JASC 2210
Service difficulty reports · 4,017
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 2008FA0000701Servo · contaminated8/11/08 INSTALLED YAW DAMPENER. 10/06/08 - CUSTOMER COMPLAINT OF INDUCED YAW WHEN ENGAGING AUTO PILOT. REMOVED YAW DAMPENER AND FOUND UNIT CONTAMINATED WITH WATER. UNIT IS MOUNTED WITH DRIVE SHAFT UP AND WITH NO DRAIN, THIS PROVIDES FOR WATER TO BE TRAPPED INSDR ASAA0853534Autopilot Sys · malfunctionedDURING AUTOLAND APPROACH AUTOPILOT DID NOT MAINTAIN GLIDE SLOPE. FCC'S FLT FAULT REVIEW SHOWS FOR FLT DISCEP OCCURRED: MAIN ELEC TRIM TRIM RELAY CHAN A MSG 22 1208. PERFORMED FIM 22 13 TASK 818 WITH INTERMITTANT FAULT. SPEED STAB CHAN BITE 20.32 AND LAND VSDR ASAA0853527Autoland Sys · malfunctionedPERFORMED AUTOLAND AS REQUESTED. ALL OK UNTIL LAST 40FT AC STARTED GOING LEFT OF CENTERLINE AND TOUCHED DOWN APPROX HALF WAY BETWEEN LEFT RUNWAY EDGE AND CENTERLINE DID NOT GET APPROACH WARN DFCS FFR SHOWS NO FAULTS. PERFORMED FULL LAND VERIFY TEST REF MM 22SDR DXTA200809223282Actuator · inoperativeA/P PITCH TRIM FAILURE IN FLIGHT. AFTER LANDING AND SECURED AT THE FBO A/P FAILS GROUND TEST. TROUBLESHOT ON GROUND WITH GPU POWER AND FOUND ALL OPS NORMAL. NO FAILURES NOTED. CHECKED ALL CLEAR. CONTACTED MCC AND REVIEW PROBLEM. RAN AUTOPILOT FOR 35 MINUSDR UIEA200800318Autopilot Sys · malfunctionedATB BOTH AUTOPILOTS A AND B WILL NOT ENGAGE. BOTH TESTED OK ON GROUND. A/P A AND B PITCH AND ROLL COMPUTERS, FLIGHT CTL HYD PWR SHUT OFF SWITCHES ALL CHECKED IN ON POSITION. ACCESS BOXES INSTALLATION OCCURRED OK. MSP ELECT CONNECTORS INSPECTION NO FAULTS.SDR DXTA200803282Autopilot Sys · malfunctionedA/P PITCH TRIM FAILURE IN FLIGHT.SDR YEN2008F00018Actuator · bindingCLIMBING THROUGH 8,000 MSL AT 250 KTS, NOTICED AILERONS WERE MORE DIFFICULT TO MOVE THAN NORMAL, AS WE CLIMBED AND INCREASED AIRSPEED TO 290 KTS THE AILERON CONTROLS GRADUALLY BECAME HARDER TO MOVE AT APPROX 20,000 MSL AND 290 KTS AILERONS BINDING FEEL AND WHESDR DXTA200809193279Trim System · out of limitsAUTO PILOT KICKS OFF WHEN IN CLIMB OR TURN. ACFT CONTROLS APPEAR TO BE LOADED WHEN AUTOPILOT KICKS OFF. PERFORMED OPS CHECK OF AUTOPILOT DISENGAGEMENT SYS TO ENSURE PROPER OPERATION. ALL CHECK GOOD. PERFORMED AHRS FUNCTIONAL TEST. ALL AHRS OPS CHECK GOOD. GAINSDR DXTA200803279Autopilot Sys · malfunctionedAUTO PILOT KICKS OFF WHEN IN CLIMB OR TURN.SDR QML2008F00013Computer · faultedWHILE RETURNING TO BASE, CREW NOTICED AN INCREASING STRONG ELECTRICAL ODOR AS THE ACFT TURNED FINAL. CONTINUED TO THE LANDING AREA AND PUT THE ACFT OUT OF SERVICE. CREW SAW NO SMOKE BUT ONLY THE ODOR. MAINTENANCE FOUND YAW COMPUTER TO BE FAULTY AND REPLACEDSDR ASAA0853481Position Sensor · out of adjustAUTOPILOT HAD SPOIL 4 SIQ FAILURE INDICATION. ADJUSTED SPOILER POSITION SENSOR.SDR DXTA200803269Warning System · activatedDURING DESCENT AUTOPILOT STAB TRIM FAIL AMBER CAS MSG CAME ON.SDR DXTA200809053262Actuator · inoperativeAUTO PILOT PITCH TRIM FAILED. INDICATED - 0.4 ON TRIM, STAYED STUCK AT -0.4 ABOVE 250KTS, WORKED OK ON SECONDARY OVERRIDE AND BELOW 250KTS. WHILE TRIM STUCK ABOVE 250 OCCASIONAL (NT) INDICATION. REMOVED AND REPLACED HORIZ STAB TRIM ACTUATOR WITH A REPAIRED ACSDR DXT2008F00005Trim System · failedAUTO PILOT PITCH TRIM FAILED. (K)SDR DXTA200803258Yaw Damper · malfunctioned"YAW DAMPER OFF LOWER" CAS MESSAGE ILLUMINATED. T/S, NO ERROR CODES NOTED. COMPLETED LINEAR ACTUATOR TEST IAW MM 27-24-00. NO DEFECTS NOTED. ACTIVATED YAW DAMPER SYS CHECKED GOOD.SDR USAA920081448Yaw Damper · leakingFLT 1740 BUF-PHL - EMERGENCY LANDING - ON APPROACH FROM BUF TO PHL, CREW STATED LOSS OF GREEN HYDRAULIC SYSTEM. ACFT LANDED SAFELY AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REMOVED AND REPLACED THE LT YAW DAMPER ACTUATOR. OPERATIONAL AND LEAK SDR SWIA200819894Computer · malfunctionedFO`S AUTOPILOT PERFORMED AN UNCOMMANDED ROLL TO THE RT. (FLIGHT NR 5485) REPLACED NR 2 AUTOPILOT COMPUTER AND NR 2 ADI. OPS CHECK GOOD IAW MM 22-10-00 AND 34-21-00. P/N 787-6173-013. S/N OFF 4544.
SDR SWIA200819858Actuator · faultyRECEIVED UNCOMMANDED YAW DURING FLIGHT. (FLIGHT NR 2512) REPLACED YAW DAMPER NR2 LINEAR ACTUATOR IAW AMM 22-22-01. OPS CHECK GOOD. P/N 622-9968-101, S/N OFF 714.
SDR AALA200801821Actuator · failedDFW INFLIGHT T1767/09JUL. CREW REPORTED YAW DAMPER FAILED ON CLIMB. FLIGHT GUIDANCE CIRCUIT BREAKER POPPED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED YAW DAMPER ACTUATOR. REPLACED LT AILERON SENSOR, LT ELEVATOR SENSOR AND DIGITAL FLIGHT GUIDANSDR UPS08M52626Autopilot Sys · failedBOTH AUTOPILOTS FAILED IN FLIGHT. FOUND HARD FAULT ON LT OB AILERON MOD LVDT. REPLACED TRANSDUCER IAW MM 27-13-34-4. ACCOMPLISHED AUTOPILOT RTS FOR FCC 2. NO FAULTS FOUND.SDR 2008UALA03293Computer · failedDUAL FMGC FAILURE. RTFL. *S/D* FMGC 2 FAILED-ARRINC INTERLOOP TEST FAILS. FMGC2 INOP UPON ARRIVAL. REPLACED FMGC2. PERFORMED AFS AND LAND TEST PER MM 22-96-00 AND MM 22-97-00. CHECKS GOOD.SDR HNAA0800189Autopilot Sys · malfunctionedWHEN AUTO PILOT SELECTED OFF F/O REPORTED POSSIBLE PITCH JAM, F/O REQUESTED HELP. CAPTAIN TOOK CONTROL, FELT NO JAM, NOTED ACFT FLEW NORMALLY. RIGGED ELEVATOR CONTROL CABLES IAW DASH 8 MM 27-32-00. MEL 30MAY08 16:52 ABE B15119 22-1 AUTOPILOT DFRL 30MAY08 16SDR 2008UALA02998Transformer · burnedSTRONG ACRID ODOR DETECTED AFTER DEPARTURE, RTFL. *S/D* BAD AUTO PILOT FLIGHT CONTROL PANEL. REPLACED CONTROL PANEL. SHOP FINDINGS: FOUND TRANSFORMER A10T1 PRIMARY BURNED. TRANSISTORS A10Q1/Q2 PARTIALLY SHORTED. REPLACED PARTS.SDR ASAA0852979Control Panel · faultedON CLIMB-OUT SELECTED VNAV AND NOTICIED 209 IMMEDIATELY REPLACED
250 ON TOP OF THE AIRSPEED TAPE THE FLIGHT DIRECTOR STARTED
PITCHING FOR 209 KNOTS. THE CLIMB PAGE ON THE FMC SHOWED
"CLIMB ACT 209" 7 COULD NOT BE MANIPULATED ALSO LOST BEST
ANGLE AND BEST SDR QXEA200800513Servo · malfunctionedPDX - FLIGHT 2332 - AFTER TAKEOFF WITH THE GEAR UP AND THE FLAPS AT ZERO ON FLAP RETRACT (STILL MOVING), THE FIRST OFFICER WAS UNABLE TO TURN THE AIRCRAFT TO THE LEFT FOR ABOUT 4-5 SECONDS. AFTER THE FLAPS WERE FULL UP CONTROL WAS RETURNED. ON LANDING IN PDXSDR DXTA200803051Pitot Head · failedCLIMBING THROUGHT 10,000 FT, WE HAD A DUAL FGC FAILURE. INSPECTED LT AND RT PITOT PROBES. FOUND RT FWD DRAIN TO BE BLOCKED. THE RT AFT DRAIN, AND BOTH LT DRAINS HAVE DEBRIS INSIDE. REMOVED FAILED LT AND RT PITOT PROBES. INSTALLED NEW LT AND RT PITOT PROBES, PSDR DXTA200803049Computer · inoperativeAUTOPILOT DISENGAGED TWICE ON CLIMB-OUT ON PFD1. REMOVED AND REPLACED 1IC-615 AND C/W SYS. OPS CHECK IAW MM 34-23-10
SDR DXTA200803013Relay · inoperativeUNCOMMANDED EMERGENCY DESCENT WITH AUTOPILOT ENGAGED AT FL400. REPLACED RELAY KC009 AND CONNECTOR. IAW MFG WIRING DIAGRAM MAN 20-10-04. OPS CHECK GOOD. RELAY P/N LMP5001P S/N NSN/CONNECTOR LMS01T-TL S/N NSN / CONNECTOR P/N LMP4001S S/N NSN.SDR DXTA200803010Computer · inoperativeYD FAIL UPPER B CAS MSG CAME ON DURING CLIMB THRU FL 350 AFTER PASSING THRU LIGHT TURBULANCE. REPLACED AND OPS CHECKED B YSAC IAW M/M 27-24-01SDR HALA08000530Module · faultyUNSCHEDULED STAB TRIM MESSAGE APPEARED INTERMITTENTLY. DISPLAYED FOR FEW SECONDS THEN DISAPPEARED. NIL MOVEMENT EVIDENT IN STAB TRIM GAUGE NIL EFFECT ON AIRCRAFT. NIL EXISTING FAULT, FOP M838 REPLACED IAW AM 27-58-01 IN P50 CARD FILE, MAD TEST 4/65 CHECKED OSDR DXTA200803001Computer · illuminatedUPPER YAW DAMP FAIL (A-B) ILLUMINATED AFTER TAKE-OFF. REPLACED B SYSTEM YSAC COMPUTER, IAW 750 MM CH 27-29-01, OP'S CHECK GOOD.SDR CA080414006Static Line · deterioratedDURING RE-ACTIVATION OF THE AIRCRAFT, THE MAINTENANCE CREW NOTICED THAT THE STATIC LINE FOR THE AUTO PILOT ALTITUDE HOLD P/N 0807-1 WAS DETERIORATED AND CRACKED. THE LINE WAS REPLACED WITH A SERVICEABLE PART. ALL OTHER AIRCRAFT IN THE FLEET WILL BE INSPECTEDSDR DXTA200802980Unknown · multiple failDURING DESCENT, AP TRIM FAIL LIGHT ILLUMINATED WITH ASSOCIATED AMBER CAS MESSAGE. REPLACED STAB CONTROL RELAYS- 504CH, 505CH, 506CH & 507CH. REPLACED STAB CONTROL PCB'S 502CH & 503CH. OPS CHECKED STAB CONTROL RELAY BOX DUE TO RELAY AND PCB REPLACEMENT. INSPECSDR DXTA20082980Trim System · malfunctionedDURING DESCENT AP TRIM FAIL LIGHT ILLUMINATED WITH ASSOCIATED AMBER (E).SDR ASAA0852805Switch · faultyAUTOPILOT "A" WILL NOT ENGAGE. COULD NOT GET AUTOPILOT "A" TO ENGAGE. PERFORMED DFCS BITE SHOWED MULTIPLE DISCONNECT FAILURES. FOUND F/O'S DISCONNECT SWITCH BAD. THE "A" SIDE OF SWITCH STICKS OPEN REQUIRES NUMEROUS PRESSES OF SWITCH TO CLOSE AND ENGAGE AUTSDR HALA0800492Autopilot Sys · malfunctionedETOPS SIGNIFICANT SYSTEM, NO LAND 3 DISPLAYED ON ASA WITH CTR A/P SYS ENGAGED IN CMD, INTERMITTENT PROBLEM-RESETS AFTER ABOUT 5 MIN. PAST FAULTS. NO LAND 3 RA C AND NO LAND 3 R/A/FCC C BITE OF CENTER RADIC ALT CHECKS GOOD. PERFORMED TEST 40. ALL CHECKS GOOSDR ASAA0852808Autopilot Sys · malfunctionedTHE "A" AUTOPILOT WILL NOT ENGAGE. UNABLE TO DUPLICATE. RAN LAND VERIFY TEST WITH NO FAILURES.SDR HALA0800488Autoland Sys · malfunctionedETOPS SIGNIFICANT SYSTEM, ON FINAL APPROACH NO LAND 3 INDICATED. RESET ASA HOWEVER, LAND 2 INDICATED ON ASA AFTER PRELAND TEST. SUCCESSFUL AUTOLAND USING LAND 2 ON RWY 340. MCDP LAST FLT FAULT NO LAND 3 ILS LOC L NCD CODE 11 2020 RESET L ILS C/B. PERFORMEDSDR SA08023Computer · malfunctionedSNA FLIGHT 139 LAS-SNA - DURING FLIGHT, EXPERIENCED A 20 DEGREE UNCOMMANDED ROLL WITH THE SPEED BRAKE APPLIED AND FLAP LOWERED. MAINTENANCE REPLACED THE NUMBER ONE SLAT AND FLAP CONTROL COMPUTER.SDR DXTA200802961Switch · inoperativeAT FL430 ACCIDENTALLY HIT TURN KNOB, AUTO PILOT WOULD NOT WORK CORRECTLY. IN HEADING MODE IT WOULD ALWAYS STOP 10 DEG SHORT OF THE HEADING BUG. NO FAULT CODES REPORTED. DISCREPANCY RELATED TO INVERTER FAULT. INVERTER SELECT SWITCH REPLACED. OPERATIONAL CHESDR DXTA20082961Autopilot Sys · inoperativeAT FL430 ACCIDENTLY HIT TURN KNOB, AUTO PILOT WOULD NOT WORK CORRECTLY. IN HEADING MODE IT WOULD ALWAYS STOP 10 DEG SHORT OF THE HEADING BUG. NO FAULT CODES REPORTED. DISCREPANCY RELATED TO INVERTER FAULT. INVERTER SELECT SWITCH REPLACED. OPERATIONAL CHECSDR ASAA0852758Switch · faultyAUTOPILOT A WILL NOT ENGAGE. CAPT'S DISCONNECT SWITCH BAD. REPLACED AND CHECKED PER MM 22 11 41, TASK 000 801, NORMAL.SDR DXTA20082944Autopilot Sys · failedAUTO PILOT PITCH FAILED. PERFORMED HORIZONTAL STABILIZER TRIM SYSTEM INTERFERENCE TEST, TRAVEL TEST, AND FUNCTIONAL TEST I.A.W. G200 M.M. 27-40-00. OPS CHECK GOOD.SDR DXTA20082928Yaw Damper · failedUPPER YAW DAMPENER CHANNEL (A) FAILED. REMOVED CHANNEL A YSAC DUE TO INTERNAL FAILURE. INSTALLED REPAIRED YSAC IAW CE750 M/M CH 27-24-01, OPS CHECKED GOOD.SDR DXTA20082921Potentiometer · out of toleranceWHILE ENROUTE FD WAS PITCHING UP AND DOWN CAUSING PLANE TO PORPISE. ALTITUDE VARIED BY AS MUCH AS +-150 FEET. TROUBLESHOT PROBLEM TO FLAP/FLIGHT DIRECTOR BIASING POTENTIOMETER. REMOVED RT. WING ACCESS PANEL TO REMOVE POTENTIOMETER. REMOVED OLD UNIT AND INSTALLSDR TRAX200800289Warning System · activatedIN FLIGHT RECEIVED STAB TRIM MACH TRIM AUTOPILOT TRIM AND AUTOPILOT NOSE UP CAUTION, A/P DISCONNECTED. DECLARED EMERGENCY LANDED IN SDF. EN ROUTE TO ATL A/C DIVERTED TO SDF DUE TO MTC. FLT 4803 DE; 325 MINS.SDR ASAA0852639Autoland Sys · malfunctionedAUTOLAND EVAL TOUCHDOWN WELL LEFT OF CENTERLINE APPROXIMATELY 37'. ACCOMPLISHED LAND VERIFY TEST BITE GROUP 49. ALL TESTS PASS (REF AMM 22 11 00 201). AIRCRAFT REMAINS CATIIIA HGS ONLY.SDR DXTA20082888Trim System · malfunctionedLT AND RT AP TRIM PITCH TRIM FAIL LIGHTS ON TRIM INDICATIONS WERE FINE, BUT NOSE DOWN PITCH WHEN AP DISENGAGED. INSPECTED PITCH TRIM SERVO, VERIFIED NO DEFECTS. PERFORMED PITCH TRIM SERVO SPIN UP TEST WITH NO DEFECTS NOTED. SYSTEM OPERATES NORMAL IAW SRM PUB SDR ASAA0852642Sensor · faultyAUTOLAND "LAND VERIFY" TEST FAILS 49.35 BITE. FCC "B" FAULTS ELEV POS SEN 2 MSG 22 11126. REPLACED ELEVATOR POSITION SENSOR 2. RIG AND SENSOR TESTS ALL CHECK GOOD. LAND VERIFY PASSES 49.35 BUT NOW FAILS 49.32 WITH SAME FAULT (ELEV POS SEN 2). REPLACED NSSSDR ASAA0852593Control Panel · faultyN1 INDICATOR LIGHTS ON BOTTOM OF MCP ARE INOP. RELAMPED MCP GROUP 70 & INTERACTIVE TESTS PASSED. REPLACED DFC MODE CNTL PNL. PERFORMED "LAND VERIFY" AND HGS SYSTEM TESTS. NO DEFECTS.
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