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 UALA2013070804741Computer · inoperativeLEFT AUTOPILOT, LEFT FCC INOPERATIVE. R & R LEFT FCC COMPUTER IAW MM, OPS GOOD. PERFORMED MCDP TEST 30 AND 40 IAW MM, OPS GOOD. ACFT FULL CAPABLE, NO FAULTS AT THIS TIME.SDR USAA2013070200009Computer · faultyCREW REPORTED "2FD2" AND SET OFFSIDE RANGE 1 MODE MESSAGE IN FLIGHT. ATTEMPTED SINGLE RESET IAW QRH WITH NO HELP. MX R & R NR 1 FMGC (1CA1) IAW AMM 22-83-34-400-001A. INSPECTED E & E RACK CONNECTORS BEHIND FMGC 1. NO DISCREPANCIES NOTED. PERFORMED SATISFACTOSDR USAA2013070100015Computer · faultySTRAIGHT AND LEVEL FLIGHT WITH AUTO PILOT 2 ON AND IN NAV GOING DIRECT TO ELZ AT FL330, THE ACFT SUDDENLY DID AN UNCOORDINATED 20 DEGREE BANKED TURN TO LT THEN BACK TO RIGHT. WE WERE GOING DIRECT TO ELZ FOR APPROXIMATELY 3-5 MINUTES EVERYTHING WAS NORMAL, THESDR SWIA201333772Computer · failedHAD AN UNCOMMANDED YAW MOVEMENT TO THE LEFT. RE-CENTERED TRIM. FLT#5623 REPLACED RT FCC COMPUTER IAW AMM. PN: 822-1308-320 SN ON: 1MNKB SN OFF: 1M2TDSDR USAA2013060400023Computer · unserviceableENROUTE, CREW REPORTED AN UNCOMMANDED MOMENTARY RUDDER INPUT. MX ACCOMPLISHED DFDR DOWNLOAD IAW JC 26T00031001, SHOWS NO ABNORMAL MOVEMENT OF THE RUDDER OR ACFT HEADING. ACCOMPLISHED TSM 27-26-00-810-801A. RESISTANCE AND INSULATION CHECK OF THE LVDT OF SERVSDR UALA2013052803689Computer · faulty"NO LAND 3", EICAS STATUS MESSAGE DISPLAYED. DEGRADATION IN AUTOLAND SYS (NOT LATCHED). REPLACED RT FCC IAW AMM. SYS CHECKS GOOD. SYS NEEDS CAT111.SDR SWIA201333280Computer · failedWITH AUTOPILOT ENGAGED AND HDG MODE SELECTED AIRCRAFT MADE UNCOMMANDED RIGHT TURN. DISCONNECTED AUTOPILOT AND RE-SELECTED HDG MODE. NO FURTHER PROBLEMS. (FLT 6405) REPLACED NR 1 FCC IAW AMM. P/N 622-9815-904 S/N ON 12DKP S/N OFF 2674.SDR UALA2013041102490Computer · malfunctionedAUTOPILOT DISC LIGHT ON & EICAS MESSAGE 'AUTOPILOT DISC' DISPLAYED WITH 2 AUTOPILOT SYSTEM ENGAGED IN COMMAND. AT CRUISE 380 M.80 CTR A-P DISCONNECTED. TRIMMED AND TRIED AGAIN, NO GO, LEFT AND RIGHT AUTOPILOT SYS OK. FOUND FAULT FCC-C. REPLACED CENTER FCCSDR SWIA201333149Computer · failedAIRCRAFT BEGAN A SERIES OF UNCOMMANDED YAWS IN BOTH DIRECTIONS AND BECAME MORE NOTICEABLE UPON DESCENT TO LANDING EVEN WITH AUTOPILOT ENGAGED AND DISENGAGED. (FLT 7374) REPLACED FCC NR 2 IAW AMM. OPS CHECKED GOOD AT THIS TIME. P/N: 622-9815-904 S/N ON: 393SDR UALA2013040102067Computer · faultyF/OS ADI HAS FD FLAG AND NO FD CROSSHAIRS WORKS ON THE LEFT FLIGHT DIR INST SEL. FLT FAULTS NO INFC FCC R MCDP, NO LAND 3 FCCR-FCCL AND FFCR-FFCC. ACCOMPLISHED FIM 22-00-0 2 FIG 110 AND STILL HAS FAULT AND FCC R TEST FAILS. REPLACED FCC R PER MM AND PASSEDSDR SWIA201333118Computer · failedYD 1 STATUS MESSAGE APPEARED AND WOULD NOT RE-ENGAGE. CONTINUOUS AIRCRAFT YAWING PULSATION IN THE RUDDER PEDALS. (FLT 7426) REPLACED NR 1 FCC IAW AMM 22-12-14. ALL FCC OPS TESTS GOOD. YAW DAMPER TEST GOOD. NO UNUSUAL RUDDER PEDAL MOVEMENTS NOTED. NO RESDR CA130211001Computer · failed(CAN) ON APPROACH BETWEEN 200-150 HAD DUEL FMGC FAILURE TWICE MOC ADVISED AND MAINTENANCE WILL MEET ON ARRIVAL REPLACED AND TESTED FMGC NR 1 DUE TO HISTORY IAW AMM - OPS CHECK SERVICE. AUTO LAND TEST PERFORMED. OPS CHHECK SERV.SDR AALA20130209005Computer · malfunctionedMIA - CREW REPORTED YAW DAMPER AND LEFT INERTIAL REFERENCE UNIT FAULTS. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLIGHT CONTROL COMPUTER A. SYSTEM GROUND CHECK NORMAL OPERATION.SDR SWIA201332591Computer · failedUNCOMMANDED ROLL IN FLIGHT, AUTO PILOT WAS HARD TO DISENGAGE. (FLT 6327) REPLACED THE A/P COMPUTER.SDR CA130115004Computer · failed(CAN) PITCH TRIM COMPUTER HAS A 3 AMP FUSE INSTALLED. THE PITCH TRIM MOTOR IS RATED TO DRAW UP TO 6 AMPS UNDER HEAVY LOAD SITUATIONS. ANY TIME PITCH MOTOR DRAWS HEAVY LOAD, INTERNAL PITCH COMPUTER 3 AMP FUSE BLOWS, DISABLING AUTO PILOT SYSTEM. THE MFG IS AWASDR WRNA201300001Computer · unserviceableDURING CLIMB BOTH AUTOPILOT SYSTEMS FAILED. CREW NOT ABLE TO RE-ENGAGE. FOLLOWED PROCEDURES, DUMPED APPROX 50K KGS FUEL TO ACCOMPLISH ACCEPTABLE LANDING WEIGHT. AIRCRAFT RETURNED TO MIAMI WITH NORMAL LANDING. MAINTENANCE FOUND DUPLEX FLAP LIMITER ACTUATOR SDR UALA2012122807446Computer · failedFCC FAIL AFTER SOL REPLACEMENT. WENT BACK WRUNG OUT SERVO FROM FCC. ALL RES CHECKED GOOD SOL CHECKED GOOD NOW. FAILED C F CC ON TEST 7. REPLACED CTR FCC COMPUTER PER MM. RECHECKED PASSES TEST 7 NOW.SDR UALA2012121007141Computer · faultyFAC 2 FAULT AFTER TAKEOFF, FLIGHT DIVERTED. CREW PERFORMED FM RESET, NO HELP. MUST HAVE BOTH FACS OPERATING NORMALLY. REPLACED NR 2 FAC PER MM. ACP TEST PER MM 22-97-00, CHECK'S OK. MAINTENANCE GOOD AFTER SEC AND FAC COMPUTER REPLACEMENT PER OPBLM & MANASDR USAA2012121000012Computer · faultyIN FLIGHT AT FL330, AIRCRAFT YAWED LEFT FOR ABOUT 2 SECONDS, 5 DEGREE BANK THAN NORMAL RUDDER TRIM L 1.3. MAINTENANCE REMOVED AND REPLACED FAC 1 PER AMM 22-66-34-000-002-A. OPS CHECK GOOD. ALSO, REMOVED AND REPLACED ELAC 1 PER AMM 27-93-34-000-001-A. OPS CSDR CA121203002Computer · failed(CAN) REJECTED TAKEOFF APPROXIMATELY 100 KTS ACCOUNT, NO V-SPEEDS. FLIGHT OPS/FLIGHT SAFETY ADVISED. FMGC 1 REPLACED AND TESTED, OK IAW AMM 22-83-34 PB401. LAND TEST PERFORMED SUCCESSFULLY. OK FOR CAT 3 APPROACHES. OBSERVED FMA DATA DISPLAYED NORMALLY DURSDR AALA20121123012Computer · malfunctionedONT - INFLIGHT SJD-LAX. CREW REPORTED BOTH AUTOPILOTS FAILED INFLIGHT. FLIGHT DIVERTED ONT LANDED WITHOUT INCIDENT. PLACARD BOTH AUTOPILOTS PER MEL. FLIGHT CONTINUED TO DESTINATION. REPLACED NUMBER ONE DIGITAL FLIGHT GUIDANCE COMPUTER AND AILERON SERVO DRSDR UALA2012111906642Computer · faultyAUTOPILOT BACKDRIVE L LEFT AUTOPILOT BACKDRIVE SYSTEM INOPERATIVE OR DEGRADED DUE TO FAILURE IN LEFT COLUMN, WHEEL OR PEDAL BACKDRIVE ACTUATOR, LEFT AFDC OR INTERCONNECTING WIRING. STATUS MSG-2214931 ACTIVE CL MODE. LEFT CONTROL COLUMN BACK DRIVE ACT INOP. MSDR SWIA201232033Circuit Card · defectiveWITH AUTOPILOT ON AND SELECTING FLAPS 45, THE AUTOPILOT AUTO TRIM STICKS IN THE NOSE UP DIRECTION. (FLT 4504) REMOVED AND REPLACED NR 2 FCC CARD SYSTEM IAW AMM. P/N: 622-9815-904 S/N OFF: HXWRSDR UALA2012101605911Computer · failedAUTOLAND AP PUMPED THE YOKE WHEN FLARE MODE ENGAGED. MCDP TEST 40 SHOW TLA R FAIL. REPLACE TMC. OP CHECK GOOD CAT 3 CHECK REF AMM. AC RETURNED TO CAT 3.SDR UALA2012091905305Computer · faultyWHILE ACP CAT 3 CHECK HAVE FAULT AIL SERVO RT FAIL. REPLACED RIGHT FCC, AIL TESTED OK.SDR 9JLA2012101804322Computer · faultyCREW REPORTED THE AUTOPILOT INTERMITTENTLY DISENGAGES WHILE IN CRUISE. TROUBLSHOOTING IDENTIFIED THE FGC-3000, AS DEFECTIVE. INSTALLED AN O/H FGC-3000 UNIT, FUNCTIONAL CHECKED SATISFACTORY.SDR SWIA201231628Computer · failedCLIMBING THROUGH 28,000 FT THE AIRCRAFT STARTED A RAPID UNCOMMANDED PITCH UP TO 4,400 FPM. (FLT 4713) REPLACED NR 1 FCC IN REFERENCE TO AMM. P/N: 622-9815-904 S/N OFF: 1N38XSDR UALA2012082004639Control Panel · faultyCENTER AUTOPILOT ENGAGED LIGHT ON WITH NO AUTOPILOT ENGAGED. REPLACED MODE CONTROL PANEL PER AMM, OPS CHECKED GOOD.SDR RJEF2012080703Computer · malfunctionedDURING TAKEOFF FLIGHT TP-09 FROM LIM TO CUZ. AUTOFLIGHT RUDDER TRAVEL LIMITER NR 1 ECAM CAUTION AT 50 KNTS, CAUTION DISAPPEARED, TAKEOFF WAS ABORTED AND RETURNED TO GATE. ACCORDING TO TSM 22-61-00-8110-803-A PERFORMED RESET OF THE FAC 1 AND OPERATIONAL TEST SDR UALA2012072704073Computer · faultedRIGHT AUTOPILOT INOPERATIVE. WILL NOT ENGAGE. NO LAND 3. SUSPECT RIGHT FCC. REPLACED RT FCC. MCDP TEST 01 AND 30, OK. REF MM.SDR UALA2012071103719Control Panel · warning messageMODE CONTROL PANEL FAULT MESSAGE. REMOVED MODE CONTROL PANEL, INSTALLED NEW PERFORMED TEST PER MM.SDR CA120523022Computer · malfunctioned(CAN) FOLLOWING INITIAL INSTALLATION OF THE ST-593 AUTOPILOT IN THIS ACFT, THE CREW WAS ON DESCENT NEAR INSTRUMENT CONDITIONS. THEY DISCONNECTED THE AUTOPILOT USING THE DISCONNECT SWITCH AND THEN ATTEMPTED TO FLY THE REMAINDER OF THE APPROACH USING NORMAL ACFSDR SWIA201230648Computer · failedRECEIVED AP TRIM IS RWD CAUTION MESSAGE AND AIRPLANE MADE AN ABRUPT TURN. (FLT 4829) REPLACED FCC NR 1, FCC NR 2, AHRS NR 1, AND AHRS NR 2.SDR USAA2012031500003Computer · faultyPILOT REPORTED A SLIGHT UNCOMMANDED YAW OCCURRED IN CRUISE FLIGHT. AT GATE, AUTO FLT YAW DAMPER - RUDDER SERVO FAULT APPEARED ON ECAM FOR APPOXIMATELY 5 MINUTES AND THEN WENT OUT. NO FAULTS NOTED ON POST FLIGHT REPORT. MAINTENANCE REMOVED AND REPLACED THE NSDR UALA2012031201609Computer · faultyWHEN USING AUTOPILOT 1FMGC DROPS OUT OF MNGDSPEED AND NAV. REVERTS TO SLCTD SPD AND HDNG :TBLSHT & SUSPECT FAC NR 1. SWAPPED FACS NR 1 & 2 PER MM. NR 2 FAC INOP. A-C IS RMV'D FROM CAT II & CAT III, REF CF982. REPLACED FAC 2 PER MM. SYSTEM TESTS OK. PERFSDR UALA2012030501395Computer · faultyRIGHT FD FAILED AND NO LAND 3 ASA. RIGHT FCC IAW MM & GROUND TEST PASSED. AC FULL CAT III STATUS.SDR UALA2012022301104Computer · failedCAPTIN FLT DIRECTOR NO ROLL MODE SEL RT FLT DIR ROLL MODE RETURNS NO LAND 3 BOTH POSITIONS. REPLACED LEFT SIDE FLT COMPUTER PER MM. NO LAND 3 ON AUTOLAND STATUS ANNUNCIATOR. REPLACED LEFT FLIGHT CONTROL COMPUTER IAW MM. ACP'D TEST PER MM. GRND CK NORMAL. SDR UALA2012022201080Computer · faultyAFTER ENGINE RUN CHECK OF EICAS, MESSAGES SHOW AUTOPILOT FLIGHT DIRECTOR CENTER COMPUTER FAULT. REPLACED AFDC COMPUTER AS PER MM.SDR UALA2012021000807Computer · faultyNO LAND III DISPLAYED ON EICAS. AUTOPILOT BITE SHOWS NO INTERFACE FCC RIGHT TO RUDDER RATIO SERVO AUTOPILOT DOWNGRADED TO CATII SECOND DEFERAL CREATED FOR RIGHT FLIGHT DIRECTOR INOP. REPLACED R FCC PER MM AND ACCOMPLISHED A-P FLIGHT CONTROL TEST PER MM, ALL SDR SWIA201229198Computer · failedAT FL370, THE AUTO PILOT PITCHED DOWN INTO AN 1100 FPM DESCENT AND THEN RECAPTURED FL370. (FLT 4681) REPLACED NR 1 & 2 FCC COMPUTERS. P/N: 822-1308-027 S/N OFF: 28HPX P/N: 822-1308-027 S/N OFF: 28HHXSDR UALA2012010300059Selector Knob · brokenHEADING SELECT KNOB BROKEN BUT USEABLE. REPLACED MCP PER MM.SDR CALA2012010300001Computer · failedAFTER TAKEOFF, GOT "AUTOPILOT" EICAS MESSAGE & RED M/C LIGHT. SWITCHED AND TRIED ALL 3 AUTOPILOTS. ALL THE SAME, HAD NO STAB TRIM. PERF'D MCDP LAST FLT FAULT REVIEW, FOUND MULTIPLE CODES REFERENCING L FCC FAULT ACROSS MULTIPLE CHANNELS. R&R'D L FCC IAW AMM SDR UALA2011122307076Computer · faultyAFDC L STATUS MSG AND NO LAND 3 STATUS MSG AND NO LAND 3 EICAS MESSAGE. ITEMS HAVE HISTORY, MSG 27 -18010. FOLLOWED FIM 27-02 T962, REPLACED LEFT AFDC PER MM AND FIM SAT. LRU REPLACEMENT TEST AND AFDC SYS TEST PASSED. NO MSG.SDR ASAA11510759Computer · malfunctionedCAPT AUTOPILOT AND FLIGHT DIRECTOR FAIL. SPEED AND MACH TRIM FAIL. AUTOTHROTTLES FAIL. ALL FAILURES OCCURED AT SAME TIME. RE-INSTALLED FCC "B" AND REPLACED FCC "A". DFCS LOGGED 22 11628 22 11356. COMPLIED WITH FIM 22 15 TASK 824 + 825. GROUND VERIFICATIOSDR UALA2011110305966Computer · faultyF/O ADI FLT DIRECTOR NO LATERAL GUIDANCE BAR. REPLACED RT FCC AND OP CHECK SATS PER MM. ACP CAT III TEST SATS PER MM.SDR UALA2011092805262Computer · faultyAUTOPILOT MOVES YOKE BACK AND FORTH INSIDE THE MARKER APP 1 INCH EACH WAY. REPLACED CENTER FCC AND RESTORED SYSTEM OPERATIONS.SDR UALA2011092005059Computer · faultyNR 1 FMG COMPUTER LOSS, FLIGHT DIVERTED. LDG ELEV FAULT DISPLAYED ON UPPER ECAM SCREEN. - CAB PR PROG TEXT: DUP ITEM PER OPBLM. REPLACED FMGC1, ACCOMP CFDS BITE REF MM.SDR UALA2011091404976Computer · faultyEICAS STATUS MESSAGE "NO LAND 3" AND "PFC CHANNEL" ARE DISPLAYED. REF SMC 5 FOR INCOMPATIBLE PFC HARDWARE & SOFTWARE. SEE PTT SEQ 6912018 FOR R AND CENTER PFC RPL.SDR UALA2011090204726Computer · failedF/O FD FAILED ROLL MODE IN CRUISE. REPLACED RT FCC PER MM. PASSED FCC RT GROUND MCDP TEST. THE FCC GENERATES F-D COMMANDS. PER MM ACCOMPLISHED CAT 3 FOR FCC REPLACED PER MM. F-D BARS COME ON WITH F/O FD SWITCH ON, MCP OK NOW.SDR UALA2011082604573Computer · faultyLEFT AUTO PILOT FAILED IN-FLIGHT. R AUTO PILOT PREVIOUSLY DEFERRED. CREW CONTINUING TO SFO. SAMC PATCHED IN, CB RESETS UNSUCCESSFUL. DESCENDING TO FL280 NON-RVSM AIRSPACE. REPLACED LEFT & RIGHT AFDC REF MM. TESTS GOOD.
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