JASC 2213
Service difficulty reports · 148
Reports filed under 2213 · Flight Controller, 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 = '2213' 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 = '2213' 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 HEEA082497Bearing · wornAFCS ACTUATOR HAS WORN BEARINGS. REPAIRED.SDR 2002UALA01783Servo · failedDURING CAT2 AUTOLAND, AT APPROX 20-30 FT, AIRCRAFT PITCHED UP AUTOMATICALLY, THEN AT 15 FT AUTOPILOT DISCONNECTED ITSELF. CAPTAIN TOOK OVER AND MANUALLY LANDED. THERE WAS A FAILURE OF THE RT AUTOPILOT RUDDER SERVO ON THIS AIRPLANE DURING A PREVIOUS FLT. AS A SDR SWIA200211328Control Panel · malfunctionedAIRCRAFT HAD SEVERAL OCCASIONS WHERE WE RECEIVED `AP TRIM` MESSAGES BOTH PITCH TRIM AND TRIM LEFTWARD. AIRCRAFT ALSO WENT INTO AN UNCOMMANDED LEFT ROLL. REMOVED AND REPLACED FLIGHT CONTROL PANEL AS REQUIRED. SYSTEM OPS CHECKS GOOD IAW 22-11-00.SDR WRNA200200004Computer · unserviceableDuring Climb to cruise altitude Both Mach Feel Fail Lights came on. Fuel dump procedures carried out for Max landing wt (26K lbs dumped). Aircraft landed normal and returned to base.Corrective Action: Removed and replaced Trim Augmentation Computer. Op's checkSDR SWIA200211130Control Panel · malfunctionedYAW DAMPER 2 WILL NOT ENGAGE. REMOVED AND REPLACED FCP 4002 IAW CRJ MM 22-11-07. OPS CHECK GOOD.SDR AWXA200200629Computer · faultyON TAKEOFF WHEN ENGAGING THE A-AUTOPILOT AIRCRAFT WENT TO CWS PITCH MODE AND NOSE PITCHED UP 5 TO 10 ABOVE NORMAL TAKEOFF ATTITUDE. SWITCHED TO B-CHANNEL AND SYS OPERATED NORMALLY. MX PLACED SYS ON MEL 22-01-11, COND 1 A-AUTOPILOT INOPERATIVE. TROUBLESHOT SSDR O2G2002F00000Control Unit · failedMACH TRIM FAILURE BY AUTOPILOT PITCH TRIM. SHORTLY AFTER THE STABILIZER CHANNEL NR1 TRIM FAILED RESULTING IN A LOSS OF ALL PITCH TRIM. REMOVED AND REPLACED HSTCU BOX, SYSTEM OPS CHECKED GOOD.SDR GTIA020780Rheostat · failedDEN - FLT 980 - IN TURN YOKE VERY JERKY, AUTO PILOT DISENGAGES. OK IN LEVEL FLIGHT, NR 2 AUTO PILOT. TROUBLESHOT AUTOPILOT SYSTEM. FOUND AILERON SERVO RHEOSTAT BAD. CHECKED WITH METER LEFT SIDE GOOD RIGHT SIDE BAD. REMOVED AND REPLACED RHEOSTAT AND AILEROSDR CA020617007Computer · failed(CAN) ENROUTE NR 2 FLIGHT DIRECTOR FLAGGED , F/D BARS COULD NOT BE REMOVED . AIRCRAFT RETURNED TO ORIGINATING STATION FOR NORMAL LANDING . NR 2 FLIGHT GUIDANCE COMPUTER REPLACED . AIRCRAFT RETURNED TO SERVICE .SDR GTIA020220Computer · malfunctionedFLT 8011 - ACY - ON STABILIZED DESCENT AUTOPILOT SUDDENLY PITCHED DOWN THEN PITCHED UP. REMOVED AND REPLACED PITCH AXIS COMPUTER IAW MM 27-13-1, OPS CHECK NORMAL. (M)SDR 372PA0002Control Unit · faultyV-NAV ON AUTOPILOT WILL NOT ENGAGE IN CLIMB. EVENTUALLY WHEN IT DOES ENGAGE IT WILL DISCONNECT FOR NO APPARENT REASON.SDR SWIA200110395Circuit Board · faultyON DESCENT, NOTICED RUDDER FLUTTER. BOTH RUDDER INDICATION & AERODYNAMIC FLUTTER OBSERVED AT VARIOUS SPEEDS. ON THE GROUND, STILL OBSERVED RUDDER FLUCTUATIONS (ABOUT 3 DEGREES BOTH SIDES). AT FL330 AND MACH .77 EXPERIENCED AN UNCOMMANDED RUDDER MOVEMENT. VERISDR SWIA200110383Computer · faultyCLIMBING OUT OF ELP THE AIRCRAFT CONTINUALLY YAWED LEFT AND RIGHT, NO MESSAGES. PERFORMED TEST OF YAW DAMPENERS IAW 22-22-01 AND NOTED FAILURE. REMOVED AND REPLACED NR 2 FCC CARD IAW 22-12-14. OPS CHECK GOOD.SDR C2XA01BT172Controller · faultyCREW REPORTED ON TAXI, SMOKE IN COCKPIT ELECTRICAL BURNING SMELL IN COCKPIT ONLY. CONTRACT MAINTENANCE FOUND FAULTY AP PUSHBUTTON SWITCH ON AUTOPILOT CONTROL PANEL. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROLLER IAW EMB145 MM 22-11-01. OPS CHECK GOOD. AIRSDR 2001UALA01853Control Unit · failedINTERMITTENT MASTER CAUTION CHIME LIGHT. INTERMITTENT BLINKING OF FEATURES DISPLAYED ON CAPTAINS PRIMARY FLIGHT DISPLAY AND NAVIGATION DISPLAY. FLIGHT CONTROL UNIT LIGHTS FLASHING ALSO. THE FCU WAS REPLACED AND GROUND CHECK WAS NORMAL.SDR AWXA0002202Controller · failedPHX- ABORTED TAKEOFF - FLT 239 - ON TAKEOFF ROLL CREW HAD NO INDICATION OF TOGA AND ABORTED THE TAKEOFF AT 70 KTS AND RETURNED TO THE GATE. MAINTENANCE TROUBLESHOT AND REPLACED THE FLIGHT CONTROL UNIT PER AMM 22-81-12-401, SYSTEM CHECKS WERE GOOD. NO FURTHERSDR DL73K011342Computer · faultyON APPROACH COPILOT ADI GOT COMPUTER FLAG, AIRSPEED BUG FLAG AND COURSE SELECTOR DID NOT RESPOND TO CHANGES. SLIGHT ELECTRICAL SMELL IN FWD GALLEY. FOUND FCC PWR SUPPLY BURNT REPLACED "B" FCC PREFORMED COMPUTER TEST PER MAINTENANCE MANUAL 22-11-331 SYSTEM CHESDR DHL2001727024Control Unit · defectiveAUTO-PILOT ON AUTOGLIDE SLOPE ABOUT 300 AGL STAB OUT OF TRIM LIGHT ILLUMINATED THEN AIRCRAFT AGGRESSIVELY WENT NOSE DOWN, BELOW GLIDE SLOPE.REPLACED PITCH CONTROL UNIT IAW B727 MM 22-11-101 OPS CK GOODSDR DHL2001805011Controller · malfunctionedAUTOPILOT IN HDG MODE, RIGHT TURN 35 DEG BANK, LEFT TURN 25 DEG BANK. REMOVED AND REPLACED AUTOPILOT CONTROLLER. PERFORMED OPERATIONAL CHECK IAW MM 22-20-0. OK FOR SERVICE.SDR DHL2001362013Controller · failedAUTO PILOT WILL NOT ENGAGE. DEFERRED NR 1 AP PER MEL 22-11-01. PLACARD INSTALLED. R&R AUTOPILOT CONT MODULE IAW M/M CH 22-11-12. OPS CHECK GOOD.SDR CA010522010Control Cable · frayed(CAN) THE FLIGHT CREW REPORTED THAT THE ROLL CONTROL FELT HEAVIER THAN STANDARD FOR TYPE. MAINTENANCE INVESTIGATION REVEALED THAT THE R/H UPPER AILERON CONTROL CABLE WAS FRAYED AT THE STEEL PULLEY, WING STATION YW 256.0, JUST OUTBOARD OF THE ENGINE NACELLE. THSDR DHL2001727011Autopilot Sys · erraticDURING HEADING CHANGES, AIRCRAFT BANKS ERRATICALLY IN SHORT, JERKY MOTION. AUTOPILOT ON. DEFERRED AUTOPILOT SYSTEM PER MEL 22-1-2 CAT-C. DMI 5360. PLACARD INSTALLED.SDR SWIA972432Control Panel · malfunctionedWITH GEAR DOWN, FLAP 25 DEGREES, FLIGHT CONTROLS GET STUCK WHILE ATTEMPTING TO ROLL TO THE RIGHT. CHECKED AILERONS. COULD NOT DUPLICATE PROBLEM. SUSPECT AUTOPILOT DID NOT DISENGAGE. INSTALLED SERVICEABLE APP-65A. OPS CHECK GOOD AT THIS TIME. P/N: 622-66SDR SWIA972012Controller · failedCAPTAIN''S FLIGHT DIRECTOR INOPERABLE. FOUND NUMBER ONE ADS 65 FAULTY. REPLACED NUMBER ONE ADS 65. TESTED AUTOPILOT IAW EMB120 MM 22-10-00. TESTED PITOT STATIC SYSTEM FOR LEAKS IAW FAR 91.411. ALL TESTS GOOD. (P/N: 622-5797-001) (S/N ON: 1678) (S/N OFFSDR SWIA972000Computer · failedYAW DAMPER FAILED INFLIGHT. REPLACED FCC NR 1 (P/N 622-9815-404) (S/N 432) OFF, (S/N 337) ON. CHECKS NORMAL IAW MM 22-12-14.SDR AWXA0000623Computer · failedEMERGENCY DECLARED, FLIGHT MGT AND GUIDANCE COMPUTER FAIL (FMGC). REMOVED AND REPLACED FMGC, OPS CHECK GOOD.SDR JBXA000197Warning System · activatedIAPS DEGRADED MESSAGE DISPLAYED. SHUTDOWN AIRCRAFT ON TAXIWAY TO TRY TO CLEAR FAULT. FAULT CLEARED, BUT APU WOULD NOT START. DEPLANED PASSENGERS ON TAXIWAY DUE TO NO AIR CONDITIONING IN AIRCRAFT. PERFORMED OPERATIONAL TEST OF IAPS IAW CL-65 AMM 22-12-00, ASDR 2000UALA00387Flight Dir · malfunctionedAUTOPILOT AND BOTH FLIGHT DIRECTORS REFUSED TO TRACK AND ARE UNRELIABLE. *S/D* ACCOMPLISHED CAT III CHECK REF MM 22-10-00, AND ILS OP CK. NO PARTS WERE REPLACED AND NO FURTHER DISCREPANCIES HAVE BEEN REPORTED.SDR 2000UALA00354Panel · failedTHE MASTER CONTROL PANEL WENT INOPERATIVE, ALL WINDOWS SHOW 8''S. BOTH AUTOPILOTS, FLIGHT DIRECTORS, AND NR 1 VOR COURSE INFORMATION IS INOPERATIVE. *S/D* REPLACED MODE CONTROL PANEL. OPERATIONAL TESTS NORMAL.SDR HEED065040Controller · failedWOULD NOT UPDATE/INDICATED LOW BATTERY. REPLACED UNIT.SDR HEED064640Controller · malfunctionedRDA DATA UNIT WOULD NOT UPDATE. INDICATED LOW BATTERY. REPLACED UNIT.SDR ERAA061861Computer · malfunctionedCOMPUTER UNIT WILL TEST MANUALLY ONLY.SDR 99FDEA00069Fcc · inop99-0052 - ASYMMETRICAL SLAT ON SLAT RETRACTION 230 KTS. REMOVED AND REPLACED BOTH NR 1 AND NR 2 FLT CONTROL COMPUTERS IAW MM 22-01-03-4 PERF RTS TEST, OPS CK GOOD. PERF CADC TEST RTS IAW MM 34-16-01-3. OPS CK NORM. NOTED ON ALL (3) CADC.SDR ARWA980808Controller · failedMIA - FLT 617 - NR 1 AND NR 2 RADAR INOP R/I. A/C RETURNED TO MIAMI, REMOVED AND REPLACED PITCH COMPUTER, OPS CHECKED NORMAL IAW MM 22-13-0. NR 2 RADAR R/T, P/N 2067151-0153 S/N 2915. (M)SDR CA980827025Computer · failed(CAN) AILERON MISTRIM DURING DESCENT. AMBER POSTED ON BOTH PRIMARY FLIGHT DISPLAYS. AUTOPILOT TRANSFERRED TO COPILOT SIDE, AIRCRAFT ROLLED VIOLENTLY TO RIGHT. A/P DISCONNECTED. CONTROL REGAINED MANUALLY. A/P RE-ENGAGED ON PILOT'S SIDE. REPLACED NR 1 FLIGSDR SIMA982094Fcc · malfunctionedLAX - FLT 3386 - UNCOMMANDED PITCH MOVEMENTS IN-FLIGHT WITH OR WITHOUT AUTOPILOT. VERIFIED THE FLAPS DID NOT APPEAR TO BE MOVING. REMOVED AND REPLACED THE FLIGHT CONTROL COMPUTER. OPERATIONAL CHECK AND TEST FLIGHT PERFORMED WITH NO FURTHER PROBLEMS NOTED. SDR VTZA98228Computer · malfunctionedIAD/BNA - FLT 6704 - DURING CRUISE AT 1755 HRS ON 6-27-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO ALTITUDE ALERT SOUNDED CONTINUOUSLY. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND PERFORMED CHECKED OF FCC SYSTEM AND COULSDR HEEA0014933Switch · intermittentSCAS ENGAGE SWITCH INTERMITTENT.SDR AU980569Controller · faulty(AUS) AUTOPILOT CONTROLLER FAULTY.SDR 97UAL900633Resistor · failedIN CRUISE FL350 GOT NO LAND 3. TRIED RIGHT AUTOPILOT, AC ROLLED HARD RIGHT. TURNED RIGHT A-P OFF AND PUT CENTER A-P ON. STRONG SMELL OF HOT ELECTRICAL INSULATION. TURNED RIGHT PACK OFF, SMELL DISSIPATED. DIVERTED TO DENVER. *S/D* FOUND RESISTOR BURNED USDR CA970618003Controller · failed(CAN) AUTOPILOT HAD UNCOMMANDED 10 TO 15 DEGREE PITCH DOWN WHILE IN LEVEL FLIGHT AT 3000 FEET ON THE LOCALIZER BELOW THE GLIDE SLOPE. FLIGHT GUIDANCE CONTROLLER REPLACED.SDR JBXA970013Fcc · failedRDU - FLT 771 - AIR RETURN DUE TO RUDDER FAULT 1 AND 2, STABILIZER TRIM 1 AND 2 AND YAW DAMPER 1 AND 2 FAULTS ALSO, HAD AFCAS MX REQUIRED MESSAGE. REMOVED AND REPLACED FLT CONTROL COMPUTER NR 1 (FCC NR 1). OPS CHECK GOOD IAW AMM 22-11-01. OPS CHECK OF RUDDESDR JBXA00032Fcc · failedRDU - FLT 552 - DURING TAKEOFF ROLL, ABORTED TAKEOFF DUE TO FLAP DISARMED MESSAGE. AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE PERFORMED AFCAS MAINTENANCE TEST, FCC NR 3 FAILED REMOVED AND REPLACED THE NR 3 FCC. NO PRESENT FAULTS REPORTED. OPS CHECK GOOSDR VTZA96415Circuit Breaker · trippedFLT 6222 - JFK-IAD - DURING APPROACH, MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY DUE TO PITCH WENT TO FULL UP. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE OPEN DMI 07424, MEL 22-1. MAINTENANCE CLOSED DMI 07424 BY CYCLING FCC CIRCUIT BREASDR USAAF96078Flt Cntrl Comptr · failedPIT - FL 1601 - AFTER TAKEOFF, CREW RECEIVED 'NO AUTOLAND'MESSAGE. NEITHER AUTOPILOT WOULD TURN ON. FLIGHT RETURNED TO PIT ANDLANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 FCC.(M)SDR AU960757Mode Control · faulty(AUS) AUTOPILOT SYSTEM MODE CONTROL PANEL (MCP) FAULTY DUE TO FAILURE OF 'POWER DROP OUT TEST' - A9Q204AND M12 REPLACEDSDR DL76E960678Flt Controller · failedON APPROACH, FLT CREW REPORTED VERY STIFF AILERONS, ALMOST UNABLE TO TURN A/C. A/C WOULD NOT TURN ON A/P BOTH THE LEFT AND RIGHT A/P WOULD DISCONNECT IF ENGAGED AND A TURN INPUT MADE, CENTER A/P NOT USED. FLT CREW DECLARED AN EMERGENCY AND A/C LANDED WITHSDR 9502803213Flt Contl Unit · inoperativeDURING CLIMB-OUT, FLIGHT CONTROL UNITS NR 1 AND NR 2 FAILED. RESET CIRCUIT BREAKERS, NO HELP. DECISION WAS MADE TO RETURN TO MSP. REPLACED FLIGHT CONTROL UNIT. SYSTEM TESTS WERE NORMAL.
Back to JASC 2213