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 HEEA072729Computer · failedKICK OFF IN FLIGHT AND WANDERS AFTER SET IN CRUISE FLIGHT. REPLACED WITH SERVICEABLE PART.SDR HEEA072671Computer · malfunctionedWONT HOLD ALTITUDE.SDR DHL2001727004Controller · failedAUTOPILOT MANUAL PITCH CONTROL DOES NOT MAINTAIN CONSISTENT CLIMBS OR DECENTS. REMOVED AND REPLACED AUTO PILOT HEAD PANEL PER B727 M/M SEC 22-11-181, OPS CK. GOOD.SDR DHL2001807008Computer · unserviceableAUTOPILOT OVER BANKS IN TURNS AND OVERTURNS BY 15 DEG. AND GAINS 100 FT IN TURNS AND LOSES 150 FT IN ROLLOUT. R&R ROLL CHANNEL COMPTR IAW 22-12-0 CHECKED OPERATION OK.SDR SWIA972480Damper · malfunctionedYAW DAMPER ENGAGED ON TAXI, WILL NOT DISCONNECT. REMOVED AND REPLACED APP65A WITH SERVICEABLE UNIT. OPS CHECK GOOD. P/N: 622-6684-006, S/N ON: 2614, S/N OFF: 344.SDR GTIA0100161Computer · malfunctionedFLL - FLT 267 - AUTO-PILOT VERTICAL SPEED MODE MALFUNCTIONED WITH VSI SET TO RN 500 FPM. A/C CLIMBS AT NR 2000-2500 FPM. SAME PROBLEM IN CLIMB AND DESCENT. RE-RACK PITCH COMPUTER SELF TEST NORMAL IAW MM 22-12-0. UNABLE TO DUPCLICATE. (M)SDR WVBA2001012Computer · unserviceableAFTER INITIAL INSTALL AIRCRAFT WAS ON CHECK FLIGHT, IN ALTITUDE HOLD, AIRCRAFT PORPOISES. IT WAS DETERMINED THAT THE PITCH COMPUTER WAS THE CAUSE. UNIT WAS REMOVED FOR ANALYSIS.SDR TI1R001401Computer · failedSPAS-COMPUTER, DC VOLTAGE IN, NO VOLTAGE OUT. REMOVED AND REPLACED.SDR SWIA972284Control Panel · malfunctionedAFTER TAKEOFF, AUTO PILOT TURNED ON BY ITS SELF. RETURNED TO FIELD. WHILE ON THE GROUND THE AUTO PILOT TURNED ON BY ITS SELF. RAN THE TRIM WHEEL FULL NOSE DOWN AFTER DISCONNECTING AND TRANSFERRING TO FIRST OFFICERS SIDE IT AGAIN TURNED ITSELF ON. REPLACEDSDR ZYWA100159Computer · faultyAIRCRAFT PORPOISES WITH PITCH LANE 2 ENGAGED IN BASIC AP MODE (INTERMITTENTLY). REMOVED AND REPLACED COMPUTER.SDR C1HA200184001Accessory Unit · failedON DEPARTURE AND CLIMB THE AUTOPILOT CRUISE TRIM WOULD NOT OPERATE (NOSE UP) NORMAL OPERATION (NOSE DOWN). REMOVED AND REPLACED A/P ACCESSORY UNIT, CHECKS GOOD.SDR AU010004Computer · faulty(AUS) AUTOPILOT COMPUTER SUSPECT FAULTY.SDR RRXA001089Computer · faultyDURING CRUISE FLIGHT AIRCRAFT REQUIRED 3 UNITS RIGHT RUDDER TRIM FOR COORDINATED FLIGHT DEPOWERED RUDDER TO MAINTAIN A/C CONTROL ACCOMPLISED QRH. REMOVED AND REPLACED YAW COMPUTER, OP'S CK'D GOOD IAW DC-8 M/M 22-11-1 AND 22-10-0. RT SPOILER SWIVEL LEAKING. SDR 20001215SH028Computer · inoperativeCSAS-COMPUTER PITCH INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR SWIA972091Control Panel · malfunctionedAUTOPILOT ENGAGED AND PITCHED UP WHILE AIRCRAFT WAS ON GROUND. FOUND WATER INSIDE AP CONTROL PANEL. REPLACED AP CONTROL PANEL. OPS CHECK GOOD. P/N: 622-6684-006, S/N ON: 2118, S/N OFF: 2803.SDR SWIA972089Servo · failedDURING DESCENT INTO SEA AT 220 IAS, 13000 FT THE AIRCRAFT MADE AN UNCOMMANDED NOSE PITCH UP TO 15 DEGREES AND AUTOPILOT DISENGAGED. THERE WAS NO FORWARD TRIM AVAILABLE AFTER THAT. FORWARD YOKE PRESSURE WAS NEEDED UNTIL LANDING TO MAINTAIN PITCH CONTROL. INSDR COMA0060847Computer · malfunctionedUNCOMMANDED 70 DEGREE ROLL DURING CRUISE FLIGHT WITH A/P ON. REPLACED THE NR 1 FCC 4000.SDR 20001219SH023Computer · malfunctionedCOMPUTER GOES OFF-LINE DURING FLIGHT. PILOT IS ABLE TO RESET. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20001018SH002Circuit Board · failedAFTER AIRCRAFT IS POWERED AND THE TRIM SYSTEM IS OPERATED FOR A FEW MINUTES, BOTH ROLL TRIM SURFACES STOP TRIMMING IN THE RIGHT WING LOW DIRECTION. REPLACING ROLL TRIM PC BOARD CORRECTS CONDITION. (X)SDR SWIA971981Computer · malfunctionedON APPROACH WITH AUTO PILOT ENGAGED (HEADING MODE) AIRCRAFT STARTED UNCOMMANDED TURN TO RIGHT. AFTER AUTO PILOT DISENGAGED AIRCRAFT MAINTAINED UNCOMMANDED TURN TO RIGHT. AUTO PILOT WAS VERIFIED AND DISENGAGED OFF. UNABLE TO TURN LEFT. DISENGAGED AILERON PESDR SWAA001699Panel · inoperativeDIVERSION, MCP INOP, DIVERTED TO CLE DUE TO WEATHER. C/W BITE CHECK AND REMOVED AND REPLACED MCP PANEL PER MM.SDR SWIA971973Warning System · activatedFIRST OFFICER''S TRIM FAIL WARNING ANNUNCIATED DURING TAKEOFF. TAKEOFF ABORTED. AUTO PILOT RED MAP LIGHT ANNUNCIATED AS WELL. REPLACED F/O''S APC-65B WITH SERVICEABLE UNIT. OPS CHECKS GOOD ON GROUND. (P/N 622-8315-402), (S/N 32445) ON, (S/N 2947) OFF.SDR HALA0000159Computer · failedFLT 197 - HNL - AIRCRAFT MADE UNCOMMANDED ROLL TO RIGHT AT TOP OF DESCENT WITH AUTOPILOT ENGAGED. TURN KNOB IS WINGS LEVEL DETENT NAV SELECTOR IN TURN KNOB MODE. ALSO, VOR COURSE WAS COMING ALIVE AT SAME TIME, ALTHOUGH NAV/LOC WAS NOT SELECTED. REPLACED ROLSDR SWIA971750Computer · failedAFTER TAKEOFF AT 1500 AGL TRIPLE CHIME AND RED TRIM FAIL AND AUTO PILOT FAIL , MAP LIGHTS ILLUMINATED, THE YAW DAMPNER FAILED. CAPTAINS AND FOS COMPUTER FLAGS WAS OBSERVED ON AHRS, ARCS FGS 1 AND FGS 2 DC CIRCUIT BREAKERS POPPED AND WOULD NOT RESET. NO FLIGHSDR GAIA00124Computer · malfunctionedFLT 713 - ICT-MCI - DURING DESCENT AND LEVEL OFF, THE AIRCRAFT HAD A HARD TIME DISENGAGING THE AUTOPILOT. AUTOPILOT WAS ERRATIC IN ROLL. PULLED CIRCUIT BREAKERS ON AUTOPILOT AND THE AIRCRAFT RETURNED TO NORMAL. EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED ASDR AU000430Diode · incorrect(AUS) ROLL AMPLIFIER POWER SUPPLY ZENER DIODE INCORRECT PART. DIODE CAUSED DRIVER TRANSISTOR TO FAIL. UNAPPROVED PART.SDR 20000406SH010Computer · damagedRECEIVED DAMAGED FROM AEC. SEVERAL BENT AND AT LEAST ONE BROKEN PIN ON J949 RECEPT. REMOVED AND REPLACED. (X)SDR WRLA99023Computer · failedAUTOPILOT NR 1 AND NR 2 FAILED ON DEPARTURE FROM PGUM. AIRCRAFT RETURNED TO PCUM FOR CORRECTIVE ACTION. REMOVED AND REPALCED NR 2 FCC. RETURN TO SERVICE TEST SATISFIED. DEFERRED NR 1 AUTOPILOT PER MEL 22-10-1. AIRCRAFT DOWNGRADED TO CAT II SINGLE LAND. ASDR HEEA065297Computer · malfunctionedFLIGHT DIRECTOR DECOUPLES WHEN IAS IS SELECTED.SDR HEEA065217Computer · failedAUTOPILOT CONTROL DOES NOT COUPLE WHEN FLIGHT DIRECTOR MODE IS SELECTED.SDR HEEA065193Computer · failedCOMPUTER TRIPS CIRCUIT BREAKER.SDR HEEA065182Computer · malfunctionedAFCS ACTUATORS SLOW TO TRIM AND RE-CENTER.SDR 20000413SH034Computer · failedACTUATOR NOT MOVING. WILL NOT TEST. REMOVED AND REPLACED. (X)SDR UPS99430617Computer · inopINSPECTION TYPE:N/A, IN CRUISE AFTER AN ATC REQUIRED SPEED REDUCTION, B AUTOPILOT ABRUPTLY PITCHED A/C NOSE UP (ADDITIONAL 2.5 - 3 DEGREES. F/O PUSHED OVER BUT COULD NOT PREVENT AN ALTITUDE DEVIATION OF 300 FT NEITHER A/P OR ALTITUDE HOLD DISENGAGED AUTOMATICSDR DHL99804006Roll Computer · malfunctionedAUTOPILOT INOPERATIVE. REMOVED AND REPLACED ROLL COMPUTER.SDR HEEA063336Computer · failedFLIGHT DIRECTOR WILL NOT HOLD PITCH.SDR HEEA063322Computer · inoperativeCOMPUTER INOPERATIVE.SDR HEEA061694Computer · fails testCOMPUTER FAILS ALTITUDE HOLD TEST STEP 35.7 AND .7.SDR HEEA061693Computer · fails testCOMPUTER FAILS ALTITUDE HOLD TEST STEP 35.5 ON SST.SDR 99ZZZX2848Computer · malfunctionedCOMPUTER FLAGGED WITH CONSTANT ERROR CODES 2E5 2E17, AND 2E62. REF: NR R019493. REMOVED AND REPLACED.SDR 99ZZZX2849Computer · malfunctionedINTERMITTENT ANNUNCIATOR LIGHT. REF: MCN NR 2.SDR 99ZZZX2856Spas Computer · failedCOMPUTER FAILED SPAS TEST, PARA 4.2.1. REMOVED AND REPLACED.SDR 99UAL900131Fmgc · malfunctionedAUTOPILOT DISENGAGED ON APPROACH ALONG WITH THE MAP NOT AVAIL FLAG ON THE CAPTAIN SIDE NAV DISPLAY. PFR SHOWS FAILURE MESSAGES FMGC2 AND FAC2. *S/D* THE POSTFLIGHT REPORT IDENTIFIED THE FLIGHT MANAGEMENT AND GUIDANCE COMPUTER (FMGC) NR 2 AND FLIGHT AUGMENTATISDR 99ZZZX1050Computer · malfunctionedUNIT WAS REPAIRED AND RETURNED TO SERVICE BY A REPAIR STATION WHICH DID NOT POSSESS REQUIRED KTS-151 TEST SET TO PERFORM REQUIRED INSPECTIONS PER MANUFACTURER'S MM INSTRUCTIONS.SDR HEEA060774Computer · failedNR 2 HELIPILOT WOULD NOT ENGAGE. CAUSES SAS AND ATT LIGHTS TO STAY ILLUMINATED.SDR HEEA060773Computer · failedAFCS COMPUTER FAILS DATT & PCPL LOGIC 14.1 TEST.SDR HEEA060727Computer · inoperativeLIGHTS ON MOTE SELECT UNIT INOPERATIVE.SDR ABXA9900081Computer · defectiveDURING CRUISE EXPERIENCED NOSE DOWN HYDRAULIC PITCH TRIM RUN-AWAY. DISCONNECTED WHEEL LONGITUDINAL TRIM CIRCUIT BREAKERS, NO PROBLEMS REMAINDER OF FLIGHT. REPLACED R-56 AND S-56 CIRCUIT BREAKERS. REPLACED PITCH AXIS COMPUTER AND INSPECTED STABILIZER SHUT-OFSDR HEEA060114Computer · failedCOMPUTER FAILED 2.1 ON SST BENCH.SDR HEEA060113Computer · malfunctionedAUTOPILOT WILL NOT TRACK IN NAV MODE.
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