JASC 2200
Service difficulty reports · 567
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 HALA20241118327Fcu · faultedETOPS - ALTITUDE SELECTOR ON FCU LOOSE. DOES NOT FUNCTION PROPERLY. REMOVED AND REPLACED FCU PER AMM 22-81-12. LAND CAT 3 CAPABILITY TEST OK PER AMM 22-97-00. OK FOR SVCSDR 4DPA2024102400002Electronic Unit · failedCREW REPORTED- RED MASTER WARNING PTRIM MAIN INOP EICAS MSG DISPLAYED AT 14000FT ON CLIMB OUT FROM KHPN. DIVERTED TO PHL. CORR ACTION- MX TROUBLESHOT TO BAD HSCU R&R'D HSCU OPS TEST GOOD.SDR YENA2024102801402Fcu · failedFLT#44, LGW-JFK. (ETOPS) 'ON TWO SEPERATE DESCENT LEGS THE AIRCRAFT DEPARTED THE FMS PATH AFTER APPROX 30S AND STARTED AN INCREASINGLY STEEP DESCENT WHILE IN A MANAGED DESCENT BOTH TIMES V/V EXCEEDED 4900 FPM AND THE AIRCRAFT WENT FROM FOLLOWING THE FMS PATH TSDR 7EMA20241015001Roll Servo · intermittentDURING CLIMB OUT, AUTOPILOT WAS ENGAGED. WITHIN 10 SECONDS, AUTOPILOT ROLL TRIM ANNUNCIATOR ILLUMINATED. AUTOPILOT WAS COMMANDED TO DISENGAGE. PILOT REPORTED THAT ALL AXIS EXCEPT THE ROLL FELT FREE. THE AILERONS STILL FELT AS IF THE AUTOPILOT ROLL SERVO REMAINSDR QR9R2024091300005Switch · inoperativeSAS/AP CHECK FAIL: P1 SAS ON SW INTERMITTENT/INOP DURING START RUN-UP. REMOVED AND REPLACED APMS2360 IAW AMM 22-10-00, 4-2. MOC OKAY.SDR 2024FA0000703Switch · defectiveIN FLIGHT PILOT NOTICED SMOKE TRAIL COMING FROM THE YOKE AND A ELECTRICAL BURNING SMELL. DISCONNECTED THE AUTO PILOT AND PERFORMED AN EMERGENCY LANDING AT KTTN.SDR HALA20240820235Bypass Valve · malfunctionedATB - DUE TO ETOPS VERIICATION FLIGHT UNSATISFACTORY PLUS ISSUES WITH MULTIPLE ECAMS. PFR FAULT AIR PACK 2 REGUL FAULT ATA 21-61 CARRIED OUT TROUBLESHOOTING OF AIR PACK 2 IAW TSM 21-61-00-810-817-A. CARRIED OUT OPERATIONAL TEST OF PACK TEMP-CONTROL SYS IAW A32SDR AALA202408199239Control Panel · faultyAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: MODE CONTROL PANEL WENT BLANK IN FLIGHT. CAPTAIN'S FLIGHT DIRECT WORKED BUT THERE IS NO WAY TO CONFIRM ALTITUDE, HEADING, COURSE OR VERTICAL SPEED; AIRCRAFT DIVERTED TO AND SAFELY AT IAD. TROUBLESHOT PERSDR COEA2024071604700Autopilot Sys · malfunctionedFLIGHT 4801 ENROUTE PHX - HII AIR TURNBACK ON CLIMB OUT, THE AUTOPILOT FAILED. AIRCRAFT WAS RETURNED TO PHX. LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ALL A/P SERVOS, CABLES AND CIRCUIT BREAKER. NO DEFECTS NOTED. RERACKED A/P AND PERFORMED OPS CHECK.SDR N6WA2024071603Actuator · inoperativeUNCOMMANDED YAW MOTION DURING CLIMB. R/R YAW DAMPER #1 LINEAR ACTUATOR IAW CRJ 550 AMM 22-22-01. OPS CHECK GOOD.SDR FDEA202407080963Csu · failedAFTER TAKEOFF ON GEAR RETRACTION THE CAPTAIN RED SPD LIM APPEARED ON PFD. THE NUMBER 2 FAC WAS DEFERRED PER MEL 22-26-34-01 AND THE OP NOTES ABOUT SPEED TREND ,VSS, VLS,VMAX,F,S SPEEDS ETC WERE ALSO INDICATED AND MISSING ON CAPT PFD. EMERGENCY DECLARED.SDR DALA2024070506820Control Panel · failedSHIP 6806 -DIV- TO ONT DUE TO ILS GLIDESLOPE FAILED. CORRECTIVE ACTION: REPLACED ILS CONTROL PANEL.SDR 2024FA0000485Servo Control · defectivePITCH CONTROL IN FLIGHT BECAME DIFFICULT TO CONTROL AFTER AUTOPILOT WAS DISENGAGED.SDR QMLA2024062120065Relay · faultedAFTER TAKEOFF, RETRACTED THE GEAR AND TURNED ON YAW DAMPER, GOT THE RUNAWAY TRIM TONE AND AIRPLANE TRIED TO CLIMB 5000 + FT PER MIN, PUSHED THE TRIM INTERRUPT SWITCH, TURNED TOWARD THE RUNAWAY AND DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. DETERMINED THE MOSDR DALA2024061706147Computer · faultedSHIP 3102 - FCNT - DUE TO AN ABRUPT UN-COMMANDED PITCH UP AND TRIM UP CONSTANTLY REQUIRING NOSE DOWN TO HOLD LEVEL. CORRECTIVE ACTION: R/R ELAC #2 (2CE2) AND ACCELEROMETER (12CE4). OPS CHECK GOOD. (LP 5810358)SDR CALA2024061001752Trim System · faultedSPEED TRIM FAIL ON CLIMBOUT THE FOLLOWING ARE IMAGES OF THE FLIGHT FAULTS ON CHANNEL A ANDB. THERE ARE ALLOT MORE JUST DOWNLOADED SOME OF THEM FOUND THE AUTOPILOT STAB TRIM SWITCH IN THE CUTOUT POSITION. PUT FAILURES. PERFORMED CATIIII AUTOLAND TEST REF AMM 22SDR QR9R2024060500001Module · faultedAFTER 3.2 HOURS OF FLIGHT, ACTUATOR CAUTION ILLUMINATED WITH PITCH AND ROLL INDICATIONS ON PFDS AND AP INDICATION ON ANNUNCIATOR PANEL. REMOVED AND REPLACED AUTOPILOT MODULE IAW AMM 22-10-00, 4-1. FUNCTIONAL TEST, MTF SUCCESSFULLY COMPLETED; NO FAULTS NOTED.SDR CALA2024060701727Computer · intermittentA/T DISCONNECT ON TAKE OFF RERACKED TMC COMPUTER AND ACP''D TEST 02, TEST 10 AMD TEST 30 ALL PASSED DUE TO RETURN TO BLOCKS AND SUGGEST REPLACING TMC PULLED AND COLLARED TMC AC, DC, &, SERVO C/B'S AND APPLIED PLACARD. REQUEST DEFERRAL. C/W MEL. REPLACED TMC PSDR CALA2024053101656Autopilot Sys · malfunctionedAUTOPILOT DOES NOT ENGAGE WHEN CMD SWITCH IS PUSHED, SWITCH LIGH TS DO NOT COME ON AND CMD STATUS DOES NOT SHOW ON THE FLIGHT MOD E ANNUNCIATOR CMD A OR CMD B PERFORM LAND VERIFY TEST PER MM 22-11-00-700-801, TEST PASS.SDR YENA2024052800785Fms · malfunctionedFLT#7, JFK-LHR. (ETOPS) ' NO POSITION ON FMS 2 ATTEMPTED RESET UNSUCCESSFUL ( FLIGHT MANAGEMENT SYSTEM (FMS) 2) FMS2 ); FMGC 1 AND 2 RERACK C/O IAW 22-83-34. AFS OP TEST C/O IAW 22-96-00. MDDR 547933 CLOSED. MCC NOTIFIED.'SDR QR9R2024052200001Motor · failedAIRCRAFT FAILED AP TEST DURING START RUN-UP. TROUBLESHOOTING REVEALED YAW PORTION OF AP TEST FAILS. REMOVED AND REPLACED YAW TRIM MOTOR IAW AMM 67-14-00, 4-1.SDR QR9R2024051700001Motor · out of adjustACTUATOR CAUTION ILLUMINATED IN FLIGHT. TAXIED BACK TO PARKING AND AVIONICS DID A RESET. SAME CAUTION CAME BACK ON SOLID WHEN ADVANCING TWIST GRIP TO FLY. DURING GROUND CHECK FOR ACTUATOR LIGHT ILLUMINATING IN FLIGHT, FOUND YAW TRIM MOTOR OUT OF ADJUSTMENT ANDSDR CALA2024052101550Trim System · malfunctionedSTAB OUT OF TRIM LIGHT ILLUMINATED ON TAKEOFF AT ABOUT 60 KTS REPLACED STAB OUT OF TRIM LIGHT M&E 29-3311-3-0062 REF FIM 22-11-851 AND AMM 22-11-00-740-806 . ACCOMPLISHED DFCS AUTOTESTS PASSED.ACCOMPLISHED DFCS SPEED/STAB CHANNEL A & B TEST THAT ENGAGES AP A ASDR CALA2024052001512Adiru · inoperativeSPEED TRIM FAIL ON APPROACH DFCS BITE LEG 1 ADRIU ADM TOTAL STATIC/ PRESS-2. #2 ADIRU BIT NO CURRENT, LEG 01 FAULT AIR/GROUND 34-21038 PERFORMED FIM TASK AND REPAIR CONFIRMATION REF. FIM 22-11TASK 849. LAND VERIFY C/W L/P 7995637. LIGHT EXTINGUISHED. DUE TO NSDR DALA2024051505248Fcu · failedSHIP 3231 DISC: AT GATE, DEPLANING COMPLETE, GROUND POWER WENT OFF LINE WITH THE APU OFF, AIRCRAFT WENT DARK, SMOKE STARTED COMING FROM BEHIND THE FCU. DEBRIEFED FLIGHT CREW. VERIFIED NO PASSENGERS ONBOARD. POWERED A /C WITH GATE POWER. POWER WAS NOT WITHIN ASDR AALA202405140884Control Panel · faultyAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: (MCP) MODE CONTROL PANEL FAILED; AIRCRAFT DIVERTED TO AND LANDED SAFELY AT MSY. REMOVED AND REPLACED MCP (AALA202405090884), PER AMM 22-11-34. MCP FAULT CLEARED BUT CAME ACROSS FAULT BUS PWR CONTROL UNSDR AALA202405141172Control Unit · faultyAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: (MCP) MODE CONTROL PANEL FAILED; AIRCRAFT DIVERTED TO AND LANDED SAFELY AT MSY. REMOVED AND REPLACED MCP (AALA202405090884), PER AMM 22-11-34. MCP FAULT CLEARED BUT CAME ACROSS FAULT BUS PWR CONTROL UNISDR AALA202405149254Control Panel · malfunctionedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: FIRST OFFICER SIDE FLIGHT DIRECTOR AND COURSE SELECTION ON (MCP) MODE CONTROL PANEL WENT OUT AT 4000 AND CAME BACK INTERMITTENTLY; AIRCRAFT DIVERTED TO AND LANDED SAFELY AT MSY. REMOVED AND REPLACED MCSDR YENA2024050700722Computer · failedFLT#8466, MLB-JFK. 'AUTOFLT: RUD TRV LIM2 ON DESCENT PASSING FL200; REMOVED AND REPLACED FAC 2 COMPUTER IAW AMM 22-66-34. PERFORMED OPS CHK OF AFS FAC 2 PASS IAW AMM 22-96-00. NO PRESENT FAULTS AT THIS TIME.'SDR YENA2024050700721Computer · faultedFLT#8466, MLB-JFK. 'AUTOFLT: FAC1 FAULT AT FL 350(NO RESET); ACCOMPLISHED DUAL ENG RUN IAW AMM 71-00-00. PERFORMED RESET OF FAC 1 COMPUTER IAW AMM 22-96-00. AFS TEST PASS FAC1. NO PRESENT FAULTS NOTED AT THIS TIME.'SDR QR9R2024042400001Gyro · illuminatedBACKUP SAS INDICATOR LIGHT ILLUMINATED (INTERMITTENTLY AT FIRST, THEN STEADY) ON CAD. TROUBLESHOOTING REVEALED AP FAILURE CODES RBKURT 1INVAL AND RBKURT 1DEF (ROLL FOG). REMOVED AND REPLACED FIBRE OPTIC GYRO FOG P1E7.SDR CALA2024041701118Unknown · unknownLEFT UNCOM ROLL AT 10K. SPEED AROUND 200KIAS FLAPS 1. FOLLOWED BY AURAL ROLL AUTHORITY CHECK IAW AMM 27-61-00, NO DEFECTS NOTED. OPS NORMAL. REF FIM 22-10 INTERROGATED OMF EXISTING FAULTS, NO FAULTS FOUND. EXTENDED MAINTENANCE LIBRARY TEST CHANNEL A AND B EXESDR QR9R2024040200001Motor · faultedAFTER PICKING AIRCRAFT UP TO A HOVER, YAW TRIM LIGHT ILLUMINATED. REMOVED AND REPLACED YAW TRIM MOTOR IAW AMM 67-14-00, 4-1.SDR QR9R2024022100001Motor · failedAP1 FAILURE IN FLIGHT. TEST FLIGHT EVAL REVEALED AP1 FAILED WITH A FLASHING Y IN ORANGE BLOCK ON PFD, FOLLOWED BY AP2 FAIL WITHIN 30 SECONDS. AFCS SUBS PFTNOTOK MESSAGE WHEN BOTH WENT OFFLINE. REMOVED AND REPLACED YAW TRIM MOTOR.SDR UIEA2024021000080Servo · leakingCENTER ELEVATOR AUTO PILOT SERVO (M272) WITH HYDRAULIC LEAK.(<P>CENTER ELEVATOR AUTOPILOT SERVO WAS REPLACED PER AMM 22-12-01-424-019, REV 140 AUG 22, 2023.</P>)SDR YENA2024021900282Unknown · vibrationFLT#2715, JFK-LAX. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'VIBRATIO IN RUDDER PEDDALS IN FLIGHT- WHEN > 190 KTS- CA AND F/O SIDE - NO OTHER ANOMALES NOTED WITH FLIGHT CONTROLS. NO CHANGE W/ AUTO PILOT ON - OFF. VIBRATION SURVEY COMPLETED; REF LG PG 38312SDR 6CBA2024012625001Ahrs · faultedAFTER DEPARTING PDK THE CREW RECEIVED MULTIPLE CAS MESSAGES, AP 1&2 FAIL, TF 1&2 FAIL, FD 1&2 FAIL, AOC UPLINK FAIL, AND AT FAIL. THE CREW DECIDED TO RETURN TO PDK. TECHNICIANS FOUND AHRS VERTICAL SPEED INERTIAL RATE OUT OF TOLERANCE AT -57.0 FT/MIN. THEY RESDR CALA2024011200089Unknown · unknownSTAB OUT OF TRIM DISCONNECTED AP+AT ELEC TRIM OPS NORMAL PERFOMED DFCS FAULT REVIEW, FOUND MESSAGE 22-11830 ON FLT LEG 01, SUSPECT CREW OPERATION. PERFORMED DFCS LIBRARY TEST 60.32 AND 60.35 IAW FIM TASK 22-11 TASK D72, NO FAULTS FOUND ALL TESTS PASSED. NO RELSDR AALA202401094696Unknown · unknownAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: YAW DAMPER MALFUNCTION. AIRCRAFT RETURN TO AND LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT.**SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).SDR DALA2024010800300Not Reported · not reportedSHIP 3121 - ATO - AT 60KTS DUE AN ELAC 1 PITCH FAULT ECAM MESSAGE. CORRECTIVE ACTION: R/R ELAC 1. OPS CHECK GOOD. OK FOR SERVICE. (4862934)SDR CALA2023122903750Actuator · faultedSTAB OUT OF TRIM LIGHT DURING TAKEOFF ROLL DFCS CURRENT STATUS AND FAULT HISTORY ONLY SHOWED FAULT FOR MCP DISPLAY. PHOTO ATTACHED. NEEDS FURTHER TROUBLE SHOOTING. REF FIM 22-11 TASK 851. PERFORMED STAB TRIM BITE TEST. SEE PICTURES FOR FAULTS. PERFORMED FIM 22SDR ABXA20231228230Unknown · unknownA/T DISC WITH SPEED FLAG AND COULD NOT SET SPEEDS OR TO1. AC RETURNED TO GATE MAINTENACE GROUNDED A/C .PERFORMED RESET AND OPS CHECKED IAW AMM 22-32-00. OPS CHECK OK. AIRCRAFT RELEASED CAT I . AND RETURNED TO SERVICE,SDR QMLA2024011220003Unknown · unknownAT FL 230 PRESSURIZATION CONTROL WAS SET TO FL 230 AND SHOULD HAVE RESULTED IN A CABIN PRESSURE OF APPROXIMATELY 6,300 FEET. THE CABIN PRESSURE INDICATOR WAS SHOWING 8,000 FEET. AS THE LAST TWO EVENTS, THERE WAS A SLIGHT SMELL, LIKE OVERHEATED RUBBER ON A MANISDR UIEA2023122201010Computer · unknownRETURN TO BLOCK AFTER LOW SPEED RTO DUE MASTER CAUTION LIGHT AND BEEPER. "AUTOTHROTTLE DISCONNECT" EICAS MSG. SPED WAS AROUND 40KTS.(<P>DEFERRED IAW MEL 22-30-01 DMI 199674 CONDITION INSP IAW AMM 05-51-14 NOT REQUIRED AS RTO WAS BELOW 40 KNOTS.R/R TMC COMPUTERSDR QXEA2023121800183Control Quadrant · malfunctioned"AT FAIL" MASTER CAUTION ILLUMINATED ON EICAS WHILE ARMING FOR TAKEOFF (AUTOTHROTTLE CHANNELS – BOTH INOPERATIVE). REMOVED FROM SERVICE. INTERROGATED CMC, FOUND FAULT CODES 22310013TA1 AND 22310013TA2. REF E175 FIM 22-31-00-810-811-A, R+R THRUST CONTROL QUADRASDR HALA20231211273Unknown · unknownETOPS - ECAM: NAV BARO REF DISCREPANCY. CAPT "PULL STD" BARO REF KNOB INOP. THE PULL STD FUNCTION DOES NOT CHANGE BARO REF TO STD, AND BARO REF VALUE DOES NOT CHANGE UNLESS PULLING KNOB. REMOVED AND REPLACED FCU PER AMM 22-81-12. ALL TEST GOOD. OK FOR SVCSDR AALA202312085501Computer · inoperativeAIRCRAFT WAS GROUNDED: AIRCRAFT DID NOT GO INTO SRS MODE ON TAKEOFF. MAINTENANCE REPLACED #2 ELAC IAW AMM 27-93-34.SDR HALA20231207263Unknown · unknownATB - AIR TURN BACK FM VERIFICATION FAIL (FM2 FAULT). REMOVED AND REPLACED FMGEC 2 PER AMM 22-83-34. AFS TEST AND LAND III CAPABILITY TEST PASSED. OK TO CONT. SERVICE.SDR YENA2023112701462Fmc · failedFLT#32, AMS-BOS. (ETOPS) 'PRIOR TO SECOND -TO-LAST OCEANIC WAYPOINT, FMS SHOWED ERRONOUS MILEAGE TO DESTINATION. ALL WAYPOINTS CHECKED, NAV SOLUTION ACCURATE THEN TIME TO GO EFOB WOULDN'T DISPLAY. POSITION WAS ACCURATE SO AFTER CONFIRMING WITH MX, CONTROL CONSDR QXEA2023102500154Control Quadrant · malfunctionedAUTO THROTTLE FAILED AT 12,000 FT REINGAGED AND IT FAILED AGAIN 9000 FT LEFT IT OFF (AUTOTHROTTLE CHANNELS – BOTH INOPERATIVE). REMOVED FROM SERVICE. REPLACED THRUST CONTROL QUADRANT PER AMM 76-11-01-000/400-801-A. OP TESTS GOOD REF AMM 22-11-00-710-801-A. A/
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