JASC 2210
Service difficulty reports · 4,016
Reports filed under 2210 · Autopilot 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 = '2210' 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 = '2210' 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 CALA2013111893004Control Panel · brokenHEADING SEL KNOB ON MCP IS BROKEN. R & R MCDP IAW AMM. PERFORMED MCDP TEST 4 & DEFECTS NOTED. PERFORMED MCDP TEST 30 & NO DEFECTS NOTED. AIRCRAFT REMAINS WITH CAT FULL CAPABILITY.SDR CALA2013111893009Unknown · malfunctionedPLANE YAWING BACK & FORTH DURING CLIMB. OSCILLATION STOPS WITH LT YAW DAMPER OFF.SDR ASAA2013111396407Computer · malfunctionedLATE FLARE DURING AUTOLAND & ACFT DRIFTED LT THRESHOLD NOT CONTAMINATED & CROSSWINDS WITHIN LIMITS. ACFT GROUNDED. PERFORMED DFCS GROUP NR 20 (FAULT REVIEW) REF FIM 22-11, TASK 801. NO RECENT FAULTS NOTED. PERFORMED DFCS GROUP NR 49, LAND VERIFY, TEST REF MSDR ASAA2013111296392Control Panel · malfunctionedAUTOPILOT HAD TWO UNCOMMANDED DISENGAGEMENTS DURING CRUISE FLT IN SMOOTH CONDITIONS. ACFT GROUNDED. DFCS A&B LOGGED MULTIPLE MCP FAILURES FAULT MSG 22-11607. R & R MCP REF MM 22-11-34, OPS CHECK NORMAL. ACCOMPLISHED MCP LWMP CHECKS REF LWMP CHECKLIST MM 22SDR ASAA2013111296385Switch · failedCOPILOTS YOKE AUTOPILOT DISCONNECT SWITCH DISCONNECTS AUTOPILOT BUT DOES NOT CANCEL AUTOPILOT WARNINGS. ACFT GROUNDED. R & R FOS AUTOPILOT DISCONNECT SWITCH IAW MM 22-11-41, OPS CHECKED NORMAL.SDR ASAA2013111196364Control Panel · failedF/O`S COURSE WINDOW IS BLANK. CRS DOES APPEAR ON THE NAV DATA DISPLAY AND WORKS NORMALLY. ACFT GROUNDED. REPLACED AND TESTED DFCS MODE CONTROL PANEL REF. MM22-11-34. OPS NORMAL. PERFORMED REQUIRED LWMP TESTS DFCS BITE TEST GROUP NR 32, DFCS LRU INTERFACE TSDR A6WA201311114040Computer · malfunctionedENTIRE ACFT VIBRATION OF MODERATE INTENSITY FOLLOWED BY UN-COMMANDED YAW MOTION IN BOTH DIRECTIONS. FOLLOWED BY AILERON CAUTION ON PFD-"AILERON MISS-TRIM". AND TWO SHARP LEFT BANKS WITH AUTO PILOT ON. DECLARED EMERGENCY AND LANDED FLAPS 8. R & R FCC 2 IAW ASDR ASAA2013110696314Knob · inoperativeCAPTAIN`S COURSE SELECTOR KNOB INTERMITTENTLY INOPERATIVE. ACFT GROUNDED. REPLACED DFCS MODE CONTROL PANEL IAW MM 22-11-34. DFCS MODE CONTROL PANEL INSTALLATION TEST NORMAL IAW MM 22-11-34. PERFORMED HGS SENSOR TEST SSM 34-36-00, OPS NORMAL. PERFORMED LANDSDR SWIA201335203Computer · failedUNCOMMANDED RT BANK WITH THE NR 1 AUTOPILOT ENGAGED. FLT 5303 REPLACED THE AILERON AUTOPILOT SERVO & NR 1 AUTOPILOT COMPUTER.SDR CALA2013110692692Computer · failedCAP MAP NOT AVAILABLE ON ND. REPLACED FMGC 1 IAW AMM 22-83-34, OPS CHECKED GOOD. LAND TEST IAW AMM22-97-710 TEST PASSED.SDR ASAA2013103196271Warning Light · false activationAMBER FWD WARNING DISPLAYED ON CAPTAINS ATTITUDE INDICATOR. ACFT GROUNDED. FOUND AFCS SYS A FCC DC CIRCUIT BREAKER OUT. RESET CIRCUIT BREAKER IAW MM 20-60-01, DFCS CHANNEL A & B DFCS/AT CRU INTERFACE GRP 35 BITE CHECKED NORMAL. DFCS LAND VERIFY GRP 49 BITESDR ASAA2013103196270Actuator · failedMACH TRIM FAIL LIGHT ILLUMINATED BRIEFLY DURING ARRIVALS AT FIRST FLAP EXTENSION. ACFT GROUNDED. REPLACED MACH TRIM ACTUATOR. OPS CHECKED GOOD IAW AMM 22-11-24.SDR CALA2013103192536Warning Message · activatedRT FCC FAILED RUDDER SERVO, FAULT MESSAGE 2 2429. TRIED CNTR FCC IN RT POSITION, NO HELP. RT FCC TESTED NORMAL IN CNTR POSITION. NEW FAULT MESSAGE 22066.SDR ASAA2013102696237Actuator · malfunctionedMACH TRIM FAIL LIGHT ILLUMINATED ON ARRIVAL TO ACFT, PARTIALLY CONFIGURED L250 KTS. ACFT GROUNDED. DFCS BITE LEG 1 BOTH A AND B CHANNELS FAULT MACH TRIM ACTUATOR IAW AMM 22-11-00. PERFORMED AMM FIM TASK 22-13 TASK 816 MACH TRIM FAIL LIGHT PROBLEM. TESTED NSDR ASAA2013102696233Warning Light · illuminatedMACH TRIM FAIL LIGHT ILLUMINATED IN FLIGHT WITH MASTER CAUTION. RECALLED IN FLIGHT BUT ON GROUND, FLT CONT DID NOT RECALL IN FLIGHT ALTITUDE 6,000 ; AIRSPEED 210 KTS C LEAN CONFIGURATION TAT -1C. ACFT GROUNDED. PERFORMED BITE OF DFCS IAW FIM 22-11-801. FOUNSDR CALA2013102992446Control Panel · damagedKNOB ON AUTOPILOT MODE CONTROL PANEL IS MISSING, BENT, STICKS & LOOSE. HEADING SELECT KNOB IS BROKEN, CANNOT SET HEADING ON MCP, KNOB LOOSE. HEADING HOLD WORKS OK. AFCS MODE CONTROL PANEL REPLACED IAW AMM 22-11-02 PP201 & AMM 22-00-02 P208 TEST 04.SDR ASAA2013102596230Control Panel · inoperativeMCP PANEL IS INOPERATIVE. ACFT GROUNDED. REPLACED MCP IAW AMM 22-11-34. PERFORMED DFCS TESTS REF AMM 22-11-00, BITE NR 32 AND NR 49 HGS SENSORS TEST REF SSM 34-36-00, ALL GROUND FUNCTIONAL TESTS PASS. DFCS LRU INTERFACE TEST FOR MCP GOOD, BITE NR 32 REF MM SDR ASAA2013101996202Indicator · malfunctionedIAS/MACH INDICATOR GOES BLANK WHEN IN VNAV MODE. REMAINS ILLUMINATED OTHERWISE. ACFT GROUNDED. PERFORMED INSTALLATION TEST OF MODE CENTRAL PANEL IAW AMM TASK 22-11-34-740-801. ALL TESTS PASS. PERFORMED DFCS FAULT REVIEW IAW FIM 22-11, TASK 801, BITE GRP SDR SWIA201334968Autopilot Sys · malfunctionedDURING CLIMB OUT WITH THE AUTOPILOT ON IN SPEED MODE (IAS) THE SPEED BUG MOVED ON ITS OWN FROM 290 KTS TO 72 KTS, AIRCRAFT BEGAN UNCOMMANDED AGGRESSIVE CLIMB. FLT#5157 FOUND NO ENTRIES IN MDC FAULT HISTORY FOR AUTO FLIGHT SYSTEM ON THE DATE OF THIS EVENT. AUSDR ASAA2013101496180Autopilot Sys · disengagedAUTOPILOT B DISENGAGED ON ATTEMPTED CAT III A. ACFT GROUNDED. ACCOMPLISHED FIM 22-11, TASK 801, DFCS BITE. OPS CHECKED NORMAL. NO HISTORY 30 DAYS.SDR SWIA201334862Protector · failedWHILE DESCENDING THRU 11000 AIRCRAFT YAWED TO THE RT UNCOMMANDED WITH NO ASSOCIATED EICAS MESSAGES. COMPLIED WITH QRH PROCEDURE. FLT#4695 R & R LIGHTNING PROTECTION UNIT IAW CRJ, PN ON OFF 822-0332-201, SN ON 2D7HJ, SN OFF 29WMP.SDR IPXA2013100900481Computer · malfunctionedNO AUTOTHROTTLES NO AUTOPILOT FMS2 WOULD NOT OPERATE. FCC1 AND FCC2 BOTH SHOW FAULTED R & R BOTH FCC1 AND FCC2, FMC NR 2 RTS IAW AMM 34-63-01. ALL OPS NORMAL.SDR IPXA201310070481Computer · failedAIR TURNBACK, NO AUTO THROTTLES NO AUTOPILOT FMS2 WOULD NOT OPERATE. R & R BOTH FCC1 AND FCC2 SEE LP 360621 ITEM 1 FOR DISCREPANCY RTS PASSED IAW AMM22-00-00.SDR ASAA2013100496109Warning Light · false activationAFTER ENGINE START, ON RECALL THE FLT CONTROL MASTER CAUTION LIGHT CAME ON WITH MACH TRIM FAIL AND AUTO SLAT FAIL LIGHTS ON THE OVERHEAD FLIGHT CONTROL PANEL. ALL LIGHTS GO OUT WHEN MC RESET IS PRESSED. ACFT GROUNDED. CYCLED POWER, C/W OPS TEST OF STALL WASDR ASAA2013100496108Autopilot Sys · malfunctionedB AUTOPILOT KICKED OFF TWICE ONCE IN LIGHT TURBULENCE & ONCE WHILE IN SMOOTH AIR. ACFT GROUNDED. FLIGHT FAULT REVIEW SHOWED NO FAULTS. CURRENT STATUS TEST PASS, NO FAULTS. ACCOMPLISHED FAULT REVIEW, BITE GROUP NR 20, AND LAND VERIFY TEST, BITE GROUP NR 49, SDR ASAA2013100396102Autopilot Sys · malfunctionedCHANNEL A AND B WHEN ENGAGING AUTOPILOT A LARGE CONTROL BUMP. ALL OTHER AUTOPILOT FUNCTIONS NORMAL. ACFT GROUNDED. PERFORMED PREV FLIGHT FAULT REVIEW, CURRENT STATUS & DFCS LAND VERIFY TEST ALL IAW AMM 22-11-00. ALL OPS NORMAL, NO DEFECTS NOTED. A/P A & B SDR CALA2013100291656Control Panel · damagedHEADING SELECT KNOB FALLING APART. HEADING SELECT INOPERATIVE. MODE CONTROL PANEL REPLACED IAW AMM 22-11-02, MCDP TEST 04 CARRIED OUT, ALL SATISFACTORY.SDR CALA2013093091576Fcu · malfunctionedCREW REPORTS AT DEPARTURE TIME AUTO FLT CH 1 FAULT DISPLAYED ON UPPER ECAM. REPLACED FCU IAW AMM. NO FURTHER DEFECTS NOTED.SDR AALA20130926001Control Panel · malfunctionedSNN INFLIGHT JFK-DUB CREW REPORTED SEVERAL AUTOPILOT RELATED ISSUES INCLUDING, LAND 2 MODE ANNUNCIATED, BANK LIMITED TO 5 DEGREE ALT CAPTURE INOPERATIVE. FLIGHT LEVEL CHANGE INOPERATIVE. FLIGHT DIVERTED SNN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SDR CALA2013092591433Autopilot Sys · malfunctionedMODE CONTROL PANEL FREEZES AT POWER TRANSFER & RT FLIGHT DIRECTOR DISAPPEARS. REPLACED MODE CONTROL PANEL IAW AMM & TESTED IAW AMM. FOUND ALL WORKING EXCEPT CENTER AUTO PILOT. DEFERRED CENTER AUTO PILOT IAW MEL 2210C. PERFORMED MCDP TEST FOR FCC LT, RT, BSDR ASAA2013092496052Unknown · unknownFLARE ARM DID NOT ILLUMINATE DURING AUTOLAND/HGS APPROACH. ACFT GROUNDED. COULD NOT DUPLICATE.SDR CALA2013092491414Unknown · malfunctionedAIRPLANE HAS PITCH OSCILLATION, PORPOISES, WITH ANY A-P CHANNEL IN CMD & V-S, ALT HOLD, FLCH, VNAV MODE SELECTED. WORSE IN VNAV PATH AT CRZ. +- 60 FEET AT ALTITUDE. ACP MCDP TEST 30 & 40 NO FAULTS FOUND. CHECKED ELEV PCA'S. ELEV OPERATIONS FOUND TO BE NORMSDR ASAA2013091795994Director · malfunctionedFLIGHT DIRECTOR DID NOT CAPTURE THE APPROACH, MADE IN THE LOCALIZER GUIDANCE, RAW DATA FUNCTIONED OK. ACFT GROUNDED. VERIFIED WITH FLIGHT CREW DEFECT ON F/O SIDE ACCOMPLISHED DFCS BITE TEST IAW AMM 22-11-00, CURRENT STATUS SHOWS NO FAULTS ON CH B. ADDITIONALSDR ASAA2013091695989Autopilot Sys · malfunctionedB- AUTOPILOT DISENGAGED DURING CRUISE FLIGHT, FOR NO APPARENT REASON. ENGAGED B- AUTOPILOT AND SYS WORKED NORMALLY FOR REMAINDER OF FLIGHT. ACFT GROUNDED. CONFIRMED DFCS LOGGED FAULT 22-11607 MCP FAULT ON AFFECTED LEG. PERFORMED FIM TASK 22-11 TASK 817. CHASDR SWIA201334619Autopilot Sys · malfunctionedAUTOPILOT UNCOMMANDED EVENT CLIMBING IN SPEED MODE BUGGED TO 265 UNCOMMANDED CHANGE TO IAS 40. ACFT PITCHED UP TO 1800 FPM CLIMB. AUTOPILOT OPERATED NORMALLY REMAINDER OF FLIGHT. FLT 5496 NO FAULT FOUND. OPS CHECKED GOOD.SDR QXEA2013091301385Button · stuckCAPTAIN`S TCS BUTTON STUCK. RETURNED TO FIELD. LANDING UNEVENTFUL. R & R CAPTAINS TCS SWITCH IAW AMM 27-31-06-400-801, STEP 4, A, 6. CW PERTINENT PARTS OF AUTOPILOT FUNCTIONAL CHECKED AMM 22-11-00-720-804 4, B, 4, C, P 540-541. AP AND TCS TESTED GOOD. RESDR ASAA2013091395972Knob · inoperativeCAPTAIN`S COURSE KNOB INOPERATIVE. ACFT GROUNDED. R &R MAIN CONTROL PANEL IAW AMM 22-11-34. MAIN CONTROL PANEL OPS NORMAL. ACFT OK CONTINUE FOR SERVICE.SDR CALA2013091091173Module · faultyUPON DOING TESTS FOR CSEU FOUND LT STAB TRIM & ELEVATOR ASSEMBLY LIMIT MODULE (SAM) FAULT B ALL ON COMPUTER UNABLE TO CLEAR. R&R LT SAM IAW AMM, ALL TESTED GOOD.SDR CALA2013090691073Control Panel · inoperativeHDG SELECT BINDS WITH BANK LIMIT. MODE CONTROL PANEL SECTOR BANK LIMIT SELECTOR INOPERATIVE. REPLACED MODE CONTROL PANEL IAW MM. TEST CHECKED GOOD.SDR CALA2013090591008Unknown · malfunctionedWHEN ENGAGING CENTER A-P TO CMD IT DISCONNECTS. AUTOPILOT DISCONNECT EICAS & MASTER. FCC-C TEST PASSED IN CMC. AILERON SERVO TEST FAILED. MESSAGE 22239, NO TIME TO T-S. AIRCRAFT DOWN GRADED TO AUTOLAND LIMIT LAND 2.SDR CALA2013102392331Unknown · malfunctionedCOMPLETE LOSS OF UPFRONT CONTROL. AUTO PILOT & AUTO THROTTLE CUT IN & OUT EVEN ONCE DISENGAGED. ALL LIGHT & CONTROLS ON MCP FLASHING & INCORRECT.SDR ASOA20130829159Controller · smokeTHE CREW REPORTED ELECTRICAL SMOKE COMING FROM THE VS BUTTON OF THE FLIGHT GUIDANCE PANEL. MX R & R THE FLIGHT GUIDANCE CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR CALA2013082890815Unknown · malfunctionedFIRST OFFICERS FLIGHT DIRECTOR AZIMUTH BAR DISAPPEARED WHEN MODE CHANGED FROM LATERAL NAVIGATION TO HEADING SELECT, NO LAST FLIGHT FAULTS. REPLACED FCC R PRECAUTIONARY IAW MM. CAT III TEST ACCOMPLISHED IAW MM. TEST PASSED NO FAULTS..SDR SWIA201334698Control Cable · brokenELEVATOR AUTOPILOT SERVO CONTROL CABLE IS CORRODED & HAS BROKEN STRANDS AT THE SERVO CAPSTAN. C-CHECK REPLACED ELEVATOR AUTOPILOT SERVO CONTROL CABLE IAW AMM.SDR REXA2013082501607Autopilot Sys · malfunctionedAT FL 290, AUTOPILOT HAD AN UNCOMMANNDED PITCH UP THAT CAUSED THE ACFT TO CLIMB APPROX 200 FT.SDR USAA2013082600014Actuator · faultyDURING CLIMB BETWEEN FL 190 AND 250, CREW REPORTED THREE UNCOMMANDED RUDDER INPUTS. EACH INPUT INCREASED IN SEVERITY. ACFT ON AUTOPILOT 1, APP 320 KIAS, VMC CONDITION, SMOOTH RIDE CONDITIONS. FLIGHT CONTROLS NORMAL WITH A/P DISCONNECTED & A/P 2 ENGAGED. NO SDR ASAA2013081695817Control Panel · inoperativeCAPTAIN`S COURSE WINDOW SHOWS ALL EIGHTS ON MAIN CONTROL PANEL. ACFT GROUNDED. DUPLICATED. REPLACED MAIN CONTROL PANEL IAW MM 22-11-34, GROUND VERIFICATION, OPS CHECKED NORMAL. ALSO ACCOMP DFCS, LRU, MCP, NR 32 TEST, LAND VERIFY NR 49 TEST, & HGS SENSOR FCSDR USAA2013081600001Computer · faultyCLIMBING WITH AUTOPILOT NR 2 ENGAGED, THERE WERE VERY NOTICEABLE RUDDER INPUTS. ACFT MOVED WITH EACH OCCURENCE. STOPPED WITH AUTOPILOT OFF (UNCOMMANDED). MX ACCOMPLISHED WIRING CHECKS BETWEEN FAC1 AND YD1. NO FAULTS NOTED. PERFORMED OPS CHECK OF YAW DAMPER SDR ASAA2013081395790Control Panel · failedA/P DISENGAGED TWICE DURING FLT WITH CMD B ENGAGED. ACFT GROUNDED. DFCS BITE SHOWED DISCONNECTS CAUSED BY FAULT 22-11607 MCP DATA INV. ACCOMPLISHED T/S FOR FAULT 22-11607 IAW FIM 22-11, TASK 817 - MCP FAILED INITIAL EVALUATION TEST (FIM 22-11 TASK 803). REPLSDR ASAA2013080795753Circuit Breaker · trippedAFCS SYS A ENGAGE INTERLINK CIRCUIT BREAKER FOUND TRIPPED. ACFT GROUNDED.
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