JASC 2200
Service difficulty reports · 567
Reports filed under 2200 · Auto Flight 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 = '2200' 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 = '2200' 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 DALA2023102408734Unknown · unknownSHIP 3316 ATTEMPTED 2 CAT 3 APPROACHES TO RWY 18R FMA REVERTED TO CAT 2 ON BOTH APPROACHES REQUIRING A GA SUCCESSFUL CAT 3 AUTOLAND 18C. CORRECTIVE ACTION: NO PFR RELATED FAULTS PERF AUTO LAND TEST, ALL SATIS AND AFS SYSTEM TEST. ALL OK. (4478061)SDR CALA2023101303042Computer · faultyAUTOTHROT DISC ON TAKE OFF AFTER SELECTING A/T A/T DISC EICAS. T/S AS PER FIM 22-32 FAULT TREE 803. REMOVED AND REPLACED THRUST :1 MANAGEMENT COMPUTER AS PER AMM 22-31-01-404-005, PERFORMED MCDP ROTABLE PARTS CHANGE WAS INDICATED - TT # 1615633 SN OFF 0085 TSDR ASAA2023100445433Control Panel · malfunctionedMCP SPEED WINDOW HAD A FEW WHITE DOTS DISPLAYED. GROUNDED - YES. (RESOLVED ON W/O: 1971086 TASKCARD: N/R-00002 ) REMOVED & REPLACED DFCS MCP REF AMM 22-11-34-400-801, OPS CK NML REF AMM 22-11-34/501 (GP 32), LAND VERIFY TEST (GP 49) REF AMM 22-11-00/201 & HGS SDR ASAA2023092945399Unknown · unknownSINGLE CHANNEL SPEED TRIM FAIL FAULT FOUND AT TOP OF DESCENT SPEED TRIM FAIL LIGHT EXTINGUISHES WITH MASTER CAUTION RESET. GROUNDED - YES. INTERROGATED DFCS BITE FAULT REVIEW & FOUND ONLY MESSAGE 22-11186 LAST TWO LEGS REF LP 60685611. REF B737-9 IFIM 22-11-00SDR QR9R2023092800001Unknown · failedAS SOON AS THE AVIONICS MASTER WAS TURNED ON THE AP BEGAN SELF-TEST, AND IT COULD NOT BE INTERRUPTED. MX CYCLED CIRCUIT BREAKERS AND POWER WITH SAME RESULT. REMOVED AND REPLACED APMS2360; TEST FLIGHT SUCCESSFULLY COMPLETED; NO FAULTS NOTED.SDR ASAA2023092245267Unknown · unknownF/C APPROACH SURVEY AUTOLAND NOT SUCCESSFUL. GROUNDED - YES. ON DEFERRAL.SDR YENA2023092201117Controller · failedFLT#2289, AMS-JFK. (ETOPS) 'DURING ENTIRE FLIGHT WE GOT GPS PRIMARY LOST INDICATING NAV ACCURACY LOW; REMOVAL AND REPLACEMENT OF FMGC #2 REF AMM 22-83-34. AFS OPS CHECK REF AMM 22-96-00 PASSED. NO FAULT PRESENT. REF LP 3828366, ITEM 2 (ACCOMPLISHED LAND CAT IISDR QR9R2023091400001Actuator · warning lightYAW ACTUATOR CAUTION CAME ON IN FLIGHT ON CAD. MAINTENANCE PERFORMED AIRBUS RESET. A/C SHUTDOWN AND CANON PLUG DISCONNECTED AND CLEANED. DURING TROUBLESHOOTING FOUND VALID SIGNAL ON PIN 9 AT YAW SAS TEST CONNECTOR BUT NO VALID SIGNAL OUT OF YAW SEMA ON PIN 17 SDR 2023FA0000536Unknown · unknownON DEPARTURE IN CLIMB MASTER WARNING (ILLUMINATED) AND A/P DISENGAGED. RESET ELEVATOR TRIM AND WHEN ENGAGED YAW (DAMPENER) THE PLANE WENT INTO A DIVE TO THE LEFT. DISENGAGED AND CHANGED (AC) INVERTER, HIT YAW DAMPENER AND AGAIN DIVE TO THE LEFT. AIRCRAFT WAS HSDR DALA2023091207454Unknown · unknownSHIP 0198 -ATB- DUE TO AUTOPILOT DISCONNECT AND NO AUTOPILOT ABLE TO RE-ENGAGE. CORRECTIVE ACTION: R/R TAT PROBE AND AUTO PILOT MODE CONTROL PANEL. DISPATCHED CAT 1. (4992444)SDR ASAA2023090845020Unknown · unknownSPEED TRIM FAIL DURING MASTER CAUTION RECALL. GROUNDED - YES. PERFORMED DFCS BITE FAULT 22-11186 IN FAULT HISTORY. IAW AMM 22-11-00-740-814. PERFORMED DFCS OPS TEST IAW AMM 22-11-00-740 801. TEST PASSED . LIGHT EXTINGUISHED. SEAMC LAMONT NOTIFIED. A/C GOOD FORSDR ASAA2023090845019Unknown · unknownSPEEDTRIM FAIL LIGHT "ON" DURING CRUISE FOLLOWED QRH. LIGHT EXTINGUISHED ON MASTER CAUTION RESET. GROUNDED - YES. PERFORMED DFCS BITE FOUND MS22-1173 LOGGED, PERFORMED CORRECTION ACTION IAW IFIM TASK 22-11-00-810-930. TST PASSED TSR CONTACTED DUE TO HISTORY.SDR ASAA2023090444923Unknown · unknownAUTO THROTTLE DISCONNECTED ON DECENT @ 11,000FT WAS UNABLE TO REINGAGE. GROUNDED - YES. ACCOMPLISHED A/T SYSTEM TEST. NO FAULTS FOUND REF AMM 22-31-00. ACCOMPLISHED A/T DFCS BITE TEST 60.04 REF AMM 22-11-00. OK FOR SERVICE.SDR ASAA2023090144925Unknown · unknownAT LEVEL OFF AT FL 350 AUTOTHROTTLES DISENGAGED AND WOULD NOT RE-ENGAGE. GROUNDED - YES. PULLED A/T C/B & RESET. ACCOMPLISHED A/T BITE REF FIM 22-31 TASK 801. NO CURRENT FAULTS. PREVIOUS LEG 01 SHOWED MSG 22-31543 @ 04:23Z ALT. 1112 FT (A/T ENG 28VDC INV. FCC-SDR UIEA2023090100824Unknown · unknownAT GLIDESLOPE / LOCALIZER INTERCEPT W/ AP ENGAGED, HAD THE AIRSPEED TAPE (RED) JUMP UP 10 KTS, CAUSING AN A/S LOW MESSAGE AND STICK SHAKER. WE PERFORMED A GO-AROUND, FLAPS 40, NORMAL APPROACH & LANDING ON NEXT ATTEMPT.(<P>PERFORMED DFCS BITE. NO FAULTS FOUND ISDR ASAA2023082544775Unknown · unknownON ARRIVAL AUTO THROTTLES TURNED OFF AND COULD NOT BE RE ENGAGED. GROUNDED - YES. ON DEFERRAL.SDR QR9R2023082500002Actuator · warning lightON RUNUP, WHEN CONDUCTING THE AUTOPILOT TEST IAW CHECKLIST, AP1 FAILURE AND TRIM ACTUATOR LIGHT REMAINED ON CAD. YAW A TRIM COULD NOT RESET. REMOVED AND REPLACED YAW TRIM ACTUATOR IAW 22-10-00, 4-9; TEST FLIGHT SUCCESSFULLY COMPLETED.SDR QR9R2023082400001Autopilot Sys · failedAUTOPILOT TEST FAILS WITH AP1 AND TRIM ON CAD ALONG WITH AMBER P ON TOP RIGHT CORNER OF PFD. AUTOPILOT TEST WILL NOT END AND RUNS IN A CONTINUOUS LOOP UNTIL ENDED BY PRESSING TEST BUTTON AGAIN. AFTER MANUALLY ENDING TEST ONLY THE TRIM MESSAGE REMAINS ON THE CASDR CALA2023082102607Yaw Damper · inoperativeMACH/SPD TRIM MSG FLAGGED FOR SDR REF. FIM 27-09 TASK 814 . NO EXISTING FAULTS IN EITHER LEFT OR RIGHT YAW DAMPER STAB TRIM MODULE. REPLACED R/H YAW DAMPER MODULE PER AMM 22-21-04 OPERATIONAL TEST GOOD, NO FAULTS NOTED AT THIS TIME. PARTS USED: 64-2221-9-0003,SDR AALA202308213436Relay · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MIA DUE TO SPEED TRIM FAIL LIGHT ILLUMINATED AT 18,0000 FEET. THE AIRCRAFT LANDED SAFELY AT MIA WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED MAIN ELECTRIC STAB TRIM RELAY R64 PER SDR YENA2023081600950Unknown · unknownFLT#2598, SDQ-JFK. 'SHORTLY AFTER TAKE OFF WE GOT CAT III DUAL UNDER INOP SYS AND CAT III SINGLE ONLY ON THE OTHER SIDE; NO FAULTS ON PFR. PERFORMED AFS TEST PER AMM 22-96-00. FOUND FMGC 1&2 FAULT RESET FMGC 1&2. AFS TEST PASS AFTER RESET SEE THE FOLLOWING ITESDR QR9R2023081500003Unknown · illuminatedDURING FLIGHT, ACTUATOR CAUTION LIGHT FAILED MULTIPLE TIMES. REMOVED AND REPLACED APMS IAW AMM 22-10-00, 4-2. MTF SUCCESSFULLY COMPLETED IAW AMM 05-60-00, 6-12.SDR QR9R2023080900008Autopilot Sys · failedDURING RUN-UP, SAS FAILED AND WOULD NOT RESET. TESTFLIGHT EVALUATION REVEALED AC FAILED AP TEST, YAW ACTUATOR CAUTION APPEARED ON PFD ALONG WITH AP1/AP2, YAW SAS, BACK-UP SAS ON CAD. REPLACED YAW FOG GYRO IAW AMM 22-10-00, 4-5. T/F COMPLETED IAW AMM 05-60-00,6SDR QR9R2023080800002Actuator · ratchetingDURING RUN-UP, RECEIVED YAW ACTUATOR FAIL. TROUBLESHOOTING FOUND YAW TRIM ACTUATOR ARM TO BE BINDING AND RATCHETING, WITH OR WITHOUT FTR ACTIVATED. REMOVED AND REPLACED YAW TRIM ACTUATOR, T/F SUCCESSFULLY COMPLETED.SDR HNAA2023080700303Unknown · unknownBURNING SMELL IN COCKPIT. FOUND AUTOFLIGHT GUIDANCE CONTROLLER TO BE THE CAUSE. RNRD FLIGHT FUIDANCE CONTROLLER IAW AMM 22-11-01-04. OPS CHECK GOODSDR QMLA2023080720059Unknown · unknownAUTO PILOT FAILURE WHILE CLIMBING OUT OF PINE RIDE TRIED TO SET CLIMB AT 130 KTS IT WOULDN’T CAPTURE ALTITUDE ALERTER KEPT RINGING THROUGHOUT FLIGHT WHEN DECENDING INTO RAP SET 1200 FT/MIN AIRCRAFT DIDN’T CAPTURE RATE JUST WENT INTO A MUCH STEEPER RATE. SHUT SDR 4DPA2023080400001Controller · failedISSUE CREW REPORTED YAW DAMPER WILL FAIL IN FLIGHT EVEN WITH THE AUTOPILOT OFF. RETURNED TO DALLAS. CORR ACTION MX R/R AUTOPILOT CONTROLLER OPS TEST GOOD.SDR QR9R2023080200002Actuator · unserviceableAFTER INSTALLING YAW TRIM ACTUATOR, T/R PEDALS WERE FOUND TO BE EXTREMELY STIFF WITH CONTROL ROD CONNECTED TO YAW TRIM ACTUATOR. ALL OTHER CHECKS FOUND SATISFACTORY WITH CONTROL ROD DISCONNECTED FROM ACTUATOR. REMOVED AND REPLACED YAW TRIM ACTUATOR.SDR YENA2023072800876Fcu · failedFLT#1621, LHR-BOS. (ETOPS) 'AUTO FLT FCU 2 FAULT X2 (RESET ON GROUND, UNSUCCESSFUL RESET IN FLIGHT); REMOVED AND REPLACED FCU. OPS CHECK GOOD REF AMM 22-81-12.'SDR CALA2023072102285Unknown · unknownTOGA DID NOT ENGAGE WHEN BOTH BUTTONS PRESSED ON TAKEOFF ROLL TOMC UPDATE. CREW REPORTED RTO WAS AT 40 KNOTS REQUEST MEL A/C DOWNGRADED TO CAT 1 NO AUTOLAND INSTALLED PLACARD. OK TO CONT ON MEL. NEEDS TS DISPATCH DESK: 35 NAME: GW DATE: 19-JUL-23- APPROVED. DOSDR QR9R2023071200001Actuator · misrepairedYAW TRIM ACTUATOR RECEIVED WITH BOLT HOLE MIS-DRILLED, SCRATCHES ON THE CASING IN MULTIPLE LOCATIONS, AND THE SPHERICAL BEARING HAS WEAR AND EXCESSIVE BUILDUP OF MATERIAL IN THE RACE.SDR ASAA2023070443892Control Panel · faultyMCP LOCKUP OCCURED DURING DECENT AT APPROX 12,000'. ATTEMPTED TO RESET F/D INITIALLY WITH NO AFFECT, EVENTUALLY IT DID RESET. COMPLETED MCP LOCKUP QRC, OPS NORMAL ON APPCH. GROUNDED - YES. REMOVED & REPLACED DFCS MCP PER AMM 22-11-34.SDR ASAA2023070443865Unknown · unknown30 DAY REQUESTED AUTOLAND- UNSUCCESSFUL. SEA 34L, WIND 340 05, CRITICAL AREA NOT CONFIRMED AS PROTECTED BUT WE SAW NO VEHICLES IN AREA. AIRCRAFT FLARED LATE, POINTED 20 DEGREES R OF CENTERLINE, DRIFTED R CLOSE TO EDGE OF RUNWAY THEN LAST SECOND CORRECTION TOWASDR AALA202307054614Fmc · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED ON DESCENT INTO CLT DUE TO A STRONG ELECTRICAL SMELL, FLIGHT CREW DONNED OXYGEN MASKS AND LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. FLIGHT CREW REPORTED THAT THE SMELL DISAPPEARED AFTER ENGINE SHUTDOWN. MAISDR CALA2023070502174Actuator · inoperativeSTAB OUT OF TRIM LIGHT LIGHT ON AT 8000FT ENGAGED A AP HAD A LARGE JOLT TO AC STAB OUT OF TRIM L IGHT APPEARED. PER FLIGHT CREW CHANNEL B WORKS NORMAL AFTER TRANSITION FROM CHANNEL A. SEE ATTACHMENT FOR FURTHER EXPLANATION. 22-11121. FIM TASK 22-12 TASK 810 SUSDR YENA2023062700736Fmc · failedFLT#371, LGA-FLL. 'TOTAL NAV FAILURE FROM MCDU, ALL NAV FIXES DISAPPEARED FROM ND. A/C WOULD NOT ROLL OUT ON HEADINGS. A/C WOULD NOT GO DIRECT TO ANY FIX. NO NAV DATA EXISTED. ROUTE SHOWED A FLIGHT DISTANCE OF 4773 NM, EVEN WHEN ALL FIXES WERE REMOVED MANUALLYSDR ASAA2023062243673Unknown · unknownRELEASED PER MEL 22-18J A/T ARM LIGHT INOP. GROUNDED - YES. PERFORMED A/T OPS TEST. TEST NORMAL, LIGHT FULL BRIGHT AND GREEN. BITE TEST NORMAL AMM 22-31-00-210-801. THIS CLEARS MEL 22-18J.SDR CALA2023062101953Motor · inoperativeSTAB OUT OF TRIM AP NOT TRIMMING DUE TO STAB OUT OF TRIM LIGHT COMES ON BOTH AUTOPILOT, BOTH AUTOPILOT PLACED ON MEL. MEL 2201C REJECT FLIGHT CREW REPORTED ONCE AIRSPEED PASSED 250KTS, AP TRIM PICS ADDED. MEL2201C WAS REJECTD BY DISPATCH PER TOMC CARLOS. ACCOMSDR ASAA2023061743606Unknown · unknownDFCS MODE CONT PANEL IS BLANK, NO DIGITS. (CREW REPORTED GATE PWR HAD DROPPED OFFLINE). GROUNDED - YES. CYCLED MCP C/B'S, SYS RESTORED AND OPS CKS NML PER B737-900 AMM 22-11-34. GND VERIFICATION SUCCESSFUL.SDR ASAA2023061643607Unknown · unknownSPEED TRIM FAIL ILLUMINATED ON RECALL, LIGHT EXTINGUISHES WHEN MASTER CAUTION SYSTEM IS RESET. GROUNDED - YES. LAST LEG B FCC FAULTED TRIM CMD RESPONSE MONITOR, A FCC NO FAULTS. PERFORMED B737-9 IFIM 22-11-00-810-D71 W/ NO DEFECTS NOTED. BITE LIBRARY TEST FOR SDR YENA2023061600662Unknown · unknownDURING HEAVY MAINTENANCE: ACCOMPLISH OPS TEST OF THE LAND CAT III CAPABILITY; C/W AS REQ PER TC #A320-22-97-00-710-001. AIRCRAFT OK FOR CAT III (FO) STATUS.SDR ASAA2023061533572Unknown · unknownIN CRUISE FL340, A AUTOPILOT KICKED OFF IN SMOOTH AIR. A AUTOPILOT REENGAGED NORMAL. GROUNDED - YES. ACCOMPLISHED LAND VERIFY TEST. TEST NORMAL. REF B737-900 AMM 22-11-00-700-801. ETOPS GROUND VERIFICATION GOOD.SDR CALA2023061201836Computer · unknownMCP FROZEN AND UNRESPONSIVE TO START OVER 3 TIMES BECAUSE #1 MCDU FROZE UP AND HAD SOME MISSING DIGITS ,GAVE VERBAL TURNOVER TO SWINGSHIFT. PARTS USED: VERIFY TEST PER AMM 22-11-00 TEST PASSED ALSO PERFORMED BITE 29-3162-9-0002,QTY :1 LIBRARY TEST FOR FCC A SDR YENA2023060800595Unknown · unknownDURING HEAVY MAINTENANCE: RUDDER TRIM SWITCH CONTROL REQUIRES REPLACEMENT PER JETBLUE REQUEST; C/W PER STS WO#W003031 NRN W003031119. NO DEFECTS NOTED.SDR UIEA2023060400561Unknown · unknownAUTO LAND SYSTEM INOP(<P>REF MDDR 186226 FOR CORRECTIVE ACTION NR-00004. ACCOMPLISHED AFDS SYSTEM TEST PER AMM 22-10-00/501. ALL TESTS PASS. AIRCRAFT RETURNED TO CAT 3B STATUS. MDDR 186226 CLEARED. PLACARD REMOVED</P>)SDR ASAA2023060343432Unknown · unknownAUTOPILOT DISENGAGE BUTTON WILL NOT SILENCE AURAL A/P DISENGAGE TONE FROM EITHER YOKE. GROUNDED - YES. VERIFIED FAULT, FOUND C/B OPEN AT P18-1 WARN LIGHT (BAT) (D1). ACCOMP INSP OF C/B OPEN [18-1 GVI NO DEFECTS NOTED, CLOSED P18-1 & CLOSED C/B (D1). ACCOMP LANSDR QR9R2023060200001Gyro · warning messageIN FLIGHT, ACTUATOR LIGHT CAME ON. DURING AP TROUBLESHOOTING, FOUND BAD YAW FOG GYRO. RECEIVED A YAW FOG FAIL, YAW FOG INVALID, AND YAW ARINC MESSAGE. VERIFIED ALL VOLTAGES WERE PRESENT AND GOOD AT THE YAW FOG GYRO. REMOVED AND REPLACED YAW FOG GYRO IAW AMM 22SDR BIGR202306050001Unknown · unknownELECTRIC PITCH TRIM MALFUNCTION WITH AUTO-PILOT DISENGAGED. ELEVATOR TRIM RUN AWAY IN THE UP DIRECTION. PILOT WAS ABLE TO OVERRIDE PITCH WITH YOKE AND DISABLED MALFUNCTION BY PULLING AUTOPILOT 115VAC CIRCUIT BREAKER. AIRCRAFT RETURNED TO FT. WAINWRIGHT WITHSDR QR9R2023052500002Actuator · illuminatedWHILE HOVERING AT STAGEFIELD THE ACTUATOR CAUTION ILLUMINATED. RETURNED TO AIRFIELD, AVIONICS WAS ABLE TO RESET THE CAUTION BUT WHEN A/C WAS PULLED UP TO A HOVER TO DEPART THE ACTUATOR CAUTION ILLUMINATED AGAIN. REMOVED AND REPLACED SEMA. MTF COMPLETED OK IAW SDR ENHA LP230674Autopilot Sys · activatedAUTOPILOT ENGAGED AND DISCONNECTED 3 TIMES. HAD TO PULL CIRCUIT BREAKER. MECHANICS RAN SELF TEST AND FOUND ELECTRONIC STABILITY AND PROTECTION (ESP) ENABLED AND WORKING NORMALLY. REF POH AND GFC600 PILOTS GUIDE 2.6.
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