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.

SDR MASA200400533Relay · failedRUDDER SYSTEM 2 FAILED RESULTING IN AN INOP AUTO PILOT. MAINTENANCE REPLACED THE RUDDER CONTROL RELAYS.Sep 17, 2004 · N831MJ · Emb EMB145LRSDR 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.Sep 14, 2004 · N8887Z · Boeing 727225SDR 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-Sep 3, 2004 · N374PA · Boeing 73736MSDR 373PA0051Coupler · damagedYAW DAMPER POPS DC CIRCUIT BREAKER. REPLACED YAW DAMPER COUPLER AND OPS CHECKED PER MM 22-12-31 AND 22-12-01.Sep 2, 2004 · N373PA · Boeing 7373Y0SDR 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 DAug 31, 2004 · N955AX · Doug DC941SDR 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.Aug 26, 2004 · N583CC · Boeing 737291SDR 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 406Aug 24, 2004 · N523XJ · Bac AVRO146RJ85ASDR 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, TAug 21, 2004 · N522XJ · Bac AVRO146RJ85ASDR 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) BEAug 16, 2004 · N275WA · Doug MD11SDR 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.Aug 15, 2004 · N234TR · Boeing 737228SDR 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.Aug 14, 2004 · N562SW · Emb EMB120ERSDR SWIA200413722Control Panel · failedAUTOPILOT ELEVATOR SERVO FAILURE ON FINAL APPROACH. REPLACED AUTOPILOT ENGAGE PANEL ASSY WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.Aug 14, 2004 · N224SW · Emb EMB120ERSDR 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.Aug 12, 2004 · N234TR · Boeing 737228SDR 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. TUAug 3, 2004 · N598JL · Beech 400BEECHSDR 249TR0034Force Limiter · malfunctionedAUTO PILOT -B- WILL NOT ENGAGE IN FLIGHT. REPLACED AILERON FORCE LIMITER AND OPS CHECKED PER MM 22-11-132.Aug 2, 2004 · N249TR · Boeing 7372K5SDR 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. OPJul 20, 2004 · N330TW · Lear 24ESDR 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.Jul 16, 2004 · N372PA · Boeing 737306SDR 151AW0025Coupler · malfunctionedYAW DAMPER DISENGAGES INTERMITTENTLY. REPLACED YAW DAMPER COUPLER PER MM 27-12-31. SYSTEM TEST NORMAL.Jul 9, 2004 · N151AW · Boeing 7373G7SDR 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.Jun 25, 2004 · N907SW · Cndair CL6002B19SDR 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. CLEAREJun 24, 2004 · N371PA · Boeing 737306SDR 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 2Jun 16, 2004 · N213SW · Emb EMB120ERSDR 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)Jun 13, 2004 · N854AE · Emb EMB135KLSDR 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.Jun 12, 2004 · N592ML · Cndair CL6002B19SDR 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 RJun 7, 2004 · N505MD · Doug DC982SDR 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.Jun 7, 2004 · N513NA · Boeing 7572T7SDR 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 Jun 3, 2004 · Cndair CL6012A12SDR 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.May 27, 2004 · N448SW · Cndair CL6002B19SDR 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.May 26, 2004 · N945SW · Cndair CL6002B19SDR HE66095154Actuator · unreliableCAUSING A YAW ACTUATOR LIGHT, AND AUTOPILOT TO FLY OUT OF TRIMMay 24, 2004 · N135CR · Urocop EC135T1SDR AUS20040423Autopilot Sys · failed(AUS) DUAL AUTOPILOT MALFUNCTION. LIMITED INFORMATION PROVIDED.May 17, 2004 · Boeing 737376SDR 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.May 17, 2004 · N251YV · Emb EMB120ERSDR QH52004F00000Housing · crackedTHIS PART WAS TESTED IAW MFG 65-40-03. CRACKED LOCATED AT THE OIL GALLERY.May 14, 2004 · N3060 · Bbavia 7ACSDR BAQA094574Autopilot Sys · failedUNIT REMOVED DUE TO AUTOPILOT HARD FAILURE. REPLACED WITH SERVICABLE UNIT. 05/19/2004May 14, 2004 · N703ME · Urocop EC135P2SDR 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 May 11, 2004 · Piper PA44180SDR AUS20040330Force Limiter · faulty(AUS) AUTOPILOT WOULD NOT ENGAGE. SUSPECT FAULTY FORCE LIMITER.May 2, 2004 · Boeing 737376SDR AUS20040311Autopilot Sys · faulty(AUS) AUTOPILOT FAULTY.Apr 29, 2004 · Swrngn SA227ATSDR 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 WApr 27, 2004 · N281KH · Boeing 7272J0SDR 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.Apr 25, 2004 · N304AW · Boeing 7373G7SDR SWIA200413145Computer · malfunctionedUPON TAXI OUT YD2 DISENGAGED, ALSO NUMEROUS TIME INFLIGHT ASSOCIATED WITH AP DISCONNECT. REMOVED AND REPLACED FCC NR 2.Apr 19, 2004 · N929SW · Cndair CL6002B19SDR 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.Apr 18, 2004 · N304AW · Boeing 7373G7SDR 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.Apr 15, 2004 · N406QX · Bombdr DHC8401SDR 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.Apr 7, 2004 · N372PA · Boeing 737306SDR 251TR0009Control Panel · inoperativeMODE CONTROL PANEL IS INOPERATIVE. REPLACED MODE CONTROL PANEL PER MM 22-11-341. OPS CHECKS GOOD.Apr 3, 2004 · N251TR · Boeing 737228SDR AUS20040457Limiter · faulty(AUS) AUTOPILOT TORQUE LIMITER FAULTY.Mar 30, 2004 · Boeing 737376SDR 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.Mar 27, 2004 · N289YV · Emb EMB120ERSDR 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)Mar 26, 2004 · N486TA · Airbus A320233SDR 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.Mar 26, 2004 · N268UE · Emb EMB120ERSDR 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.Mar 26, 2004 · N371PA · Boeing 737306SDR 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 1Mar 25, 2004 · N298SW · Emb EMB120ERSDR 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.Mar 22, 2004 · N466SW · Cndair CL6002B19
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