JASC 2200
Service difficulty reports · 568
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 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.SDR QR9R2023052300002Autopilot Sys · illuminatedDURING FLIGHT, DEGRADED LEVEL 3 "ACTUATOR" CAUTION ILLUMINATED ON THE CAD WITH "P" PITCH FLASHING ON THE PFD. AFTER A SUCCESSFUL RESET ON THE GROUND BY MAINTENANCE, IT ILLUMINATED A SECOND TIME IN FLIGHT. TEST FLIGHT EVALUATION REVEALED ACTUATOR CAUTION ILLUMISDR 2023FA0000621Servo · misinstalledOU RING ON INSPECTION, TNO GARMIN GSM 86 ELEVATOR AUTOPILOT SORVO GEAR OOX CABLES WE,E FOUND 10 BE ROUTED INCORRCCUY WILH THO CABLES BEHIND LHE GUARD PINS AT THO LD!AR PULLEY. LNSTRUCTJONS IN !HO MANUAL DO NOT SHOW LHO CORROCL ROUTING OL THO COBLCS OR PROVIDE SDR ASAA2023050443137Unknown · unknownGLARESHIELD PANEL GAUGES WENT BLANK AFTER GROUND POWER KICKED OFF AND AC POWERED BY APU. GROUNDED - YES. CYCLED AFCS MCP DC1 & DC2 C/B, MCP RESTORED TO NML. ACCOMPLISHED MCP TEST REF B737-900 FIM 22-11 TASK 803 ALL TESTING PASS.SDR HALA2023042400092Unknown · unknownATO - F/CTL PITCH TRIM/MCDU/CG DISAGREE. PERFORMED TSM 27-40-00-810-805. PERFORMED AFS BITE TEST PER AMM 22-96-00-740-801. TEST OK.SDR UIEA2023040600324Yaw Damper · unknownVERTICAL STABILIZER REAR SPAR, RIGHT YAW DAMPER SERVO WITH EVIDENCE OF HYD LEAK(<P>VERTICAL STABILIZER REAR SPAR, RIGHT YAW DAMPER WAS REPLACE , NO LEAK FOUND IAW AMM 22-21-02-014-001 REV. 132 DATE 22 DEC. 2022</P>)SDR UIEA2023040600323Servo · unknownVERTICAL STABILIZER REAR SPAR, LEFT YAW DAMPER SERVO WITH EVIDENCE OF HYD LEAK(<P>VERTICAL STABILIZER REAR SPAR, LEFT YAW DAMPER SERVO TORQUE WAS PERFORMED, THEN CHECK FOR LEAK, NO LEAK FOUND, THE TEST WAS PERFORMED OK FOR SERVICE IAW AMM 22-21-02-414-016 REV SDR YENA2023040700331Display · failedFLT#8026, LGW-BOS. (ETOPS) 'RH MCDU P/N D50A000-100 S/N D1006102 . IS A L3 AVIATION LOANER PART INSTALLED; REMOVED AND REPLACED MCDU 2 IAW AMM 22-92-12. OPS CHECK NORMAL. THIS CLEARS MDDR # 505981. PLACARD WAS REMOVED. MX-4 UPDATED.'SDR YENA2023040700329Fmc · failedFLT#8026, LGW-BOS. (ETOPS) 'CA+FO MCDU LOST ALL DATA FOR "UTC" "SPD/ALT" "DIST" AND "EFOB" FIELDS. FO WAS FLYING PILOT W AUTOPILOT 2 ENGAGED RESET PROCEDURE FMGC1 WAS RESTORED, RESET PROCEDURE FOR FGMC2 WAS ATTEMPTED 3 TIMES BUT NOT RESTORED #2 DATA RETUSDR 9JLA2023041425571Actuator · failedTHE FLIGHT CREW REPORTED THAT DURING FLIGHT THE FLIGHT GUIDANCE COMPUTER B FAILED. THE MAINTENANCE PROVIDER TROUBLESHOT AND DETERMINED BOTH YAW DAMPENER LINEAR ACTUATORS FAILED. THE ACTUATORS WERE REPLACED WITH REPAIRED UNITS. FAILED UNITS P/N 7002800-901 S/N SDR QR9R2023032800002Actuator · failedAUTOPILOT SYSTEM #1 AND #2 FAILED TEST SEQUENCE AFTER AVIONICS RESET X3. TEST FLIGHT EVALUATION REVEALED AP TEST FAILED AP1/AP2 ACTUATOR ON CAD WITH "P" IN AMBER ON PFD. REMOVED AND REPLACED SEMA ACTUATOR; TEST FLIGHT SUCCESSFULLY COMPLETED.SDR AALA202303277080Relay · brokenAIRCRAFT WAS GROUNDED: SPEED TRIM FAIL LIGHT ILLUMINATED. FLIGHT AIR INTERRUPTED BACK TO CLT. FOUND STABILIZER TRIM CUTOUT SWITCH IN CUTOUT POSITION CAUSING SPEED TRIM FAIL LIGHT. CREW VERIFIED THEY DID NOT MOVE SWITCH. REMOVED AND REPLACED STAB TRIM CUTOUT RESDR AALA202303076237Control Unit · noneAIRCRAFT WAS GROUNDED: DURING FLIGHT AIRCRAFT WENT INTO DESCENT ON NUMEROUS OCCASIONS WITHOUT REGARD TO PILOT INPUT OR ALTITUDE WINDOW ON MAIN CONTROL PANEL. AIRCRAFT WOUD NOT LEVEL OFF ON SUITED WINDOW NO MANAGED VERTICAL CONTROL AT ALL. MAINTENANCE ACCOMPLISSDR ENHA LP217387Ahrs · faultyMAINTENANCE DISCREPANCY: AUTOPILOT DISENGAGES ON ITS WON, TAKES YOU INTO A DIVE AND ALL CONTROLS GET STIFF. CORRECTIVE ACTION: REMOVED AND REPLACED GMC605, UPDATED SOFTWARE, GROUND FUNCTION TESTED GOOD. AIRCRAFT FLOWN FOR MAINTENANCE CHECK FLIGHT AND SYSTEM FUSDR HALA2023021000022Unknown · unknownETOPS-MCDU#2 INOP. REPLACED #2 MCDU PART # OFF 4089740 SN OFF 36044227 PART # ON D50A000-100 SN #ON D1006228 PART EFFECTIVITY VERIFIED PER A/C IPC R/R PER A330 AMM 22-83 STANLEY BOWMAN 568951. PERFORMED AFS TEST PER A330 AMM 22-96-00 TEST PESSED OK FOR SERVICSDR AALA202301254650Control System · faultedAIRCRAFT WAS GROUNDED: SPEED TRIM FAIL LIGHT ANNUNCIATED IN CLIMBOUT. EMERGENCY DECLARED; FLIGHT RETURNED TO CLT LANDING SAFELY. MAINTENANCE FOUND DIGITAL FLIGHT CONTROL SYSTEM (DFCS) FAULT CODES FOR AUTO STAB TRIM CUTOUT, TRIM COMMAND RESPONSE FAIL, AND TRIM SDR DALA2023012400595Autoland Sys · faultedDIVERSION DUE TO LOSS OF CATEGORY 3 AUTOLAND WITH WEATHER IN SEA. REENABLED SOFTWARE ENCRYPTED APPLICATION KEYS AND RTS.SDR 2023F00077Unknown · unknownAUTOPIOT SYSTEM A FUSE DOES NOT ENGAGE WHEN CMD SWIRCH IS PUSHED, AUTO PILOT ACTUADOR ELEV A WASRE´ÑACED IAW AMM 22-11-26-000-801, AUTO PILOT ACTUATOR,SDR 2023F00053Servo · inoperativeAPPROX 15 MINUTES INTO FLIGHT, AFCS DEGRADE CAUTION LIGHT ILLUMINATED WITH ASSOCIATED FAULT CODE AFCS COLL TRIM 008. COLLECTIVE TRIM "BEEP SWITCH" WOULD NOT MOVE COLLECTIVE LEVER UP OR DOWN. ASSOCIATED EMERGENCY PROCEDURE PERFORMED AND AFCS DEGRADE CAUTION LIGSDR CALA2023011100090Adiru · failedSPEED TRIM FAIL, THE RIGHT ADM AND RIGHT ADIRU REPLACED AS WELL AS A PITOT STATIC FLUSHING/LEAK CHECK ACCOMPLISHED ALL TESTS PASSED. SPEED TRIM PORTION OF LAND VERIFY TEST PASSED.SDR ASAA2023010741439Unknown · unknownON DEP, HDG BUG WAS STUCK ON RWY HDG. UNSELECTABLE IN HDG MODE OR IN LNAV. F/D HDG MODE WAS NOT WORKING. APPROX 5 MINS LATER, HDG WAS AGAIN SELECTABLE. F/D HDG MODE AVAILABLE. NO FURTHER ISSUES. GROUNDED - YES. ACCOMPLISHED B737-900 FIM 22-11 TASK 803. OPS TESSDR ASAA2022122041202Autoland Sys · faultedCAT III AUTOLAND & HGS (7R RWY) NOT SUCCESSFUL.APPROACH WARN LEFT OF CENTERLINE APPROX 150' AGL. GROUNDED - YES. ACCOMPLISHED LAND VERIFY TEST & HGS SYSTEM TEST. ALL TESTS PASSED IAW AMM 22-11-00/201, SMM 34-36-00, SECTION 500.SDR CALA2022122103455Relay · failedSTAB OUT OF TRIM LIGHT LIGHT ON MAIN ELECTRIC AND AUTO PILOT STAB TRIM FAIL. STAB OUT OF TRIM L IGHT SPEED TRIM FAIL LIGHTS ILLUMINATED. PLACED MAIN ELECTRIC AND AUTO PILOT TO CUTOFF AND USED MANUAL TRIM TO RETURN TO EWR. VERBAL FROM CREW. RIGHT AFTER TAKE OFSDR DALA2022121908205Switch · faultedATB, FL 370, DURING CRUISE FLIGHT, BEGAN GETTING SPURIOUS MESSAGES. XPDR1, WXR1, TCASS1, ABSB TFC1, ADSB RPTG1, FQMS1, FUEL LEAK DET, PART DOOR/SLIDE POS, IFE BAY SMOKE DET. ALSO LOST FMS, ACARS, CPDLC, AND NUMEROUS CABIN FNCTS, AC BUSS 1A AND AC BUSS 1B FAULTSDR 2022F00492Autopilot Sys · failedAUTOPILOT FAILED TO DISCONNECT A/P LIGHT WAS EXTINGUISHED.SDR YENA2022120501202Actuator · failedFLT#799, FLL- HAV. AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL, AUTO FLT YAW DAMPER 1, YAW DAMPERS - SYSTEM 1. INSTALLED NEW YAW DAMPER SERVO ACTUATOR IAW AMM 27-26-51. REQUIRES OP CHECK AND LEAK CHECK. REF LOG PAGE 3586051, FOR REMOVAL AND REPLACEMENT OF YSDR UIEA2022120301204Fseu · faultedCLIMBING THROUGH 10,000FT FLAPS UP & IN VNAV, NOTICED THE AIRPLANE SPEED BUG WAS AT 250KTS & THAT THE OVERSPEED TAPE WAS DOWN TO 250KTS. GIVEN A CLIMB TO FL230, BUT ELECTED TO STAY BELOW FL200 AND LEVELED OFF AT FL190 250KTS OF NOTE AT APPROX 14000FT, SLOWED SDR AALA202211278506Computer · faultedAIRCRAFT WAS GROUNDED: ON CLIMB OUT, AUTOPILOT A AND B WOULD NOT ENGAGE. FLIGHT RETURNED TO DFW LANDING SAFELY. REPLACED FLIGHT CONTROL COMPUTER A. REPLACED AILERON POSITION SENSOR M937. ADJUSTED AILERON ACTUATOR INPUT ARM A. ACCOMPLISHED SATISFACTORY OPERSDR ASAA2022112040877Unknown · unknownDURING PREFLIGHT WITH CA FD AS MASTER, NO MODES WOULD ENGAGE. WITH F/O FD AS MASTER, NO LNAV/VNAV MODES WOULD ENGAGE, BUT OTHER MODES ENGAGE OKAY. AIRSPEED WINDOW WOULD NOT CHANGE, WHEN SPINNING SPEED KNOB, WITH FDS OFF AND WITH CA FD ON AS MASTER. SPEED KNOB SDR 2022F00472Computer · inoperativeFLIGHT DIVERTED TO SLCB DUE TO AUTO PILOTO NOT ENGEGNG BOTH LH AND RH. CORRECTIVE ACTION: WAS REPLACED FCC RH IAR AMM22-11-33/401. OPERATIONAL TEST ON GROUND OK.SDR QMLA2023111720005Autopilot Sys · malfunctionedWITH AP ON, IN HEADING MODE, WITH ALT HOLD, UPON INITIATING A 300 FPM DESCENT AND USING THE HEADING BUG TO TURN LEFT OR RIGHT, THE AIRCRAFT ENTERS A DESCENT AT A RATE MUCH HIGHER THAN 300 FPM, FOLLOWED IMMEDIATELY BY A CLIMB WELL IN EXCESS OF 1000 FPM, FOLLOWESDR AALA202210274317Computer · faultyAIRCRAFT WAS GROUNDED: AFTER TAKEOFF FROM MIAMI LOST BOTH FLIGHT DIRECTORS. THEY CAME BACK WHEN LNAV RE-ENGAGED. WHEN ATTEMPTING APPROACH TO BOSTON, BOTH FLIGHT DIRECTORS FAILED. FLIGHT DIVERTED TO PVG, LANDING SAFELY. REPLACED FLIGHT CONTROL COMPUTER A PER AMSDR SWIA202266621None · warning messageMACH TRIM AND STAB TRIM CAUTION MESSAGES ON TAKEOFF. WOULD NOT RE-ENGAGE NORMALLY. SELECTED STAB TRIM DISCONNECT BUTTON. BOTH TRIMS ENGAGED AFTERWARDS. (FLIGHT #4312 FILED CLOSED) COMPLIED WITH FAULT ISOLATION PROCEDURE FOR STAB TRIM MACH TRIM CAUTION MESSSDR CALA2022101202779Control Panel · inoperativeMCP FUNCTIONS IRRATIC AND UNCONTROLLABLE AFTER TAKEOFF. VARIOUS FUNCTIONS ON MODE CONTROL PANEL WERE REPORTED AS INOPERATIVE ONCE THE AIRPLANE WAS AIRBORNE. REPLACED MCP REF AMM 22-11-34 ,ACP INSTALLATION TEST AND LAND VERIFY TEST ,PASSED AMM 22-11-00 ,AIRCRSDR YENA2022092600958None · failedFLT#373, BOS-AUA. '(AIRCRAFT PERFORMED AN AIR TURN BACK TO BOS) ' MCDU 1 BLANK ON CLIMBOUT AT FL 200. THE COMPUTER RESET PROCEDURE WOULD NOT FIX MCDU1; REMOVED AND REPLACED CAPT'S MCDU PER AMM 22-82-12. OPERATIONAL TEST OF MCDU SATISFACTORY.'SDR AALA202209238698Actuator · noneAIRCRAFT WAS GROUNDED: UNCOMMANDED YAW TO THE LEFT IN CRUISE FLIGHT AUTO PILOT1 ENGAGED. NO INDICATIONS ON ECAM. MAINTENANCE REPLACED THE RUDDER TRIM ACTUATOR PER AMM 27-22-51. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.SDR YENA2022092800975Fcu · failedFLT#1388, LAX-BOS. 'FO FD PUSHBUTTON COVER FELL OFF UNABLE TO LOCATE; REMOVED AND REPLACED FCU REF AMM 22-81-12. OPS CHECK OK. AC OK FOR SERVICE.'SDR YENA2022091900926None · failedFLT#41, FLL-MDE. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) ' IN-FLIGHT FMGC 1 FAILED AND BLANKED CAUSING AP1 TO TRIP. CAME BACK AND THEN FAILED WITH 2FD2 DISPLAYED ON PFD PATCH WITH DISPATCH AND MTC MADE JOINT DECISION TO RETURN TO FLL; REMOVED AND REPLACEDSDR QMLA2023090620069Button · inoperativeON FINAL TO KLOM FOR FUEL, EXPERIENCED SUDDEN AND CONSISTENT UN COMMANDED MOVEMENT OF THE CYCLIC IN MULTIPLE AXES, WITH & WITHOUT THE AFCS ENGAGED, AND WITH AND WITHOUT THE FORCE TRIM BUTTON BEING DEPRESSED. ADDITIONALLY, FELT AS IF FORCE TRIM WAS ACTUATING DESDR AALA202209060231None · frozenAIRCRAFT WAS NOT GROUNDED: ON IMC APPROACH ILS 18R, CLEARANCE CANCELED TO NOW FLY RVAV-Z 13R APPROACH. DURING FMS LOADING PRECISELY WHEN RNP .3 WAS ENTERED BOTH FMS 1 & 2 FROZE, BACKUP NAV APPNUCIATED, ALL PERFORMED CALCULATIONS LOST, NO INIT LOAD AND NO SEC FSDR CALA2022083102222None · noneAUTOTHROTTLE DISC ON T/O SUSPECT TMC COMPUTER NIL STK LHR TMC PLACED ON MEL 3 C/BS PULLED AND COLLARED TMC AC, TMC DC AND PLACARDS INSTALLED. MEL 2230A COMPLIED WITH. 22-02-00-815-801. TMC SERVO ON THE P11.AIRCRAFT DOWNGRADED TO AUTOLAND LIMIT 2, DISPATCH DESKSDR YENA2022090200856Computer · faultedFLT#44, LGW-JFK. (ETOPS) 'CREW REPORTS FMGC 1 FAULTED IN FLIGHT; PERFORMED AFS TEST AND LAND CAT II TEST PER AMM 22-01-00. OPS CHECK IS GOOD. NO FAULTS NOTED.'SDR QXEA2022082600278None · noneAUTOTHROTTLE UNCOMMANDED DISENGAGEMENT WHILE ON APPROACH AND SOURCE ON CAPTAIN SIDE. REMOVED FROM SERVICE. PLACED ON MEL 22-30-00(A). CLEARED 8/25/22 REPLACEDTHRUST CONTROL QUADRANT IAW E175 AMM 76-11-01-000/400-801-A. PERFORMED OPS TEST OF THRUST REVERSERS ISDR ASAA2022081539563Computer · warning messageAPP SURVEY NOT SUCCESSFUL APCH WARN AND NO AIII AT APPROX 50' AGL 6 KT TAILWIND RWY 34L ILS AREA CLEAR, SEEMED TO BE DIVING BEFORE FAULT. GROUNDED - YES. ACCOMPLISHED B737-800FIM 22-12 TASK 803 INITIAL EVALUATION (SPD/STB TRIM TEST) IT IS GOOD WITHIN LIMITS, FSDR QMLA2022081920055None · noneSUPPLEMENTAL INFO FOR SDR QMLA2022081920055 AC WAS EXPERIENCING UN-COMMANDED "ROLL" INPUTS WITH AP1 SHOWING "DEGRADED" AND AP2 NORMAL OPERATION. THE FLIGHT SYSTEMS PAGE SHOWED ROLL COMMAND INPUTS-UP SLIGHTLY AND THEN DOWN SLIGHTLY THAT CORRESPONDED WITH CYCLICSDR GTIA2022081136579None · fault messageON DEPT OUT OF PHL HAD A YAW DAMPER 1 FAULT SYSTEM RESET W/MOC PRIOR TO DEPT W/ CB RESET ONCE AIRBORNE STARTED GETTING 2FD2 W/AP DISC THEN GOT CONT WINDSHEAR AURAL WARNINGS AND OCCAL SPEED WARNING NO ECAM. DID FAC 1 RESET W/ NO SUCESS.-PERFORMED A TROUBLESHOOTSDR CALA2022072501877None · faultyA AUTOPILOT WOULD NEVER ENGAGE B A/P WOULD ENGAGE FOR A SECOND AND FAIL .SYSTEM SUSPECTS FAULTY ELEVATOR AUTOPILOT PRESSURE ENGAGE BUTTONS. REPLACED ELEVATOR A/P PRESSURE SWITCH, NO HELP. REPLACED ELEVATOR POSITION SENSOR M929 CAPABILITY.OPS CKS GOOD.SDR QMLA2022071120039Circuit Breaker · faultedAFTER TAKEOFF WHILE AT CRUISE FLIGHT AT 1000 AGL HELISAS AUTO PILOT FAILED IN FLIGHT. AIRCRAFT PITCHED NOSE UP ABOUT 5 DEGREES IN A CLIMB. PIC ARRESTED CLIMB AND ATTEMPTED TO REENGAGE HELISAS MUT SYSTEM WOULD NOT REENGAGE. LANDED BACK AT BASE MECHANIC RESET THSDR YENA2022062900633None · noneFLT#44, LGW-JFK. (ETOPS) 'MCDU 2 NOT PROVIDING SNED PROMPT (*) FOR FLIGHT PLAN-RELATED REQUESTS. SPECIFICALLY: NO PROMPT FOR: INIT / INIT REQUEST AND F.PLN / WIND TEMP/ WIND / TEMP REQUEST. MCDU 2 DID PROVIDE SEND PROMPTS FOR ACARS-DRIVEN FUNCTIONS; RESET FMGCSDR AALA202206072671None · noneAIRCRAFT WAS NOT GROUNDED: REJECTED TAKEOFF APPROXIMATELY 80 KNOTS DUE TO FLIGHT DIRECTOR ISSUES. UPON CONSULT WITH MAINTENANCE CONTROL, PERFORMED INSPECTION AFTER APPLICATION FOR OVERHEAT PER AMM 05-51-16-200-001-A. MAINTENANCE NOTED NO FAULTS ON THE PFR AN
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