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 SWIA200412891Computer · faultyFIRST OFFICERS' AUTOPILOT FAILED AND THE ELEVATOR SERVO LIGHT ILLUMINATED. CHECKED ASSOCIATED WIRING ON CONNECTORS BEHIND APC NR 2, NO DEFECTS. REMOVED AND REPLACED APC NR 2. OPS CHECK GOOD ON GROUND OPERATIONS IAW MM 22-10-00.SDR GAIA04022OPComputer · malfunctionedDURING CRUISE, THE AUTOPILOT OVER CORRECTS ON LOCALIZER. REMOVED AND REPLACED THE ROLL CHANNEL COMPUTER. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M)SDR SWIA200412880Computer · faultyAIRCRAFT OSCILLATES UP AND DOWN WITH NR 2 AUTOPILOT ENGAGED. COMMAND BARS MOVE AROUND. REPLACED NR 2 APC-65B WITH SERVICEABLE UNIT. OPS CHECK GOOD.SDR SWIA200412860Computer · malfunctionedCOMPUTER FLAG ON F/O'S ADI INTERMITTENTLY. ASSOCIATED CAUTIONS AND A/P DISCONNECTED. RECEIVED ONE NOSE DOWN PITCH ABOUT 3 DEGREES AND THEN CORRECTED ITSELF. REMOVED AND REPLACED NR 2 A/P COMPUTER. OPS CHECKED GOOD ON GROUND TEST. P/N 622-8315-402, S/N ONSDR GAIA04020OPComputer · malfunctionedDURING CRUISE, THE AIRCRAFT PITCHES UP AND DOWN WITH THE AUTOPILOT IN B-MODE. REMOVED AND REPLACED THE PITCH CHANNEL COMPUTER. OPS CHECK GOOD. AIRCRAFT WAR RELEASED FOR SERVICE. (M)SDR BAQA092357Computer · malfunctionedDH LIGHT ON PILOT AND CO-PILOTS ADI DOESN"T EXTINGUISH. REPLACED WITH SERVICABLE UNIT. 01/26/2004SDR BAQA092793Computer · inoperativeUNIT IS BEING SENT TO AEC FOR WARRANTY REPAIR. REASON FOR REMOVAL, BOTH ROLL ACTUATORS WERE INOPERATIVE. REPLACED WITH SERVICEABLE UNIT FROM ASSET (S/N 545)SDR BAQA092756Computer · inoperativeAPI LIGHT STAYS ON AND A/P WILL NOT TEST. REPLACED WITH SERVICABLE ASSET UNIT. 02/20/2004SDR AWXA200400056Computer · malfunctionedJFK - AIR TURNBACK - FLT 0011 - AFTER TAKEOFF FROM JFK EN ROUTE TO PHX RECEIVED A DUAL FLIGHT MANAGEMENT GUIDANCE COMPUTER FAIL AND IR 3 FAULT, TURNED BACK TO JFK. MAINTENANCE PERFORMED A COMPLETE SYSTEM RESET. PERFORMED AUTO FLIGHT SYSTEM TEST IAW AMM 22-46SDR 03353634Computer · faultyDURING AIRCRAFT OPERATION THE CREW REPORTED UNCOMMANDED RUDDER MOVEMENT. THE FLIGHT CONTROL COMPUTER WAS IDENTIFIED AS THE SOURCE OF THE PROBLEM AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVSDR 03348672Computer · faultyDURING DESCENT THE CREW REPORTED THE AIRCRAFT ROLLING TO THE RIGHT 2 TO 3 DEGREES PER SECOND. FLIGHT LANDED WITHOUT INCIDENT AND PASSENGERS DEPLANED NORMALLY. THE FAULT WAS FOUND TO BE FLIGHT CONTROL COMPUTERS AND THEY WERE REPLACED. A SATISFACTORY OPERATIOSDR SWIA200312687Computer · malfunctionedAUTOPILOT SELF-DISCONNECTED SEVERAL TIMES ON APPROACH. REMOVED AND REPLACED FCC NR 2 IAW MM 22-12-14. AUTOPILOT OPS CHECK GOOD IAW MM 22-11-00.SDR 03340311Computer · inoperativeDURING APPROACH TO IAD CREW REPORTED THE AUTOPILOT SYSTEM PITCHING UP AND DOWN WHILE AIRCRAFT WAS UNDER CAPTAINS CONTROL. NO EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFUL AND PASSENGER DEPLANED NORMALLY. THE FCC WAS FOUND TO BE FAULTY AND WAS REPLACED.SDR COMA0360509Computer · malfunctionedFLIGHT 5184 IAPS DEGRADED RESET THE IAPS.SDR SWIA200312590Computer · faultyCAPTAIN'S COMMAND BARS ON THE FLIGHT DIRECTOR ALWAYS INDICATE ABOUT 4 DEGREES TOO LOW. REPLACED APC-65B COMPUTER. OPS CHECK GOOD IAW MM 22-11-00.SDR 304AW0002Connector · dirtySPEED TRIM FAIL LIGHT ILLUMINATED DURING FLIGHT. PLACED ON MEL 22-10. CLEANED AND RESECURED CANNON PLUG ON FCC PER MM 22-11-33. PERFORMED BITE TEST PER MM 22-11-01. TEST PASSED. CLEARED MEL.SDR SWIA200312585Computer · malfunctionedYAW ENGAGED, RUDDER TRIM AT 6, WHEN AUTO-PILOT ENGAGED, PLANE YAWED LEFT AND RIGHT HARD MOMENTARILY. REMOVED AND REPLACED F/O'S APC 65B IAW MM 22-10-02. OPS CHECK GOOD.SDR CA031023001Circuit Card · malfunctioned(CAN) IN CRUISE THE RUDDER MOVED WITH NO INPUT CAUSING YAW. THE MOVEMENT WAS INTERMITTENT ALWAYS RETURNING TO NEUTRAL. REPLACED FCC CARD AND YAW DAMPER ACTUATOR, CHECKS SERVICABLE.SDR SWIA200312540Computer · faultyWHEN AP ON CAPT'S SIDE, TRIM FAIL AND RED AUTO PILOT FAIL ON MAP AND COMPUTER FLAG ON CA ATTITUDE. FGS 1 DC CIRCUIT BREAKER POPPED. REMOVED AND REPLACED NR 1 APC-65 IAW MM 22-10-02. OPS CHECK GOOD. 622-8318-402, S/N ON: 1641, S/N OFF: 3788.SDR SWIA200312537Computer · faultyCAPTAIN'S AUTOPILOT FAILED IN FLIGHT DURING CLIMB. REMOVED AND REPLACED CAPTAIN'S APC-65B. OPS CHECKS GOOD.SDR SWIA200312524Computer · malfunctionedDURING FLIGHT, THE CAPTAIN'S FLIGHT DIRECTOR COMMAND BARS DEVIATED FROM LEVEL TO +/- 5 DEGREES. NOSE DOWN PITCH, FOLLOWED BY AN AUTOPILOT FAILURE MAP INDICATION. REMOVED AND REPLACED NR 1 AUTOPILOT COMPUTER IAW EMB-120 MM 22-10-02. OPS CHECK NORMAL.SDR 03289317Computer · faultyTHE ELECTRIC ELEVATOR TRIM WAS IDENTIFIED AS BEING INOPERATIVE AND THE AUTOPILOT SYSTEM WAS DISENGAGED TO IN ABLE MANUAL TRIM VIA THE TURN WHEEL. THE FCC CARD IN THE AUTOPILOT COMPUTER WAS REPLACED.SDR BAQA088952Computer · inoperativeCSAS COMPUTER UNIT IS INOPERATIVE. REPLACED WITH REPAIRED, SERVICEABLE UNIT.SDR BAQA089232Computer · failedPITCH AND ROLL CSAS KEEP KICKING ON AND OFF. REPLACED WITH SERVICEABLE UNIT. 9/23/03SDR SWIA200312406Computer · malfunctionedALTITUDE HOLD ON CAPT SIDE WILL DRIFT 150' DOWN. REPLACED AUTO PILOT COMPUTER APC-65B. OPS CHECK GOOD IAW MM 22-10-00.SDR 250TR0023Computer · inoperativeFIRST OFFICER'S FLIGHT DIRECTOR FLAG IN VIEW DURING FLIGHT. REPLACED NR 1 AND NR 2 FLIGHT CONTROL COMPUTER IAW MM 22-11-331.SDR SWIA200312373Computer · malfunctionedF/O'S A/P - F/D INTERMITTENTLY DISCONNECTED INFLIGHT WITH ASSOCIATE A/P FAILED. REPLACED NR 2 A/P COMPUTER. INSTALLED NEW PINS/SOCKETS ON PITCH TRANSFER RELAYS K0311, K0310, K0312 AND K0256. INSTALLED NEW RELAY SOCKETS FOR RELAYS K0310 AND K0312 AND REPLACESDR SWIA200312360Computer · malfunctionedAUTOPILOT FAILS WHEN SELECTED TO F/O'S SIDE. TRIM FAIL & AUTOPILOT FAIL ON MAP & T, P, & E ON AUTO PILOT PANEL. ILLUMINATE WITH ASSOCIATED FAILURE. F/O'S FLIGHT DIRECTOR BARS AT TIMES ERACTIC WITH PITCH UP COMMANDS. REMOVED AND REPLACED AUTOPILOT COMPUTER SDR SWIA200312353Computer · malfunctionedF/O AUTOPILOT FAILING AFTER 2 MINUTES INFLIGHT. INDICATION LIGHTS: R & E AMBER, FCP AP, GLARE AP FLICKERING DURING FAILURE. REPLACED NR 2 AUTOPILOT COMPUTER. OPS CHECK GOOD.SDR COMA0360389Computer · malfunctionedFLIGHT 5307 RUDDER YAWS IN FLIGHT WITH AUTO-PILOT OFF. REPLACED THE NR 1 FCC CARD.SDR SWIA200312303Computer · malfunctionedFO AUTOPILOT FLIGHT DIRECTOR NOSE DOWN 10 DEGREES. AUTOPILOT FAIL AND TRIM FAIL MASTER WARN ON MAP ASSOC WITH RED TRIM AND AP LIGHTS ALSO GREEN VS AND AMBER DIS. REMOVED AND REPLACED NR 2 APC 65B IAW 22-10-00. OPS CHECK GOOD.SDR AUS20030870Computer · failed(AUS) FLIGHT DIRECTOR COMPUTER FAILED.SDR AUS20030800Panel · faulty(AUS) MODE CONTROL PANEL (MCP) FAULTY. INVESTIGATION FOUND ANALOGUE SENSOR Q145 FAILED. CONNECTORS CONTAMINATED WITH METAL PARTICLES.SDR U30A200300028Computer · inoperativeDURING DESCENT ON FLT 581 ATL-CUN, NR 1 FCU (FLIGHT CONTROL UNIT) WENT INOP.UNIT WAS DEFERRED PER MEL 22-81-01 ON GND IN CUN. IN ORD ON 5 AUG 03, REPLACED FCU IAW AMM 22-81-12-401 AND ALL SYSTEM CHECKS PERFORMED GOOD. AIRCRAFT RETUNED TO SERVICE. NOTE REVISED SDR ARWA20030701Computer · malfunctionedLOG PAGE 504844. RUDDER KICKING AFTER TAKEOFF AND OSCILATING. FOUND YAW CHANNEL COMPUTER; REMOVED AND REPLACED YAW CHANNEL COMPUTER AND PERFORMED OPERATIONAL CHECK SYSTEM IAW MM 22-10-37 CHECKED GOOD. CHECKED AND PERFORMED RUDDER OPERATIONAL CHECK IAW MM 27SDR WRLA200313Computer · failedDURING CLIMB-OUT WITH AUTO PILOT OFF, A PULSATION OR HYSTERESIS IS FELT IN THE PTICH AXIS, CONTINUED DURING CRUISE FLIGHT. MORE PRONOUNCED AT HIGHER SPPEDS, INTERMITTENT ASYMMETRIC FLUTTER OF ELEVATOR DISPLAY ON CONFIGURATION SYNOPTIC PAGE. THE AIRCRAFT RETUSDR AUS20030643Computer · faulty(AUS) LT FLIGHT CONTROL COMPUTER (FCC) FAULTY.SDR USAASB03076Servo · malfunctionedON CLIMB-OUT FROM CLT, EN ROUTE TO BOS, CAPTAIN LOST HIS AUTO PILOT AND VOR. HE SWITCHED TO THE FIRST OFFICERS AUTO PILOT AND LOST THAT AS WELL. AT THE SAME TIME, SEVERAL INSTRUMETNS WERE GIVING ERRONEOUS DATA ALONG WITH THE MACH TRIM FAIL LIGHT AND SPEED TRSDR BAQA086809Computer · will not testSPAS COMPUTER WILL NOT TEST. REPLACED WITH REPAIRED, SERVICEABLE UNIT.SDR ABXA030141Computer · malfunctionedWITH AUTOPILOT ON DURING TURNS, THERE WAS EXTREME AND EXCESSIVE UNCOMMANDED ELEVATOR INPUTS. VERIFIED. RERACKED PITCH AND ROLL COMPUTERS. VERSINE LIFT CHECKED GOOD IAW DC-9 AMM CHAPTER 22.SDR SWIA200311924Computer · malfunctionedCAPTAIN'S AUTOPILOT SPONTANEOUSLY DISENGAGES WITH CORRESPONDING RED A/P LIGHTS AND AURAL WARNING. CAPTAIN FLIGHT DIRECTOR AND F/O'S A/P OPERATE NORMALLY. REPLACED NR 1 APC-65B. OPS CHECK GOOD.SDR 250TR0010Computer · malfunctionedB-AUTO PILOT CREATES JERKING OF ELEVATORS WHILE AIRCRAFT BANKED; OK WITH -A- AUTO PILOT. SWAPPED FCC'S FOR FURTHER TROUBLESHOOTING.SDR HEEA084961Computer · malfunctionedNR 1 HELIPILOT COMPUTER PITCH HARDOVER. REPAIRED.SDR HEEA084960Computer · malfunctionedAFCS COMPUTER PITCH CHANNEL MOVES FORE/AFT WITHOUT PILOT INPUT. REPAIRED.SDR HEEA084959Computer · damagedAFCS COMPUTER PIN BROKEN ON CONNECTOR "B".SDR HEEA084958Computer · malfunctionedAFCS COMPUTER NR 1 PITCH MOTORS ALL THE WAY UP IN SAS MODE.SDR U30A200200033Computer · malfunctionedDURING CRUISE ON FLT 9518, ORD-CUN, AUTO PILOT NR 2 (AP2) FAULTED. UPON ARRIVAL IN CUN, DEFERRED PER MEL 22-83-01. REPLACED FMGC NR 2 IN ORD ON DEC. 9, 2002 IAW AMM 22-83-34-400-001. AFS TEST OK PER AMM 22-96-00-710-001. AIRCRAFT RETURNED TO SERVICE.SDR CA021209005Computer · intermittent(CAN) AUTO PILOT NR 2 - TRIM WHEEL MOVED IN THE WRONG DIRECTION ON TRIM LIGHT/TRIM WHEEL CHECK. LIGHT ILLUMINATION WAS INTERMITTENT.SDR AALA20021725Computer · defectiveJFK - FLT 647 - EN ROUTE JFK-SJU, DURING CLIMB-OUT, AIRCRAFT ENCOUNTERED TURBULENCE AND AIRCRAFT YAWED SEVERAL TIMES. SLATS EXTENDED WITH TAKEOFF SLATS SET. AIRCRAFT RETURNED TO JFK WITH NO FURTHER INCIDENT. REPLACED NR 1 FLIGHT AUGMENTATION COMPUTER. SYSTSDR 0203639993ComputerOn takeoff at 1000 feet the flight crew experienced rapid yaw movements to both left and right. Required full yoke deflection to maintain control of the aircraft. COM complied with and both yaw damper and rudder servo were turned off. Flight returned to an une
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