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 ASAA2013040694403Control Panel · inoperativeMCP VERTICAL SPEED MODE INOPERATIVE. R & R MODE CONTROL PANEL IAW AMM 22-11-34-000-801 AND 22-11-34-400-81. OPS CHECK GOOD IAW MODE CONTROL PANEL INSTALLATION TEST - AMM 22-11-34-740-80.SDR UIEA2013040400171Computer · failedUNABLE TO ENGAGE ANY OF THE THREE AUTOPILOTS, CMC SHOWS AILERON SERVO C/FCC- C /FCC FAIL. R & R CENTER AND LEFT FCC IAW AMM 22-11-01-004-026. PERFORMED CMC TEST ON CENTER AND LT FCC PASSED REF 22-11-01 ALSO PERFORMED AUTOLAND UNIQUE TEST PASSED.SDR IPXA3M77726Computer · inoperativeSTICK SHAKER AT FL280 FOLLOWED BY FCC2B DATA FAULT. "SEL YAW UPR A " OFF" AND "SEL LSAS LOB OFF" COMPLIED WITH CHECK LIST 2. DUMPED FUEL, AT DUMP TERMINATION, RT DUMP VALVE DISAGREE. FLOW STILL SHOWING ALTHOUGH DUMP VALVE SHOWED CLOSED. R & R FCC-2 AND SDR ASAA2013033094291Fmc · inoperativeDURING DESCENT, VERTICAL SPEED WOULD NOT RESPOND TO INPUTS USING THE VERTICAL SPEED KNOB WITH A FCC AS THE MASTER. RESPONSE WAS IDENTICAL WITH AUTOPILOT ON OR OFF. VERTICAL SPEED WORKED NORMALLY WITH B FCC AS MASTER AND DURING CLIMB WITH EITHER FCC AS MASTER.SDR 2013FA0000212Servo · defectiveTHE PITCH SERVO OVERHEATED CAUSING SMOKE IN THE COCKPIT. THE CURRENT LIMITING RESISTOR HAD MELTED. THE PILOT REPORTED THAT THE AIRCRAFT HAD EXPERIENCED SOME MINOR PORPOISING PRIOR TO THE SMOKE. THIS IS THE THIRD TIME THIS ACFT HAS EXPERIENCED THIS PROBLEM ASDR UALA2013032802021Computer · failedC ADFC EICAS MESSAGE, WOULD NOT RESET. REPLACED C AFDC IAW MM 22- 11-01, TEST PASSED ACFT FULL AUTOLAND CAPABLE.SDR UALA2013032701971Computer · inoperativeF/O'S HEADING FLIGHT DIRECTOR INOPERATIVE. REPLACED RIGHT FCC, SYSTEM CHECKED OK PER MM 22-10-00, AIRCRAFT IS AUTOLAND CAPABLE.SDR CA130326002Actuator · failed(CAN) THE ACFT ENCOUNTERED A GREEN HYDRAULIC FAILURE MESSAGE AT THE TOP OF DESCENT TO RUNWAY. AS A PRECAUTION, THE FLIGHT CREW DID DECLARE AN EMERGENCY AND CFR WERE ON STANDBY. AFTER LANDING, THE ACFT WAS INSPECTED BY CFR ON THE RUNWAY WITH NIL ADVERSE RESULTSSDR UALA2013031801646Control Panel · failedRIGHT LAMP OF C CMD A-P ENGAGE IS OUT. REMOVED AND REPLACED MODE CONTROL PANEL IAW AMM 22-11-02, ACCOMPLISHED MCDP TEST 30 NO FAULTS, ACFT IS FULL CAT CAPABILITY.SDR ASAA2013031294150Control Panel · inoperativeCPTS COURSE SELECTOR KNOB INOPERATIVE. FFR SHOW NO FAULT. UNABLE TO DUPLICATE DUE TO HISTORY R & R MCP. INSTALLATION TEST GOOD REF MM 22-11-34. BITE TEST GROUP 49 32 AND 58 GOOD. REF MM 22-11-00.SDR UALA2013031301476Knob · bindingFCU ALTITUDE CONTROL KNOB VERY DIFFICULT TO PULL FOR OPEN DESCENT. LUBRICATED KNOB AND EXERCISED IN ALL DIRECTIONS. NO DIFFICULTIES IN MOVEMENT.SDR ASAA2013031194146Autopilot Sys · malfunctionedCAPTAIN SIDE MCP COURSE SELECTOR KNOB TURNS, BUT WILL NOT ALLOW NEW COURSE SELECTION. UNABLE TO DUPLICATE, RAN COURSE SELECTOR 360 DEGREES BOTH CW AND CCW SEVERAL TIMES. NO HISTORY LAST 30 DAYS. PERFORMED INSTALLATION TEST REF MM 22-11-34-740-801, DFGS BITESDR ASAA2013031094129Warning Light · false activationWHEN LEVEL CHANGE SELECTED AIRBORNE OR LIGHTS TEST SELECTED AIRBORNE AMBER ACTUATION LIGHT WITHIN THE BUTTON DOES NOT ILLUMINATE. COULD NOT DUPLICATE, ALL MODE CONT PANEL LIGHTS ILLUMINATE WITH LIGHTS TEST AND OPS CKS NORMAL IAW DFCS LIBRARY TEST NR 50.SDR UALA2013030801395Computer · failedCENTER AUTOPILOT FAILED, NO LAND 3 DISPLAYED LEFT RIGHT AUTOPILOT. REPLACED CENTER FCC PER AMM, TESTED IAW FIG 117 PER AMM. AIRCRAFT MAINTAIN CAT III STATUS.SDR SWIA201332917Autopilot Sys · malfunctionedAUTOPILOT DISENGAGED MULTIPLE TIMES AND PITCHED DOWN AGGRESSIVELY. (FLT 5594) PERFORMED OPERATIONAL CHECK OF AUTOPILOT, OPS CHECK GOOD AT THIS TIME. AIRCRAFT UPGRADED TO CAT II AND RVSM STATUS.SDR A6WA201302124013Yaw Damper · faultyDURING CRUISE FLT WITH A/P ON A/C YAWED SUDDENLY BOTH RT & LT YAWING MOVEMENTS LESSENED AT SPEEDS 250 KIAS OR LESS. YAWING MOVEMENTS WOULD LAST APPROXIMATELY 1-2 MINUTES THAN SUBSIDE FOR 10 MINUTES AND THAN BEGIN AGAIN. REMOVED AND REPLACED LEFT & RIGHT YAW SDR CA130212005Cable · loose(CAN) VENTRAL RUDDER FAIL" CAS UPON LANDING. VENTRAL AUTO-PILOT SERVO CABLE FOUND AT O LBS TENSION. CABLE TENSIONED TO 45 LBS AND FUNCTION SYS IS SERVICEABLE.SDR SWIA201332869Unknown · malfunctionedAUTOPILOT RWD CAUTION MESSAGE APPEARED AND AIRCRAFT TURNS TO LEFT UNCOMMANDED. (FLT 4859) OPERATED AUTOPILOT AND AILERON SERVO OPS CHECKS IAW AMM. OPS CHECKS GOOD.SDR UALA2013020700752Control Panel · failedON DESCENT, COULD NOT CONTROL MCP IAS-MACH SPEED SUSPECT STUCK HUNDRED DIGIT. REPLACED MODE CONTROL PANEL PER MM.SDR UALA2013020700751Computer · no testCAT III FAILS LEFT FCC TEST. REPLACED L FCC. NEED TO ACP CAT III, OP CHECK.SDR ASAA2013013193794Autopilot Sys · malfunctionedWHILE AT 37,000 FT IN SMOOTH AIR, AUTOPILOT DISCONNECTED. RECONNECTED IMMEDIATELY (COMMAND A SIDE). ACCOMPLISHED FLT FAULTS REVIEW AND CURRENT STATUS TEST, NO FAULTS AND ALL TEST PASSED. ACCOMPLISHED LAND VERIFY TEST, GRP BITE 49, ALL TEST PASSED, REF MM 2SDR ASAA2013012993792Control Panel · inoperativeA/P B ENGAGED SWITCH LIGHT IS INOPERATIVE. A/P FUNCTIONS ARE NORMAL. REPLACED DFCS MODE CONTROL PANEL. ALL OPS NORMAL, REF MM 22-11-34. ACCOMPLISHED DFCS LRU INTERFACE TEST FOR MCP, BITE GROUP NR 32, LAND VERIFY TEST, BITE GROUP NR 49 AND HGS SENSOR TEST FSDR 39LA200401240003Pitch Control · unserviceableENROUTE, IN CRUISE FLIGHT THERE WAS A SUDDEN AND INADVERTENT PITCH UP AND ROLL OF ACFT, WHILE TRYING TO RECOVER UNUSUAL ATTITUDE ACFT PITCH AND ROLL CONTINUED INADVERTENTLY. THE CO-PILOTS VGI HAD NOT TUMBLED AT THAT POINT AND WAS INDICATING THE UNUSUAL ATTITUSDR 39LA2004012400003Pitch Control · unserviceableENROUTE, IN CRUISE FLIGHT, THERE WAS A SUDDEN AND INADVERTENT PITCH UP AND ROLL OF ACFT, WHILE TRYING TO RECOVER, UNUSUAL ATTITUDE ACFT PITCH AND ROLL CONTINUED INADVERTENTLY. THE CO-PILOTS VGI HAD NOT TUMBLED AT THAT POINT AND WAS INDICATING THE UNUSUAL ATTISDR 39LA2013012400003Pitch Control · unserviceableENROUTE, DIVERTED, DUE TO SUSPECTED CONTROL ISSUE. REMOVED SUSPECTED MALFUNCTIONING COPILOT PITCH AND ROLL GYRO, PN 121672-01-17, SN 0000450. INSTALLED SERVICEABLE COPILOT PITCH AND ROLL GYRO, PN 121672-01-17, SN 0000507 IAW S61 MM CH 22-10-18, PG 201. OPS CSDR UALA2013012400419Computer · failedLEFT FCC FAILURE MESSAGE. REPLACED LEFT FCC, OPS CHECKED GOOD.SDR UALA2013012400418Autopilot Sys · inoperativeAUTOPILOT ASA DISPLAYED NO LAND 3 WITH F-D ON. LEFT AUTO PILOT INOPERATIVE.SDR ASAA2013011993706Autoland Sys · malfunctionedAUTOLAND FAILED, TOUCHDOWN WAS GREATER THAN 35 LT OF CENTERLINE, BUT IN THE TOUCHDOWN ZONE OF THE RUNWAY. NO FAULT LOGGED IN DFCS FFR, CURRENT STATUS PASSED. PERFORMED LAND VERIFY TEST REF FIM 22-11 TASK 825. ACFT REMAINS CAT IIIA AUTOLAND & HGS QUALIFIED, SSDR SWIA201332604Control Panel · failedWHILE LEVEL AT 17,000 FEET, THE AUTOPILOT BEGAN TO PITCH UP AND DOWN, THEN THE NOSE ABRUPTLY PITCHED DOWN AND THERE WAS A "TRIM FAIL" MESSAGE. (FLT 5457) REPLACED AUTO PILOT CONTROL PANEL. OPS CHECK GOOD AT THIS TIME. P/N: 622-6684-006 S/N ON: 440 S/N OFF:SDR SIMA20130109009Unknown · malfunctionedON FLIGHT 3442 THE CREW REPORTED THAT WHILE LEVELING OFF AT FL 200 THEY EXPERIENCED THE AIRCRAFT OSCILLATING WITH THE AUTOPILOT ON. IT WAS QUICKLY FOLLOWED BY AN AIRFRAME VIBRATION OF INCREASING MAGNITUDE. THE CREW DETERMINED THAT IT WAS MECHANICAL AND NOT WSDR ASAA2012123093579Autoland Sys · malfunctionedAUTOLAND FAILED - FLAIR WOULD NOT ARM. ACCOMPLISHED DFCS FAULT REVIEW BG 20 FOR 30DEC12. NO RELEVANT FLIGHT LEG FAULTS AND ALL FAULT LRU TESTS PASS 20.01, 20.18, 20.24. ALSO ACCOMPLISHED LAND VERIFY BG 49. ALL TESTS PASS.SDR JBZA20121231005Autopilot Sys · malfunctionedPASSING THROUGH 8000FT MSL, THE AUTOPILOT SYS WENT INTO AN UNCOMMANDED NOSE PITCH OVER RAPID DESCENT. PILOT TRIED THE AUTOPILOT DISCONNECT SWITCH WHILE TRYING TO ARREST THE DESCENT WITH THE ELEVATOR BACK PRESSURE. SWITCH DID NOT DISENGAGE THE AUTOPILOT. TRISDR FDEA201212204342Unknown · unknownTWICE, A LOWER ALTITUDE WAS SELECTED AND ACFT FAILED TO DESCEND, OVER RODE WITH VERTICAL SPEED. COULD NOT CONFIRM ANY FAULTS LAST FLIGHT. NO PREVIOUS HISTORY PAST 30 DAYS. PERFORMED MCDP GROUND TESTS 30 & 40 IAW MM 22-00-02-2. NO DISCREPANCIES NOTED. OK SDR ASAA2012120693415Control Panel · inoperativeMCP IAS/MACH KNOB INOPERATIVE, F/O SIDE ONLY. UNABLE TO VERIFY FAULT. R & R MCP IAW AMM 22-11-34-000-801 AND AMM 22-11-34-400-801. OPS CHECKED GOOD. BITE GROUP 32 GOOD IAW MM 22-11-34. BITE GROUP 49 GOOD IAW MM 22-11-00. HGS SENSOR TEST GOOD IAW SMM 34-36SDR CA121205010Control Panel · failed(CAN) UNABLE TO ENGAGE EITHER AUTO-PILOT AFTER TAKEOFF. WITH NO AUTO PILOT, WE CANNOT FLIGHT RVSM. CREW WAS DIVERTED FOR MAINTENANCE. SEVERAL SECONDS AFTER TAKEOFF BOTH FLIGHT DIRECTORS DISAPPEARED ON CAPTAIN & F/O PRIMARY FLIGHT DISPLAYS. MODE CONTROL PANESDR ASAA2012120593406Computer · failedWHEN F/O SIDE IS THE MASTER ON THE AFDS WITH A/P ON OR OFF SELECTED SPEED IN MCP WINDOW DOES NOT CHANGE W/SPEED SELECTOR KNOB MOVEMENT. ALL MODES TOGA, LVL CHANGE, SPEED, VNAV SPEED INTV, INOP WHEN CAPTS SIDE IS AFDS MASTER EVERYTHING APPEARS TO OPERATE NORMASDR SIMA20121203003Unknown · malfunctionedON FLIGHT 3309 THE CREW REPORTED THAT 5 MINUTES AFTER TAKEOFF A/P FAILED FOLLOWED BY RUDDER SYS 1-2 INOP MESSAGE. THE CREW FOLLOWED AOM PROCEDURES. NO RESET WAS ACCOMPLISHED. THE CREW DECLARED AN EMERGENCY AND RETUNED TO MOB. THE AIRCRAFT LANDED WITHOUT INCSDR UALA2012112806831Module · faultyCREW REPORTS DURING DESCENT INTERMITTANT YAW FLUTTER LEFT AND RIGHT. WITH RIGHT YAW DAMPER TURNED OFF WIGGLE GOES AWAY. REPLACED RIGHT YAW DAMPER MODULE PER AMM, TEST OKAY.SDR ASAA2012112393337Autopilot Sys · unknownON APPROACH, WITH AUTOPILOT B ENGAGED. WHEN ACFT INTERCEPTED LOCALIZER 16R BOTH AUTOPILOT AND AUTOTHROTTLES DISENGAGED AND F/OS GLIDE SLOPE AND FLIGHT DIRECTORS HID FROM VIEW. ATTEMPTED TO ENGAGE AUTOPILOT AGAIN, BUT SYS WOULD NOT ACCEPT. FLEW APPROACH FROSDR L7OA2012F00256Pitch Control · failedAUTOPILOT PITCH TRIM FAIL. FLIGHT CREW SQUAWKED THAT IN LEVEL FLIGHT WITH THE AUTOPILOT ENGAGED, WAS GETTING A RUNAWAY STAB IN THE NOSE DOWN POSITION. ACFT SYSTEMS PRESENTLY BEING TROUBLESHOT FOR PROBLEM.SDR AALA20121120008Control Panel · inoperativeDFW - CREW REPORTED DIGITAL FLIGHT GUIDANCE COMPUTERS FAILED, LOST ALL NAVIGATION AND AUTOPILOT AND AUTO THROTTLES DISCONNECTED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBERS ONE AND TWO DIGISDR ASAA2012112093336Autopilot Sys · malfunctionedDURING CRUISE, FL 380, AUTOPILOT A DISENGAGED. QRH ACCOMPLISHED AND AUTOPILOT A DID ENGAGE. LRU TESTS PASSED REF AMM 22-00-01-730-801. ACFT REMAINS CAT IIIA A/L & HGS QUALIFIED. STATUS IND REFLECTS SAME.SDR UALA2012111406571Servo Control · faultyCENTER FCC AND CTR RUDDER SERVO FAIL GROUND TESTS. AFTER SERVO CNTR REPLACE, FCC AND RUDDER SERVO TEST PASS IAW MM 22-10-00.SDR SWIA201232155Control Panel · malfunctionedDURING APPROACH DISCONNECTED AUTO PILOT ON CENTER CONSOLE. AILERONS FELT TIGHT. RAN QRH FOR JAMMED AILERON. (FLT 7782) RECONNECTED AILERON DISCONNECT SYSTEM, REMOVED AND REPLACED AP PANEL.SDR UALA2012102906218Control Panel · faultyMODE CONTROL PANEL LANE STS MESSAGE. REPLACED MCP PER MM, ACFT RETURNED TO FULL AUTOLAND STATUS.SDR ASAA2012102793189Control Panel · defectiveLIGHT IN APP BUTTON BURNED OUT. CONFIRMED APP SWITCH (REAR SOCKET) DEFECTIVE. R & R DFCS MCP REF AMM TASK 22-11-34. OPS CK NORMAL REF AMM 22-11-34/501 GP32 DFCS LRU INTERFACE TEST, AMM 22-11-00/201 GP49 LAND VERIFY TEST, AND SMM 34-36-00 HGS TEST.SDR ASAA2012101793147Actuator · out of adjustREF T/C SB737-22A1224-NG-1-1, LAND VERIFY TEST FAILS 49.32 (S051, ELEV POS SENSOR 1). BITE NR 32 STAB TRIM TEST INTERMITTENTLY FAILS ELEVATOR POSITION SENSOR ON CHANNEL A ONLY. ACCOMPLISHED STAB AND ELEVATOR RIGGING TEST REF MM 22-11-00, ALL VALUES ARE WITHISDR UALA2012101605910Yaw Damper · faultyLEFT YAW DAMPER INOPERATIVE. TROUBLESHOT TO BAD LEFT YAW DAMP MODUAL REPLACE SAME AS PER AMM. OPS CHECKS NORMAL. AC REMAINS CAT FULL CAPABLE. INSTALLED BORROWED PART PN 99-222 1-9-0001 SN 0937 MG PN 285T0013-123.SDR ASAA2012101393108Computer · failedAFTER SOFTWARE LOAD FCC A SHOWS CH A UNAVAILABLE DURING DFCS BITE. R & R FCC A COMPUTER, REF MM 22-11-33-400-801-8, C/B OPEN & CLOSED OPS NORMAL. REF LOG 7061279 FOR LWMP TESTING & CAT STATUS. PART VERIFIED SEAM C.SDR P4YA2012101200001Display · failedTHE AUTOPILOT DISPLAY WENT BLACK (ID-802) AND COULD SMELL BURNING WIRE. R & R NR 1 ID-802 ADVISORY DISPLAY.
Back to JASC 2210