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 UALA2012042702517Computer · faultyRIGHT PFC COMPUTER REQUIRES REPLACEMENT PER LINE COA 209901. REPLACED RIGHT PFC COMPUTER PER AMM.SDR RYNA201203200016Unknown · malfunctionedAIR TURNBACK LOST AUTOTHROTTLES, AUTO PILOTS, BOTH FMA AND FLIGHT DIRECTORS. PERFORMED RETURN TO SERVICE CHECK ON NR 1 AND NR 2 FMGS IAW AMM 22-01-05. NO FAULTS NOTED. BOTH SYSTEMS CHECK OK.SDR HNAA2011111400383Circuit Card · failedDURING TAXI, AFTER STARTING NR1 ENGINE, DC BUSS CAUTION LIGHT ILLUMINATED. AFTER SELECTING NR 1 DC GENERATOR OFF, POPPING SOUND UNDER LT GLARESHIELD, FOLLOWED BY MINIMAL SMOKE. MX INSPECTED AND FOUND AUTOPILOT CIRCUIT CARD FOR ANNUNCIATOR PANEL BURNED AND CIRSDR HALA2011100500428Warning Light · illuminatedETOPS SIGNIFICANT SYS - "AUTO FLT FM 1 FAULT" IN FLIGHT AT CRUISE. STATUS CAT 3 SINGLE ONLY INOPERATIVE SYS API FM1 CAT 3 DUAL. ACCOMPLISHED TSM 22-70-00. NO FAULTS NOTED. TEST PASS.SDR CA110714005Ahrs · malfunctioned(CAN) DURING FLIGHT TEST, IN HOVER AT APPROXIMATELY 5FT ABOVE GROUND, PILOT ENCOUNTERED FLIGHT CONTROL ANOMALIES. AIRCRAFT LANDED SAFELY. INVESTIGATING ROOT CAUSE(S).SDR CA110606015Cable · bindingUPON CARRYING OUT A SECONDARY INSPECTION OF THE S-TEC-65, AUTOPILOT INSTALLATION OF THE SERVOS, FOUND THAT THE SECONDARY OR RETURN PITCH SERVO CABLE WAS CAUGHT ON THE PITCH SERVO ON ONE OF THE SCREWS. THE WAY THAT THE CABLE BECAME CAUGHT ON THE PITCH SERVO SDR 2011F00091Instrument Panel · multiple failDURING CRUISE FLT, CREW REPORTED, LOST BOTH NR1 AND NR2 DFGC. NO AUTO PILOT, NO AUTO THROTTLES, NO FLIGHT DIRECTORS. DISPATCH WAS ADVISED, ADVISED AND REROUTED ACFT FOR REPAIRS.SDR CA110228013Servo · malfunctioned(CAN) SERVO PRODUCING UNCOMMANDED MOVEMENT DURING FLIGHT, NOT APPARENT DURING GROUND OPERATION.SDR UALA2011021800839Cap · out of toleranceA-T DISC LIGHT ON P1-3 PANEL INOP. REPLACED LIGHT SWITCH CAP, OPS CHECKED OKAY.SDR CA110120001Servo · failedDURING CLIMB OUT, A MASTER CAUTION KEPT APPEARING SAYING "AUTOPILOT AILERON TRIM LT WING LOW". THIS CAME ON AND OFF SEVERAL TIMES. QRH WAS RUN AND IT ORDERED THE DISCONNECTION OF AUTOPILOT WHICH WAS DONE. SO THE PILOT IS IN A POSITION WHERE THE MEL FOR THE FSDR UALA2011011300219Autopilot Sys · disengagedAUTOPILOT DISENGAGED, FLIGHT DIVERTED. THIS OCCURRED 4 TIMES IN FLIGHT, ALSO HAD THE AUTOTHROTTLE DISENGAGE, AND THE NAV SCREENS GO BLANK WITH THE AUTOPILOT KICKING OFF. MX REMOVED FCU TO CHECK FOR DAMAGED PINS OR SOCKETS - NONE FOUND. REPLACED FCU CONTROSDR UALA2010122004644Iru · faultyNO LAND 3 IN ASA AFTER ADIRU ALIGNED. MCDP TEST 30 FAILED "ADC-I RU R" WITH INTERMITTENT NR2 IVSI INOP. FLAG IN VIEW. NEW IVSI AND ADC, NO HELP. NEW IRU CORRECTED PROBLEM. ORIGINAL IVSI AND ADC REINSTALLED--ALL UNITS TEST OK.SDR UALA2010112304333Servo · failed2 YAW DAMPER DISPLAYED ON EICAS AND YAW DAMP INOP LIGHT ILLUMINATED RIGHT AFTER TAKEOFF. TESTED RIGHT YAW DAMPER. TEST FAILED FAULTING THE RIGHT YAW DAMP ACTUATOR. LEFT YAW DAMPER OPS NORMAL PER MM, FAILED RT YAW DAMPER ACTUATOR. REPLACED RT YAW DAMPER SERSDR C8GA201000058Unknown · unknownDURING TAKEOFF ROLL WITH THROTTLES ADVANCED AND EPR CALLED, THE THROTTLERS DID NOT ENGAGE FOR TAKEOFF. THE TAKEOFF WAS ABORTED. POST FLIGHT INSP WAS PERFORMED WITH NO DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR QXEA2010101900654Unknown · unknownCLIMBING THROUGH 25,500 WITH SPEED AT 290 KTS. SELECTED, THE SELECTED SPEED ROLLED BACK TO 270K. RETURNED TO THE FIELD, LANDING UNEVENTFUL. COMPLIED WITH SL REV E. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.SDR DXTA2010101204258Autopilot Sys · unknownCLIMBING THROUGH FLIGHT LEVEL 380 WITH THE AUTO PILOT ON AND FLIGHT LEVEL CHANGE SET TO .65, THE ACFT PITCHED UP TO APPROX 10 DEGREES. THE VERTICAL SPEED INDICATED A CLIMB OF OVER 3000 FT PER MINUTE. ACFT LOST 18 KNOTS INDICATED AND STARTED TO EXPERIENCE BUFFSDR 2010F00194Computer · failedDURING CRUISE, THE PILOT NOTICED A BURNING ODOR AND THAN NOTICED THAT THERE WAS SOME LATERAL INPUTS IN THE HELICOPTER , THE PILOT THAN PERFORMED A PRECAUTIONARY LANDING. IT WAS LATER DETERMINED THE THE BURNING ODOR WAS COMING FROM OUTSIDE AND THAT THE HELIPILSDR HALA2010021100062Autopilot Sys · unknownETOPS SIGNIFICANT SYSTEM - TUNED AND IDENTIFIED APPROACH ARMED, AUTOPILOT AND FLIGHT DIRECTOR WOULD NOT CAPTURE LOCALIZER OR GLIDESLOPE, NO GLIDESLOPE INDICATION ON ADI. PERFORMED LOCALIZER, GLIDESLOPE AND ILS TEST WITH CURRENT CALIBRATED RAM TEST SET T-300 BSDR UALA2010011300173Control Panel · faultyFMGC NR 2 FAULT, RTFL. IN FLIGHT CB RESET: F-O MAP MODE WAS NOT AVAILABLE. REPLACE FMGC 2 AND PERFORM CAT 3 TEST. PFR FAULTS FMG2-RMP2. REPLACED FMGC2 AND RMP 2. PERFORMED AFS AND LAND TEST. OPS CHK NORMAL. RETURNED AC TO CAT III, NO MESSAGES.SDR CA090808002Autopilot Sys · malfunctionedREPORTING TO FLIGHT OPERATIONS: AFTER ROTATION F/O CALLED FOR "GEAR UP, SPEED MODE". AFTER PRESSING SPEED MODE BUTTON THE FMA REFERENCE REPORTED CLB 40 AND THE FLIGHT DIRECTOR SLOWLY BEGAN COMMANDING A HIGHER PITCH ATTITUDE THAN NORMAL. ACFT WAS BEING HANDFLSDR ULXR2009070282608Unknown · multiple failLOW TORQUE INDICATION (30-40 PERCENT) ON BOTH PILOT'S AND COPILOT'S PFD/MFD DURING MAX GROSS WEIGHT TAKEOFF. CAS INDICATIONS: 1 AP FAIL, AVIONIC FAULT, 1 AHRS FAIL, AFCS DEGRADED.SDR 2009F00027Cable · damagedFAILURE OCCURRED WITH THE AUTOPILOT ROLL SERVO BRIDLE CABLE. THE BRIDLE CABLE APPARENTLY JUMPED AND OVERLAPPED ITSELF ON THE SERVO SPOOL, EFFECTIVELY JAMMING THE AILERON DURING CLIMB OUT IN A TURN TO THE LT. THE AP WAS NOT ENGAGED AT THE TIME AND THE PIC WAS ASDR HEEA123787Transducer · inoperativeDURING CRUISE FLIGHT, AFTER CLIMBOUT, ACFT YAWED 2 OR 3 TIMES, NR 2 ENGINE OUT LIGHT ILLUMINATED AND AUDIO SOUNDED FOR ABOUT 2 SECONDS THEN RETURNED TO NORMAL. RETURNED TO BASE AND NOTIFIED MX. MX REPLACED THE DECU COLLECTIVE POSITION TRANSDUCER.SDR CA090428001Autopilot Sys · malfunctioned(CAN) PILOT REPORTS THAT THEY GOT AN AUTO PILOT PITCH TRIM CAUTION MSG. FOLLOWED THE QRH AND DISC THE AUTO PILOT AND TRIM THE PLANE MANUALLY. ACFT WOULD NOT TRIM. TRYING TO NOSE THE ACFT OVER TOOK EXCESSIVE FORCE AT WHICH TIME THE ACFT ROLLED TO THE RT. THE CRSDR DXTA2009010103454Servo Drive · inoperativeDURING DESCENT, AUTOPILOT BEGAN TO ASCILLATE (ROLL). DISENGAGED THE AUTOPILOT. AFTER LEVELING AR 15,000, WE ATTEMPTED TO RE-ENGAGE THE AUTOPILOT, BUT WERE UNABLE. CONCURRENTLY, THE "YD FAIL LOWER B" CAS MESSAGE WAS OBSERVED. AUTOPILOT WOULD NOT ENGAGE. ONSDR U0GA2009122580145Autopilot Sys · malfunctionedWHILE ON A FULLY COUPLED ILS 15, ON THE PILOT SIDE (NR 1 SIDE), SEVERAL SECONDS BEFORE THE OCCURRENCE, ACFT WAS HUNTING FOR THE GLIDE SLOPE. WHILE COUPLED THE AFCS WAS MAKING CORRECTION FOR THE GLIDE SLOPE THEN MADE AN ABRUPT NOSE UP OF ABUT 40-60 DEGREES NOSSDR UIE2008F00036None · noneATB. BOTH AUTOPILOTS A AND B WILL NOT ENGAGE (BOTH TESTED OK ON GROUND). A/P A AND B PITCH AND ROLL COMPUTERS, ASTU AND M AND LU BITE CHECK ALL OK. FLT CTL HYD POWER SHUT OFF SWITCHES ALL CHECKED IN ON POSITION. A/P ACCESS BOXES INSTALLATION SECURED. MSP ELECSDR J4P2008F00000Autopilot Sys · failedFLIGHT ORIGINATED AT PBI TO CCO AT 1319L WITH 2 PAX, WHILE EN ROUTE AUTO PILOT FAILED AND DIVERTED TO SGT AND WITHOUT INCIDENT. (A)SDR 2008FA0000502Amplifier · inoperativeAFTER (1) HOUR DISENGAGES AUTOPILOT. PRELIMINARY INSPECTION RESULTS, NO DEFECTS NOTED AFTER BENCH CHECK. (K)SDR 2008FA0000496Trim Switch · inoperativeAFTER INSTALLATION OF NEW AUTOPILOT SYSTEM, AUTOPILOT COMPUTER TRIM CIRCUITRY FAILED ON INITIAL CHECK OUT, OCT 02, 2007. COMPUTER WAS RETURNED TO MFG AND REINSTALLED AFTER REPAIR. TRIM CIRCUITRY FAILED AGAIN AND WAS RETURNED TO MFG ON JAN 18, 2008. MFG TECHSDR 2008FA0000486Trim Switch · failedAFTER INSTALLATION OF NEW AUTOPILOT SYSTEM, AUTOPILOT COMPUTER TRIM CIRCUITRY FAILED ON INITIAL CHECK OUT, 10/02/2007. COMPUTER WAS RETURNED TO MFG AND REINSTALLED AFTER REPAIR. TRIM CIRCUITRY FAILED AGAIN AND WAS RETURNED TO MFG ON 1/18/2008. TECH SUPPORT SDR ARWA20080403Control Panel · damagedHEADING KNOB WORKING IN FAST MODE ONLY. ENTERED ON DMI NR 21598 AS PER MEL 22-1-(L) CAT "C". REMOVED AND REPLACED HDG GUIDANCE CONTROL PANEL IN ACCORDANCE WITH M/M 22-00-00. CHECK GOOD IN ACCORDANCE WITH M/M 22-00-00. CLEARED DMI NR 21598; PLACARD REMOVED.SDR WGEA200800041Autopilot Sys · malfunctionedON FLIGHT FROM SAV TO GNV DURING CRUISE, AUTO PILOT TRIMMED 79 PERCENT LWD. AIRPLANE FLEW NORMALLY WITH A/P DISCONNECTED, 79 PERCENT LWD EARLIER LEGS, AILERON TRIM 0 TO 10 PERCENT LWD. PERFORMED FLIGHT CONTROL CHECKS IAW EA500 AMM 27-00-00. NO DEFECTS NOTEDSDR N93A23032008Unknown · malfunctionedFLYING THRU MODERATE TURBULENCE THE AUTO PILOT , YAW DAMPENER, FLIGHT GUIDANCE COMPUTER, AND MACH TRIM. ALSO, STICK SHAKER ACTIVATED ALTHOUGH AIRCRAFT WAS TRAVELING AT 270 KNOTS. AIRCRAFT WAS INSPECTED AND SYSTEM OPS CHECKS COMPLETED. NO DEFECTS FOUND.SDR IXXA080007OTransfer Valve · defectiveAFTER ROTATION FROM KLRD AIRCRAFT DID A UNCOMMANDED YAW TO THE LEFT AND RIGHT, THE CREW TURNED YAW DAMPER OFF AND OSCILLATION DAMPENED OUT. THE CREW RETURNED TO KLRD AND LANDED WITH OUT INCIDENT. MAINTENANCE DEFERRED THE AUTO PILOT SYSTEM IAW ATI MEL 22-01-0SDR WGEA200800030Ahrs · malfunctionedON CLIMB-OUT , AHRS FAILED AND STICK PUSHER FAILED. SUPPLEMENTAL INFORMATION, REMOVED AND INSTALLED AHRS NR 1 IAW EA 500 AMM 34-20-11. PERFORMED ATTITUDE AND DIRECTION SYSTEM ADJUSTMENT TEST FOR AHRS. SYSTEM CHECKS GOOD IAW 34-20-10. DURING TROUBLESHOOTINGSDR E0X2008F00001Unknown · unknownON APPROACH, AT 3000 FT, EXPERIENCED A PARTIAL PANEL FAILURE ON THE CAPT EADI, EHSI, MFG. TRANSFERRED CONTROL OF AC TO THE F/O. SELECTED THE NR 2 AFSC AND 30 SECONDS THE AC DEPARTED LEVEL FLIGHT AND STARTED AN UNCOMMANDED DESCENT. AT 2700 FT BOTH FLIGHT CRESDR MALA070174Relay · unknownL ROLL INDICATION TRAVELED FULL UP ON ITS OWN. ALL CAUTION LIGHT CAME UP. AUTOPILOT WAS ON. RETRIMMED THE L AILERON. REPLACED AUTOPILOT TRIM SERVO RELAYS, FLIGHT CONTROL COMPUTER, AILERON TRIM ACTUATOR, TRIM CONTROL PANEL. REF CONT CARD FOR DETAILS. NR 1SDR 753003Yaw Damper · faultyHAD SEVERAL HARD RUDDER KICKS. FOUND THAT SHUTTING DOWN LOWER YAW DAMPER PROBLEM WENT AWAY. DEFERRED ITEM IN ACCORDANCE WITH DDPG PROCEDURES 22-3. REMOVED AND REPLACED LOWER YAW DAMPER COMPUTER IN ACCORDANCE WITH AMM 22-16-02. OPERATIONAL CHECK GOOD. DEFERRSDR DXTA200702459Autopilot Sys · malfunctionedCLIMBING OUT OF 5,000 FT, AUTOPILOT WAS ENGAGED THEN DISENGAGED WITH AN ABRUPT PITCH UP MOMENT. SHORTLY AFTER RETRIMMING, A/P DISENGAGED AGAIN, BUT WITH NO PITCH CHANGE. IT WAS DECIDED NOT TO RE-ENGAGE THE A/P. A SHORT TIME LATER WE RELIZED THAT WE HAD A JASDR HEEA116983Autopilot Sys · unknownDURING HOVER FOR TAKEOFF, AFCS KICKED HARD. LANDED AIRCRAFT GROUND TAXIED TO PARKING. MAINTENANCE INSPECTED THE AIRCRAFT, CONNECTED A HYDRAULIC MULE AND WORKED ALL CONTROLS. THEY WERE UNABLE TO DUPLICATE THE DISCREPANCY.SDR HEEA116943Control Switch · malfunctionedDURING TAKEOFF, AFTER RELEASING THE FORCE TRIM BUTTON AT (4), CYCLIC WOULD COME AFT. MAINTENANCE INSPECTED THE AIRCRAFT, CONNECTED A HYDRAULIC MULE AND WORKED ALL CONTROLS. THEY WERE UNABLE TO DUPLICATE THE DISCREPANCY.SDR SIMA200721404Switch · pinchedPTRIM MAIN INOP MESSAGE FOLLOWED BY PTRIM BACKUP INOP MESSAGE. FOUND PILOTS AUTO PILOT/TRIM/PUSHER DISCONNECT SWITCH PINCHED. REPOSITIONED WIRES. SYSTEM OPERATIONAL CHECK GOOD IAW EMB 27-11-00-700-803A AND AMM 27-40-00. AIRCRAFT RETURNED TO SERVICE.SDR DXTA200702284Unknown · unknownAT 13,000 FT, WITH THE AUTOPILOT ENGAGED, THE AIRCRAFT BEGAN AN UNCOMMANDED ROLL TO THE RT. THE ALTITUDE REMAINED LEVEL. [07-12-07] INSPECTED AUTOPILOT SYSTEM NO FAULT CODES WERE RECORDED IN THE FCC COMPUTER. FOUND CIRCUIT BOARD CARD A194 LOOSE. RESECURESDR 07FDEA02033Unknown · unknownSHORTLY AFTER T/O A/C ACTED AS IF THERE WAS GROUND SENSING PROBLEM, MALFUNCTIONS TO INCLUDE; ATS 1, PITCH TRIM 1, ALL THREE PITOT PROBE, CAPT TAT, BOTH PRESS CONTROLERS: GEAR WOULD NOT RETRACT SYS 1, A/P 1&2 INOP. INSTALLED NEW NOSE STRUT SENSOR 55GB PRSDR FDKA200705192Unknown · unknownAUTO PILOT ROLLED RIGHT IN FLIGHT AND AUTO PILOT FAILED IN FLIGHT. MX PERFORMED OPS CHECK OF AUTO PILOT SYSTEM AND OPS CHECK NORMAL.SDR 2007UALA01161Power Supply · failedFLIGHT DIVERTED WITH A RUDDER PROBLEM. *S/D* REPLACED ELAC 1. UNIT FAILED MPS STRESS TEST AT OVERHAUL AND MPS T1 WAS REPLACED.SDR 2007FA0000317Transducer · malfunctionedALTITUDE HOLD WAS INOPERATIVE. WHEN SELECTED THE A/C WOULD PITCH EITHER UP OR DOWN IMMEDIATELY, OR THE A/C WOULD MAINTAIN ALTITUDE FOR A SHORT TIME AND THEN PITCH IN EITHER DIRECTION. COMPUTER AND PRESSURE TRANSDUCER WERE SENT TO STEC FOR TESTING. BOTH UNITS SDR 2007FA0000316Transducer · malfunctionedALTITUDE HOLD WAS INOP. WHEN SELECTED THE A/C WOULD PITCH EITHER UP OR DOWN IMMEDIATELY, OR THE A/C WOULD MAINTAIN ALTITUDE FOR A SHORT TIME AND THEN PITCH IN EITHER DIRECTION. COMPUTER AND PRESSURE TRANSDUCER WERE SENT TO STEC OF TESTING. BOTH UNITS WERE RETSDR 2007FA032201Servo · malfunctionedDIFFICULTY OCCURRED UPON DESCENT. PILOT DISENGAGED AUTO-PILOT AND FELT RESISTANCE IN THE ELEVATOR CONTROL SYSTEM. ON INSPECTION OF THE SYSTEM THE AUTO-PILOT ACTUATOR WAS FOUND PARTIALLY ENGAGED. UNIT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THIS A
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