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.

SDR ASAA11510227Computer · malfunctionedAUTOTHROTTLE DISENGAGES AUTOMATICALLY FAULT CODE 223 130 00. T/S PER FIM FAULT CODE 223 130 00. CURRENT BITE PASSES NO FAULT. A/T SERVO TEST PASSES. PREVIOUS LEG FAULTS ASM 1 RATE MONITOR 4 TIMES ON 2ND FLT LEG. PER FIM 22 31 TASK 805 FCC A SHOULD BE REPLAug 11, 2011 · N586AS · Boeing 737890SDR ASAA11510096Computer · failed"FD" CAUTION FLAG ON CAPTAINS PFD + NO MA LIGHT ON FLIGHT DIRECTOR WHEN CAPTAINS F/D ON SWITCH SELECTED. FCC A CURRENT STATUS BITE FAILS MSG 22 11303 INTERNAL FAILURE. CYCLED FCC A C/B'S, NO HELP. REPLACED FCC A REF MM 22 11 33, OPS CHECK NORMAL.Jul 15, 2011 · N532AS · Boeing 737890SDR UALA2011062903209Computer · faultyNO FLIGHT DIRECTOR INDICATION ON CAPTAINS ADI. LEFT AUTO PILOT INOP DEFERRED PER MEL 2210A. MAINTENANCE PROCEDURE ACCOMPLISHED ACFT DOWN GRADED TO CAT 2 PER MEL. REPLACED LEFT FCC PER MM, TESTED GOOD.Jun 29, 2011 · N646UA · Boeing 767322SDR UALA2011050602239Computer · malfunctionedCENTER AUTOPILOT WENT DISCONNECTED AT FL330-.80. CONTINUED FLIGHT WITH LEFT A-P AND NO CAP FD. HAS HISTORY. PLZ WORK WITH LM8469. RPL- REF LM8469 BITE TEST CHECK OKAY WITH NO NOTICEABLE DIFFERENCE IN READINGS. REPLACED THE CENTER FCC PER MM. ACP'D CAT IIIMay 6, 2011 · N653UA · Boeing 767322SDR CA110502005Computer · malfunctioned(CAN) LOST FAC 1 ENROUTE, HAS SINCE COME BACK. FAC 2 IS ALREADY UNDER MEL. FAC 1, RESET 4 TIMES. FAULT CLEARED.Apr 29, 2011 · Airbus A320211SDR ANCF2011040400076Computer · malfunctionedDURING T/O ROLL FMGC 1 & 2 FAILED. NO V1, VR, NO FD, NO ATHR, RTO. AS PER TSM 22-83-00-810-901 RESET FMGC 1 & 2. PERFORMED AFS TEST ALL PASSED REF AMM 22-91-00-710-001. IN ADDITION, AIRCRAFT WALK AROUND OUTSIDE INSPECTION WAS FOUND NORMAL. RII ITEMApr 22, 2011 · N961AV · Airbus A320214SDR UALA2011032901504Computer · faultyBOTH AP'S INOP WITH RUDDER TVL LIMITER FAULT, BOTH PFD'S ON SAME FAC MESSAGE. FAC 1 IS FAULTED IN CFDS. SWAPPED FAC 1 AND 2. CHECKED NORMAL. REPLACED TAT PROBE 1, ALL SYST CKD NORMAL. CAT III CKD NORMAL IAW AMM. CURRENT POSITIONS. FAC 1, MR22675-126, FACMar 28, 2011 · N460UA · Airbus A320232SDR UALA2011022800967Knob · brokenKNOB ON HEADING ON MCP FELL OFF. REPLACED MODE CONTROL PANEL SYSTEM. SERVICEABLE PER MM.Feb 25, 2011 · N677UA · Boeing 767322SDR ASAA1159063Panel · damagedMCP IAS/MACH WINDOW BACKGROUND HAS CHIPS ALLOWING BACKLIGHTING TO SHINE THROUGH SMALL CHIPS DOES NOT INTERFERE WITH OPERATION. DUPLICATED DEFECT. REPLACED DFCS MCP REF MM 22 11 34, OPS CHECK NML. ALSO ACCOMP DFCS LRU MCP #32 TEST LAND VERIFY NR 49 TEST AND Feb 21, 2011 · N566AS · Boeing 737890SDR NSVA2011029Computer · malfunctionedAPPROXIMATELY 65NM FROM CRW AT 12000 FT, WHILE ON AUTOPILOT AIRCRAFT DID AN UNCOMMANDED ROLL. DISCONNECTED AUTOPILOT AND LANDED AT CRW WITHOUT FURTHER INCIDENT. IN ADDITION TO AUTOPILOT, CREW WAS RECEIVING ERRONEOUS INDIACTIONS ON ADF. REMOVED AND REPLACED AFeb 15, 2011 · N251CJ · Saab 340BSDR CA110215007Transistor · failedA CUSTOMER SENT AUTOPILOT COMPUTER FOR REPAIR WITH THE DEFECT DESCRIPTION A/P WILL NOT DISCONNECT/DISENGAGE. BENCH TROUBLESHOOTING CONFIRMED THAT PITCH BOARD SOLENOID DRIVE TRANSISTOR Q211 WAS LEAKING CURRENT TO THE PITCH AND ROLL SOLENOID OUTPUTS J1922-3. TFeb 14, 2011 · Cessna 208BSDR N5C2011F00000Capacitor · failedAUTOPILOT FAILED DURING DESCENT, PILOT SMELLED ELECTRICAL ODOR/FUMES. PILOT SAW SMOKE COMING FROM AUTOPILOT ENGAGE BUTTON. PILOT PULLED AND SECURED AUTOPILOT CIRCUIT BREAKER, SMOKE CLEARED IMMEDIATELY. AN INTERNAL INVESTIGATION OF THE AUTOPILOT COMPUTER REVFeb 14, 2011 · N811FL · Cessna 208BSDR 2011F00038Capacitor · burnedAUTOPILOT FAILED, PILOT SMELLED ELECTRICAL ODOR/FUMES. PILOT SAW SMOKE COMING FROM AUTOPILOT ENGAGE BUTTON. PILOT PULLED AND SECURED AUTOPILOT CIRCUIT BREAKER, SMOKE CLEARED IMMEDIATELY. AN INTERNAL INVESTIGATION OF THE AUTOPILOT COMPUTER REVEALED A BURNED Feb 12, 2011 · N811FL · Cessna 208BSDR UALA2011012800486Computer · malfunctionedCAPT FLT DIRECTOR DISAPPEARED WHEN CTR AUTOPILOT WAS DISCONNECTED AND NO AUTOLAND 3 APPEARED. REPLACED LT FCC REF MM, ALL CHECKS OK. PERFORMED CATIII CHECK IAW MM AND ALL OPS NORMAL. ACFT RECERTIFIED TO CATIII STATUS.Jan 28, 2011 · N642UA · Boeing 767322SDR 2ARF201101006Rheostat · damagedCAPTAIN REPORTED THAT DURING TAXING AND WHEN IT WAS TURNED WITH AUTOPILOT SELECTED, THE FLIGHT CONTROLS DID VIBRATION. MX PERSONNEL REPLACED THE DUPLEX AILERON SERVO BRACKET RHEOSTAT IAW MM 22-11-01 AND THE DFGS STATUS/TEST (STP) PANEL WAS CHECKED IAW MM 22-01Jan 16, 2011 · N848SH · Doug MD83SDR 2ARF201101004Servo Drive · damagedACFT RETURNED TO PLATFORM DUE TO DURING TAXING AND WHEN IT WAS TURNED WITH AUTOPILOT SELECTED, THE FLIGHT CONTROLS VIBRATED. MX PERSONNEL REPLACED THE DUPLEX SERVO AILERON DRIVER IAW MM 22-11-00 AND THE DFGS STATUS/TEST (STP) PANEL WAS CHECKED IAW MM 22-01-05Jan 14, 2011 · N848SH · Doug MD83SDR WRNA201000007Computer · unserviceableCLIMBING THRU 12K FT, AURAL WARNING "LANDING GEAR" THEN THE INDICATIONS WERE THAT THE GEAR WAS UP AND RETRACTED, HOWEVER, THE AURAL WARNING "LANDING GEAR" NEVER STOPPED. CYCLED THE GEAR BY PUTTING IT DOWN AND BACK UP, WHEN THE GEAR WAS DOWN THE WARNING STOPPEDec 20, 2010 · N952AR · Doug MD11FSDR HYIA26514AP1128Computer · shortedCREW REPORTED, ON FINAL APPROACH, A SMALL PUFF OF SMOKE CAME FROM THE NAV/COM PANEL. CREW ACCOMPLISHED SMOKE IN COCKPIT CHECKLIST, SMOKE QUICKLY SUBSIDED AND NO FURTHER SIGNS OF THE PROBLEM EXISTED. ADVISED THE TOWER, AND LANDED WITHOUT INCIDENT. MX INSPECTNov 28, 2010 · N26514 · Cessna 402CSDR CA101104002Computer · malfunctioned(CAN) FMGC1 FAIL ALL FLAP/SLAT RETRACTION INFO ON NR 1 PFD LOST INSIDE THE MARKER ALL FLAP/SLAT INFO ON NR 2 PFD DISENGAGED. NO FMGC NR 2 FAILURE. MAP NOT AVAILABLE DISPLAYED ON BOTH. BOTH FMGC RESET DONE. FMGC NR 1 REPLACED PER 22-83-34-400-001-A.Nov 3, 2010 · Airbus A320214SDR UALA2010102904014Damper · faultyRT YAW DAMPER INOPERATIVE. ACCOMPLISHED YAW DAMPER SYS BITE. SYS TESTED NORMAL. STORED FLIGHT LEG FAULTS IN RT YAW DAMPER MODULE FAULTING RT YAW DAMPER ACTUATOR. LT YAW DAMPER MODULE HAS NO FAULTS.Oct 27, 2010 · N641UA · Boeing 767322SDR DXTA2010102604271Computer · failedDURING CLIMB OUT OF 28,000 FT, WITH RT SEAT PILOT FLYING, THE ATTITUDE AND HEADING FAILURE MESSAGE ILLUMINATED IN THE LT SIDE PFD AND THE MFD. THE AUTO-PILOT ALSO FAILED. PUSHED THE LT SIDE ATTITUDE AND HEADING REVERSIONARY BUTTONS AND THE RT SIDE INFORMATIONOct 25, 2010 · N686QS · Cessna 560XLSDR HEEA129496Transducer · defectiveENGINE OUT LIGHT AND AUDIO WITH ASSOCIATED YAW KICK ON TAKEOFF. TROUBLESHOT AND FOUND TRANSDUCER DEFECTIVE. REPLACED TRANSDUCER.Sep 28, 2010 · N714P · Skrsky S76CSDR CA100730003Mount · malfunctionedLOSS OF GLIDESLOPE FUNCTION ON S-TEC 55X. ACFT HAS BEEN TO 2 DIFFERENT AMO`S THAT CONCLUDED THAT THE AUTOPILOT COMPUTER WAS AT FAULT. THE UNIT WAS SENT AWAY TWICE AND TESTED BY THE MFG WITH NOT FAULTS FOUND. IT WAS FOUND THAT TRACKING OF THE AUTOPILOT COMPUJul 29, 2010 · Cirrus SR22SDR DALA1016593146Computer · malfunctionedDURING FINAL APPROACH TO ATL RECEIVED LDC CLS 1 A/F Y/D1 MSG AND THEN NOTICED FUMES IN FLIGHT DECK. FUMES BECAME WORSE AFTER A FEW MINUTES AND COULD BE DETECTED THROUGHOUT THE CABIN, LANDING WAS UNEVENTFUL. REPLACED FAC (FLIGHT AUGMENTATION COMPUTER) AND THEJul 16, 2010 · N346NB · Airbus A319114SDR AALA20100710DFW01Computer · inoperativeDFW - CAPTAIN RECEIVED STICK SHAKER INDICATION AFTER TAKE-OFF, SWITCHED FROM CAPT TO FO" FLIGHT DIRECTORS AT FL 10000. WHEN SWITCHED THE STICK SHAKER STOPPED AND AUTO SPOILER EICAS MESSAGE ALERTED. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIJul 10, 2010 · N933AN · Boeing 737823SDR NOCA02310Computer · malfunctionedAILERON LOCKOUT EICAS MSG. ACCOMPLISHED FIM TASK 27-11-00 FIG 104. ACCOMPLISHED BITE CHECKS, ALL CHECKS OK. REF AMM 22-00-02, MCDP TST 07 ACCOMPLISHED, NO FAULTS NOTED. RUDDER RATIO EICAS MSG. ACCOMPLISHED FIM TASK 27-21-00 FIG 104. ACCOMPLISHED BITE CHEMar 1, 2010 · N765NA · Boeing 767306SDR HALA2009120400570Computer · inoperativeETOPS SIGNIFICANT SYS - FD FLAG IN VIEW AND NO FD CMD BARS ON CAP'S ADI. INSTR INDICATION NORMAL W/INSTR SOURCE SEL AT C POS. NO LAND 3 DISPLAYED REMOVED AND REPLACED LT FCC AND OPS CKD OK IAW AMM 22-11-01-004-001 AND 22-11-01-404-007. RAN A TEST 40 AND PASDec 4, 2009 · N586HA · Boeing 7673G5SDR UALA2009100603141Control Panel · frozenMCP IS FROZEN. REPLACED MCP. MCP FOUND FAULTY. REPLACED AUTOPILOT MODE CONTROL PANEL. OP CKS GOOD.Oct 5, 2009 · N671UA · Boeing 767322SDR CHQA200900211Computer · malfunctionedFLIGHT 6025, CVG TO SBN. ON TAKEOFF THE CREW NOTICED A ELECTRICAL BURNING SMELL, UNSURE IF IT WAS JUST IN THE COCKPIT OR IN CABIN ALSO. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TRACED THE SMELL TO THE FLIGHT GUIDANCE COMPUTER. THSep 28, 2009 · N574RP · Emb EMB145LRSDR USAA2009092892645Computer · defectiveFLT 71 PHX-SEA - ATO - TAKEOFF WAS ABORTED AT 80 KNOTS DUE TO THRUST SEQUENCING ECAM WARNING. MAINTENANCE REPLACED NR 1 FMGC RACK CONNECTOR AND BOTH FLIGHT MANAGEMENT GUIDANCE COMPUTERS.Sep 25, 2009 · N622AW · Airbus A320231SDR SWIA200922374Computer · malfunctionedUNCOMMANDED RUDDER INPUTS IN FLIGHT. (FLT 6730) REPLACED FCC CARDS.Aug 12, 2009 · N906SW · Cndair CL6002B19SDR ASAA0956372Computer · malfunctionedB AUTOPILOT DISCONNECTED 3X ARRIVING IN OGG, OK IN CRUISE A AUTOPILOT SELECTED DURING ARRIVAL OK. REMOVED AND REPLACED "B" FCC PER 22 11 33 OPS CHECK NORMAL PER MM PT II 22 11 33/401 TEST NR 35 FOR DFCS LRU INTERFACE TEST FOR FCC. PERFORMED S/W CROSS LOAD FRAug 3, 2009 · N517AS · Boeing 737890SDR DL764091210Computer · malfunctionedRTB, DUE AFTER PUSHBACK F/O PFD SHOWED 0 MAGENTA FOR A/S AND 0 MAGENTA FOR ALTITUDE MCP AND CAPTS PFD SHOWED CORRECT NUMBERS. ALSO PFD SHOWED A/S AND ALT AT 0 /C FWD TO MCO RT FCC. REPLACED RT FCC.Jul 19, 2009 · N831MH · Boeing 767432ERSDR HNAA2009052100159Servo · defectiveELEVATOR TRIM VERY STIFF TO MOVE AND BINDING, UNABLE TO MOVE IT WITH STANDBY SWITCH. REMOVED AND REPLACED ELEVATOR TRIM SERVO.May 15, 2009 · N335EN · Dhav DHC8311SDR 2009FA0001037Computer · malfunctionedA NEW AUTOPILOT SYS WAS INSTALLED ON 2/5/09 AT ACTT 15821.5. PERFORMANCE OF AUTOPILOT WHICH IS CERTIFIED FOR CATEGORY 1 APPROACHES IS VERY POOR AND ERRATIC. AUTOPILOT WILL FLY THE ACFT AS MUCH AS 2 DOTS OFF LATERALLY FROM THE RUNWAY CENTER LINE. AUTOPILOT ALSFeb 5, 2009 · N200NY · Beech C12CSDR HALA2008122200898Computer · malfunctionedETOPS SIGNIFICANT SYSTEM, AUTOPILOT DISCONNECT LIGHT ILLUMINATED. EICAS MESSAGE-AUTOPILOT DISCONNECT DISPLAYED AND LAND 3 DISPLAYED ON ASA. WITH CENTER AP SYSTEM ENGAGED IN COMMAND 2202084 3863 5203 CTR. PERFORMED MCDP TEST, FAULTS NO INFLT. FCC CENTER GRODec 22, 2008 · N598HA · Boeing 767332SDR 2008FA0000887Autopilot Sys · malfunctionedWHEN A DISCREPENCY BETWEEN THE NAVDATA DATABASE & ACTUAL IMPLEMENTATION OF A LOCALIZER NAVAID, GFC700 WILL NOT INTERCEPT & TRACK LOCALIZER SIGNAL CORRECTLY. IT EITHER FLIES THROUGH COURSE OR WILL ACTIVATE LOC MODE & IMMEDIATELY TURN OFF COURSE. AFCS APPEARS Oct 28, 2008 · N510AZ · Cessna 510SDR ASAA0853520Computer · failedAUTOTHROTTLE LIM ILLUMINATED IN CLIMB FROM 370 390 WITH AUTOTHROTTLES ENGAGED. NORMAL OPS WITH AUTOTHROTTLE OFF (NOTE: 2 KNOB SPLIT WITH AUTOTHROTTLE LIMIT ILLUMINATED AND CLIMBING). TS FAULT CODES FOUND AT CURRENT STATUS TEST WOULD NOT ENGAGE. RESET FCC A Sep 18, 2008 · N587AS · Boeing 737890SDR COMA0860323Computer · failedFLIGHT 5675. EN ROUTE FROM VHZ TO BOS FELT AND SAW (1/2 SLIP INDICATOR) UNCOMMANDED RUDDER MOVEMENT. REMOVED AND REPLACED NR 1 FCC. (A)Jul 11, 2008 · N420CA · Cndair CL6002B19SDR 2008FA0000437Trim Switch · failedAFTER INSTALLATION OF NEW MFG AUTOPILOT SYS, AUTOPILOT COMPUTER TRIM CIRCUITRY FAILED ON INITIAL CHECK OUT. COMPUTER WAS RETURNED TO MFG AND REINSTALLED AFTER REPAIR. TRIM CIRCUITRY FAILED AGAIN AND RETURNED TO MFG. MFG TECH SUPPORT ADVISED REPLACEMENT OF SUSJun 18, 2008 · N362MC · Beech C90SDR DXTA200803077Warning System · activated"FGC- B FAIL" CAS MESSAGE CAME ON 45 MIN INTO FLIGHT. DID NOT RESET.May 22, 2008 · N936QS · Cessna 750SDR ASAA0852873Computer · faultySPEED TRIM FAIL AND MACH TRIM FAIL LIGHTS CAME ON DURING RECALL CHECK AFTER ENGINE START. F/O'S FD FLAG ALSO CAME ON. VERIFIED FAULT. FCC "B" COMPUTER INOP. REPLACED FCC "B" COMPUTER. PERFORMED LRU TEST FOR FCC & LAND VERIFY TEST. HGS SENSOR TEST FOR FCCMay 3, 2008 · N570AS · Boeing 737890SDR BB08044Computer · inoperativeMUC FLT 707 - MUC TO PHL. AFTER TAKEOFF, ALL AUTOPILOT SYSTEMS WERE INOPERATIVE. AFTER SEVERAL ATTEMPTS TO RESET, THE FLIGHT RETURNED TO MUC WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CENTER FLIGHT CONTROL COMPUTER. OPERATIONALLY CHECKS OK.Mar 28, 2008 · N256AY · Boeing 7672B7SDR ASAA0852701Computer · malfunctionedCAT IIIA AUTOLAND AIRCRAFT TRACKED AND TOUCHED DOWN APPROX 35' LEFT OF CENTERLINE. NO FLIGHT FAUTLS LOGGED. CURRENT STATUS CHECKED NORMAL. PERFORMED "LAND VERIFY" TEST PG 201. TEST PASSED. PERFORMED HGS SENSOR TEST, ALL NO DEFECTS.Mar 9, 2008 · N558AS · Boeing 737890SDR 68JV02Computer · failedON CLIMBOUT FROM DSM CREW RECEIVED AUTOPILOT PITCH TRIM FAIL ANNUNCIATOR. AIRCRAFT RETURNED TO DSM, LANDING WAS UNEVENTFUL. AFTER LANDING, CREW PERFORMED PREFLIGHT OPS CHECKS OF AUTOPILOT SYSTEM AND COULD NOT DUPLICATE FAILURE. REPOSITIONED AIRCRAFT FROM DSFeb 22, 2008 · N68JV · Beech 400ASDR 2008UALA00147Computer · faultyFLIGHT DIVERTED DUE TO A FAULTING FMGC. FMGC FAILURE (SHOP FINDINGS NFF). REPLACED FMGC, OPS CHECKED NORMAL.Jan 8, 2008 · N824UA · Airbus A319131SDR 2008UALA00051Computer · shortedNO LAND 3 DEGRADATION IN AUTOLAND SYSTEM PRIOR TO APPROACH (BEFORE LAND 3 AUTOLAND STATUS ANNUNCIATION). AUTOPILOT FLIGHT DIRECTOR COMPUTER (RIGHT) A LIVE CIRCUIT IS OPEN OR SHORTED. REPLACED AFDC RT. RT LRU TEST PASSED. RETURNED TO CAT 3 STATUS. AC OK FOJan 3, 2008 · N799UA · Boeing 777222SDR USAASA07082Computer · intermittentCLT - FLT 1480 EN ROUTE MSP TO CLT. DURING THE FLIGHT, AUTOPILOT 2 DISENGAGED. THE CREW RE-ENGAGED THE AUTOPILOT, AND IT DISCONNECTED AGAIN, ALONG WITH AUTOPILOT 1. AFTER HAND FLYING FOR ABOUT 20 SECONDS, THE STAB TRIM WHEEL JERKED WHILE AUTO-TRIMMING, THEDec 11, 2007 · N769US · Airbus A319112SDR 754004Computer · no testAUTOPILOT A WILL NOT ENGAGE AND AUTOPILOT B IS ALREADY DEFERRED. DUMPED FUEL AND DIVERTED INTO RKSI. AUTOPILOT A ROLL COMPUTER DOES NOT PASS SELF TEST. REPLACED AUTOPILOT A ROLL COMPUTER AND AUTOPILOT B MONITOR LOGIC UNIT.Nov 27, 2007 · N754SA · Boeing 747228FSDR 717311162007Computer · failedDURING FLIGHT, YAW CSAS CAUTION LIGHT ILLUMINATED. DIVERTED LANDING FROM HELIPAD TO AIRPORT 4 MILES AWAY. COMPLETED APPROPRIATE EMERGENCY PROCEDURE IAW AFM.Nov 16, 2007 · N155SC · Bolkms BK117B1
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