JASC 2200
Service difficulty reports · 568
Reports filed under 2200 · Auto Flight System, newest first.
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 = '2200' 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 = '2200' 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 AJXA2021040700008Autopilot Sys · faultedDURING CLIMB AUTOPILOT FUNCTIONS WOULD NOT ENGAGE AND PILOT RETURNED TO KFXE. WHEN THE AIRCRAFT LANDED WE PERFORMED AN OPERATIONAL TEST OF THE AUTOPILOT SYSTEM AND WE WERE UNABLE TO DUPLICATE THE FAULT. WE SIGNED THE MAINTENANCE OFF AND THE AIRCRAFT HAS SINCE SDR HALA2021021600020Fcu · defectiveETOPS - DUE TO FCU FAULT IN OGG- MOC REQUEST TO REPLACE FCU. // INSTALLED NEW FCU PER AMM 22-81-12, OPS TEST AND "LAND TEST" PASSED PER AMM 22-97-00. OK FOR SERVICE. UNIT, FLIGHT CO OFF 43-2281-9-0002 02025 ON 33-2281-9-0001 01281SDR IPXA2021021265598Flt Controls · malfunctionedINSPECTION TYPE:NA**ATB -EMERGENCY DECLARED - NO EMERG EQUIP USED - LANDED W/OUT INCIDENT - AC TAKEN OOS** DUE OT EXTREMELY LOUD POPPING SOUNDS UNDER FLOOR. ONCE AIRBORNE THE AIRCRAFT WANTED TO MOVE SIDE TO SIDE. WE DID EXPERIENCE SOME HANDLING ISSUES. TREMENDSDR F3LA2021020100007None · noneRAD NAV PAGE BLANK AND ACFT DIDN'T CAPTURE THE ILS SIGNAL. FOUND RMP 1&2 STYBY NAV SWITCH SELECTED. PLACED RMP'S TO NORMAL CONFIG. PERFORMED AFS TEST, TEST OK NO DEFECTS FOUND. ACFT OK FOR SERVICE. AMM 22-96-00-710-001ASDR SWIA202155397Mcu · malfunctionedMACH TRIM AND STAB TRIM MESSAGE, 200 FEET AFTER TAKEOFF. FLIGHT 5141-FILED CLOSED. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22160283 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT PER CRJ200 FIM 27-40-00 PG 28,29 LABEL 273 BIT 16 AND 17. REMOVED ANSDR HALA2020110900199Control Unit · defectiveETOPS-CAPT'S EFIS PANEL LTS-DIM. FD/LS/CSTR. REMOVED AND REPLACED FCU, PER AMM 22-81-12-400-801-A. TESTS PASSED, OK FOR SERVICE. UNIT, FLIGHT CO OFF 43-2281-9-0003 04089 ON 43-2281-9-0003 04071.SDR DALA2020111003652Adiru · faultedMISC/DE. CREW RECEIVED AN NAV ADR DISAGREE, AP AND A/T KICKED OFF, AIRCRAFT REVERTED TO ALTERNATE LAW PASSING FL240 ON CLIMB OUT. ADR 3 WAS ALREADY ON MEL. DECLARED EMERGENCY. CORRECTIVE ACTION: REPLACED ADIRU NR 3.SDR QR9R20200925001Actuator · unreliableSUBMITTED TO SHOW THE SYSTEMIC FAILURE OF THE SEMA ACTUATOR. CALENDAR YEAR 2020 REVEALS MORE THAN 80 ORDERS FOR THIS PART.SDR HALA2020080310165Fcu · unknownETOPS SIGNIFICANT SYSTEM - "MAP NOT AVAIL" STAYED ON CAPT ND. REMOVED AND REPLACED FCU PER AMM 22-81-12. OPS TEST GOOD. NO FAULTS NOTED. PERFORMED LAND CAT III CAPABILITY TEST PER AMM 22-97-00. TEST PASSED. OK FOR SVC.SDR CALA2020072701076Control Panel · faultyON TO ALT SEL HEAD A/S ON MODE CONTROL FAIL REENGAGE ATTEMPTED NO LUCK DFCS BITE PERFORMED PER AMM 22-11-00-810-801. MX MSG 22-11607 MCP DATA INV. PERFORMED FIM TASK 22-11-00-810-817 R/R MCDP PER AMM 22-11-34. PERFORMED LAND VERIFY TEST PER AMM 22-11-00. OPS CSDR FDEA2020063071373Unknown · malfunctionedAT 6000' ON DESCENT WITH AUTOPILOT ENGAGED GOT SEVERAL EICAS INDICATIONS ON NOTICEABLE "THUMP" EICAS AND STATUS MSG INCLUDED: ALT CALLOUTS, TERR POSS, SATCOM, NO LAND 3 STATUS PAGE SATCOM SYSTEM, AFDC-L, NO LAND 3 PACK L AND CAPT FSS LIGHT CAME ON FOR 2 SECONDSDR RU3A202005054020Warning System · activatedRED "TRIM" ANNUNCIATOR ILLUMINATED ON MFD'S AND AUTOPILOT WOULD NOT ENGAGE.SDR AALA2020031639004Computer · malfunctionedAIRCRAFT NOT GROUNDED - DURING DESCENT BOTH NAVIGATIONAL DISPLAYS INDICATED "MAP NOT AVAIL" FOR ABOUT 15-20 SEC THEN RETURNED TO NORMAL. RESET FLIGHT MANAGEMENT GUIDANCE COMPUTER 1 & 2, OPERATIONAL CHECKS SATISFACTORY PER AMM 22-96-00-0501. PERFORMED LAND TESSDR AALA202003039002Unknown · malfunctionedAIRCRAFT WAS GROUNDED: DIVERTED TO BNA. DURING FLIGHT FO'S PFD/ND BLANKED. ECAM MSG'S N1 MODE #1/#2 ENG 2 GEN FAIL A/T FAIL RIGHT WINDOW HEAT FAIL. COMPLETED ALL ECAM MSG'S STARTED APU PER ECAM RECOVERED A/C INTO BNA LOST RH WINDOW HEAT, AUTO THRUST, #2 ENG GESDR SOKF202001270001Flt Controls · malfunctionedDURING FLIGHT FROM SJO TO BOG THE AIRCRAFT DIVERTED TO PTY DUE TO ECAM WARNING LOST OF FLIGHT CONTROLS AT FL 370 DUE TO AIRBUS REFERENCE : 80742128/008 ACTION: PERFORMED AFS TEST IN ACCORDANCE WITH AMM TASK 22-96-00-710-001-A, TEST OK. DUE TO PFR AUTO FLT A/THSDR 2020F00264Computer · overheatedAT AN ALTITUDE OF FL410 ABOUT AN HOUR OF FLIGHT, THE CREW DETECTED A SMOLDERING ODOR OF WHAT APPEARED TO BE ELECTRICAL IN NATURE. THE CREW SELECTED GALLEY AND CABIN POWER OFF AND REFERENCED THE QRH FOR SMOKE OR FIRE IN FLIGHT. THE ODOR QUICKLY SUBSIDED AND IT SDR CALA2019121302178Yaw Damper · disengagedYAW DAMPER DISENGAGED AUTOMATICALLY, YAW DAMPER LIGHT CAME ON AT ROTATION YAW DMPR LIT E CAME ON. QRH DONE. CAM E BACK ON. AL SO RUDR TR IM WAS 1 UNIT LEFT L PERFORMED SMYD MODULE INSTALLATION TEST, PER AMM 27-32-42-400-801, PERFORMED SWEEP TEST ON VTHE SMYD,SDR RU3A20191206070Computer · malfunctionedRUDDER BOOST LIGHT ILLUMINATED INFLIGHT 3+20. EXTINGUISHED DURING DESCENT PASSING 20,000 FT. MX REPLACED BOTH FLIGHT GUIDANCE COMPUTERS. AWAITING QAF. CONTINUE TO MONITORSDR YENA201911183652Fcu · failedFT # 1006, LGB-SEA. EMERGENCY DECLARED. UNABLE TO CONTROL SELECTED SPEED ON FCU CAN PULL BUT NOT SELECT A SPEED TO FLY; REMOVED AND REPLACED FCU IAW AMM 22-81-12-000-001-A AND 22-81-12-400-001-A. PERFORMED OPS CHECK OF FCU IAW AMM 22-96-00-710-001-A. OPS CHECKSDR AALA2019101549009Ils System · malfunctionedAIRCRAFT WAS GROUNDED: PILOT REPORTS AT CRUISE FLIGHT JUST BEFORE TOP OF DESCENT, APPR PUSH BUTTON ARMED ITSELF W/O ANY CREW INTERACTION RECEIVED AUDIO TRIPLE-CLICK,THEN A/C REVERTED TO V/S. PFD WAS FLASHING "ILS" IN AMBER. MAINTENANCE RESET FCU 1&2. SUCCESSFUSDR AALA2019100329013Computer · inoperativeAIRCRAFT NOT GROUNDED: PILOT REPORTS ON TAKEOFF AFTER TOGA PUSHED, NO FLIGHT DIRECTOR DISPLAYED CAPTAIN OR FO. REAPPEARED AFTER HEADING AND VNAV SELECTED. MAINTENANCE REPLACED FCC B IAW AMM 22-11-33, ALL TESTS PASSED.SDR CALA2019081091333Control Panel · malfunctionedON CLIMB, MCP ALTITUDE SELECTOR WENT TO 50000 AND WOULD NOT MOVE. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN. PLEASE REPLACE MODE CONTROL PANEL IAW AMM 22-11-34-400-801. TEST IAW AMM 22-11-34-740-801. REPLACED MODE CONTROL PANEL IAW AMM 22-11-34-400-801. TESDR CA190708014Bridal Cable · broken(CAN) PILOT REPORTED AUTOPILOT PITCHES NOSE UP 1000 FT/MIN. AUTOPILOT INITIALLY DEFERRED PER MEL. AME FOUND DURING TROUBLE SHOOTING THE PITCH SERVO BRIDLE CABLE HAD BROKEN, AND PART OF THAT CABLE WAS STUCK AROUND A MOUNTING FASTER FOR THE PITCH SERVO. SEE ATTASDR CA190627010Autopilot Sys · malfunctioned(CAN) AUTOPILOT REMAINING IN THE `ON` POSITION IN FLIGHT AND MAKING UNCOMMANDED ROLL & PITCH MANEUVERS. DISCONNECT `RED` BUTTON ON STICK, PUSHING CONTROL STICK, AUTOPILOT SOFT-KEY, AND AUTOPILOT BREAKER ALL UNRESPONSIVE. AUTOPILOT WAS DISABLED BY PULLING NAV2 SDR CA190625023Control Panel · faulty(CAN) THE HDG KNOB ON FLIGHT CONTROL PANEL WAS REPORTED ERRATIC IN AIR. PILOT SWITCHED TO MANUAL CONTROLLING AND ELECTED TO DIVERT. CORRECTIVE ACTION: THE FCP WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICES (TC# 20190625023)SDR CA190624016Fmc · faulted(CAN) DURING LEVEL FLIGHT THE A/C WOULD DESCEND 100FT AND THEN CLIMB BACK UP TO SELECTED ALTITUDE AND LEVEL OFF. ON APPROACH WITH GLIDE-SLOPE CAPTURED THE A/C WOULD BEGIN TO DESCEND 2 DOTS BELOW GLIDE-SLOPE. IN BOTH SITUATIONS THE AUTOPILOT WAS SELECTED ON WITSDR CA190620001Autopilot Sys · faulted(CAN) FLT CREW EXPERIENCED AN UNCOMMANDED YAW MOTION, FULL DEFLECTION NOSE RIGHT WITH AP ON WHILE CRUISING AT MACH 0.74. MAINTENANCE ACTION: PERFORMED OPS TEST OF THE RUDDER CONTROL SYS AND RUDDER TRIM SYS WITH NO DEFECTS NOTED IAW AMM 27-21-00-710-801 & 802SDR AALA201906179004Autopilot Sys · malfunctionedAIRCRAFT WAS GROUNDED: PILOT REPORTS CLIMBING THOUGH 8000 FT GOT THE ECAM AUTO FLT RUD TRL LIM 1. AUTO PILOT DISCONNECTED AND AUTO THRUST DISCONNECTED. AFTER ABOUT 30 SEC ECAM WENT AWAY, REENGAGED AUTO PILOT AND AUTO THROTTLE. MAINTENANCE RESET FAC1, FAULTS CLSDR CALA2019060700901Switch · inoperativeAUTOPILOT 1 AND 2 DO NOT ENGAGE. REMOVED AND REPLACED CAPT''S AND F/O''S A/P DISCONNECT SWITCHES IAW AMM 22-11-41-400-801. OPS CHECK GOOD.SDR ASAA2019042639116Unknown · unknownUNSUCCESSFUL AIII PRACTICE APPROACH; JUST INSIDE THE MARKER, LOCALIZER WENT ALMOST FULL SCALE TO THE RIGHT (A/C L OF COURSE) = APPRCH WARN & NO AIII, PLANE CORRECTED TO CENTERLINE. HUD DISPLAY WENT BLANK & WAS INTERMITTENT. GROUNDED - YES. ACCOMPLISHED HGS SENSDR HALA2019042200193Control Unit · malfunctionedETOPS SIGNIFICANT SYSTEM - IN DESCENT AUTO FLT FCU FAULT. TROUBLESHOOT AUTO FCU FAULT PER TSM 22-81-00-810-801-A. RESET FCU. PERFORMED AFS TEST PER AMM 22-96-00. TEST OK NO FAULTS NOTED. OK FOR SERVICE.SDR HALA2019040500178Computer · malfunctionedON ILS W/ AUTO PILOT ON #2 AT 800 FT FLT DIR ROLL BAR DISAPPEARED & AUTO PILOT KICK OFF. RAW DATA OK. // REMOVED AND REPLACED FCC #2 PER BOEING 717 AMM 22-01-03. PERFORMED FCC #2 RTS TEST PER BOEING 717 AMM 22-00-00. CHECK OK.SDR AALA201904021903Unknown · multiple failAIRCRAFT NOT GROUNDED: PILOT REPORTS THAT ON APPROACH PRIOR TO FLAP EXTENSION, AUTO THROTTLE WOULD NOT RESPOND. A/P WOULD NOT ENGAGE DURING G.A. NO FAULTS NOTED ON ECAM. MAINTENANCE TROUBLESHOT IAW TSM 24-00-00-810-818-A. PERFORMED CAT III LAND CAPABILITY TESTSDR GTIA2019022303182Autopilot Sys · malfunctionedABORTED TAKE OFF APROXIMATELY 90KTS, AUTO FLT A1 THR OFF & MAP NUT AVAIL MSG.-PERFORMED TEST IAW TSM 22-83-00-810-893-A. NO DEFECTS NOTED. PERFORMED AFS TEST IAW AMM 22-96-00. NO FAULTS NOTEDSDR ASAA2018121077252Fcu · noneFCU # 1 INOP GROUNDED - YES. PERFORMED POWER-UP TEST AND BITE TEST OF AFS REF AMM 22-96-00 PB 501:OK FCU # 1SDR AALA201903119019Unknown · unknownDURING CLIMB OUT, AT APPROXIMATELY 7000 FT HAD AN UNCOMMANDED 6.0 DEGREE LEFT RUDDER INPUT. DISCONNECTED THE NR 2 AUTOPILOT AND MANUALLY RESET THE RUDDER TRIM TO ZERO. USED THE NR 1 AUTOPILOT FOR THE REMAINDER OF THE FLIGHT. NO FAULTS FOUND DURING AFS TEST SDR ASAA2018081085731Autopilot Sys · malfunctionedON RNAV AT APPROXIMATELY 1500 MSL, VNAV PATH AND HUD GUIDANCE DEVIATE QUICKLY TO SHOW APPROXIMATELY 500' LOW ON PATH. AT THIS POINT THE AUTOPILOT FOLLOWS THIS GUIDANCE, PITCHES UP. AIRPORT WAS IN SIGHT, AUTOPILOT WAS DISCONNECTED AND GUIDANCE WAS IGNORED WITH SDR QMLA2018072018086Actuator · unserviceableON TAKE OFF PILOT FELT UNCONTROLLED ROLL. ABORTED TAKE OFF AND RETURNED TO BASE.SDR HALA2018060800288Autopilot Sys · malfunctionedAUTO FLIGHT FCU FAULT. PERFORMED AFS TEST IAW AMM 22-96, FOUND TEST OK. NO FAULT MESSAGE SHOWED. ACFT OK FOR SERVICE.SDR QMLA2018053118066Switch · malfunctionedSAS FORCE TRIM SWITCH ENGAGES UNCOMMANDED. WHEN SAS IS ENGAGED VIA CONTROL PANEL THE FORCE TRIM RELEASE SWITCH WILL OVERRIDE THE FORCE TRIM UNCOMMANDED RESULTING IN UNCOMMANDED PITCH AND ROLL CHANGES WHEN THE CYCLIC IS NOT GUARDED OR HELD. WHEN SAS IS OFF, THESDR HALA2018052300242Unknown · unknownON ILS, AUTOPILOT CMD, ON GS, FMA G/S FLAGGED AT 2400 MSG WITH AUTOPILOT DISCRETE LIGHT AND EICAS MSG. DISCONNECTED A/P AND FMA G/S FLAG NOTICED.//MCDP LAST FLT FAULT SHOWS A/P CTN ILS BEAM ERR . PERFORMED TEST 30,40 OPS CHECK OK IAW FIM 22-03-00. CENTER MMRSDR UIEA2018042000749Control Module · malfunctionedSTAB TRIM STATUS MESSAGE WITH NO LAND 3 MESSAGE. REPLACED THE STAB TRIM POSITION TRANSMITTER, CONTROL MODULE, AND STAB TRIM / RUDDER MODULE.SDR MASA2018033013101Yaw Damper · failedEMERGENCY DECLARED FOR UNCOMMANDED YAW. REPLACED THE YAW DAMP ACTUATOR NR 2. TEST FLT GOOD.SDR HALA2018032600122Unknown · unknownAPPROXRIMATELY 30 MINUTES INTO FLT, OVERHEAD LIGHTS IN COCKPIT AND MAIN CABIN FLICKERING. SHORTLY AFTER, ECAM MESSAGE AUTO FLT FM 2 FAULT. ECAM ACTION TO SWITCH BOTH ON 1, AFTER COMPLYING, RETURNED TO DEPARTURE. DURING DECENT, AT APPROXIMATELY FL 150, LISDR HALA2018030500067Fcu · faultedAUTO FLT FCU FAULT, STATUS PAGE INDICATES PART FCU. ILLUMINATED WHEN CHANGING ALTITUDE FROM FL 400 TO FL 410. FAULT NOT CONFIRMED ON ARRIVAL. TROUBLESHOT IAW TSM 22-81-00-810-859A. NO FAULTS. NO 30 DAY HISTORY. PERFORMED LAND CAT 3 CAPABILITY TEST IAW AMSDR ASAA2018021623586Warning Light · false activationPILOT REPORTS OVERHEAD SPEED TRIM FAILED ANNUNC ON. ACFT GROUNDED. CONFIRMED SPEED TRIM FAIL LIGHT ILLUMINATED. ACCOMP DFCS BITE TEST GROUP 32 SPEED/STAB TRIM INTERACTIVE & SURFACE TESTS IAW AMM 22-11-00, OPS NORMAL, NO FAULTS AND SPEED TRIM FAIL LT EXTISDR AALA201711069001Relay · faultyFLIGHT RETURNED TO DEPARTURE DUE TO OSCILLATION WITH BOTH YAW DAMPERS ENGAGED. WITH THE RIGHT YAW DAMPER DE-SELECTED, THE OSCILLATION STOPPED. EMERGENCY DECLARED. LANDING UNEVENTFUL, AND AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED AIR GROUND RELAY K199 (ASDR AALA20171105005Relay · faultyFLIGHT RETURNED TO DEPARTURE DUE TO OSCILLATION WITH BOTH YAW DAMPERS ENGAGED. WITH THE RIGHT YAW DAMPER DE-SELECTED, THE OSCILLATION STOPPED. EMERGENCY DECLARED. LANDING UNEVENTFUL. REMOVED AND REPLACED AIR GROUND RELAY K199 AND RELAY K293 (AALA2017110690SDR AALA201709189002Unknown · malfunctionedDURING APPROACH INTO BGI, AROUND 500 FEET, AIRCRAFT EXPERIENCED A NOSE DOWN PITCH AT THE SAME TIME THE AUTO THROTTLE BECAME UNRESPONSIVE. THE FLIGHT CREW INTERVENED AND DISCONNECTED THE AUTOPILOT AND AUTO THROTTLES TAKING MANUAL CONTROL. AIRCRAFT EXPERIENCED TSDR A6WA2017091345270Actuator · malfunctionedRECEIVED AN UNCOMMANDED YAW IN FLIGHT, 2 BALL WIDTHS ON THE SIDE SLIP INDICATOR. COMPLIEC WITH QRH. YD 1 AND 2 OFF UNCOMMANDED YAW CONTINUED FOR 10 MINUTES THEN CLEARED. COULD FEEL YAW MOTION IN RUDDER PEDALS. REMOVED AND REPLACED THE NR 1 YAW DAMPER ACTUAT
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