JASC 2721
Service difficulty reports · 686
Reports filed under 2721 · Rudder Tab Control 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 = '2721' 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 = '2721' 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 BB04085Trim System · inoperativeAFTER TAKE-OFF, CREW NOTED THAT THE RUDDER TRIM WAS INOPERATIVE. CREW ALSO REPORTED THAT THE ANTI-SKID WAS INOPERATIVE. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A RUDDER TRIM CHECK IAW THE FIM AND A VISUAL INSPECTIONSDR SWIA200413822Control Panel · malfunctionedABORTED TAKEOFF CONFIG TRIM WITH TAKEOFF CONFIG OK RUDDER TRIM. REMOVED AND REPLACED RUDDER TRIM PANEL, OPERATIONAL CHECKS GOOD IAW 27-21-00.SDR HNAA0400117Switch · stuckFLIGHT 4039 NORFOLK TO LGA REPORTED HAVING A RUDDER TRIM ACTUATOR RUNAWAY CONDITION. CREW FOLLOWED THE ABNORMAL PROCEDURES CHECKLIST AND CONTINUED THE FLIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE IN LGA TROUBLESHOT SYSTEM AND FERRIED AIRCRAFT TO MIDDLETOWN FSDR SWIA200413757Control Panel · malfunctionedRUDDER TRIM RESPONDS VERY SLOWLY WHEN SELECTED TO THE LEFT. REMOVED AND REPLACED RUDDER TRIM PANEL IAW 27-24-00. OPERATIONAL CHECK GOOD.SDR QXEA200400586Trim System · malfunctionedONT - FLIGHT 4099 - ON TAKEOFF ROLL, AND ON CLIMBOUT, THE RUDDER TRIM WAS OBSERVED TO MOVE APPROXIMATELY 25 PERCENT LEFT DEFLECTION. ON BOTH OCCASIONS, IT DID NOT APPEAR THAT THE RUDDER ACTUALLY MOVED. ALL MOVEMENT INDICATIONS WERE UNCOMMANDED WITH THE AUTO SDR SWIA200413609Control Panel · malfunctionedWITH RUDDER TRIM NOSE RT, WILL NOT RE-CENTER. REPLACED RUDDER/AILERON TRIM PANEL, OPERATIONAL CHECK GOOD.SDR SWIA200413547Knob · stuckRUDDER TRIM STICKS TO LEFT. CLEANED AND RE-ADJUSTED RUDDER TRIM KNOB. OPERATIONAL CHECK GOOD.SDR 2004UALA00621Warning Light · illuminatedRETURN TO FIELD DUE TO RUDDER TRIM PROBLEM. REPLACED RUDDER TRIM ACTUATOR.SDR 2004UALA00562Trim System · malfunctionedPLANE HAD RIGHT RUDDER TRIM PROBLEM. ADDITIONAL PROBLEMS WITH SPOILERS. FAILED RUDDER TRIM ACTUATOR INHIBITED ABILITY TO TRIM RUDDER. REMOVED AND REPLACED SUBJECT RUDDER TRIM ACTUATOR WITH NEW SERVICABLE ACTUATOR. THE NR 9 SPOILER ACTUATOR WAS REPLACED TO ADSDR SWIA200413315Control Panel · malfunctionedDURING ORIGINATING CHECK, RUDDER TRIM WOULD ONLY MOVE RIGHT, NOT LT. REMOVED AND REPLACED TRIM CONTROL PANEL IAW CRJ 200 MM CHAPTER 27-12-10. OPS CHECK GOOD.SDR CA040515001Trim Switch · failed(CAN) RUDDER TRIM GOES FULL RT WITHOUT INPUT COMMAND. WITH NOSE LT SELECTED, TRIM MOVES FURTHER RT. AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED RUDDER TRIM PANEL AND OPS CHECKED. NO FURTHER DEFECTS NOTED.SDR SWIA200413134Actuator · malfunctionedRUDDER TRIM CB 2F6 POPPED. REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW MM 27-22-01. OPS CHECK GOOD.SDR FTU2004F00002Chain · misinstalledFIRST TIME AC WAS IN OUR SHOP DURING AN ANNUAL INSP, THE RUDDER TRIM CHAIN IN THE CENTER PEDESTAL WAS FOUND NOT INSTALLED CORRECTLY. WERE THE CHAIN IS SUPPOSE TO RIDE OVER THE IDLER TENSIONING SPROCKET, IT WAS FOUND OFF THE SPROCKET AND JUST RESTING ON THE SPSDR SWIA200413014Trim Switch · intermittentRUDDER TRIM SWITCH INOP INTERMITTENTLY TO THE LEFT. REMOVED AND REPLACED RUDDER/AILERON TRIM PANEL. SYSTEM OPS CHECK GOOD.SDR AUS20040135Arm · cracked(AUS) RUDDER TRIM ARM ASSEMBLY SEPARATED FROM RUDDER PEDAL BAR.SDR SWIA200412940Circuit Card · failedRUDDER TRIM WHEEL, IN CLIMB AND CRUISE, VIBRATES AND FEELS RATCHETY. RETENSIONED RUDDER TRIM CABLE CIRCUIT AS REQUIRED REFERENCING MM 27-00-01 AND COMPLETED RII CARD 27-314. OPS CHECK GOOD.SDR QXEA200400125Trim Panel · malfunctionedGEG - FLIGHT 2356 IN CRUISE PHASE OF FLIGHT, RUD TRIM WENT FULL RIGHT UNCOMMANDED. CREW NEUTRALIZED SITUATION AND RAN CHECK LIST, AND PULLED CIRCUIT BREAKERS. REPLACED AILERON/RUDDER TRIM PANEL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR A6WA20034ASwitch · failedRUDDER TRIM FAILED, NOSE LEFT. REMOVED AND REPLACED RUDDER TRIM SWITCH. (M)SDR A6WA200440003Trim Switch · failedRUDDER TRIM FAILED, NOSE LEFT. REMOVED AND REPLACED RUDDER TRIM SWITCH. (M)SDR SWIA200412745Actuator · malfunctionedUNABLE TO USE RUDDER TRIM AT HIGH ALTITUDES AND COLD TEMP. REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW EMB 120 MM 27-23-02. OPS CK GOOD.SDR SWIA200312718Trim Panel · damagedRUDDER TRIM SPORATIC TO LT SIDE, HARD TO USE. REMOVED AND REPLACED RUDDER/AILERON TRIM PANEL IAW CRJ MM 27-12-10. OPS. CHECK GOOD.SDR SWIA200312704Control Cable · damagedDURING FLIGHT RUDDER TRIM JAMMED AND WOULD NOT TURN LEFT OR RIGHT. REMOVED AND REPLACED FORWARD RUDDER TRIM CABLES WITH NEW SERVICEABLE CABLES AND TENSIONED IAW EMB 120 MM 27-00-01.SDR COMA0370055Panel · malfunctionedDURING TAKE OFF RUDDER TRIM MOVED 1 UNIT LT. REPLACED THE RUDDER TRIM SWITCH PANEL.SDR SWIA200312634Control Panel · malfunctionedON DEPARTURE FROM BZN AT ABOUT 500 FT RUDDER TRIM DEFLECTED ALMOST FULL SCALE NR RUDDER TRIM SWITCH WAS ABLE TO BRING TRIM BACK TO LESS THAN 1/2 DEFLECTION. REMOVED AND REPLACED RUDDER/AILERON TRIM CONTROL PANEL. RUDDER TRIM SYSTEM OPS CHECK GOOD. P/N: 601SDR AUS20031201Actuator · corroded(AUS) PITCH TRIM ACTUATOR TOP ATTACHMENT FITTING CORRODED. SUSPECTED INTERGRANNULAR TYPE CORROSION IS CAUSING THE SURFACE PROTECTIVE COATING TO LIFT.SDR 328031Wheel · lockedAIR RETURN DUE TO MANUAL RUDDER TRIM WHEEL LOCKING UP IN CENTER POSITION, PILOTS RUDDER PEDALS RESPONDED NORMAL.SDR AWXA200301482Servo · wornEN ROUTE AIRFRAME VIBRATION WAS FELT IN ALL PHASES OF FLIGHT, MOST NOTICEABLE IN CLIMB & CRUISE AT SPEED OF 310 KTS. MX VISUALLY INSPECTED WING TO BODY FAIRING SEALS, MLG DOORS, AIR COND & PAX ENTRY DOORS, NO DEFECTS NOTED. PERFORMED ELEVATOR FREE PLAY CHECKSDR CA031114008Thrust Bearing · worn(CAN) SPRING TAB WAS STIFF, IT WAS LUBED AND WORKED NORMAL. ON SCHEDULED WINTER MAINTENANCE INSPECTION BEARING WAS FOUND TO BE WORN PAST LIMITS.SDR P5CA0300983Computer · failedRUDDER RATIO LIGHT CAME ON AFTER T/O AT 250 KTS. LIGHT REMAINED ON & WENT OUT AFTER LANDING. REMOVED AND REPLACED ELEVATOR FEEL UNIT PER MM 27-31-14 , CHECK OK.SDR SWIA200312576Control Panel · inoperativeRUDDER TRIM IS INOPERATIVE, SWITCH WILL TRIM NOSE RT BUT WILL NOT TRIM NOSE LT. REMOVED AND REPLACED RUDDER/AILERON TRIM PANEL WITH SERVICEABLE UNIT IAW MM 27-12-10. OPS CHECK GOOD.SDR P5CA0300951Control Quadrant · faultyRUDDER RADIO LIGHT CAME ON WHEN FLAPS MOVING 5 TO 1 AT 220KNTS. REMOVED AND REPLACED RUDDER UPPER CONTROL IAW 27-21-13 LEAK CHECK GOOD.SDR P5CA0300953Actuator · defectiveRUDDER RATIO LIGHT CAME ON AFTER FLAPS UP. REPLACED LOWER RUDDER RATIO CHANGER ACTUATOR IAW MM 27-21-12SDR P5CA0300952Actuator · defectiveRUDDER RATIO LIGHT CAME ON AFTER FLAPS UP. REPLACED UPPER RUDDER RATIO CHANGER ACTUATOR AND ADJUSTED UPPER RUDDER IAW MM 27-21-12 AND 27-21-00.SDR SWIA200312396Control Panel · malfunctionedRUDDER TRIM INOP NOSE LEFT. REMOVED AND REPLACED RUDDER TRIM PANEL. OPS CHECK GOOD. P/N: 601R51226-23/01SDR SWIA200312395Control Panel · malfunctionedRUDDER TRIM TEST FAILED DURING ORIGINATING CHECK, TRIM WOULD NOT TRIM BACK TO LEFT. REMOVED AND REPLACED RUDDER/AILERON TRIM CONTROL PANEL. OPS CHECK GOOD. P/N: 601R51226-23.SDR AUS20030826Arm · cracked(AUS) RUDDER TRIM ARM CRACKED. FOUND DURING INSPECTION IAW AD/PA28/23 AMDT2.SDR CA030625007Switch · failed(CAN) DURING CLIMB ALTITUDE PASSING 3,000 FT, PILOT PUT RUDDER TRIM SWITCH TO A/C LT DIRECTION. HEARD STRANGE SOUND & RUDDER TRIM CONTINUED MOVING TO A/C LT DIRECTION UNTIL FULL LT DIRECTION. TRIED TO PUT SWITCH TO RT DIRECTION BUT COULDN`T CONTROL A/C WITH USDR COMA0360287Trim Switch · malfunctionedRUDDER TRIM WENT TO FULL NOSE LEFT WITH NO CREW COMMAND. REPLACED THE RUDDER TRIM CONTROL PANEL.SDR AUS20030573Actuator · faulty(AUS) RUDDER TRIM TAB ACTUATOR FAULTY.SDR COMA0360246Panel · malfunctionedRUDDER TRIM INTERMITTENTLY STICKS WHEN SELECTIG TO THE RIGHT. REPLACED THE RUDDER TRIM PANEL, SUSPECT TRIM SWITCH WORN.SDR COMA0360232Switch · uncontrollableRUDDER TRIM RUNAWAY DURING FLIGHT. REPLACED THE RUDDER/AILERON TRIM CONTROL PANEL.SDR 2003FA0000606Sprocket · wornRUDDER TRIM SYST DID NOT SEEM TO BE RESPONDING TO INDICATED TRIM INPUT. INSP OF RUDDER TRIM SYS, IT WAS DISCOVERED THAT TRIM WHEEL SPROCKETS, PN 07612101 WERE NOT SHIMMED CORRECTLY TO ALLOW FOR PROPER ENGAGEMENT OF GEAR TEETH. TWO SPROCKETS ENGAGE AT 90 DEGRSDR AUS20030372Actuator · failed(AUS) RUDDER TRIM ACTUATOR FAILED.SDR SWIA200311848Switch · looseRUDDER TRIM KNOB LOOSE - WILL NOT OPERATE RUDDER TRIM. TIGHTENED SWITCH AND RESOLDERED CONNECTIONS. OPS CHECK GOOD OF SWITCH PER CRJ MM 27-22-00.SDR CA030321001Actuator · failed(CAN) DURING THE DAILY INSPECTION THE NUT SECURING THE RUDDER TRIM TABACTUATOR UPPER BOLT WAS NOTICED MISSING. THE NUT SECURING THE LOWER BOLT WAS LOOSE WITH NO COTTER PIN INSTALLED. 5.7 HOURS HAD ELAPSEDSINCE THE PHASE 1 THRU 4 INSPECTION. THE UPPER AND LOWSDR CA030317001Trim Panel · failed(CAN) 6 TO 7 MINUTES AFTER TAKE OFF RUDDER STARTED MOVING FULL RIGHT, RUDDER TRIM. APPLIED LT TRIM - STOPPED AT 1.25 RT DEFLECTION. RUDDER TRIM STUCK. EMERGENCY DECLARED AND DIVERTED TO TPA. R&R'D AILERON TRIM PANELSDR SWIA200311742Trim Panel · malfunctionedRUDDER TRIM INOP, RUDDER TRIM STUCK IN THE FULL RIGHT POSITION. REMOVED AND REPLACED TRIM PANEL IAW CRJ MM 27-12-10. OPS CHECK GOOD.PN ON 601R51226-23/01.SDR UPS03240119Skin · crackedINSPECTION TYPE: C&SI, LOWER RUDDER TAB HAS AN AREA OF DELAM AT LWR AFT CORNER RT SIDE. SKIN CRACK AND LARGE DENT ON LT SIDE 12TH FROM BOTTOM ON T/E AREA LOWER RUDDER TAB REPLACED IAW MM 27-20-11.SDR AWXA200201196Control Switch · inoperativeAIR TURN BACK ON CLIMB OUT, EXPERIENCED RUDDER AND TRIM PROBLEMS. UNABLE TO TRIM THE RUDDER, WITH AN INDICATION OF ONLY 2 UNITS, LEFT TRIM WILL NOT MOVE. REQUIRED AILERON 20 UNITS TO THE RIGHT IN ORDER TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. TURNED BACK TO AISDR AUS20021324Control Panel · faulty(AUS) RUDDER TRIM CONTROL PANEL SUSPECT FAULTY.
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