JASC 2710
Service difficulty reports · 2,967
Reports filed under 2710 · Aileron 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 = '2710' 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 = '2710' 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 26N2008F00004Selector · frozenACFT FLIGHT CONTROLS FROZE AT ALTITUDE ENROUTE. THIS IS THE SECOND SITUATION WHERE THIS CONDITION HAS HAPPENED TO THIS ACFT. ACFT PREVIOUS REGISTRATION N1693L. A TECH WAS WITH THE ACFT. INSPECTED AREAS OF PREVIOUS CONCERN AND SERVICE PREVIOUSLY WORKED BY MFG,SDR 26N2008F00003Control Cable · frozenON CLIMB OUT, AT 20,000 FT THE AILERONS FROZE WITH AN OAT OF 0 DEGREES C. PILOT WAS GETTING THE AMBER AP LIGHT. HE WOULD TURN THE AP "OFF" AND FREE UP THE CONTROLS ABOUT EVERY 15 TO 20 MINUTES BY EXERTING A LOSS OF FORCE TO FREE THE ICING. AT 33,000 FT WITH ANSDR DXTA200808263250Switch · inoperativeCLIMBING THROUGH FL 300, WITH AUTOPILOT ON AND FGC B IN CONTROL, "AILERON RATIO LOW" CAS MESSAGE APPEARS. AUTOPILOT BEGAN AN AGRESSIVE LT AND RT INPUT. HYD SYS NORMAL, WITH AUTOPILOT OFF INPUTS NORMAL. REMOVED BELLY PNL 166AB TO LOOK AT AILERON SELECTOR, CHECSDR DXTA200808213235Servo · inoperativeON DEPARTURE AFTER AUTOPILOT WAS DISCONNECTED AND ACFT HAND FLOWN TO LEVEL FLIGHT AILERON AND ELEVATOR SEEMED TO BE LOCKED IN POSITION. AFTER APPOX 30 SECONDS, FORCE APPLIED TO AILERON APPEARED TO BREAK THEM FREE. ACFT ROLLED SMARTLY TO THE RT, ROLL WAS SUCCESDR SWIA200819976Bushing · wornAILERONS FEEL DIFFICULT TO MOVE. FLIGHT 3604. INSPECTED CABLE RUNS, PULLEYS AND BELL CRANKS. REPLACED AILERON CONTROL QUADRANT BUSHINGS ON THE LEFT SIDE. OPS CHECK OF AILERON CONTROL SYSTEM IS NORMAL.
SDR DXTA200808153227Trim System · malfunctionedCLIMBING THROUGH FL230 AT 270 KNOTS INDICATED, "RETRIM L WING DOWN" AP DISENGAGED & ACFT REQUIRED 50 PERCENT LT AILERON TRIM. TRIM STAYED 50 % LT UNTIL DESCENT WHEN WE HAD A "RETRIM R WING DOWN" AT FL200, 340 KIAS. FUEL BALANCED WITH ZERO CTR FUEL AT ALL TIMESDR CA080902001Control Cable · frayed(CAN) DURING IMPORT INSP, THE LT AFT AILERON CABLE WAS CHAFING ON THE PHANOLIC RUB STRIP ATTACHED TO THE RIB EXTENSION AT WS 71.125 RESULTING IN SEVERE DAMAGE TO THE CABLE. CABLE REPLACED. UNFORTUNATELY THE CABLE HAD BEEN REMOVED BEFORE PICTURES WERE TAKEN OF SDR 26N2008F00001Control Cable · frozenCREW REPORTED AILERONS FROZE AFTER FLYING THROUGH MOISTURE. AC REPOSITIONED FOR FURTHER EVALUATION AND RESOLUTION. (K)SDR NWAA083569853Pulley · defectiveFLIGHT RETURNED TO A SAFE LANDING AT DTW AFTER CREW DETERMINED AILERONS WERE BINDING DURING LT TURNS. CONTROL CHECK WAS NORMAL ON THE GROUND BOTH BEFORE TAKEOFF AND DURING TAXI IN AFTER RETURN. LT TURNS REQUIRED THE MOST EFFORT BUT AILERON CONTROL WAS DIFFICSDR NWAA083469874Crank Assy · wornFLIGHT RETURNED TO DTW AFTER TAKEOFF DUE TO UNRESPONSIVE OR SLOW TO RESPOND FLIGHT CONTROLS (AILERONS). CREW NOTICED 2 TO 3 INCHES OF YOKE TRAVEL BEFORE ANY FLIGHT CONTROL INPUT RESULTED IN AIRCRAFT CONTROL. PER DISPATCH REPORT MAINTENANCE CONTROL WAS CONTACSDR CA080728003Pcu · failed(CAN) ENROUTE, CREW NOTICED HYD SYS (A) QUANTITY DECREASING RAPIDLY. SYS (A) HYDR WERE SHUTOFF AND EMERGENCY DECLARED. UPON ARRIVAL AT DESTINATION, A/C REQUIRED TOWING TO RAMP WHERE MAINT DISCOVERED THE AILERON PCU HAD FAILED. THE AILERON PCU WAS REPLACED AND SDR DXTA200807183182Aileron · out of rigDURING OCF FLIGHT FOR CONTROL CABLE CHANGE, WITH THE AILERON AND RUDDER TRIM WHEELS CENTERED, THE PLANE ROLLED LT AGGRESSIVELY ON TAKEOFF AND AT CRUISE SPEED. THE AILERON TRIM IS ABOUT .2500 INCH TO THE RT WHEN LEVEL. PERFORMED AILERON TRIM FLT NEUTRAL RIGGINSDR DXTA200803182Trim System · out of adjustDURING OCF FLIGHT FOR CONTROL CABLE CHANGE, WITH THE AILERON AND RUDDER TRIM WHEELS CENTERED, THE PLANE ROLLED LT AGGRESSIVELY ON TAKEOFF AND AT CRUISE SPEED. THE AILERON TRIM IS ABOUT .25 INCH TO THE RT WHEN LEVEL. (S)SDR SWIA200819915Control Cable · stiffAILERON CONTROLS FEEL STIFF IN FLIGHT. (FLIGHT NR 5536) ADJUSTED LT AND RT AILERON TENSIONS IAW MM 27-00-00. OPS CHECK GOOD.
SDR CA080709003Control Cable · misinstalled(CAN) FOUND BALL END OF LT AND RT AILERON CONTROL CABLES NOT FULLY ENGAGED IN WW BELLCRANK CABLE SLOT.(FWD CABLE) BALL END OF LT AND RT AILERON CONTROL CABLES IN WW BELLCRANK CABLE SLOT.(FWD CABLE) REENGAGED PROPERLY IN ACCORDANCE WITH AMM 27-11-03-400-801. SDR SWIA200819846Actuator · wornFLT 4083 - AILERON CONTROLS FEEL STIFF. REPLACED AILERON SERVO IAW CRJ MM 22-11-21 AND COPILOT'S CONTROL YOKE BEARING IAW MM 27-11-01. OPS CHECK GOOD.
SDR CA080709006Control Cable · broken(CAN) DURING CONTROL CABLES INSPECTION ON LT AND RT WINGS, FOUND AILERON CABLES (LT PN 190-04212-401, PN 190-04209-401, PN 190-05549-401, RT PN 190 -05551-401, PN 190-05550-401, PN 190-04209-401) WORN AND WITH SEVERAL WIRES BROKEN AT FAIRLEAD. EMBRAER CAME SDR DXTA200803141Control Cable · out of rigTHE AIRCRAFT HAS AN AGGRESSIVE ROLL LEFT WITH THE ASSOCIATED TRIM TAB CENTERED. PLACED A YOKE LEVEL ON THE YOKES AND OPENED THE AFT CABIN FLOOR. INSERTED A RIG PIN IN THE AILERON SECTOR. PLACED THE AILERON TRIM TO NEUTRAL. FOUND THE RT AILERON ABOVE STREAM LISDR 2008UALA03499Computer · failedELEVATOR - AILERON COMPUTER (ELAC) 2 INOP. CHANNEL 4 CPU FAILURE (INTERNAL) ON ELAC 2. REPLACED ELAC 2, OPS CHECKED GOOD.SDR 08FDEA02248Pulley · corrodedINTERMITTENTLY, THE LEFT OUTBOARD AILERON WILL NOT GO FULL DEFLECTION WHEN UNLOCKED. REMOVED AND REPLACED OB AILERON PULLEY AT WRAP AROUND FOR CABLE RUNS 7G AND 8G AND PERFORMED ADJUSTMENT/TEST IAW AMM 27-10-00-5.SDR A6WA200840491Regulator · out of rigAIRCRAFT REQUIRES 50% LT AILERON TRIM FOR LEVER FLIGHT, THE YOKE HAS LT TO RT SLOP FEEL ON FINAL APPROACH. THE YOKE HAD TO BE MOVED APPROXIMATELY 2-3 INCHES BEFORE RESPONSE. (A) RIGGED LT AND RT AILERON TENSION REGULATORS & RIGGED LT AND RT AILERON OUTBOARD SDR 2008UALA03196Computer · faultyELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN, F-CTL. ELAC NR 1 FAULTY. REPLACED ELAC-1 - OPS TEST OK. LAND CAT III CAPABILITY TEST OK.SDR DXTA200803086Unknown · malfunctionedDURING FLIGHT THE AILRON TRIM LIGHT CAME ON. TRIED TO MOVE AILERON TRIM KNOB, BUT IT WOULD NOT MOVE WITH AUTOPILOT OFF.SDR SWIA200819662Aileron · malfunctionedFLT 5721 - THERE IS A SLIGHT BIND WHEN THE AILERONS ARE MOVED LEFT TO RIGHT. INSPECTED AILERON CABLES, FITTINGS AND PULLEYS IAW MM 27-11-00. COULD NOT DUPLICATE THE DISCREPENCY. AILERONS CHECK GOOD.
SDR DXTA200803057Feel Sensor · bindingIN FLIGHT, AILERON FLIGHT CONTROLS ARE BINDING WHILE TURNING BOTH LT AND RT. REMOVED AND REPLACED ARTIFICIAL FEEL BUNGEE. PERFORMED OPS CHECKS AND ADJUSTMENTS ALL OK.SDR GUUA05090802Shroud · brokenFLIGHT: 9144, DURING FINAL APPROACH AILERONS JAM WITH AUTO PILOT OFF.
INSPECTED, FOUND LT AILERON IB BALANCE WEIGHT TABS BROKEN AND NOT ATTACHED. INSTALLED NEW LT BALANCE WEIGHT ASSY SHROUD. OPS CHECK, AILERONS NORMAL.SDR USAABB08084Control Quadrant · bindingPHL - FLT 703 - FRA TO PHL. DURING THE FLIGHT, THE FIRST OFFICER'S CONTROL WHEEL WAS BINDING WHILE USING THE AILERONS. THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S AILERON CONTROL QUADRANT.SDR A6WA200840365Nut · looseDURING AILERON CHECK, BONDING OF CONTROLS FROM LEFT TO RIGHT FROM NEUTRAL AND BACK TO NEUTRAL FROM RIGHT ON BOTH YOKES. TORQUED PILOTS AND CO-PILOTS CONTROL WHEEL LATCHING NUT IAW AMM 27-11-01. OPS CHECK GOOD. OK FOR FURTHER SERVICE. (K)SDR CWQR200803Control Cable · improper partDURING A ROUTINE CABLE REPLACEMENT OF AILERON CABLE PN 6660002-12, WE FOUND THAT THE CABLE HAD A SWAGED BALL AND A CLEVIS END INSTALLED. THIS CABLE ASSY SHOULD HAVE BEEN MANUFACTURED WITH THE SWAGED BALL WITHOUT THE CLEVIS. THE CABLE ASSY HAS BEEN SENT BACK TOSDR UALA2008111302182Servo · malfunctionedLT AILERON FAULT DISPLAYED ON UPPER ECAM SCREEN. CHRONIC A/C. MX WANTS TO WATCH THE LATEST FIX BEFORE CLOSING. REPLACED L B AILERON SERVO. ALL OPS NORMAL.SDR HALA0800532Module · malfunctionedAILERON STUCK 1/2 WAY LEFT OF CENTER IN FLIGHT. CKED FREEDOM OF MOVEMENT OF AILERON, NO DEFECT NOTED. FOUND AILERON TRIM IND OF CONFIG PG 1/2 LWD OF CENTER. ACCOMP FIM 27-10-00 TASK 801 MAINTENANCE MSG ON ATCL WAS NR 43 ACCOMP FIM 27-10-00 TASK 812. REPLACSDR HALA0800523Aileron · malfunctionedETOPS SIGNIFICANT SYSTEM ON CLIMB TO 320 W/AUTO PILOT ON BOTH (LT AND RT) INBD AILERON INDICES ON THE FLIGHT CONTROL STATUS DISPLAYS WERE 1/3 OF TOTAL SCALE ABOVE THE MEDIAN LINE. AT LEVEL, BOTH INDICES WENT TO 1/4 SCALE ABOVE MEDIAN. TURNING AUTO PILOT OFF SDR HALA0800526Aileron · unknownETOPS SIGNIFICANT SYSTEM RT INBD AILERON SEEMS TO FLOAT UP AT HIGH SPEEDS. 2 UNITS OF LEFT YOKE AT 330-340 KNOTS IS REQUIRED TO KEEP WINGS LEVEL. BOTH LT AND RT INBD AILERON INDICATORS SHOW 1/2 OF FULL DISPLACEMENT. AT SLOWER SPEEDS (BELOW 300 KNOTS) INBD ASDR BB08046Actuator · faultyPHL FLT 799 AMS TO PHL. PILOT REPORTS THAT THE AILERONS WERE BINDING FROM BOTH CAPTAIN'S AND F/O'S CONTROL WHEELS, ON THE GROUND AND IN FLIGHT. MAINTENANCE REPLACED THE LEFT UPPER LATERAL CENTER CONTROL ACTUATOR. OPERATIONALLY CHECKS OK.SDR HALA0800421Warning System · malfunctionedETOPS SIGNIFICANT SYSTEM, AILERON LOCKOUT LIGHT ILLUM. AT LOW SPEED EICAS "AILERON LOCKOUT" DISPLAYED. TEMPORARY CONDITION LIGHT ON AT 13,000' AND 250KT. STAYED ON 30SEC TO 1 MIN. PERFORMED FIM 27-11-00, NO FAULTS NOTED, OK FOR SERVICE.SDR WGEA200800051Bellcrank · bindingFOUND LT AILERON JOINT AND BELLCRANK BINDING. REMOVED LT AILERON, REPLACED LT BELLCRANK AND JOINT ASSY WITH NEW. REINSTALLED LT AILERON. VERIFIED RT AILERON DOES NOT HAVE ANY BINDING. COMPLIED WITH SATISFACTORY OP'S CHECK OF LT BELLCRANK AND JOINT. COMPLISDR WGEA200800050Bellcrank · bindingIN FLIGHT AILERON FLIGHT CONTROL SIDE STICK FEELS VERY NOTCHY WHEN ROLLING LEFT OR RIGHT. SUPPLEMENTAL INFORMATION-GAINED ACCESS TO RT AILERON JOINT, FOUND IT TO BE BINDING. REPLACED JOINT AND BELLCRANK WITH NEW. CHECKED LT AILERON JOINT AND FOUND IT TO BE SDR A6WA200840182Aileron · stuckIN FLIGHT, 4 SECONDS AFTER DISCONNECTION AUTOPILOT, AILERONS STUCK AND MOMENTARILY AILERONS COULD NOT BE TURNED LEFT OR RIGHT, ON 4 MILE FINAL. (M)SDR 08FDEA00877Guide · wornIN LT MLG AREA; ALL CABLE GUIDES INBD OF THE LT TRUNNION FOR THE AILERON CABLES ARE WORN. REMOVED AND INSTALLED 3 NEW CABLE GUIDES ON THE INBD SIDE OF THE LT MLG TRUNNION FOR THE AILERON CABLES IAW A310-300 AMM 20-21-12 AND AMM 27-10-00-6.SDR WGEA200800045Aileron · out of rigCOMPLIED WITH ECLIPSE TSR 27-030508G REV C. NO DEFECTS NOTED. PERFORMED AILERON FRICTION TEST, AILERON TENSION TEST AS PRESENTED IN SEC 12.3, PAGE 35 OF FLT CONTROL RIGGING SPEC. 27-109846 REV. 5, PERFORMED MEASUREMENT OF AILERON SKIN CONTOUR EAC AERO 07-500SDR IU6R232726Manifold · brokenFILTER BOWL BORE OF MANIFOLD BROKE OFF AT THE THREADS.SDR 2008UALA01227Seal · leakingRT OTBD AILERON INBD PCA ACTIVE LEAK 50 DROPS PER MINUTE. FOUND LEAKING ROD SEAL ON PCA. REPLACED RT OUTBOARD AILERON INBOARD PCA.SDR C2XA08ON099Manifold · inoperativeFLT 7822 - LAX - DURING PREFLIGHT CHECK CREW REPORTED NOT GETTING AILERON 2 INOP MSG ON EICAS WHILE AIRCRAFT WAS POWER UP WITH HYD SYSTEM OFF. MX PERSONNEL REMOVED AND REPLACED NR 2 AILERON HYD MANIFOLD OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASSDR CA080303002Control Cable · damagedDURING CONTROL CABLES INSPECTION ON LT AND RT WINGS, FOUND AILERON CABLES (LT P/N 170-05825-401) WORN AND WITH WIRES BROKEN AT FAIRLEADS, LOCATED AT LT WINGS INB OF THE RIB 17. THE WORN AREAS AND BROKEN STRANDS ARE LOCATED UNDER NYLON GROMMETS (P/N PE49068-50SDR 2008UALA01057Aileron · bindingAILERONS BINDING WHEN ROLLING TO THE LEFT. BINDING IS NOT SEVERE BUT CAN BE FELT, ABOUT EVERY THIRD TRY.SDR WGEA200800038Bellcrank · bindingAILERONS STIFF, A/P HAS DIFFICULTY RESPONDING TO FD COMMANDS ALSO. INSTALLED A NEW LEFT AILERON BELLCRANK IAW EA500 AMM 27-11-17. INSTALLED A NEW LEFT AILERON JOINT ASSEMBLY IAW EA500 AMM 27-11-18. C/W FLIGHT CONTROLS ADJUSTMENT/TEST (FUNCTIONAL CHECK) IAW SDR SWIA200819260Gear · lack of lubeFLT 6577 - AILERON ACTION IS NOT SMOOTH. LUBRICATED AILERON PRIMARY SERVO GEAR TEETH PER CRJ 700 SERVICE LETTER SL-22-004. OPS CHECK GOOD.
SDR WGEA200800037Bellcrank · bindingINSPECT LEFT AND RIGHT AILERON BELLCRANKS FOR CONDITION AND SECURITY. INSPECTED AILERON CONTROLS FROM AFT SECTOR TO BELLCRANK AND FOUND RIGHT BELLCRANK WITH EXCESSIVE FRICTION SEE NR-00002. REMOVED RIGHT AILERON TO GAIN ACCESS. REPLACED AILERON JOINT FITTINGSDR CA080222008Control Cable · worn(CAN) DURING CONTROL CABLES INSPECTION ON LT AND RT WINGS, FOUND AILERON CABLES (LT P/N 190-04212-401, P/N 190-04209-401, RT P/N 190 -05551-401, P/N 190-04209-401) WORN AND WITH SEVERAL WIRES BROKEN AT FAIRLEAD, LOCATED AT LT AND RT WINGS RIB 4A WS -3025.80 MISDR CA080222009Control Cable · wornDURING CONTROL CABLES INSPECTION ON LT AND RT WINGS, FOUND AILERON CABLES (LT P/N 170-05825-401, P/N 170-05826-401, RT P/N 170-05827-401, P/N 170-05828-401) WORN AND WITH WIRES BROKEN AT FAIRLEADS, LOCATED AT LT AND RT WINGS INB OF THE RIB 17. THE WORN AREAS
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