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 MASA200600282Unknown · unknownASH 6530 PHX - RUDDER LIMIT FAULT STATUS MESSAGE. MX RESET SYSTEM. OPS CHECK GOOD.SDR MASA200600072Trim Panel · inoperativeASH 7286 CAE - RUDDER TRIM INOP. MAINTENANCE REPLACED THE RUDDER TRIM PANEL.SDR ASAA0680026Spline · corrodedC-CHECK, RUDDER TAB TORQUE TUBE SPLINE CORRODED. REPLACED RUDDER TAB TORQUE TUBE. (K)SDR ASAA0680025Crank Assy · corrodedC-CHECK, RUDDER TAB TORQUE TUBE CONTROL CRANK SPLINES CORRODED. REPLACED TORQUE TUB CONTROL CRANK ASSY. (K)SDR ASAA0680024Torque Tube · corrodedC-CHECK, RUDDER TAB TORQUE TUBE LOWER SPLINES CORRODED. REPLACED RUDDER TAB TORQUE TUBE SHAFT ASSEMBLY. (K)SDR 05FDEA04399Indicator · smokeN CRUISE BURNING SMELL IN COCKPIT, DIVERTED AND LANDED. STRONGEST SMELL FROM THROTTLE QUADRANT AREA, FIRE CREW TEMP DETECTOR SHOWED HIGHEST HEAT IN THAT LOCATION. NEVER ANY VISIBLE SPARKS OR FLAMES, SOME SMOKE. INSPECTED THROTTLE QUADRANT AREA AND FOUND THE SDR AU510001509Cable · faultyRUDDER TAB CONTROL CABLE OVERRAN RUDDER TAB ACTUATOR CABLE DRUM. INVESTIGATION FOUND THE CABLE RIGGING WAS OUT OF ADJUSTMENT.SDR SWIA200515974Limiter · malfunctioned"RUDDER LIMIT FAULT" STATUS MSG. REPLACED NR 1 RUDDER LIMIT NR 1 RVDT IAW 27-25-05, PN BA670-90540-1, SN OFF A1166.SDR CA051019004Trim Tab · debonded(CAN) DURING COMPLIANCE WITH RAYTHEON S/B 55-2365 REV.2 ISS. OCT 2005 MAINTENANCE FOUND THE RUDDER TAB DISBONDED ON LOWER END. MAINTENANCE REPLACED THE RUDDER TAB AND RELEASED THE AIRCRAFT. RESEARCH ON THIS AIRCRAFT DISCOVERED THAT RAYTHEON S/B 2 365R1 (A/D SDR 2005FA0001463Servo · intermittentINVESTIGATED PILOT REPORT OF INTERMITTENT (RUDDER BOOST FAIL) ANNUNCIATOR LIGHT DURING TAKEOFF, CRUISE, AND CLIMB SEGMENTS. FOUND RUDDER SERVO WOULD SPIKE HIGH VOLTAGE BUT YAW DAMPER WOULD STAY ENGAGED. REPLACED RUDDER BOOST SERVO W/OVERHAULED REPLACEMENT UNSDR SWIA200515632Actuator · malfunctionedRUDDER TRIM INEFFECTIVE IN DESCENT. REPLACED UPPER RUDDER ACTUATOR IAW 27-22-02. OPERATIONAL CHECK GOOD.SDR SF20050923Trim System · malfunctionedFLIGHT 7578, IAD-ABE, PILOT CALLED ON THE RADIO SHORTLY AFTER TAKEOFF REPORTING AN AUTO TRIM LIGHT WARNING WITH YAW DAMPER ENGAGED. PILOT REPORTED YAW TRIM WAS 4 UNITS TO THE RIGHT AND 1/2 UNIT AILERON TRIM. AIRCRAFT RETURNED TO FIELD.SDR V2J2005F00003Actuator · failedSYSTEM FAILED IN PRIMARY, SECONDARY SYSTEM OPERATION NORMAL TROUBELSHOT SYSTEM IAW THE MM, FOUND PROBLEM TO BE AN INTERNAL FAULT WITH THE ACTURATOR ASSEMBLY. INSTALLED AN O/H UNIT SAME PN, SN-70. SECURITY AND FUNCTION CHECKS PERFORMED WITH NO FAULTS FOUND. SDR DXTA200500975Trim System · malfunctionedIMMEDIATELY AFTER TAKEOFF THE NORMAL PITCH TRIM FROZE AT 2.6 DEG SETTING. AFTER SEVERAL MINUTES AND SEVERAL ATTEMPTS AT NOSE DOWN TRIM, SYSTEM WORKED NORMAL, HOWEVER SPEED WAS < 180 KIAS. ITEM IS UNDER INVESTIGATION.SDR DL76K050553Actuator · inoperativeRUDDER TRIM INOP. REPLACED RUDDER TRIM ACTUATOR.SDR MASA200500690Trim System · out of adjustASH 2897 PHL. ABORTED A TAKEOFF DUE TO A TAKEOFF CONFIG ISSUE. AFTER BRINGING THE PLANE TO A STOP THE CAPTAIN NOTICED HIS RUDDER TRIM WAS NOT ALIGNED. RE-ALIGNED TRIM AND THE MESSAGE WENT AWAY.SDR 2005UALA00873Trim System · malfunctionedEXCESSIVE RUDDER AND TRIM, NEEDED 4 UNITS LT RUDDER TRIM AND 3 UNITS LWD TRIM PLUS YOKE INPUT, TO MAINTAIN WINGS LEVEL. EMERGENCY EQUIPMENT REQUESTED. A BROKEN NR 6 SPOILER CONTROL CABLE (WSB2-4) INHIBITED FLIGHT SPOILER MOVEMENT OF THE NR 6 SPOILER CREATING SDR SWIA200515452Control Panel · malfunctionedRUDDER TRIM WILL NOT ACTUATE NOSE RIGHT. REPLACED RUDDER TRIM/AILERON TRIM CONTROL PANEL. OPERATIONAL CHECK GOOD REF MM 27-12-10.SDR SWIA200515434Control Panel · intermittentRUDDER TRIM SWITCH INTERMITTENT. REPLACED TRIM CONTROL PANEL FOR AILERON AND RUDDER . OPERATIONAL CHECK GOOD.SDR SWIA200515432Trim Switch · stuckRUDDER TRIM STUCK. REPLACED TRIM PANEL. OPERATIONAL CHECK GOOD.SDR DXTA200500826Bearing · wornAIRFRAME VIBRATION ABOVE 260 KIA APPEARS TO BE COMING FROM RUDDER. RUDDER PEDALS DANCING BACK AND FORTH. CAN BE FELT IN YOKE AS WELL. VIBRATION GOES AWAY BELOW 250 KIAS. CHECKED WITH YAW DAMP OFF AND VIBRATION STILL PRESENT. FOUND ELEVATOR AND RUDDER TRIM TASDR SWIA200515216Trim Panel · inoperativeRUDDER TRIM KNOB INOP. REPLACED RUDDER/AILERON TRIM CONTROL PANEL. OPERATIONAL CHECK GOOD IAW CRJ MM 27-22-00 AND 27-12-10.SDR CA050527001Switch · burnedFLIGHT CREW REPORTED DURING THE APPROACH PHASE OF FEELING UNWELL, IT WAS THEN NOTED THE RUDDER TRIM SWITCH WAS HOT AND UNABLE TO FULLY OPERATE. THE C/B FOR RUDDER TRIM ACTUATOR WAS THEN NOTED AS TRIPPED. MAINTENANCE FOUND RUDDER TRIM SWITCH BURNT. THE SWITCHSDR DHL2005807541Hinge · crackedRUDDER CONTROL TAB HINGE NR 3 CRACKED. REMOVED RUDDER TAB IAW MM 27-21-2 PG 201-202. REMOVED AND REPLACED NR 3 HINGE BRACKET IAW SRM 51-1-21 PG 1-2. REINSTALLED RUDDER TAB IAW MM 27-21-2 PG 202-205. ADJUSTED RUDDER TRIM CONTROL SYSTEM IAW MM 27-20-0 PG 505SDR CA050527002Actuator · lack of lubeDURING CRUISE, A/C BEGINNING TO PITCH UP & DOWN SLIGHTLY WITH AUTOPILOT ENGAGED. DISENGAGED AUTOPILOT IN ORDER TO RE-TRIM A/C. DURING PROCEDURE RUDDER TRIM FOUND IMMOBILE. ATTEMPTED SMALL RUDDER DEFLECTION WITH RUDDER PEDALS & FOUND THEM TO BE IMMOBILE. DESDR SWIA200514961Control Panel · malfunctionedRUDDER TRIM WILL NOT MOVE LEFT MANUALLY. REPLACED AILERON/RUDDER TRIM CONTROL PANEL IAW CRJ MM 27-12-10. OPERATIONAL CHECK GOOD.SDR SWIA200514952Control Cable · tightPITCH DISCONNECT HANDLE CABLE IS TIGHT. ITEM FOUND AT C-CHECK INSPECTION. PITCH, ELEVATOR DISCONNECT SYSTEM RIGGED IAW CRJ MM 27-32-00-830-801.SDR 0500529860Computer · malfunctionedDURING TAKEOFF ROTATION, THE AIRCRAFT YAWED TO THE LT EVENTUALLY REQUIRING FULL RT RUDDER TRIM AND RT WING DOWN. COMPLIED WITH COM PROCEDURES AND FLT WAS ABLE TO CONTINUE TO SCHEDULED DESTINATION. CREW STATED THE LT RUDDER PEDAL WAS ABOUT 5 INCHES FORWARD ANSDR COMA0560258Control Panel · malfunctionedFLIGHT 5220 RUDDER CONFIG MESSAGE DURING T/O. REPLACED THE RUDDER TRIM PANEL.SDR SWIA200514717Control Panel · inoperativeRUDDER TRIM DOESN'T MOVE RUDDER TRIM. REMOVED AND REPLACED RUDDER TRIM/AILERON TRIM CONTROL PANEL. OPERATIONAL CHECKS GOOD.SDR 2005FA0000355Torque Tube · elongatedDURING INSPECTION, TECH DISCOVERED PLAY IN RUDDER TORQUE TUBE FITTING. TECH INSTALLED SERVICE KIT 764-100V. AD AND SB ADDRESSES INSP AN REPLACEMENT OF THE STEEL TORQUE TUBE FITTING WITH A STEEL REPLACEMENT PART. THIS AC HAD THE STEEL TORQUE TUBE FITTING INSSDR SWIA200514650Switch · malfunctionedRUDDER TRIM SWITCH DOES NOT RESPOND NORMALLY TO THE RIGHT. REPLACED RUDDER TRIM PANEL IN REFERENCE TO CRJ700 MM27-12-10. OPERATIONAL CHECK GOOD.SDR 2005FA0000161Connector · brokenRUDDER TRIM CONNECTOR FOUND BROKEN OFF DURING ANNUAL INSPECTION.SDR QXEA200500297Control Panel · failedSEA - FLIGHT 2184 - THE FLIGHT RETURNED TO FIELD WHEN THE CREW WAS UNABLE TO TRIM THE RUDDER TO THE RIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AILERON/RUDDER TRIM PANEL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SWIA200514539Trim Switch · inoperativeRUDDER TRIM SWITCH INOPERATIVE. REMOVED AND REPLACED RUDDER TRIM PANEL IAW AMM 27-41-25, OPERATIONAL CHECKED GOOD.SDR SWIA200514533Switch · failedAILERON TRIM SWITCH ONLY WORKS IN ONE DIRECTION. REMOVED AND REPLACED AILERON/RUDDER TRIM PANEL IAW CRJ MM 27-22-00. OPERATIONAL CHECK GOOD.SDR UPS05643671Control Cable · out of rigA/C REQUIRED 5 UNITS OF RUDDER TRIM IN CLIMB, 3 UNITS IN CRUISE. T/S IN PROGRESS. ACCOMPLISHED FIM 27-21-00 FIG 109 TO STEP 36 NO FAULTS FOUND. CHECKED RUDDER RATIO CHANGER SYS PER 27-21-00-5 RUDDER TRIM CONTROL SYS AND YA YAW DAMPNER 27-21-00-5 NO FAULTS FOUSDR HALA0500078Module · stuckAILERON TRIM STUCK IN LT WING DOWN. REMOVED AND REPLACED AILERON AND RUDDER TRIM CONTROL MODULE IAW SRM. (K)SDR CA050110005Spring · out of adjust(CAN) AIRCRAFT VIBRATION REPORTED WHEN LEVEL AT 12,000 FT. SHAKING STOPPED AT POWER SETTING LESS THAN 40 PERCENT AND SPEED BELOW 150KTS. AIRCRAFT INSPECTED ON ARRIVAL AND NOFAULTS FOUND. AIRCRAFT RELEASED SUBJECT TO SATISFACTORY TEST FLIGHT, VIBRATION STILSDR SWIA200514332Trim Panel · malfunctionedRUDDER TRIM WILL NOT MOVE NOSE LEFT. REPLACED RUDDER TRIM PANEL. OPERATIONAL CHECK GOOD.SDR SWIA200414333Trim Panel · faultyRUDDER TRIM FFOD TEST. REMOVED AND REPLACED RUDDER TRIM PANEL IAW CRJ MM 27-12-6, OPERATIONAL CHECK GOOD.SDR A6WA200440239Control Panel · malfunctionedABORTED TAKEOFF DUE TO CONFIG TRIM WARNING. ABORTED AT 60 KNOTS, RUDDER IN GREEN BAND, WILL TRAVEL TO LEFT BUT NOT TO THE RIGHT. REMOVED AND REPLACED RUDDER TRIM CONTROL PANEL, IAW AMM 27-10-01, OPS CHECK GOOD. (M)SDR SWIA200414329Trim Panel · defectiveRUDDER TRIM WON’T GO NOSE LEFT. REPLACED RUDDER TRIM PANEL. OPERATIONAL CHECK GOOD.SDR 2005FA0000086Pin · out of adjustTRANSIT CUSTOMER HAD RUDDER TRIM STICK IN FULL RT TRIM CONDITION AND COULD NOT TRIM LT. FOUND THAT IF TRIMMED TOO FAR TO RT. THE INDICATOR PIN WOULD JUMP OUT OF TRIM WHEEL TRACK AND COULD LOCK TRIM WHEEL. WE READJUSTED INDICATOR PIN AND CENTERED CONTROLS. SDR SWIA200414248Wheel · wornRUDDER TRIM WHEEL DOES NOT TURN. REPLACED RUDDER TRIM WHEEL SPLICED SHAFT AND BEARING IN CENTER CONSOLE PER EMB 120 MM 27-23-01. OPERATIONAL CHECK GOOD.SDR MASA200400649Trim System · out of alignmentASH 6268 MFR - THE PILOT REJECTED TAKEOFF FOR A TAKEOFF CONFIG MESSAGE. THEN NOTICED THE AILERON TRIM WAS VERY CLOSE TO THE LIMIT, HE CYCLED THE TRIM INTO THE MIDDLE OF THE GREEN WITH NO FURTHER DEFECTS.SDR ASOA04884Control Panel · malfunctionedDURING CLIMB-OUT, AT APPROXIMATELY 10,000 FEET THE CREW EXPERIENCED A FULL SCALE NOSE LT RUDDER TRIM DEFLECTION. THE CAPTAIN CORRECTED FOR THE TRIM PROBLEM USING RUDDER AND AILERON INPUTS. AN EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES REQUESTED TO BE ON SSDR GTIA040824Actuator · malfunctionedRUDDER TRIM HAS 6 UNITS RT TO MAINTAIN STRAIGHT AND LEVEL. FOUND YAW DAMPER ACTUATOR OUT OF MOUNTS. REMOVED AND REPLACED YAW DAMPER ACTUATOR, OPS CHECK NORMAL.SDR SWIA200413917Control Knob · stuckLEFT RUDDER TRIM KNOB STICKS ALLOWING TRIM TO RUN TO FULL DEFLECTION. INSTALLED SERVICEABLE AILERON/RUDDER TRIM PANEL IAW 27-00-07, OPERATIONAL CHECK GOOD.SDR SWIA200413884Trim Panel · malfunctionedRUDDER TRIM RANAWAY TO THE LT WHILE TRYING TO TRIM AIRCRAFT IN THE CLIMB. RETURNED TO AIRPORT. REMOVED AND REPLACED RUDDER TRIM/AIL TRIM PANEL ASSY. OPERATIONAL CHECK GOOD. PN OFF 601R51227-13
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