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 AALA202205177458None · defectiveAIRCRAFT WAS GROUNDED: ON APPROACH TO DCA ILS FMA NORMAL WE DIDN'T INTERCEPT LOC MISSED APPROACH TRIED RNAV APPROACH WOULD NOT ARM. AIRCRAFT DIVERTED TO PIT AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY IN PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLSDR AALA202205101709Adiru · noneAIRCRAFT WAS GROUNDED: ON TAXI DURING 90 DEGREE TURN ENCOUNTERED ADR 1 FAULT WHICH SELF CLEARED. ON CLIMB (FL200) AND AT CRUISE (FL330) ENCOUNTERED UN-COMMANDED YAW MOVEMENT WITH ACCOMPANYING ADR1 FAULT MOMENTARILY (1/2 SECOND) BEFORE CLEARING ITSELF. AP2 WSDR CALA2022050901169Shift Mechanism · failedSTAB TRIM LITE ILLUMINATED IN FLIGHT WITH A SPEED TRIM FAILURE BOTH AIRCFAFT HAD TO BE FLOWN BY HAND NO AUTOPILOT PERFORMED STAB TRIM TEST, COLUMN SWITCHING MODULES AND NEUTRAL SHIFT SENSOR FAILED SEVERAL TIMES. FURTHER T/S REQUIRED. REF L/P 8537413, FOUND PHASDR DALA202206904027Computer · unknownPD: NO TROUBLE FOUND / CA: TESTED BY VC: 10016116, DATED: 31 MAY 2022, FM TN: RO522133062, WO: 3504931126, PO: 4701281555. GVI.SDR AALA202205022769Warning System · false indicationAIRCRAFT WAS GROUNDED: ABORTED TAKE OFF UNDER 80 KNOTS DUE TO MASTER CAUTION LIGHT. RETURNED TO GATE. PERFORMED AUTOMATIC FLIGHT SYSTEM GROUND TEST PER AMM 22-96-00. ALL CHECKS GOOD. PERFORMED OPERATIONAL CHECK OF FULL AUTHORITY DIGITAL ENGINE CONTROL SYSTEMSSDR 1UPA20220419038Controller · defectiveDEFECTIVE FLIGHT CONTROLLERSDR CALA2022041801011Computer · inoperativeA/T LIMIT INDICATION SHOWS ON AUTOTHROTTLE THRUST MODE DISPLAY ADDED INFLIGHT FAULT 01 DISPLAYED ON CDU PERFORMED A/T BITE, CURRENT STATUS NO FAULTS. PERFORMED EEC BITE AND THRUST LEVER - T/R POS ADJ TEST IAW AMM 73-21-00-700-806-F00, NO FAULTS NOTED. REPLACEDSDR QR9R20220318002Actuator · fault messageFLT 1 : ACTUATOR LIGHT CAME ON INTERMITTEDLY IN FLIGHT. T/F EVAL REVEALED ACTUATOR CAUTION ADVISORY ILLUMINATED IN FLIGHT ALONG WITH AN AMBER Y ON THE PFD. REPLACED SEMA ACTUATOR IAW AMM 67-20-00, 4-14. COMPLETED MTF IAW AMM 05-60-00, 6-1 MOC OK.SDR QR9R20220318001Gyro · illuminatedBACKUP SAS CAUTION LIGHT ILLUMINATED IN FLIGHT. STAGEFIELD MECHANIC CONDUCTED AN AIRBUS RESET AND CAUTION WENT OUT. FLIGHT CONTINUED BUT CAUTION LIGHT RETURNED. REMOVED AND REPLACED FIBRE OPTIC GYRO IAW AMM 22-10-00, 4-5. T/F SUCCESSFULLY COMPLETED.SDR AALA202203180278None · noneAIRCRAFT WAS GROUNDED: IN FLIGHT, LOST FLIGHT DIRECTOR 1 AND 2, AUTOPILOT 1 AND 2. AUTOTHROTTLE INOPERATIVE AND NO FLIGHT MODE ANNUNCIATOR. FLIGHT DECLARED AN EMERGENCY LANDING SAFELY AT PHX. RESET #1 FMGC. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECKS OF FLIGHSDR AALA202203167348Computer · false indicationAIRCRAFT WAS GROUNDED: Ï¿½AUTO FLT A/THR OFFÏ¿½ ECAM DISPLAYED AFTER TAKEOFF. AUTO THROTTLE WOULD NOT RE-ENGAGE. BOTH FLIGHT DIRECTORS FAILED AND WOULD NOT RESET. FLIGHT RETURNED TO ABQ LANDING SAFELY. ACCOMPLISHED SATISFACTORY AUTOMATIC FLIGHT SYSTEM TEST AS SDR HALA2022031000073None · noneETOPS - FO CONSTRAINT BUTTON CRACKED // REMOVED AND REPLACED FLIGHT CONTROL UNIT PER AMM 22-81-12. AFS TEST GOOD. LAND CAT 3 TEST GOOD. OK FOR SVC.SDR QR9R20220302001Actuator · failedAP TEST FAILED. AP2 AND TRIM WOULD NOT PASS TEST DURING AIRCRAFT RUN-UP. REPLACED YAW TRIM ACTUATOR IAW AMM 22-10-00, 4-9. MTF MOC COMPLETE IAW RFM & AMM 67-20-00,5-1SDR QR9R20220301001Actuator · illuminatedON RUN-UP, THE YAW SAS AND BACKUP SAS CAUTIONS WOULD NOT EXTINGUISH. AVIONICS WAS ABLE TO GET THEM TO TURN OFF. AFTER TAKEOFF THE ACTUATOR CAUTION ILLUMINATED AND DID NOT EXTINGUISH. 0 VDC PRESENT AT AFCS CONNECTOR J75537 PIN 17; INDICATING YAW SEMA REQUIRES RSDR QR9R20220225001Actuator · failedUPON TAKEOFF INTO HOVER, A TRIM YAW FAILED. A TEST FLIGHT EVALUATION REVEALED YAW TRIM REPEATEDLY FAILED IN FLIGHT. REMOVED AND REPLACED YAW TRIM ACTUATOR IAW AMM 67-14-00, 4-1.SDR AALA202202227326Computer · defectiveAIRCRAFT WAS GROUNDED: NOTICEABLE PULSATING PULL TO THE LEFT ON TALE OFF ROLL, AT CRUISE AP ON 1.8 UNITS LEFT, RUDDER TRIM. AT LF 230 310 KIAS L 1.6 AT 4,000FT 250 KIAS L 1.6 THRUST SYMMETRICAL AND ENGINE NORMAL. REPLACED #1 FLIGHT AUGMENTATION COMPUTER AND SDR QMLA2022021020009None · noneAFTER CLIMB OUT FROM BASE AIRPORT (KCPS), PILOT BEGAN LEVEL OFF TO ASSIGNED ALTITUDE USING THE FLIGHT DIRECTOR AND ARMED ALTITUDE SELECTOR FOR LEVEL OFF. PRIOR TO REACHING THE ASSIGNED ALTITUDE PILOT ENGAGED THE AUTO-PILOT FOR CAPTURE OF ALTITUDE FOR LEVEL OFFSDR UIEA2022020800097None · noneITEM #1 POSSIBLE 5G INTERFERENCE AUTO THROTTLES ATTEMPTED TO TRANSITION TO IDLE AT 100 FT AGL.(<P>PERFORMED LEFT, RIGHT AND CENTER RADIO ALTIMETER OP'S TEST, ALL TEST PASSED, PERFORMED LEFT AND RIGHT AUTO THROTTLE SYSTEM TEST, ALL TEST PASSED IAW B777 AMM 22-3SDR AALA202202077845None · noneAIRCRAFT WAS GROUNDED: AIRCRAFT REPORTED DURING CLIMB WITH NO FAULT MESSAGES. AIRCRAFT SKIPPED FROM TAKE-OFF (CLIMB) MODE TO DESCENT MODE WHILE CLIMBING OUT OF MIA. DFDR DOWNLOAD EVALUATED BY ESC NO ABNORMALITIES OBSERVED PER ESC CHIEF DISPATCH FOUND NO ISSUESSDR QR9R20220124003Actuator · warning lightIN FLIGHT, AFTER 25 MINS, ACTUATOR CAUTION CAME ON CAD. LANDED, MAINTENANCE DID RESET, PULLING PITCH CAUTION CAME BACK ON. T/F EVALUATION REVEALED YAW SERVO LIGHT ILLUMINATES WITH ANY AMOUNT OF COLLECTIVE INPUT. REPLACED YAW SEMA ACTUATOR IAW 67-20-00, 4-8. TESDR AALA202201214603Fcu · noneAIRCRAFT WAS NOT GROUNDED: DUEL FCU FAILURE INFLIGHT. COMPUTER RESET ACCOMPLISHED. FCU #2 RESTORED. FCU #1 REMAINED INOPERATRIVE. AN EMERGENCY WAS DECLARED ON APPROACH TO LGA AND FLIGHT LANDED SAFELY. RESET FCU #1 PER TSM 22-81-00. NO FAULTS NOTED.SDR AALA202201182145Fcu · noneAIRCRAFT WAS NOT GROUNDED: AT FL 320 W/6000 SET IN FCU ,SELECTED MANAGED DESCENT .AC WENT TO CLIMB POWER AND CLIMBED 500 -700 FEET ABOVE FL320 .WOULD NOT DESCEND IN MANAGED UNTIL BELOW FL 280.AIRCRAFT IN DESCENT MODE ON PERFORMANCE PAGE.. NO PFR FAULTS NOTED-SDR CALA2022010500035Autothrottle Sys · failedAUTO THROTTLES FAILED TO ENGAGE ON TAKEOFF THRUST MANAGEMENT SYS (INCLUDING A/T SYS) PLACED ON MEL. MEL STICKER AND C/B COLLARED F16 ON THE P11. DOWNGRADED A/C TO "AUTOLAND LIMIT-LAND 2". DISPATCH DESK: 82 NAME: JERRY DATE: 02-JAN-22- NOC SDR QR9R20211210001Actuator · illuminatedDURING AN IFR FLIGHT, ACTUATOR LIGHT ILLUMINATED RESULTING IN A PRECAUTIONARY LANDING. A TEST FLIGHT EVALUATION REVEALED 15 MINUTES INTO FLIGHT DURING DECENT FROM 3000FT TO 2000FT, THE ACTUATOR LIGHT ILLUMINATED AND REMAINED ON FOR THE DURATION OF FLIGHT. NO ASDR HALA2021121000185Fmc · inoperativeETOPS - MCDU WENT INTO INDEPENDANT MODE // PERFORMED AFS TEST AND FMGEC 1 FAIL. R/R FMGEC 1 PER A330 AMM 22 -83-34. AUTO LAND TEST PASS. AC OK FOR SVC. COMPUTER, FMGEC OFF 43-2283-9-0002 S/N 03010 ON 43-2283-9-0002 S/N 00739SDR AALA202112017940None · noneAIRCRAFT WAS GROUNDED: UNCOMMANDED YAW INPUTS AT FL260 DURING TURN AND AT FL200 DURING DESCENT, NO TURN. **SUPPLEMENTAL REPORT WILL BE SUBMITTED ** (OPEN)SDR A6WA202111297997None · noneWHILE ENROUTE TO PWM THE CREW REPORTED RECEIVING A STAB TRIM AND MACH TRIM CAUTION. THEY DECLARED AND EMERGENCY AND WILL CONTINUE TO PWM. AT FL310 RECEIVED STAB & MACH TRIM CAUTIONS. C/W QRH, TRIM WOULD NOT RE-ENGAGE. ***AIRCRAFT REMOVED FROM SERVICE*** SDR AALA202111294751Computer · unserviceableAIRCRAFT WAS GROUNDED: AIRCRAFT HAD A BRIEF UNCOMMANDED RIGHT RUDDER INPUT AT CRUISE ALTITUDE. AIRCRAFT BANKED ABOUT 5 DEGREES RIGHT AND YAWED SIGNIFICANTLY RIGHT THEN RETURNED IMMEDIATELY TO LEVEL FLIGHT. EMERGENCY DECLARED, FLIGHT DIVERTED TO DFW, LANDING SASDR ABXA20211122122None · noneAUTOTHROTTLE DISC LIGHT CAME ON DURING PUSHBACK RETURNED TO GATE AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE CONDUCTED TEST 02 AND 10, NO FAULTS FOUND. REF AMM 22-00-02. A/C RELEASED PENDING TEST 30/40 TO CAT I PLACARD ROTATED.CONDUCTED TEST 30/40 PER AMM 22-SDR 9JLA2021111731071Autopilot Sys · failedTHE FLIGHT CREW REPORTED THAT DURING AIRCRAFT POWERUP THE NO2 YAW DAMPENER DISPLAYED INOPERATIVE. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE AUTO-PILOT CONTROLLER WAS DEFECTIVE AND WAS REPLACED WITH AN OVERHAULED CONTROLLER. OPS CHECKS WERE SATISFACSDR HALA2021110500154None · noneETOPS - FOUND MCDU #3 BRT/DIM BUTTON BROKEN // REMOVED AND REPLACE MCDU #3 PER AMM 22-82-12. OPS TEST GOOD. NO DEFECT NOTED. OK FOR SVC UNIT, DISPLAY, OFF 33-2282-9-0003 S/N 53441 ON 33-2282-9-0003 S/N 49347SDR CALA2021110502037None · inoperativeCAPTAIN STATED, ON INITIAL LEVEL OFF AT 5000 FT OUT OF HNL, LEFT AUTO THROTTLE UNABLE TO RETARD THRUST BACK TO MATCH RIGHT ENGINE. AFTER AUTO THROTTLE DISCONNECTION UNABLE TO MANUALLY RETARD THROTTLE TO MATCH RIGHT SIDE ALSO. LEFT THROTTLE WAS 20 PERCENT N1 HISDR ENHA LP196783Autopilot Sys · abnormalPILOT REPORTED: AUTOPILOT ENGAGED UNCOMMANDED AND PITCHED AIRCRAFT NOSE DOWN. AUTOPILOT WOULD NOT REMAIN DISENGAGED. MAINTENANCE HAS NOT TROUBLE SHOT SYSTEM TO DETERMINE CAUSE OF FAILURE. AUTOPILOT SYSTEM WAS INSTALLED 74.4 HOURS AND 32 DAYS BEFORE OCCURRENCE.SDR CALA2021100101759None · noneDURING INTIAL CLB AUTO THROTTLE DISARMED ON IT S OWN. AFTER RE-E NGING A/C ACCELERATED TO UNCOMMANDED SPEED. (CONTINUED LANGUAGE FROM LP 7143700) REF LP 7146211 FOR CORRECTIVE ACTION. ENG IDG WAS RUN AND PROVIDED CLEAN PWR. ACP''D A/T MCDP TEST 2 TMC REF 22-00SDR AALA202110016250Computer · faultedAIRCRAFT WAS NOT GROUNDED: DURING CLIMB OUT HAD NUMEROUS MASTER WARNING LIGHT AND CHIME WITHOUT A CORRESPONDING ECAM MESSAGE. REPLACED #2 SPOILER ELEVATOR COMPUTER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 27-94-00.SDR 9WGA2021091154602Unknown · multiple failINITIAL CLIMB OUT, SIMULTANEOUS FAILURE 3 SYSTEMS - RADAR ALTIMETER "ERRONEOUS AUDIO ALTITUDE", AUTO PILOT 1 & 2 FAIL - AUTO THROTTLE.SDR QR9R20210827002Actuator · warning messageACTUATOR LIGHT CAME ON WHILE HOVERING AT PAD; MAINTENANCE ATTEMPTED RESET BUT COULD NOT CURE. DURING T/F EVALUATION FOR ACTUATOR CAUTION, APPROXIMATELY 15 MINUTES AT A HOVER AND THE AP1 &AP2 ON, YAW A TRIM, CYCLIC A TRIM AND FORCE TRIM ON; RECEIVED NO ACTUATORSDR QR9R20210825002Actuator · faultedDURING FLIGHT, ACTUATOR CAUTION ON CAD WITH AMBER Y ON PFD. DURING MULTIPLE AP TEST ATTEMPTS, THE AP TEST WOULD NOT FINISH AND YIELD AN "AP TEST OK". INSTEAD, THE AP2 AND ACTUATOR WOULD APPEAR ON THE CAD ALONG WITH DFACTO XXXXX2 APPEARING ON THE SYSTEM STATUS SDR QR9R20210824001Actuator · warning messageACTUATOR, AP1 ILLUMINATED DURING FLIGHT; ACTUATOR ILLUMINATED ON/OFF DURING MANEUVERS. TF EVAL: APPROXIMATELY 10 MINUTES IN TO FLIGHT, ACTUATOR CAUTION APPEARED WITH AMBER Y ON PFD. NO CODES DISPLAYED ON SYSTEM STATUS PAGE.SDR AALA202108243438Autopilot Sys · faultedAIRCRAFT WAS NOT GROUNDED: AT TAKE OFF PLUS 3:45 HED ON ND WARNING "OFF SIDE FM CONTROL" AT FL 330. "NAV" TRANSITIONED TO "HEADING" UNCOMMANDED. REVIEWED QRH PAGE 3-4 AND SWITCHED TO AUTO PILOT#2. PROBLEM SELF CLEARED AND RETURN TO AUTO PILOT #1. RESET FMGC 1SDR 9WGA2021081041501Unknown · unknownLOST AUTOPILOT AND FCP SELECTION DURING DEPARTURE. AIR TURN BACKTO ICN DUE TO ABOVE DESCRIPTION.SDR QR9R20210728001Trim Cylinder · no indicationDURING FLIGHT, CYC A TRIM OFF INDICATION DOES NOT ILLUMINATE WHEN SWITCHED OFF. AMBER INDICATION ON PFD SHOWS OFF WHEN SELECTED.SDR QR9R20210719001Actuator · warning messageACTUATOR ADVISORY ILLUMINATED IN FLIGHT. TEST FLIGHT EVALUATION REVEALED ACTUATOR CAUTION WITH AN AMBER Y APPEARED AT A HOVER. IN CRUISE FLIGHT AIRCRAFT CONSTANTLY HUNTS FOR THE HEADING WITH HDG IN AMBER WITH HEADING ENGAGED.SDR QR9R20210623002Motor · failedDURING PRE-FLIGHT, AP TEST FAILED FOR TRIM. DURING TROUBLESHOOTING, DETECTED YAW RVDT EXCEEDED 25.5 DEGREES BOTH WAYS. YAW TRIM MOTOR WAS DEEMED BAD PER AIRBUS REP. PART ACCUMULATED 3 HOURS SINCE REPAIR.SDR QR9R20210623001Motor · ratchetingDURING PREFLIGHT, MTF DETECTED PILOTS SIDE R/H TAIL ROTOR PEDAL TO HAVE RATCHETING FEEL WHEN RIGHT PEDAL IS FULL AFT DURING INITIAL PUSH FORWARD. CAN HEAR AND FEEL UNDER RIGHT SIDE PANEL.SDR QR9R20210622002Autopilot Sys · no testDURING RUN-UP AUTO PILOT FAILED TEST. TEST FLIGHT EVALUATION REVEALED AIRCRAFT FAILED AP TEST WITH ACTUATOR/YAW SAS/BACKUP SAS CAUTIONS ON CAD.SDR QR9R20210622001Actuator · warning messageFAILED AP TEST DURING RUN-UP. DURING T/F EVAL WITH ALL AVIONICS POWERED ON, ACTUATOR MESSAGE ON CAD WITH YAW DISPLAYED ON PFD AND AP1 AND AP2 BOTH TURNED ON. WHEN CONDUCTING AP TEST, HAD AP1, AP2, YAW SAS, ACTUATOR AND BACKUP SAS DISPLAYED ON CAD WITH YAW DISPSDR UG8A21P04261349JFI/O Module · malfunctionedRED TRIM ANNUNCIATOR ILLUMINATED CONTINUOUSLY DURING ALL MODES OF FLIGHT, CLIMB, CRUISE AND DESCENT. THE LIGHT WOULD ILLUMINATE SHORTLY AFTER AP WAS ENGAGED. WE VERIFIED AIRCRAFT WAS PERFECTLY TRIMMED PRIOR. THE AP KEPT ADDING NOSE-UP TRIM, EVEN WHEN NOT RESDR DALA2021042102337Fault Message · odorSHIP 3144 - AFTER T/O IN KATL GOT F/CTL ELAC 2 PITCH FAULT . ON LANDING AT KXTP GOT SAME FAULT AGAIN. ON RESET CAPTAIN SMELLS BURNING ELECTRICAL FUMES. CORRECTIVE ACTION: C/W NO GO ODI ATA 2172 W/C. NO DISCREPANCIES FOUND OR ODORS. AIRCRAFT OK FOR SERVICE.SDR AALA202104139022Display · malfunctionedAIRCRAFT WAS NOT GROUNDED: FLIGHT CREW ABORTED TAKE OFF AT 80 KNOTS DUE TO FLEX IN COLUMMN 1 BLANK. MAINTENANCE RESET BOTH FMGCS AND RELOADED FLIGHT PLAN. FMGCS BITE TESTED OK PER AMM 27-96-00.
Back to JASC 2200