JASC 2211
Service difficulty reports · 588
Reports filed under 2211 · Autopilot Computer, 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 = '2211' 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 = '2211' 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 C2XA07CL092Computer · shortedCLEVELAND MAINTENANCE REPORTED THE GUIDANCE CONTROL UNIT (GC-550) HAD SMOKE COMING FROM IT. MAINTENANCE INSPECTED AND REPLACED THE GUIDANCE CONTROL COMPUTER. OPERATIONAL CHECKS WERE GOOD.SDR 2007UALA04298Computer · unknownAIRPLANE HAS PITCH OSCILLATION (PORPOISES) WITH ANY A-P CHANNEL IN CMD AND (V-S, ALT HOLD, FLCH, VNAV) MODE SELECTED. SUSPECT THRUST MANAGEMENT COMPUTER. REPLACED THRUST MANAGEMENT COMPUTER, GROUND TEST OK. AUTOPILOT CAT III CKS GOOD. ACFT OK FOR SERVICESDR 721608242007Computer · failedPATIENT FLIGHT, DURING THE FLIGHT THE MASTER CAUTION ILLUMINATED WITH ACCOMPANYING ROLL SAS CAUTION LIGHT, IMMEDIATELY FOLLOWED BY A STRONG ACRID BURNING ODOR IN THE COCKPIT. NO OTHER ADVERSE INDICATIONS WERE NOTED. SWITCHED OFF ALL SAS CHANNELS AND THE ODOSDR HEEA116156Computer · malfunctionedIN FLIGHT TRIM FAILURE WITH CODE 23-20. COMPLIED WITH EMERGENCY PROCEDURE BUT FAILURE OCCURRED TWICE MORE. EACH TIME RESET AP NR 2 AND TRIM LIGHT WENT OUT. MAINTENANCE REPLACED FLIGHT CONTROL COMPUTER.SDR UPS07M49843Computer · failedINSPECTION TYPE:N/A ATB - FLAP INDICATOR RIGHT SIDE SHOWED FLAPS 14/X WITH FLAP HANDLE UP CYCLED FLAPS TWICE IN FLIGHT. LSAS FAILED MOMENTARILY AFTER AUTO PILOT DISCONNECT. T/S PER AMM 22-00-00 & 27-54-00 FOUND NR 1 FCC FAIL, REPLACED NR 1 FCC & CFDS FCC, AFSDR SWIA200718205Computer · malfunctionedWHILE CRUISING AT 32,000 FEET WITH AUTOPILOT ENGAGED, STAB TRIM AND MACH TRIM MESSAGES APPEARED. NEITHER STAB OR MACH TRIM WOULD RE-ENGAGE. AUTOPILOT WORKED NORMALLY. REPLACED THE NR 2 FCC CARD PER MM 22-12-14. P/N: 622-9815-904, S/N ON: 10JXC, S/N OFF: 1LSDR UIEA200700133Valve · unserviceableWHEN "A" AUTOPILOT IS CONNECTED THE ACF GOES INTO A STEEP DIVE WITH STAB TRIM "A" LIGHT ON ALL ATTITUDE. WHEN AUTOPILOT "B" IS CONNECTED A/C PORPOISES + - 1,200 FRM WITH STAB TRIM "B" LIGHT ON. THIS HAPPENED ABOVE FL 27.0. IF FLYING AT 27.0 IT MAINTAINED A GSDR NOCA00107Computer · malfunctionedCENTER AUTOPILOT FLUCTUATES DURING CLIMBOUT AND CRUISE. LEFT AND RIGHT AUTOPILOT OPERATES NORMAL. REMOVED AND REPLACED CENTER FCC COMPUTER PER MM 22-11-01.SDR CA061211007Computer · faulted(CAN) LEVELING OFF AT 4000 FT, AFCS FAILED, ID802 SHOWED LINES, YD AND FLIGHT DIRECTOR FAILED, CAPT AND F/O ADI`S FLAGGED OFF. AIRCRAFT RETURNED TO ORIGINATING AIRPORT FOR NORMAL LANDING. MAINTENANCE INSPECTION OF FLIGHT FAULT SUMMARY SHOWED FAILURE OF RIGHT SDR MASA200602597Circuit Card · unsecureASH 7295 IAD. Y/D 2 INOP. MX FOUND THE FCC CARD NOT PROPERLY SECURED IN THE IAPS CAGE. MX RESECURED AND OP CHECKED GOOD.SDR 06FDEA03903Computer · malfunctionedNR 1 IRU DEFERRED. ON TAKEOFF ROLL, ALL CAPT AIRSPEED SYMBOLOGY ON AIRSPEED TAPE DISAPPEARED (V1, V2, GREEN DOT, ZIPPER ECT.) WITH FLASHING "SPD LIM" IN RED IN LOWER LEFT CORNER OF PFD. SELECTED ADC INST, SYS 2 ON CAPT SW PANEL. ALL OTHER AIRSPEED INDICATIOSDR DXTA200601682Computer · failedAFTER 1.18 HRS FLT AUTO PILOT KICKED OFF AND WOULD NOT RE-ENGAGE. MT WAS ALSO OFF. REPLACED NR 2 FCC WITH AN OVERHAULED UNIT FROM ROCKWELL COLLINS. OPERATIONAL CHECK GOOD. WORK DONE IN ACCORDANCE WITH F2000 COLLINS DIAGNOSTIC GUIDE 523-0777634.SDR 2006UALA01826Computer · unknownMADE AN UNPLANNED STOP AT DEN DUE TO AUTOPILOT PROBLEM. CREW COMMENTS: UNABLE TO ENGAGE AUTOPILOT L-C-R, L AND C AUTOPILOTS CMD SW GIVES HORN AND LT WARN, R CDM SW NOTHING. THE DISCREPANCY IS ATTRIBUTED TO A MALFUNCTIONING FLIGHT CONTROL COMPUTER. REPLACED SDR HALA0600690Computer · malfunctionedETOPS SIGNIFICANT SYSTEM - NO F/D BARS OR F/D FLAG ON F/O ADI. IND NORMAL WITH INST SOURCE SEL SW "C". NOTE: F/D BARS DISAPPEAR ON F/OS ADI WHEN LNAV AND VNAV SELECTED, F/O BARS RE APPEAR IF HDG SEL AND ALT HOLD SELECTED. PERFORMED TEST 01 30 AND 40 FOUND NOSDR NOCA12806Computer · inoperativeLT FLIGHT DIRECTOR INOPERATIVE. REMOVED AND REPLACED LT FLIGHT CONTROL COMPUTER.SDR HALA0600583Computer · malfunctionedFCC FAIL LIGHT ILLUMINATED ALONG WITH STALL WARN FAULT. REPLACED NR 2 FCC COMP. OPS CHECK OK PER M/M 22-01-03.SDR HALA0600587Computer · faultyON TAXI IN WITH FLAP HANDLE SET TO 18 DEG PFD READS 17 DEG. ALSO WITH 13 DEG SET PFD READS 12 DEG. ALL OTHER SETTINGS READ OK. REPLACED NR 2 FCC PER AMM 22-01-03. OPS CHECK OK. MPN 4083700-902; S/N ON 00070251; S/N OFF 01020323.SDR F3LA200600047Computer · faultyFLIGHT CREW REPORTED A/C DISPLAYED LATERAL WOBBLE (RIGHT) DURING CLIMB ANYTIME RUDDER TRIM >.3 UNITS LEFT, A/S >270. AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. REPLACED NO. 1 FAC AND OPERATIONAL CHECK FLIGHT SHOWED NO VIBRATION. AIRCRAFT RETURNESDR NOCA8606Computer · faultyCENTER AUTOPILOT WILL NOT ENGAGE, ACP BITE CHECK AND MCDP IAW FIM 22-00-02. CENTER AUTOPILOT WILL NOT ENGAGE, PERFROMED FIM 22-00-01, REPLACED CENTER FCC, OPERATION NORMAL.SDR PIDA06044Computer · malfunctionedWHEN AUTO PILOT -B- SYSTEM IS ENGAGED, PITCH MODE FLUCTUATES. REPLACED FCC -B- COMPUTER. OPS NORMAL PER MM 22-11-331.SDR FCPR20060050Computer · failedAUTOPILOT COMPUTER FAILED CAUSING PILOTS ALTIMETER/AIRDATA COMPUTER TO FAIL.SDR 481749002Computer · malfunctionedPILOT REPORTED AUTOPILOT TRIM WHEEL WOULD NOT TRIM AIRCRAFT AS COMMANDED. PROBLEM WAS CAUSED BY THE AUTOPILOT COMPUTER. THERE WAS NO EMERGENCY ACTIONS REQUIRED.SDR PIDA06032Computer · malfunctionedAIRCRAFT WILL NOT DESCEND IN AUTO-PILOT USING VERTICAL SPEED; REVERTS TO LEVEL CHANGE MODE. FOUND FCC B-SYSTEM AT FAULT. PLACED ON MEL 22-1. 03/20/2006: REPLACED FCC -B- AND PERFORMED SATISFACTORY OPS CHECK PER MM 22-11-331.SDR 2006FA0000257Autopilot Sys · intermittentINTERMITTENT PITCH TRIM AND ACCELEROMETER FAILURES. POSSIBLY CAUSED BY INADEQUATE CONNECTOR ENGAGEMENT WITH THE MOUNTING RACK CONNECTORS, CAUSED BY IMPROPER POSITIONING OF THE TOP COVER.SDR PIDA06022Computer · faultyFIRST OFFICER'S FLIGHT DIRECTOR INOP. REPLACED AFCS COMPUTER NR 2. OPS NORMAL PER MM 22-11-331.SDR DL76P060127Computer · failedELECTRICAL ODORS NOTED ON APPROACH, EMERGENCY DELCARED. REPLACED CENTER FCC.SDR HEEA107969Computer · malfunctionedDURING CRUISE AIRCRAFT STARTED UNCOMMANDED DESCENT WITH NOSE PITCH UP. ROTOR SPLIT HIGH TO 107. ESTABLISHED CONTROL. FOUND COLLECTIVE WANTED TO DRIVE FULL DOWN. DISENGAGED COLLECTIVE TRIM AND PROBLEM CEASED. SWAPPED FROM FD NR 1 TO FD NR 2 AND PROBLEM CESDR AU510001587Computer · faulty(AUS) AUTOPILOT COMPUTER SUSPECT FAULTY. (CASA NR 510001587)SDR XN0A1279Control Unit · failedNR 2 YAW DAMPER WILL NOT ENGAGE. TRANSFERRED TO DMI LOG 5951 IAW ENA MEL REFERENCE 22-21-01 CAT-A. REMOVED AND REPLACED YAW DAMPER ENGAGE UNIT, OPS CHECK OK IAW A300 AMM 22-11-12. THIS CLEARS DMI 5951. PLACARDS REMOVED.SDR AU510001850Control Panel · failedAUTOPILOT MODE CONTROL PANEL (MCP) FAILED.SDR AU510001518Computer · faultyAUTOPILOT COMPUTER INTERMITTENT FAULT.SDR DXTA200500783Computer · malfunctionedNR 1 IAC FAILED IN FLIGHT, DU 1, 2, 3, RED X THROUGH SCREENS, NR 1 FMS INOP, NR 1 RMU STILL WORKS, NO HEADING BUG OR ALTITUDE SETTING CAPABILITY EITHER. REMOVED AND REPLACED HONEYWELL PRIMUS 2000 IC800 WITH A REPAIRED UNIT FROM HONEYWELL NR LV2R992K S/N ON : SDR 237TR0010Computer · malfunctionedTHE A-AUTO PILOT WILL NOT ENGAGE IN CWS OR CMD. PLACED A-AUTO PILOT ON MEL 22-1. 03/17/2005: REPLACED A-SYSTEM AFCS PER MM 22-11-331. OPS CHECKS GOOD.SDR TXER100210Potentiometer · inoperativePOTENTIOMETER INOPERATIVE. INCORRECT READINGSSDR 0402225516Computer · burnedDURING DESCENT FLIGHT CREW REPORTED ELECTRICAL SMELL IN COCKPIT. FLIGHT ATTENDANT INDICATED FUMES/SMOKE COMING OUT OF OVERHEAD VENTS AND SOME FLOOR VENTS IN CABIN. DECLARED EMERGENCY AND DID AIR CONDITIONING SMOKE/FUME CHECK LIST. SMOKE LESSENED AFTER PACKSSDR RAIA00407013Computer · malfunctioned5534 - STL - TRIM WARNING LIGHT CAME ON. MAINTENANCE DEFERRED ELECTRIC TRIM IAW MEL. SUBSEQUENTLY REMOVED AND REPLACED AUTO PILOT COMPUTER.SDR CA040601011Annunciator · inoperative'FD' ANNUNCIATOR LIGHT INOP. FLIGHT DIRECTOR COMMAND BARS FUNCTION OK. UNIT REPAIRED AT LOCAL AVIONICS FACILITY, REINSTALLED.SDR BAQA094415Control Unit · inoperativeSTRONG LAT. INPUTS WITH YAW CSAS IN ON POSITON OR STANDBY POSITION, GOES AWAY WHEN SYSTEM IS TURNED OFF. UNIT LASTED 83.6 HOURS SINCE LAST REPAIR. LAST REPAIR, CJ RO 9-090006-17 ; INVOICE NR S29024201.SDR AUS20040385Computer · faulty(AUS) AUTOPILOT COMPUTER FAULTY.SDR AALA20040466Computer · inoperativeLAX - INFLIGHT T032 RETURNED TO LAX DUE TO AILERON LOCKOUT, RUDDER RATIO EICAS MESSAGE AND ALL THREE AUTOPILOTS INOPERATIVE. LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION AND REPLACED LEFT AND RIGHT HAND AIR DATA COMPUTERS (40408009SDR SROM200400052Computer · malfunctionedDURING POST D-CHECK FERRY FLIGHT, RETURNED TO DEPARTURE DUE TO AUTO PILOT CAPTURE LOC VERY SLUGGISH AND OVERSHOOTS DURING CORRECTION. WILL NOT CAPTURE GLIDE SLOPE. ALSO, RADIO ALTIMETER DH LIGHT COMES ON WHEN DH IS SET ABOVE 2500 FT AGL STARTS INDICATING WHESDR SWIA200413122Computer · faultyAT 28,000 FT MACH TRIM STAB TRIM CAUTIONS ON EICAS. UNABLE TO RESET. REMOVED AND REPLACED FCC CARD NR 2 WITH A SERVICEABLE UNIT IAW 22-10-00. OPS CHECKS GOOD. ALSO REMOVED AND REPLACED HSTCU WITH A SERVICEABLE UNIT ALONG WITH STAB TRIM/MACH TRIM ENGAGEMENTSDR SWIA200413101Computer · malfunctionedFIRST OFFICER'S SIDE AUTO PILOT HAD SEVERAL -TRIM FAIL- AURAL WARNINGS WITH ASSOCIATED RED -TRIM- FAIL LIGHTS. REPLACED FIRST OFFICER'S AUTO PILOT COMPUTER. OPS CHECK GOOD.SDR HE66094001Autopilot Sys · intermittentAUTO PILOT FAILED INFLIGHT. AFTER RESETTING AUTOPILOT, IT WOULD FAIL AGAIN.SDR BAQA093736Computer · failedAUTOPILOT FAILS SELF-TEST. CODE 1E17. REPLACED WITH SERVICABLE ASSET UNIT. 03/12/2004SDR 2004UALA00191Computer · malfunctionedLIGHTNING STRIKE ON FWD RADOME AND F/O WINDSHIELD WITH STATIC DISCHARGE. POSSIBLE RADIOS/NAVIGATION INTERMITTENT. ON APPROACH TO ICN, CREW REPORTED THE AUTOPILOT DISCONNECTED, IT WAS RESET BY CREW AND TRIPPED AGAIN. THERE WERE ALSO ABNORMAL ILS INDICATIONS.SDR SWIA200412969Computer · faultyAFTER SELECTING A NEW HEADING WHILE IN HDG MODE, THE A/C CONTINUED TURNING THROUGH THE NEW HEADING (OPPOSITE THE FLIGHT DIRECTOR COMMANDS) AND THEN JERKED SUDDENLY TO THE LEFT TWICE. THE A/P DISCONNECTED ON ITS OWN. REMOVED AND REPLACED FCC NR 1 IAW MM 22-12SDR GAIA04037OPComputer · malfunctionedFLT 578 - SFO-PHX-FWA - AUTOPILOT DIFFICULT TO ENGAGE IN CRUISE. REMOVED AND REPLACED THE PITCH CHANNEL COMPUTER. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR HEEA093675Amplifier · burnedSMELLED ELECTRICAL FUMES DURING FLIGHT. LANDED AT MP299B. MAINTENANCE FOUND YAW CHANNEL AMP BURNED.SDR GAIA04029OPComputer · malfunctionedDURING CRUISE THE AIRPLANE OCCASIONALLY TURNS RIGHT AND WILL NOT RESPOND BACK TO THE LEFT WITH FULL AUTOPILOT HEADING DEFLECTION TO THE LEFT. FLIGHT CONTINUED AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED THE AUTO PILOT ROLL CHANNEL COMPUTER. SYS
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