TO SERVICE 26 JULY 24.SDR DALA2024061406093Throttle · faultedSHIP 3735 -ATO- DUE TO LEFT ENGINE THROTTLE RESPONSE ISSUES AND APPROACHING N1 OVERSPEED. CORRECTIVE ACTION: REPLACING LEFT THROTTLE RESOLVER ASSEMBLY.SDR S9BA2024060403Mount Fitting · brokenCREW REPORTED; WHEN RIGHT FUEL LEVER SELECTED OFF, RIGHT ENGINE DID NOT SHUT DOWN. MAINTENANCE INSPECTED ENGINE CONTROL CABLES AND FOUND CABLES IN BIND. FURTHER INSPECTION FOUND THE RIGHT OUTBOARD ENGINE MOUNT BROKEN. REMOVED AND REPLACED ENGINE MOUNT IAW ASDR 454A2024F00142Spring · wornAFTER LEVELING OUT FROM TAKE-OFF FROM KSAT TO HOUSTON THE LOW RPM WARNING LIGHT WITH AUDIO STARTED GOING OFF. I VERIFIED THE WARNING BY OBSERVING ROTOR RPMS BELOW 95% ON THE TRIPLE TACH. I IMMEDIATELY REDUCED POWER RESULTING IN LITTLE EFFECT ON THE RPMS. I CONSDR QXEA2024051600126Throttle · malfunctionedAUTOTHROTTLE DISCONNECTED 3 TIMES WHILE IN FLIGHT. OCCURED WHILE ON DESCENT AT 1000' PER MINUTE 280 KNOTS. REMOVED FROM SERVICE AND PLACED ON MEL 22-30-00B. RETURNED TO SERVICE. MEL CLEARED 5/15. INTERROGATED CMC, FOUND FAULT 22310020TA2, REF. E175 FIM 22-31-0SDR QXEA2024051300124Power Lever · excess play#2 POWER LEVER HAS LOTS OF PLAY, REMOVED FROM SERVICE. REPLACED THRUST CONTROL QUADRANT PER E175 AMM 76-11-01-000-801-A76-11-01-400-801-A. OPS TEST GOOD. FUNCTIONAL TEST GOOD. A/C REMAINS CAT III QUALIFIED. COCKPIT PLACARD REMAINS CAT III. MTX CTRL NOTIFIED. RSDR V6NA2024022701.1Throttle · faultedDURING THE FIELD ACCIDENT INVESTIGATION FOR N823KD CL604 S/N 5584, IT WAS MENTIONED THAT SEVERAL YEARS AGO A CHALLENGER 600 SERIES, DURING TAXI ACROSS AN ACTIVE RUNWAY, HAD A DUAL ENGINE FAILURE CAUSED BY THE AUTO THROTTLE SYSTEM. IN AN INTERNAL INVESTIGATION,SDR DALA2024021302016Sensor · faultedSHIP 3119 - ATO - AT 40KTS DUE TO A MOMENTARY #2 THRUST LEVER ANGLE SENSOR FAULT. CORRECTIVE ACTION: DEFERRED TLA SENSOR PER MEL 76-11-01. LATER REPLACED #2 THRUST CONTROL MODULE.SDR DALA2024012901215Control Lever · faultedSHIP 3278 DISC: (DIV) ENG 2 THR LEVER DISAGREE CATION ECAM MSG. PERFORMED ECAM ACTIONS FOLLOWED BY QRH PROCEDURES. DECLARED EMERGENCY. OVERWEIGHT LANDING 144800LBS. THRUST DID REDUCE SIGNIFICANTLY ON ENG 2. C/A: C/P 407VC BACKED OFF SEVERAL TURNS-SECURED SAME-SDR QXEA2024012500022Throttle · malfunctionedDUE TO AHEAD PRO FAULT CODES FOR THROTTLE SPLIT, REPLACE THE THROTTLE QUADRANT. QUADRANT REPLACED IAW AMM 76-11-01-000-801-A AND 76-11-01-400-801-A.
Back to JASC 7603