JASC 2211
Service difficulty reports · 588
Reports filed under 2211 · Autopilot Computer, 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 = '2211' 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 = '2211' 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 AALA201704049011Fmc · false indicationREJECTED TAKEOFF AT APPROX. 50 KTS, DUE TO MASTER CAUTION, ECAM, GPWS FAULT AND ECAM BRAKE HOT, MLG WHEEL NR 3 INDICATED 995 DEGREES, THEN AMBER XX, FIRE DEPT PERSONNEL MEASURED WHEEL 3 TEMPATURE AT 97 DEGREES F, WHILE STOPPED ON RUNWAY, FMGC 1 INDICATED INOPESDR A6WA2017020344780Servo · malfunctionedAT 1000FEET, FIRST OFFICER DISENGAGED AUTOPILOT, CAVALRY CHARGE SOUNDED, BUT AUTOPILOT DID NOT ACTUALLY DISENGAGE UNTIL CONSIDERABLE FORCE WAS APPLIED TO CONTROL YOKE, HE PUSHED FORWARD AND A LOUD POP SOUND WAS HEARD.SDR AALA20161228024A/C Pack · faultyAIRCRAFT NOT GROUNDED. AUTOPILOT MADE AN UNCOMMANDED DESCENT IN VERTICAL NAVIGATION PATH FL380, NEGATIVE TURBULENCE, CENTER AUTOPILOT ENGAGED IN COMMAND DESCENT STOPPED WHEN ALTITUDE HOLD SELECTED. REMOVED AND REPLACED FLIGHT CONTROL COMPUTER IAW AMM 22-11-01SDR SCNA20161223377Sensor · misinstalledON CLIMOUT IN HDG MODE AP ENGAGEMENT CAUSED A VIOLENT TURN TO THE RIGHT. DISCONECTED AP AND TRIED CMD A AGAIN WITH SAME RESULT. WE TRIED CMD B WITH SAME RESULT. DISCONECTED AP AND DID NOT ATTEMPT AGAIN. FOUND AILERON SENSOR INTALLED 180 OUT. TRANSFERD AND ACCSDR HALA2016122000556Computer · faultedFM2 FAULT ON ECAM. REMOVED AND REPLACED FMGEC2 PER AMM 22-83-34 . AFS TEST PASSED, LAND 3 CAPABILITY TEST PASSED. OK FOR SERVICE. COMPUTER, FMGEC OFF 43-2283-9-0002 00740 ON 43-2283-9-0002 03002SDR FDEA201612064346Computer · failedON TAKEOFF ROLL AT 80 KTS HAD "ALT" MISCOMPARE ALERT AND REJECTED TAKEOFF. COMPLIED WITH QRH. ALERT CLEARED AT 60 KTS. ATTEMPTED SECOND TAKE OFF WITH SAME RESULTS AND A MOMENTARY LEVEL 1 WINDSHEAR DETECT FAIL MESSAGE. COMPLIED WITH QRH AND TAXIED BACK TO RSDR AALA201611099002Controller · misalignedAIRCRAFT WAS NOT GROUNDED. ABORTED TAKEOFF INVALID DATA ON MCDU. MAINTENANCE REALIGNED FMGC'S AND PERFORMED SATISFACTORY LAND CAT CAPABILITY TEST PER AMM 22-97-00.SDR HALA2016102500376Computer · malfunctionedETOPS SIGNIFICANT SYSTEM, FM ON CAPTAINS SIDE DOES NOT CALCULATE FUEL REMAINING AND TIMES
OVER WAY POINTS. RESET FMG EC 1 AND 2. PERFORMED AFS BITE TEST. TEST OK. OK FOR SERVICE AMM 22-96-00.SDR ASOA20160927053CController · faultyTHE CREW REPORTED A VERY STRONG ODOR OF ELECTRIC BURNING IMMEDIATELY AFTER DEPARTURE. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLIGHT GUIDANCE CONTROLLER, OPERATIONAL CHECKS WERE GOODSDR SWAA2016082355059Rod · out of adjustPASSING 17,000 IN CLIMB ON AUTO PILOT B IN VNAV AND LNAV, AIRCRAFT BEGAN ROLLING LEFT REQUIRING MANUAL INTERVENTION. DISCONNECTED AUTOPILOT B, RE-ESTABLISHED LATERAL CONTROL. ENGAGED AUTOPILOT BUT ONLY HAD "CWS" MODE EVENTUALLY LOST BOTH AUTOPILOT B & A ANDSDR FDEA201607052278Computer · malfunctionedON DEPARTURE AFTER RT AUTOPILOT WAS ENGAGED FOR A FEW SECONDS. ACFT MADE A RAPID ROLL TO THE RT AND A/P DISENGAGED. ATTEMPTED TO ENGAGED A/P SECOND TIME WITH SAME RESULTS. ALL OTHER A/P'S WORK NORMAL, CORRECTION A/P DIDNOT DISENGAGE, F/O HAD TO DISENGAGE ITSDR AALA201605029012Computer · malfunctionedAIRCRAFT WAS NOT GNDED. LOST PRESSURIZATION AT 3500, SELECTED MANUAL. EVALUATED & FOUND NO CABIN PRESS FAILURES ON POST FLIGHT. CABIN PRESS LDG ELEV FAULT CAUSED BY LOSS OF FLIGHT MANAGEMENT GUIDANCE COMPUTER, FMGC 1. RESET FMGC. OPERATIONAL CHECKED NORMASDR FDEA201604131201Computer · failedSTAB TRIM WAS SET AT 6.2 FOR TAKEOFF WHICH WAS IN THE MIDDLE OF THE GREEN BOX. AT 80KTS STAB FLICKERED TO 6.2, WENT AMBER, STAB TRIM AURAL WARNING WENT OFF TWICE, REJECT AT 95 KTS. REVIEWED FCC 1 & 2 CURRENT & FAULT REVIEW, NO CURRENT FAULTS & LAST LEG TO HASDR AALA20160404003Computer · faultyAIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING FLIGHT MULTIPLE SYSTEMS BECAME UNAVAILABLE, INCLUDING MACH TRIM, SPEED TRIM, AUTO THROTTLE & CAPTAINS FLIGHT DIRECTOR. ACCOMPLISHED BITE OF FLIGHT CONTROL COMPUTER A WITH FASDR WX0A2016040173117Computer · malfunctionedON CLIMB OUT, DUAL PLATFORM FAIL WAS INDICATED AFTER LOSING FLIGHT DIRECTOR, AUTO THROTTLE & AUTO PILOT. SYS CAME BACK AFTER 25 MIN RETURN TO FIELD. BOTH 1 & 2 VG'S, NR 1 DFGC R & R & WIRING CHECKS OF VGS SEE LOG PAGE 677417 & WO 293781, 293769, 293770 & 29SDR HYIA20160122001Computer · faultyPILOT REPORTED ELEC SMELL IN THE COCKPIT 15 MINUTES INTO FLIGHT. INSPECTED & FOUND THE AUTOPILOT COMPUTER TO BE AT FAULT. R & R AUTOPILOT COMPUTER.SDR CA160120018Computer · failed(CAN) AUTO-PILOT ENGAGED BY ITSELF. ADDITIONAL INFORMATION TO COME. AUTO-PILOT STC HOLDERS ARE TROUBLESHOOTING SYS. TROUBLESHOOTING INSTRUCTIONS HAVE BEEN FORWARDED TO CLIENT. NO FURTHER ANOMALIES REVEALED, DIGITAL FLIGHT CONTROL COMPUTER SENT OUT FOR INVESTISDR FDEA201512274099Computer · inoperativeDURING CLIMB OUT, FCC 2 B DATA FAULT, LEVEL TWO ALERT DISPLAYED. QRH PROCEDURE APPLIED. CURRENT FAULT ON SENSOR READ OUT SHOWS FCC 2 FAULTED. FCC 2 CURRENT FAULT SHOWS FCC 2 FAULTED. CARRIED OUT INSPECTION AT FCC 2 AVIONICS RACK BACK SHELL SOCKET PINS & WISDR CA151106003Computer · failed(CAN) FLIGHT CREW REPORTING ACFT OSCILLATING PITCH UP TO 200 FT. RESOLUTION ALL 3 FCC`S REPLACED IAW AMM TASK 22-11-01, PB 401. CHECK SERVICEABLE.SDR CA150916008Fmc · failed(CAN) DURING THE DESCENT THE CREW EXPERIENCED A DUAL FMGC FAILURE. APPROACH AND LANDING WAS UNEVENTFUL. SYS RESET ITSELF ONCE ACFT WAS ON THE GROUND. RESOLUTION FMGC 1 AND 2 REPLACED AND TESTED SERVICE IAW AMM 22-83-34 PB401,SDR CALA2015082894242Computer · malfunctionedAT F340 LEVEL OFF SELECTED, VNAV & AUTO PILOT ABRUPTLY NOSED DOWNWARD. RT FCC FAULTED IAW FIM FAULT TREE. R & R RT FCC, LOAD SW, OPERATIONS CHECKED GOOD.SDR AALA20150730005Computer · faultyAIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL & AIRCRAFT OVERWEIGHT. DURING CLIMB CREW ENGAGED VNAV & SIMULTANEOUSLY LOST BOTH THE CAPTAIN’S & FIRST OFFICER`S FLIGHT DIRECTORS. R & R NUMBER 1 FCC COMPUTER IAW AMM 22-11-33. ALL REQUIRED TESTS PASSED.SDR CALA2015062600529Computer · failedAFTER TAKEOFF MULTIPLE FAILURES IN NR 1 NAV SYS INCLUDING NO F/D, PWS FAIL, CONTINUOUS WARNING HORN, UNSILENCEABLE, BOTH F/D INDICATED "MA", RADIO ALTITUDE INOPERATIVE, NR 1 SPEED BUG INOPERATIVE. FOUND FCC-A FAILED, REPLACED FCC-A IAW MM22-11-33. OPERATIONSSDR CA150611001Computer · failed(CAN) CLIMBING THRU 27000 FT AT SPEED OF 262 KTS, UNCOMMANDED CHANGE TO A SPEED OF 106 KTS. ACFT STARTED TO PITCH UP TO ACQUIRE THAT SPEED. CAPTAIN ASSUMED MANUAL CONTROL & RESET SPEED.SDR ABXA20150528065Computer · malfunctionedFUMES IN COCKPIT AFTER LOSS OF AUTOPILOT. REPLACED FAULTY CTR FLIGHT CONTROL COMPUTER.SDR CALA2015051193763Computer · malfunctionedLOSS OF NR 1 ILS, FLIGHT MGMT & GUIDANCE CMPT FMGC NR 2 INOPERATIVE. ACCOMPLISHED RESET OF FMGC 1/2. ACCOMPLISHED AFS TEST IAW AMM 22-96-00-501. AUTOLAND DOWNGRADED.SDR FDEA201504051154Computer · failedFCC NR 1B DATA FAULT ALERT, NR 1 AUTOPILOT UNAVAILABLE. ACCOMPLISHED QRH AT ARRIVAL DEBRIEFED WITH CREW & FOUND FCC NR 1B STILL IN FAULT, WAS UNABLE TO ACCESS THE NR 1 FCC VIA CFDS. RESET BOTH CB'S OF FCC NR 1 & WAS ABLE TO ACCESS FCC NR 1. CHECKED FCC NRSDR WX0A2015021672413Computer · malfunctionedRUDDER OSCILLATION FELT ON CLIMB OUT. TRIM WAS MOVING RAPIDLY BETWEEN L 0.2 & L 0.4. MOVEMENT FELT IN RUDDER PEDALS WITH AP1 ON , AP2 ON & AP OFF. OSCILLATION MORE PRONOUNCED ON APPROACH AT LOW SPEEDS. TRIM MOVED RAPIDLY BETWEEN L 0.2 & R 0.4. R & R FAC 1SDR USAA2014121500002Computer · faultyAIRSPEED WENT FROM V2+15 TO VLS-15 AT 500' MSL, AUTO PILOT ON AUTO THRUST ON, FLAPS 2. AIRSPEED TREND ARROW WAS BELOW 2 PROT UNTIL AUTO PILOT WAS MANUALLY DISCONNECTED & HAND FLOWN. REPLACED THE NR 2 FLIGHT AUGMENTATION COMPUTER.SDR USAA2014120900001Computer · malfunctionedAVIONIC SMOKE ECAM, FOLLOWED QRH & ECAM PROCEDURE. FOUND SMOKE SOURCE TO BE NR 2 FLIGHT MANAGEMENT & GUIDANCE COMPUTER. REPLACED NR 2 FLIGHT MANAGEMENT & GUIDANCE COMPUTER IAW AMM 22-83-34. ACCOMPLISHED OPERATIONS TEST IAW AMM 22-96-00 & 22-10-00. ALL CHECSDR AALA20141023009Computer · faultyAUTOPILOT WOULD NOT ENGAGE IN CRUISE. THE FLIGHT DIRECTOR WAS ON MEL & THE LMP STATUS WAS DOWNGRADED. FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED SYS B FLIGHT CONTROL COMPUTER. SYS GND CHECKED NORMAL OPERATION CLOSED.SDR SIMA20141003003Computer · malfunctionedDURING CRUISE AT 360 IN STRAIGHT & LEVEL FLIGHT. AP DISCONNECTED & BEGAN A RIGHT TURN & A 400 FT DECENT FLIGHT CREW CORRECTED & RETURNED TO CRUISE COURSE & ALT, NO AP AURAL WARNING WAS NOTED. RECONNECTED AP & IT WORKED NORMALLY WE DISCONNECTED IT MANUALLY & SDR CALA2014071191442Computer · malfunctionedFMGC NR 1 INOPERATIVE. R & R NR 1 FMGC IAW MM 22-83-34-000-001-A & 22-83-34-400-001-G. PERFORMED OPERATIONS TEST OF LAND CAT III CAPABILITIES IAW 22-97-00-710-001-A. LAND TEST PASSED, ACFT REMAINS FULLY CAT CAPABLE.SDR 9JLA201405281691Computer · defectiveTHE CREW REPORTED THAT THE AUTO PILOT PITCH TRIM HAD FAILED DURING FLIGHT DURING A TRIP TO HOME BASE. TROUBLESHOOTING IDENTIFIED THAT THE NR 1 FCC WAS DEFECTIVE & REQUIRED REPLACEMENT. THE DEFECTIVE COMPUTER WAS R & R BY A NO FAULT FOUND OVERHAULED UNIT SN 2SDR 9JLA201405217963Circuit Card · dirtyCREW REPORTED THAT THE AUTOPILOT TRIM FAILED IN FLIGHT. THE MAINTENANCE TEAM POWERED UP THE ACFT & ENGAGED AUTOPILOT, THE LT AUTOPILOT PITCH TRIM FAILED. REMOVED THE FCC CARDS FROM THE IAPS RACK, CLEANED & REINSTALLED CARDS. FAULT CLEARED, NO DEFECTS NOTED.SDR USAA2014041000003Computer · faultyON TAKEOFF, AFTER GEAR RETRACTION, CAPTAIN'S AIRSPEED WENT TO ZERO & THE ALTITUDE WENT TO 50K. NO AUTO THROTTLES EVEN WITH GREEN LIGHT SWITCH ON. FLIGHT RETURNED TO FIELD AT PBI. AFTER LANDING, THE ALTITUDE IN WINDOW WENT TO 500 FEET. R & R FCC CHANNEL B & SDR USAA2014032100017Computer · faultyDESCENDING THRU FL240 AT 320 KNOTS, CREW FELT A TAIL KICK, BUMP, MULTIPLE TIMES. OBSERVED RUDDER ON FLIGHT CONTROL PAGE MOVING RT & LT. DISCONNECTED AUTO PILOT & BUMP CONTINUED. SLOWED ACFT TO 270 KNOTS & IT SUBSIDED BUT FELT IT & OBSERVED IT AGAIN MULTIPLESDR CALA2014030390501Computer · malfunctionedSTATUS MESSAGE DISPLAYED ON EICAS AFDC C & NO LAND 3. MX MESSAGE 22-18802 SHOWN AS ACTIVE, NEED AFDC C MR22412. REPLACED C AFDC IAW AMM 21-11- 01. SOFTWARE CHECKED CORRECT. MESSAGE CLEARED, AIRCRAFT RETURNED TO AUTO LAND 3 STATUS.SDR CALA2014021790384Computer · faultyGPWS TERRAIN FAULT LIGHT. RESET FMGC 1, ACCOMPLISHED AFS TEST IAW AMM22-96-00, FAULT CLEARED.SDR USAA2014020700013Computer · faultyCLT FLT 1729 EN ROUTE PHL TO CLT. C AUTOPILOT COMMANDED AN ABRUPT INCREASE IN PITCH APPROACHING 30 DEGREES & RESULTING RAPID LOSS OF AIRSPEED AT 1400 FT AFTER TAKEOFF, IMMEDIATELY AFTER ENGAGING. MX PERFORMED FAULT ISOLATION PROCEDURES, NO TROUBLE FOUND. RESDR SWIA201436082Computer · faultyAIRCRAFT INITIATED A SEVERE CLIMB TO CAPTURE GLIDE SLOPE, DISCONNECTED THE AUTO PILOT, GOT THE AIRCRAFT STABLE & RESUMED THE APPROACH. WHEN THE AUTO PILOT WAS RECONNECTED, AT APPROXIMATELY 3500 ', THE FLIGHT DIRECTOR COMMANDED A 15 DEGREE NOSE DOWN PITCH. DISDR CALA2014011590162Computer · inoperativeFMGC NR 2 INOPERATIVE, FAILED IN FLIGHT.SDR DBCA2013123100011Computer · faultyAFTER DEPARTURE FROM MKE THE CREW NOTED THAT WHEN THE AUTOPILOT WAS COUPLED TO THE NR 1 FLIGHT DIRECTOR THE AILERONS SEEMED TO, TWITCH, NOT MOVE SMOOTHLY. EVERYTHING WAS NORMAL WHEN COUPLED TO NR 2 FLIGHT DIRECTOR. CREW RETURNED TO MKE. TROUBLESHOT TO AUTOPSDR SWIA201335738Computer · faultyRECEIVED TWO PRONOUNCED RUDDER INPUTS, THEN THE AIRCRAFT BEGAN TO YAW. YAW DAMPER NR 1 DISCONNECTED, THEN RECEIVED YD 1 INOPERATIVE STATUS MESSAGE. FLT 4632 REPLACED FCC COMPUTER & LIGHTING PROTECTION UNIT HIRF LT & RT IAW AMM. PN 622-9815-904, SN ON 719, SSDR CALA2013120293387Computer · faultyAFTER TWO, CONTINUOUS LT & RT YAWING UP TO FL280 LIKE BOTH YAW DAMPERS INOPERATIVE BUT NO EICAS OR LIGHTS. R & R RT YAW DAMP COMPUTER IAW AMM 22-21-04, OPERATIONS CHECKED NORMAL. PERFORMED MCDP TEST 30 IAW AMM 22-00-02, NO FAULTS NOTED, AIRCRAFT REMAINS FULSDR CALA2013100791772Computer · malfunctionedCTR FCC PROBLEM, RTFL UNABLE TO ENGAGE CENTER OR RT AUTO PILOT NO EICAS MESSAGE. TROUBLE SHOT IAW FIM 22-00-02, PREV FLIGHT FAULT, NO INFC FCC C MCDP SHOWN. REPLACED FCC CENTER IAW MM. MCDP GROUND TEST 1 & TEST 56 PASSED.SDR CALA2013092391370Computer · faultyCAT SINGLE ONLY MESSAGE, WITH LOWER ECAM CAT 3 DUAL INOPERATIVE. CYCLED FMGC CB B2 & 17 WITH NO CHANGE, CYCLED MMR 1 & 2 CBS G12 & L7 WITH NO CHANGE, CYCLED ELAC #1 SW & FAULT CLEARED BUT CAME BACK ON & ELAC CB B11 NO HELP. SHUT DOWN BOTH DENGES & CYCLED BOTSDR CALA2013092391363Computer · faultyAUTO FLIGHT YAW DAMPENER STATUS MESSAGE. TROUBLE SHOT YAW DAMPER 1 MSG. NO ASSOCIATED CFDS MSGS. PERFORMED GROUND SCAN OF THE AFS. TEST FAULTED FAC 1. REPLACED FAC 1 IAW MM, OPERATIONS TEST OF THE AFS FAC 1 TEST PASSED.SDR CALA2013082690759Computer · inoperativeCAPTAIN FLIGHT DIRECTOR INOPERATIVE. REPLACED LT FCC IAW MM. ACCOMPLISHED CAT III TEST IAW MM. ACFT RETURNED TO FULL CAT III CAPABILITY.SDR AALA20130720005Computer · faultyBOTH AUTOPILOT DISCONNECTED IN FLIGHT. REPLACED BOTH DIGITAL FLIGHT GUIDANCE COMPUTERS. SYSTEM GROUND CHECKED NORMAL.
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