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 UALA2011062003026Control Panel · faultyAUTOLAND NO LAND 3 ILLUM CB E34 POPPED. REPLACED AFCS MODE CONTROL PANEL PER MM.SDR ASAA1159822Control Panel · defectiveAUTOPILOT A DISENGAGED TWICE WITHOUT COMMAND. FIRST TIME AT CRUISE FL380 M.80 SECOND TIME IN V/S DESCENT FL350 M.79. DFCS LOGGED NUMEROUS MCP DATA INV FAULTS NR 22 11607 ON CH: A&B REF FIM:22 11/817 & 801 FAULT ACTIVE. REPLACED MCP REF MM:22 11 34 OPS CHECKSDR CHQA201100222Autopilot Sys · malfunctionedCREW REPORTED THAT DURING CLIMB AT 22,000 FEET, RECEIVED AN AUTO-PILOT AILERON MISTRIM MESSAGE. THEN AT 27,000 FEET RECEIVED AN AUTO-PILOT FAIL MESSAGE. THE PILOT DISENGAGED THE AUTO-PILOT SYSTEM AND REPORTED HE COULD NOT MOVE THE AILERONS AND THAT THE AUTO-SDR ASAA1159747Autopilot Sys · malfunctionedAUTOPILOT DISCONNECTED WHEN AIRCRAFT BEGAN FLARE CRITICAL AREA CLEAR NO OTHER AIRCRAFT AROUND RUNWAY 16C. VERIFIED MAINT MSG 22 11479 ON CHANNEL A PERFORMED FIM 22 11 00 810 801 DFCS BITE PROCEDURE ALL TESTS PASS SUCCESSFULLY, NO FAULTS NOTED NO HISTORY 90 DASDR UALA2011052302512Valve · faultyNO LAND 3 ON BOTH AUTOLAND STATUS INDICATORS. MAINT TEXT: MCDP LAST LEG FAULT WAS "ILS CP-ILS L" AND "AIL SER VO-FCC L". MCDP TEST 7 INTERMITTANTLY FAILS "AIL SRVO R". SOME MCDP HISTORY FOR THIS FAULT SEVERAL LEGS AGO. DUE TO FAULTS ON BOTH SIDES A-C WAS SDR ASAA1159674Control Panel · failedAUTOPILOT DISCONNECTED FOR NO REASON AT CRUISE BOTH IN CMD A & CDM B SEVERAL TIMES AT CRUISE. A&B LOGGED MCP FAILURES MSG 22 11627 AND 22 11607. REMOVED AND REPLACED MCP REF MM 22 11 34 OPS CHECK NORMAL. ACCOMPLISHED ALL MCP LWMP CHECKS REF LWMP CHECKLIST MSDR ASAA1159665Unknown · malfunctionedUPON MASTER RECALL SPEED TRIM FAIL AND MACH TRIM FAIL LIGHT ILLUMINATED LIGHTS EXTINGUISH WITH MASTER CAUTION RESET. FAILURE ON CHANNEL A SIDE RE-RACKED "A" FCC OPS CHECK GOOD MM REF 22 11 00 740 806 COMPUTER RE-RACK IAW REF 22 11 33. COMPLETED DFCS LRU INTESDR UALA2011051102338Iru · faultyCENTER AUTOPILOT DISCONNECTED AT FL340 .79M LOST CAPT FLT DIRECTOR. LEFT A-P SELECTED. SAMC TEXT: CREW REPORTED CENTER AUTOPILOT DISENGAGED AND CAPTS FD BARS BIASED OUT OF VIEW SIMULTANEOUSLY. ENGAGED LEFT AUTOPILOT. MAINT TEXT: CREW REPORTED WHEN CTR AUSDR ASAA1159620Panel · failedAT TOP OF DESCENT (FL360) WHEN WE SET 12,000 FT IN ALTITUDE ALERTED FOR ATC RESTRICTION ALTITUDE ALERTER RESET TO 50,000 FT & ALTITUDE DEVIATION TONE SOUNDED. ALTITUDE ALERTER WOULD NOT RESPOND TO INPUT & ALTITUDE DEVIATIION TONE SOUNDED CONTINUOUSLY TO TOUCHSDR UALA2011050202148Computer · faultyCREW REPORTED THE CENTER AUTOPILOT DISENGAGED IN STEADY STATE CRZ, SMOOTH AIR, FL360, M.80. HAD STAYED ENGAGED FOR 5:20 BEFORE DISENGAGING. OPBLM BRENDEL. SAMC TEXT: REVIEW HISTORY. SUGGEST CHECKING MCDP INFLT FAULTS AND SAMS TO SEE IF ANY FAULT BALLS SET. SDR UALA2011050202150Control Panel · faultyMCP IAS-MACH SWITCH INOP STAYS IN MACH ONLY. REPLACED MCP PER MM, ACP CATIII TEST PER MM. TEST PASSED.SDR UALA2011050202143Control Panel · faultyMCP SPEED IAS-MACH WINDOW'S FIRST DIGIT STUCK AT .9. REPLACED AUTOPILOT MODE CONTROL PANEL, OPS CHECK NORMAL.SDR UALA2011042802069Unknown · malfunctionedAIRPLANE NOT SMOOTH (JERKY) IN ROLL WITH ANY A-P IN CMD & (HDG HOLD, HDG SEL, LNAV, LOC, B-CRS) MODE SELECTED. CREW COMMENTS: ALL AUTOPILOTS CAUSED A-C ROLLING BACK AND FORTH FL410 IN LT CHOP, LNAV AND HDG MODE. SAMC TEXT: PER CONVERSATION WITH INBD CREW, ACSDR ASAA1159496Unknown · malfunctionedDURING PREFLIGHT THE MODE CONTROL PANEL DISPLAYS ARE BLANK. NO CIRCUIT BREAKERS OUT CYCLED AIRCRAFT POWER. RESTORED MODE CONTROL PANEL DISPLAYS AND ACCOMPLISHED DFCS GP49 LAND VERIFY TESTS AND HGS TEST IAW AMM 22 11 00.SDR UALA2011041801878Unknown · malfunctionedAUTOPILOT DISCREPANCY, RTFL.SDR UIEA2011041600247Power Unit · shortedAIR TURN BACK. NO FUEL DUMPED. DURING CLIMBOUT WHEN EITHER "A" OR "B" AUTOPILOT SELECTED , ACFT MODERATE TO SEVERE ROLL LT AND RT. FOUND ROLLOUT CONTROL POWER PACKAGE B, A/P LVDT HAD SHORT TO GROUND, REPLACED ROLLOUT CONTROL POWER PACKAGE, OPS CKS IAW MM SATISDR HALA2011041100152Module · malfunctionedETOPS SIGNIFICANT SYS - ATB - AT FL 370 A/P ON - ACFT DOVE 100' AND YAWED RT. OCCURRED 3 TIMES. DISENGAGED A/P - NORMAL OPERATION ON RETURN. BIT CHECK ALL SCM. FOUND FAULT ON 3 RT SCM BOX. SCM FAULT APL 767 SHELF. NO OTHER FAULTS ON THE REST OF BOXES.
SDR ASAA1159387Unknown · malfunctionedF/O'S FD FLAG IN VIEW. CURRENT STATUS TEST FOR FLIGHT DIRECTOR PASSED REF MM 22 11 00.SDR UALA2011040401598Panel · faultyFCU VERTICAL SPEED AND FLIGHT PATH ANGLE CONTROL INOP. CAN ONLY SELECT ZERO VSI. REPLACED FCU PER MM, OPS CHECKED PER MM. OPS CHECKS GOOD. ALSO ACCOMPLISHED OPS TEST OF AFS PER MM AND LAND CAT III CAPABILITY PER MM, ALL TESTS CHECK GOOD.SDR ASAA1159351Unknown · malfunctionedATTEMPTED AUTOLAND WITH HGS UNSAT. "NO AIII" AND NO "FLARE ARMED" ANNUNCIATED FOR APPROACH. DFCS SHOWS NO INFLIGHT FAULTS. CURRENT STATUS BITE GOOD BOTH AUTOPILOT A & B. DFCS OPS TEST GOOD REF MM 22 11 00. HGS CURRENT STATUS AND CAPABILITY CHECKS GOOD. HSDR ASAA1159350Unknown · malfunctionedFL 350 CRUISE (3 MINUTES AFTER L/O) M.787/AS 266 KTS.AIRCRAFT ON TRIM: A/P B UNCOMMANDED DISCONNECT RE-ENGAGED A/P B AIRCRAFT FLOWN NORMALLY REMAINDER OF FLIGHT TILL 1500 WITH NO OTHER PROBLEMS. AFCS BITE PROCEDURE REF FIM 22 11 00 810 801 CURRENT STATUS QUICSDR REXA201100208Unknown · malfunctionedUNCOMMANDED CLIMB OCCURED WITH AUTOPILOT ENGAGED, REPORTED BY CREW. DFDR WAS PERFORMED & SENT TO ENGINEERING.SDR ASAA1159349Control Panel · faultyUNCOMMANDED AUTO PILOT DISENGAGE. WHEN LEVELING OUT AT FL 300 .76 MACH ALSO AT 2000FT 160 KTS GEAR DOWN FLAPS 15 COUPLED TO ILS AIRCRAFT IN TRIM ON BOTH OCCASIONS. ALSO ON 3/29/11 FLT 889 FL 350 CRUISE (3 MINUTES AFTER L/O) M.787/AS 266 KTS. AIRCRAFT ON TRISDR ASAA1159273Unknown · malfunctionedEVAL AUTO LAND {OUT OF TOLERANCE LEFT OF CENTER}. DFCS GROUP 20 (FAULT REVIEW) PER FIM 22 11 00 810 801 SHOWED NO RELATED FAULTS BUT HGS FAULT HISTORY SHOWED MULTIPLE FAULTS WITH "ILS ANOMALY DET" AS CAUSE FOR LEG 6. PERFOMED DFCS GROUP 49 (LAND VERIFY) TESTSDR ASAA1159272Transducer · failedTHE "A" AUTOPILOT WILL NOT ENGAGE IN CAMD OR CWS. CONFIRMED F/O'S PITCH FORCE X DUCER FAULTY. REPLACED RT PITCH FORCE TRANSDUCER REF MM 22-11-92. CHECKS NORMAL REF FIM 22-11T802. ACCOMPLISHED DFCS BITE TEST GRP 49. PASSES WITHOUT ERROR. A CHANNEL AUTOPILSDR UALA2011030201026Autopilot Sys · malfunctionedAIRPLANE HAS PITCH OSCILLATION (PORPOISES) WITH ANY AUTOPILOT IN COMMAND AND (V-S, ALT HOLD, VNAV, FLCH) MODE SELECTED. CREW COMMENTS: CTR AP PORPOISES 300FPM +-- 20FTL AP 400 FPM +-- 20FTRT AP OK. PERFORM CAT3 FUNCTION TEST. ALL PASSED BY CMC AND NO MSG FSDR ASAA1159133Control Panel · malfunctionedMCP HEADING DISPLAY FLICKERS. REMOVED AND REPLACED MODE CONTROL PANEL PER MM'S 22 11 34 000 801 AND 22 11 34 400 801. PERFORMED GOOD TEST PER MM 22 11 34 740 801.SDR HAEA201100219Selector · shortedHEADING/COURSE REMOTE SELECTOR EMITTED SMOKE. DISCONTINUED USE OF REMOTE SELECTOR AND SMOKE WENT AWAY. MAINTENANCE DISCOVERED REMOTE SELECTOR SHORTED INTERNALLY. REPLACED REMOTE SELECTOR WITH A REPAIRED UNIT. PERFORMED SYSTEM OPERATIONAL CHECK. SYSTEM OPERATIOSDR ASAA1159062Unknown · malfunctionedAUTOLAND UNSAT AIRCRAFT LINED UP WITH LEFT SIDE OF APPROACH END OF RUNWAY AND WANTED TO DRIFT FURTHER LEFT. TOUCHDOWN HOWEVER WAS IN TOUCHDOWN ZONE. ACCOMPLISHED DFCS LAND VERIFY GP49 TESTS REF AMM22 11 00 OPS CHECK NML. PER NEW PROCESS CHECKED FOR REPETITISDR ASAA1158988Unknown · malfunctionedON PRACTICE AUTOLAND INTO FAI THE AUTOLAND FUNCTION WAS OUT OF LIMITS TO THE LEFT OF CENTER LINE UPON TOUCHDOWN. HUD APPEARED NORMAL. COULD NOT DUPLICATE. ACCOMP FIM:22 11/825 LAND VERIFY TEST CK NML NO FAULTS & PRECAUTIONARY PERFORMED ILS SYSTEM TEST REF MSDR UALA2011020700641Computer · faultyON ARRIVAL AUTOPILOT BACKDRIVE FAILED. REPLACED RT AUTO PILOT FLIGHT DIRECTOR COMPUTER IAW MM. CAT 3 CHECKED OK IAW AMM.SDR HALA2011020200066Adiru · malfunctionedETOPS SIGNIFICANT SYS - BTB - ON TAXI, AUTOFLT, A/P OFF. REALIGNED ADIRU'S, IAW AMM 34-10-00-806-802. NO AUTOPILOT FAULTS NOTED. OK FOR SERVICE.SDR NSVA2011016Autopilot Sys · malfunctionedRETURNED TO GATE DUE TO PRE TAKEOFF FLIGHT CHECKS CREW FELT A BINDING IN THE YOKE. FOUND TO BE AUTO PILOT, MEL'D AUTO PILOT.SDR HALA2011020100065Computer · failedETOPS SIGNIFICANT SYS - CTR AUTO PILOT DISENGAGED AND WOULD NOT RE-ENGAGE ALSO LT AUTO PILOT WOULD NOT ENGAGE. REPLACED RT FCC. GROUND OPS CHECK OK, AMM 22-11-01. ACCOMPLISHED LMP MCDP TEST 01 AND 30, TEST PASSED. ACFT OK TO REMAIN AT LAND 3.SDR ASAA1158935Autoland Sys · malfunctionedAUTOLAND PERFORMED 10R AT PDX FLARE WAS INCOMPLETE. ALL HGS INDICATIONS WERE NORMAL. ACFT GROUNDED. FFR LOGGED NO FAULTS DFCS NOR HGS. LAND VERIFY OP CK NORMAL PER BITE GROUP NR 49. VERIFIED TWO SUCCESFUL AUTOLAND WAS ACCOMPLISHED. OPS NORMAL.SDR ASAA1158931Unknown · malfunctionedCAPT F/D INOP. AFTER ENG START ON RECALL SPEED TRIM FAIL LIGHT AND MACH TRIM FAIL LIGHT ILLUMINATED. CYCLED POWER TO "A" FCC COMPUTER. PERFORMED FCC LRU INTERFACE TEST REF MM 22 11 33/401 & LAND VERIFY TEST REF MM 22 11 00/201 BITE 49, ALL TESTS PASSED. HGSDR ASAA1158934Unknown · malfunctionedDURING AUTOLAND "NO FLARE ARMED" DISENGAGED CAPT'S AUTOPILOT. HGS AIII NORMAL ROLLOUT ARMED ANNUNCIATED. PERFORMED FIM 22 11 TASK 801 BITE GROUP 20 "FAULT REVIEW" AND 22 11 00 PG 201 BITE GROUP 49 "LAND VERIFY TEST" FAULT REVIEW LAST 10 LEGS ONLY HAD ONE GLIDSDR HALA2011012200039Autopilot Sys · malfunctionedETOPS SIGNIFICANT SYS - AUTO FLT FM 1 FAULT. PERFORMED AFS TEST RESET POWER TO FMGEC 1 IAW 22-83-00, MSG CLEARED. NO HISTORY.SDR ASAA1158744Unknown · malfunctionedTHE "STAB OUT OF TRIM" LIGHT ILLUMINATED WITH AUTOPILOT ON. MAIN ELECTRIC TRIM WORKS NORMAL. FCC B RECORDED TWO OCCURRENCES OF FAULT CODE 22 11830 "ELEVATOR AUTHORITY LIMITED". PERFORMED DFCS GROUP NR 1 (CURRENT STATUS) NR 11 (AUTOPILOT) AND NR 49 LAND VERISDR ASAA1158743Autoland Sys · malfunctionedAUTOLAND UNSUCCESSFUL AIRCRAFT LINED UP ON APPROACH LIGHTS & RUNWAY CENTERLINE. DURING THE LAST 20FT IT STARTED TO DRIFTING LEFT WITHOUT CORRECTING TO RUNWAY CENTERLINE TOUCHED DOWN ON LEFT HALF OF RUNWAY & DRIFT CONTINUED. CAPT INTERVENED TO RETURN AIRCRAFSDR DBCA2010122900031Yaw Damper · malfunctionedAIRCRAFT DEPARTED TEB EN ROUTE TO RST. IN CRUISE FLIGHT AUTOPILOT DISCONNECTED AND YAW DAMP FAIL MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO TEB. LANDING WAS UNEVENTFUL. DEFERRED YAW DAMP CHANNEL "A" PER MEL 22-20-2. AIRCRAFT REPOSITIONED TEB-MKE. STERLINGSDR ASAA1158710Unknown · malfunctionedAUTOLAND TOUCHDOWN APROX. 37' RIGHT OF CENTERLINE, 7 KT TAILWIND. ILS PROTECTED AREA CLEAR. HUD GOOD STEER LEFT. DFCS BITE SHOW NO FAULTS IN HIST PAGE. ACCOMPLISHED LAND VERIFY DFCS BITE TEST GRP NR 49 VERIFIED ALL TESTS PASSED.SDR UALA2010122004637Module · faultyELEV ASYM STATUS MSG CAME ON. REPLACED LEFT STCM PER 27-09-00 BECAUSE MODULE PREVIOUSLY INSTALLED HAD ALL FAULT BALLS DISPLAYED & WOULD NOT RESET. NEW UNIT TESTED OK. THEN PERFORMED AUTOPILOT ADJ TEST PER MM.SDR QXEA2010122200929Autopilot Sys · malfunctionedFLIGHT DIVERTED. CLIMBING THROUGH FL 280 IN CLIMB, IRS MODE NOTICED SPEED BUG MOVE UNCOMMANDED TO 65 KTS. F/O PUSHED IAS/MACH REF. BUTTON TO MACH AND ROTATED AIRSPEED BUG TO .74. THERE WAS NO CHANGE IN PITCH. ACFT/ FLIGHT GUIDANCE OPERATED NORMAL, FOR REMSDR MASA2010121301439Unknown · malfunctionedAP RWD CAUTION. AILERON TRIM WENT FULL RIGHT WING DOWN AND AFTER CREW CENTERED THE TRIM IT MOVED 3/4 LEFT UNCOMMANDED. MX OPS CHECKED SYSTEM AND SPC, OPS GOOD, CLEARED MEL.SDR ASAA1058538Control Panel · failedF/O AUTOPILOT WOULD NOT ENGAGE. NR 1 ENGAGED OK. REPLACED AUTO PILOT MODE CONTROL PANEL PER MM 22 11 34/401 DFGS TEST FOR MCP LAND VERIFY & HGS SENSOR TEST FOR FCC/AT CHECKS GOOD. VERIFICATION AUTOLAND SUCCESSFUL.SDR QXEA2010112300795Autopilot Sys · malfunctionedCLIMBING THROUGH 13,000 FT USING F/O FLIGHT DIRECTOR IN AIRSPEED MODE AND WITH AUTOPILOT ENGAGED, AIRSPEED BUG WENT TO 40 KNOTS AND FLIGHT DIRECTOR COMMANDED PITCH UP TO CAPTURE AIRSPEED. PITCH MODE WAS SELECTED TO OBTAIN NORMAL PITCH ATTITUDE. AIRSPEED MODESDR QXEA2010111000727Switch · stickingCAPTAIN'S TCS BUTTON STUCK. RETURNED TO THE FIELD, LANDING UNEVENTFUL. R & R CAPTAIN'S TCS SWITCH AND A/P FUNCT TEST GOOD IAW TASK 22-11-00-720-801. ACFT REMAINS CAT III. PLACARD CAT III. ALL CHECKS GOOD IAW MX 6221101. RETURNED TO SERVICE.SDR CLCA10142010.2Autopilot Sys · faultyBOTH AUTOPILOTS FAILED DURING CRUISE, RETURNED TO SBKP. PERFORMED FCC NR 1 AND FCC NR 2 RTS OF THE AUTO FLIGHT SYSTEM. ALL TESTS PASSED IAW MM 22-01-10 AND FCC NR 1 AND NR 2 CAT 111B RTS ALL TEST PASSED IAW MM 22-00-00. AIRCRAFT RETURNED TO SERVICE.SDR CA101014005Bridal Cable · failedAUTOPILOT LOST ROLL CONTROL. CREW DISENGAGED AUTOPILOT AND CONTINUED TO HOME BASE. ON TROUBLESHOOTING AUTOPILOT THE ROLL BRIDLE CABLE WAS FOUND TO BE BROKEN.
Back to JASC 2210