JASC 2210
Service difficulty reports · 4,019
Reports filed under 2210 · Autopilot 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 = '2210' 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 = '2210' 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 MASA200400533Relay · failedRUDDER SYSTEM 2 FAILED RESULTING IN AN INOP AUTO PILOT. MAINTENANCE REPLACED THE RUDDER CONTROL RELAYS.SDR C7WA200400038Transducer · inoperativeAIR RETURN: DURING CLIMBOUT UPPER RUDDER DEFLECTED TO FULL RT YAW DAMPER POSITION THEN BEGAN OSCILLATING LT TO RT CONTINUOUSLY. REMOVED AND REPLACED UPPER YAW DAMPER TRANSDUCER. SYSTEM OPERATIONAL CHECKS NORMAL.SDR 374PA0012Circuit Breaker · failedAUTO PILOT DISENGAGES BY ITSELF AND AURAL WARNING CIRCUIT BREAKER KEEPS POPPING OUT AFFECTING AUTO PILOT DISCONNECT HORN. REPLACED AURAL WARNING CIRCUIT BREAKER PER MM 31-26-00 AND OPS CHECKED. PERFORMED SELF TEST OF AUTO PILOT SYSTEM PER MM 22-02-10 AND 22-SDR 373PA0051Coupler · damagedYAW DAMPER POPS DC CIRCUIT BREAKER. REPLACED YAW DAMPER COUPLER AND OPS CHECKED PER MM 22-12-31 AND 22-12-01.SDR ABXA040320Computer · malfunctionedAIRCRAFT INITITATED DUTCH ROLL DURING CLIMBOUT AND PROGRESSIVELY GOT WORSE WITH THE HIGHER CLIMB. ROLL TOOK PLACE WITH OR WITHOUT AUTO PILOT ON AND OFF, WITH YAW DAMPER SWITCH ON OR OFF. ACCOMPLISHED RUDDER CONTROL TAB INSP/TEST IAW DC9 MM 27-20-02-04. NO DSDR 583CC0004Transfer Valve · inoperativeYAW DAMPER WILL NOT ENGAGE WHEN SELECTED. YAW DAMPER PLACED ON MEL 22-3-1. 08/27/2004: REPLACED TRANSFER VALVE PER MM 22-11-71 AND 22-12-01. OPS AND LEAK CHECK NORMAL.SDR MALA040539Computer · malfunctionedTHRU 12,000 FT A/P KICKED OFF WITH ELEVATOR TRIM FAULT AND WINDSHEAR INOPERATIVE LIGHT CA SIDE FD ALSO FAILED. PFD AND ND ALSO FLICKERED AND CAME BACK WITH AN ALT FLG. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED DFGC, OP CHECKS GOOD. P/N ON/OFF 406SDR MALA040537Computer · malfunctionedAFTER TAKEOFF TRP FAILED, UNABLE TO RESET. SUBSEQUENTLY, FTC ELTRIM YD STALL IDNTZ FGC1 YD1 NO CAT 3 ALL ILLUMINATED. A/P AND A/T FAILED. AIR RETURN TO DTW. MAINTENANCE REVEIWED AND CLEARED FAULTS. PERFORMED HARD RESET AND RTS ON DFGC, Y/D, TRIM SYSTEM, TSDR WLDA200489Computer · inoperativeUNCOMMANDED ELEV MOVEMENT. CONSIDERABLE CONTROL COLUMN PULL FORCE REQUIRED DURING INITIAL ROTATION TO ATTAIN REQUIRED T/O CLIMBOUT PITCH ATTITUDE UNTIL 500-800 FT AGL. AFTER FLAP RETRACTION, FORCE REQUIRED RETURNED TO NORMAL, CNTRL COLUMN OSCILLATED(TWICE) BESDR 234TR0021Computer · inoperativeAUTO PILOT A SIDE KICKED OFF BY ITSELF AND THEN WILL NOT REENGAGE. REPLACED A CHANNEL FCC IAW MM 22-11-331 AND OPS CHECKED IAW MM 22-11-01.SDR SWIA200413725Computer · malfunctionedFO'S AUTOPILOT KICKED OFF AT LEVEL OFF , 25,000 FT. REMOVED AND REPLACED AUTOPILOT COMPUTER IAW MM 22-10-02, OPERATIONAL CHECKED GOOD.SDR SWIA200413722Control Panel · failedAUTOPILOT ELEVATOR SERVO FAILURE ON FINAL APPROACH. REPLACED AUTOPILOT ENGAGE PANEL ASSY WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.SDR 234TR0020Computer · malfunctionedBOTH A&B AUTO PILOTS DISENGAGE IN SMOOTH AIR, LEVEL FLIGHT, WITHOUT PROVOCATION. REPLACED B-SYSTEM FCC COMPUTER. OPS CHECKS NORMAL PER MM 22-11-331.SDR JX62004F00000Computer · malfunctioned(LG NR 000173) AIRCRAFT DEPARTED, CLIMBING THROUGH FL370 AT M.58, THE YAW DAMPER BEGAN A SERIES OF LT TO RT INPUTS INCREASING TO FULL SCALE DEFLECTION AT A RATE OF APPROXIMATELY ONE PER SECOND. THE AUTOPILOT WAS TURNED OFF, AND THE MALFUNCTION CONTINUED. TUSDR 249TR0034Force Limiter · malfunctionedAUTO PILOT -B- WILL NOT ENGAGE IN FLIGHT. REPLACED AILERON FORCE LIMITER AND OPS CHECKED PER MM 22-11-132.SDR HAEA200400158Autopilot Sys · malfunctionedAIRCRAFT PITCHES DOWN WHEN AUTOPILOT IS ENGAGED (ALT HOLD). THE FLIGHT DIRECTOR DOES THE SAME THING , EVEN WITH THE AUTOPILOT TURNED OFF. REPAIRED SHOULDER PORT DRAIN CAN SYSTEM AND REMOVED FLIGHT DIRECTOR FOR REPAIR. INSTALLED FLIGHT DIRECTOR AFTER REPAIR. OPSDR 372PA0047Computer · failedFIRST OFFICER'S FLIGHT DIRECTOR INOPERATIVE AND SPEED TRIM FAIL AND MACH TRIM LIGHTS ILLUMINATED ON RECALL DURING LANDING CHECKS (SINGLE CHANNEL FAILURE). REPLACED B-CHANNEL FCC. BITE TEST AND OPS CHECKS NORMAL PER MM 22-10.SDR 151AW0025Coupler · malfunctionedYAW DAMPER DISENGAGES INTERMITTENTLY. REPLACED YAW DAMPER COUPLER PER MM 27-12-31. SYSTEM TEST NORMAL.SDR SWIA200413509Autopilot Sys · malfunctionedSHORTLY AFTER DISCONNECTING THE AUTOPILOT THE ELEVATOR JAMS. COULD NOT DUPLICATE PROBLEM WITH AUTOPILOT SYSTEM. OPS CHECKS GOOD IAW MM 32-11-00.SDR 371PA0046Autopilot Sys · malfunctionedDURING DESCENT ON -B- AUTO PILOT -AP- WARNING LIGHT FLASHES WITH -CWSP & CWSR- ANNUNCIATIONS AT SAME TIME. PLACED AUTO PILOT -B- CHANNEL ON MEL 22-1. 6/29/04: BITE CHECKED NORMAL. SWAPPED DAA'S FOR FURTHER EVALUATION. BOTH AUTO PILOTS BITE PASSED. CLEARESDR SWIA200413476Computer · malfunctionedAUTOPILOT ON CAPTAIN'S SIDE INFLIGHT WILL GET THE AUTOPILOT WARNING WITH NO DISCONNECT OF THE AUTO PILOT AP LIGHT ON FCP. REMOVED AND REPLACED CAPTAIN'S AUTO PILOT COMPUTER IAW MM 22-10-02 AND AUTO PILOT PANEL IAW MM 22-10-04. OPERATIONAL CHECK GOOD IAW MM 2SDR SIMA200416703Control Unit · malfunctionedDFW - FLT 3582 - DUAL PITCH TRIM FAILURE ON LANDING WITH AUTO PILOT ON. DECLARED EMERGENCY AND LANDED WTHOUT INCIDENT. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR MASA200400330Actuator · faultyABORTED T/O AND RETURNED TO GATE WHEN YAW DAMP 2 W/N STAY ENGAGED. FERRIED TO PHL. MX REPLACED THE NR 2 YAW DAMP ACTUATOR.SDR ASMF200406006Computer · failedAIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF FAIL IN LT FLIGHT GUIDANCE SYSTEM INDICATION. SYSTEM WAS REACTIVATED AND ELECTRICAL BUSS TURNED OFF, AUTO TEST IN BOTH SYSTEMS WAS PERFORMED, ALL CORRECT. DURING OVERNIGHT SERVICE, FLIGHT GUIDANCE COMPUTER WAS RSDR 513NA0007Indicator · malfunctionedON DESCENT INTO KSFB, NO AUTO LAND DISPLAYED ON AUTO LAND STATUS INDICATOR. RESET RIGHT FCC AND RAN MCDP TEST PER MM 22-10-00. ALL AUTO PILOT ENGAGE AND FCC CHECKS GOOD.SDR CA040603004Aileron · mismanufactured(CAN) WHILE INVESTIGATING A SNAG, DISCOVERED AN AILERON A/P QUADRANT ASSEMBLY P/N 40E22-84-1069-1 WHICH DID NOT MEET THE MANUFACTURER'S DRAWING IN THE INSTALLATION OF THE NR 1 COLLINS A/P SERVO, LOCATED IN THE LT MLG WHEEL WELL. FOR THE DISABLING OF THE NR1 SDR SWIA200413358Actuator · malfunctionedYAW DAMPER NR 1 WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR IAW CRJ MM 22-22-01. OPS CHECKS GOOD.SDR SWIA200413353Damper · inoperativeYAW DAMPER NR 2 INOPERATIVE, STATUS MESSAGE DURING TURBULENT FLIGHT. UNABLE TO RE-ENGAGE. COULD NOT DUPLICATE DISCREPANCY. SWAPPED FCC CARDS IN THE IAPS CARD CAGE FROM NR 1 TO NR 2 SIDE. OPS CHECKS GOOD.SDR HE66095154Actuator · unreliableCAUSING A YAW ACTUATOR LIGHT, AND AUTOPILOT TO FLY OUT OF TRIMSDR AUS20040423Autopilot Sys · failed(AUS) DUAL AUTOPILOT MALFUNCTION. LIMITED INFORMATION PROVIDED.SDR SWIA200413339Computer · malfunctionedON ROTATION RECEIVED TRIPLE CHIME WITH TRIM FAIL AND AUTO PILOT, APT AP/FD FAILURE WITH FD FLAG ON CAPT EADI. CB E33 POPPED. RERACKED CAPT AP COMPUTER, TESTED AP SYSTEM, ALL CHECKS GOOD AT THIS TIME.SDR QH52004F00000Housing · crackedTHIS PART WAS TESTED IAW MFG 65-40-03. CRACKED LOCATED AT THE OIL GALLERY.SDR BAQA094574Autopilot Sys · failedUNIT REMOVED DUE TO AUTOPILOT HARD FAILURE. REPLACED WITH SERVICABLE UNIT. 05/19/2004SDR CA040517002Control Cable · frayed(CAN) WHILE REMOVING AN ELECTIC TRIM SERVO FOR THE STABILATOR SYSTEM, IT WAS NOTICED THAT THE FORWARD STABILATOR TRIM CABLE WAS FRAYED AT THE AREA THAT IT WAS WOUND AROUND THE ELECTIC TRIM SERVO PULLEY. THE CABLE WAS REPLACED WITH A NEW ONE. THIS AREA SHOULD SDR AUS20040330Force Limiter · faulty(AUS) AUTOPILOT WOULD NOT ENGAGE. SUSPECT FAULTY FORCE LIMITER.SDR AUS20040311Autopilot Sys · faulty(AUS) AUTOPILOT FAULTY.SDR GAIA04071Coupler · malfunctionedDEPARTURE, FLIGHT, WITH AIRSPEED CHANGES, AIRCRAFT YAW CHANGES NOTICEABLY. AFTER RUDDER IS RETRIMMED AIRCRAFT DUTCH ROLLS A FEW TIMES IN A JERKING MANNER. WITH INCREASING SPEEDS MORE RT TRIM IS REQUIRED. CREW RETURNED TO DEPARTURE AIRPORT, WHERE A LANDING WSDR 304AW0006Panel · malfunctionedMODE CONTROL PANEL SWITCHES, N1, SPD, VNAV, LNAV, ALT HLD & V/S INDICATORS INOP. PLACED ON MEL 22-15-8. NOTE: MAINTENANCE INDUCED PROBLEM WHILE REPLACING ONE LIGHT BULB IN PANEL. 04/26/2004: REPLACED MCP AND OPS CHECKED PER MM 22-11-34. CLEARED MEL.SDR SWIA200413145Computer · malfunctionedUPON TAXI OUT YD2 DISENGAGED, ALSO NUMEROUS TIME INFLIGHT ASSOCIATED WITH AP DISCONNECT. REMOVED AND REPLACED FCC NR 2.SDR 304AW0005Coupler · damagedYAW DAMPER POPS DC CIRCUIT BREAKER. PLACED ON MEL 22-3-1 AND PERFORMED RUDDER PRESSURE REDUCER SYSTEM TEST PER MM 22-12-01. 04/22/2004: REPLACED YAW DAMPER COUPLER PER MM 22-12-13. SYSTEM CHECKS NORMAL PER ADJUSTMENT/TEST.SDR QXEA200400271Actuator · malfunctionedYAW DAMPER DISENGAGE MESSAGE ON BOTH PFD'S. RAN CHECKLIST AND MESSAGE REAPPEARS. REMOVED AND REPLACED YAW DAMPER ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 372PA0044Actuator · shortedDFCS HISTORY SHOWS AUTO-PILOT TRIM SERVO HAS NO RESPONSE. AUTO-PILOT COLUMN SWITCHING MODULE CHECKS OK PER MM 27-41-00. FOUND OPEN IN AUTO-PILOT STABILIZER TRIM ACTUATOR. REPLACED AUTO-PILOT STABILIZER TRIM SERVO AND OPS CHECKED PER MM 22-11-81.SDR 251TR0009Control Panel · inoperativeMODE CONTROL PANEL IS INOPERATIVE. REPLACED MODE CONTROL PANEL PER MM 22-11-341. OPS CHECKS GOOD.SDR AUS20040457Limiter · faulty(AUS) AUTOPILOT TORQUE LIMITER FAULTY.SDR SWIA200413094Computer · malfunctionedCAPTAIN SIDE RED TRIM AND AP LIGHTS ILLUMINATED ON FCP. REPLACED CAPTAIN'S AUTO-PILOT COMPUTER. CAPT'S AUTO-PILOT/FLIGHT DIRECTOR SYSTEM OPERATES NORMALLY PER MM 22-11-00.SDR 2004F00164Computer · malfunctionedSJO - FLT 641 - DURING APPROACH DUAL FMGC MESSAGE CAME ON, DUE TO THIS CONDITION AIRCRAFT RETURNED TO SAN JOSE AIRPORT. ON GROUND MAINTENANCE, RESET BOTH FMGC SYSTEMS PER AMM 22-83-00, AND FOUND NORMAL, THEM RETURNED THE AIRCRAFT TO SERVICE. (M)SDR SWIA200413090Computer · malfunctionedWHEN AUTOPILOT IS SELECTED TO FIRST OFFICER'S SIDE, AUTOPILOT TRIES TO CAPTURE LOCALIZER WHEN STILL FULL SCALE (AT LEAST 1.5 MILES OFF COURSE). REPLACED NR 2 APC-65B WITH SERVICEABLE UNIT. OPS CHECK GOOD.SDR 371PA0041Transfer Valve · inoperativeYAW DAMPER INOPERATIVE. RELEASED ON MEL. 03/29/2004: REPLACED RUDDER POWER CONTROL UNIT TRANSFER VALVE PER MM 22-12-21. OPS CHECKS GOOD.SDR SWIA200413091Computer · malfunctionedRIGHT AFTER TAKEOFF TRIM FAIL LIGHT ILLUMINATED ON MAP AND TRIM LIGHT ON FCP AND SINGLE CHIME. ALL LIGHTS WENT OUT WHEN AUTOPILOT WAS SWITCHED TO FIRST OFFICER'S SIDE. ALL ILLUMINATED AGAIN WHEN SWITCHED BACK TO CAPTAIN'S SIDE. REMOVED AND REPLACED APC NR 1SDR SWIA200413084Switch · jammedYAW DAMPER NR 1 ENGAGE SWITCH JAMMED IN FLUSH POSITION. UNABLE TO ENGAGE YAW DAMPER 1. REMOVED AND REPLACED YAW DAMPER CONTROL PANEL. OPS CHECK GOOD. P/N: 601R51594-1.
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