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 UALA2013060603954Servo · out of adjustRT AILERON FAILED FREE PLAY CHECK WITH INBD SERVO ACTIVE R & R RT AILERON SERVO. ADJUSTED SERVO FREEPLAY, CHECKED GD SERVO & OPS CK SERVO IAW MM 27-14-51-000-001-A, 27-14-51-400-001-A, 27-14-00-220-0014, 27-14-00-820-001-A AND 27-14-00-710-001-A. OPS CK & FRSDR UALA2013060603929Bolt · scoredLEFT AILERON ATTACH BOLTS SCORED. REPLACED DAMAGED BOLTS IAW MM.SDR UALA2013060503882Actuator · stuckLEFT INBD AILERON STUCK, FLT DIVERTED. FLT CREW ATTEMPTED TO MOVE AILERON. NO MOVEMENT NOTED. REPLACED LEFT INBD AILERON OTBD PCA IAW MM.SDR USAA2013060300009Computer · malfunctionedAFTER ELAC FAILURE THERE WAS A REPETITIVE AIRFRAME JOLTING THAT SEEMED TO BE ASSOCIATED WITH UNCONTROLLED RT AILERON MOVEMENT VERIFIED ON F/CTL PAGE. R & R NR 1 ELAC IAW AMM 27-93-00-710-001-A.SDR DXTA2013053105405Aileron Sys · lack of lubeDURING GROUND FLIGHT CONTROL CHECK, AIRLERON MOVEMENT APPEARED STIFF BETWEEN MID TO FULL TRAVEL. INFLIGHT, THE STIFFNESS INCREASED SPECIFICALLY WHEN ROLLING TO THE RT. PROBLEM DETECTED WHILE AUTOPILOT WAS SELECTED OFF. INSPECTED AND LUBED AILERON PULLEYS ASDR ASOA20130530161Fitting · wornDURING C-CHECK THE RT AILERON PCA FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MX R & R THE FITTING IAW EC5750-01177. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR HNAA2013052900313Control Cable · out of adjustLEFT ROLL CONTROL JAMMED DURING FLARE. CREW WAS ABLE TO OVER POWER JAM DURING ROLLOUT. INSPECTED ROLL CONTROL SYS AND FOUND AILERON CABLE TENSIONS TO BE LOW. TENSIONED AILERON CABLES TO THE CORRECT TENSION IAW AMM 27-00-00. NO OTHER DEFECTS NOTED.SDR DXTA2013052905402Trim System · contaminatedAT FL 400, AUTOPILOT DISENGAGED, DISCOVERED THE AILERON TRIM ALMOST UNMOVABLE. ABLE TO MOVE TRIM WITH EXCESSIVE FORCE. DURING POST-FLIGHT, AILERON TRIM MOVES FREELY. POSSIBLE FREEZING ISSUE AT ALTITUDE. CHECKED AILERON TRIM TENSION & AILERON WING CABLE TESDR UALA2013052403624Actuator · leakingLEFT OTBD AILERON (OTBD ACT) REPLACEMENT IAWL AMM SUP: COMPLIED WITH STEPS UP TO 2G ,(2C) BY- 236406. CW WITH LT OTBD AILERON PCA IAW MM. REPLACED LT OTBD AILERON (OTBD) ACT IAW AMM. WITNESSED INSTALLATION OF LT OTBD AILERON PCA IAW MM.SDR CA130531001Control Cable · mislocated(CAN) DURING B CHECK THE AILERON CABLE SYSTEM WAS MODIFIED AS PER REF/A/. FOLLOWING THE AIRFRAME VISIT, CABLE CONTACT WAS NOTED ON THE GROMMET AT THE WHEEL WELL, THE CABLE ORIENTATION WAS ALSO FOUND ROTATED APPROXIMATELY 90DEGREES FROM THE SB ILLUSTRATION. FOLSDR UALA2013051703432Aileron Sys · unknownON TAXI OUT, FLT CREW OBSERVED A MISMATCH BETWEEN THE LT AND RT INBD AILERONS. OBSERVED FROM THE AILERON INDICATION ON SECONDARY EICAS. NO MESSAGES GENERATED, VISUAL INSPECTION ACCOMPLISHED FOR FULL AILERON TRAVEL IN BOTH DIRECTIONS. NO BINDING EVIDENT IN SDR UALA2013050703211Actuator · malfunctionedDURING CRUISE, NO RT INBD AILERON INDICATION MOVEMENT. DISCONNECTED AUTOPILOT AND ACCOMPLISHED SERIES OF TURNS. CONFIRMED RT INBD AILERON WOULD NOT MOVE DOWN DURING TURNS. AILERON ALSO NOT FAIRED IN NEUTRAL POSITION AND REQUIRED LT AILERON TRIM TO MAINTAIN SDR CA130429005Aileron Sys · binding(CAN) THE CREW FIRST NOTICED AN AIL AMBER INDICATION ON THE PFDS FOLLOWED SHORTLY BY THE AP TRIM IS LWD CAUTION MESSAGE. THE CREW DID NOT NOTICE ANYTHING ABNORMAL ON THE F/CTL SYNOPTIC PAGE. THE QRH CHECKLIST WAS RUN AND UPON AP DISCONNECT, AILERON CONTROL WASDR GUX220130527001Cable · misinstalledAIRCRAFT IN FOR BRIDGING CHECK. DURING INSPECTION, THE LT WHEEL WELL AREA,NOTED THAT THE AILERON CONTROL BUSS CABLE WAS INCORRCTLY ROUTED AND CHAFFING WITH THE PULLEY BRACKET ASSEMBLY.SDR UALA2013042202780Actuator · leakingHYDRAULIC LEAK COMING FROM LEFT OUTBD AILERON. LEAK WAS FROM AILERON ACTUATOR ROD, APPROX 15 DRIPS PER MINUTE WITH PRESSURE ON 0 WITH PRESSURE OFF.SDR UALA2013042202774Servo · faultedDURING FLIGHT CONTROL CHECK, RIGHT AILERON DOES NOT SHOW FULL DOWN TRAVEL INICATOR DOES NOT ENTER. REPLACED SERVO 33CE2 RIGHT GREEN SERVO ACTUATOR PER AMM. RIGGED AND OPS & LEAK CHECKED GOOD.SDR 9JLA2013042204660Line · chafedDURING ROUTINE MX, A HYD SEEP WAS DISCOVERED IN THE LT INBD FLAP AREA. TROUBLSHOOTING FOUND THE LT SPEED BRAKE RETRACT RIGID HYD LINE WAS BEING CHAFED BY THE MOVEMENT OF THE LT INBD FLAP PUSH/PULL ROD BONDING JUMPER. THE HYD LINE WAS REPLACED AND THE BONDINGSDR CA130416019Fairlead · broken(CAN) THE MRO FOUND A FAIRLEAD BROKEN ON THE AILERON SYS IN FWD CARGO AFTER INVESTIGATION. FOUND WRONG FLANGE BUSHINGS INSTALLED AT INBD SIDE. BUSHINGS REPLACED IAW AMM 20-10-08, GOUGES PERMANENTLY REWORKED IAW PP ERJ190-54-49951.SDR UALA2013041502560Actuator · leakingRIGHT WING OTBD AILERON ACTUATOR LEAKING. REPLACED RIGHT OTBD AILERON CONTROL PACKAGE PER AMM.SDR 2013FA0000228Motor · failedPILOT REPORTED AUTO-PILOT INOPERATIVE AND AILERONS FLOPPING AROUND MUCH MORE FREELY THAN USUAL. ON ANNUAL INSEPECTION, REMOVAL OF THE LT AILERON WELL INSPECTION PANEL REVEALED THE ROLL/AILERON TRIM MOTOR ACTUATOR ARM BUNGEE TOTALLY SHEARED OFF OF MOTOR DRIVESDR UALA2013040402243Control Unit · no testRIGHT AILERON FAILS FREE PLAY CHECK. REMOVED AND REPLACED BOTH INBD AND OTBD RIGHT AILERON SERVOS CONTROL UNITS IAW AMM, OPS CHECKED GOOD IAW AMM. FREE PLAY CHECKED GOOD.SDR CA130325017Control Cable · damaged(CAN) AILERON CABLE FOUND UNSERVICEABLE ON LT WING T/E, ONLY 1 STRAND WAS REMAINING.SDR HNAA2013032600185Control Cable · frayedAILERON CABLE FOUND UNSERVICEABLE ON LT WING T/E, ONLY ONE STRAND WAS REMAINING. OPENSDR CA130325004Pcu · separated(CAN) DURING ROUTINE MAINTENANCE, WITH "B" PUMPS ON AND HYDRAULIC INTERCONNECT "OPEN" TO LOWER THE FLAPS, WHEN NORMAL OPERATING PRESSURE WAS REACHED IMMEDIATE LOSS OF HYDRAULIC PRESSURE WAS NOTICED ALONG WITH MASSIVE AMOUNTS OF HYDRAULIC FLUID GUSHING OUT OF TSDR VNAA2013032200018Pcu · leakingCREW REPORTED HYD 3 LOW PRESSURE CAUTION MESSAGE AND INBOARD GROUND SPOILERS CAUTION MESSAGE AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED SAFELY. AIRCRAFT TOWED FROM RUNWAY DUE TO INOPERABLE NOSE WHEEL STEERING AND PASSENGERS TAKEN BY BUS TO TERMINAL. MSDR CA130320005Bearing · rough(CAN) FLIGHT CREW REPORTED STIFF AILERONS WITH AUTO PILOT DISCONECTED. RT WING AILERON QUADRANT BEARINGS FOUND SIEZED. RT WING QUADRANT ASSY REMOVED DISASSEMBLED, BEARINGS REPLACED IN QUADRANT HSG. AILERON TERMINAL QUADRANT INSTALLED IAW 27-12-31 OF THE AMMSDR 2013FA0000168Control Cable · chafedDURING ANNUAL INSPECTION, BOTH RT AILERON CABLES WERE CHAFING ON FAIRLEAD JUST INBD OF THE AILERON AUTOPILOT SERVO AT WS 101. ON REMOVAL FRAYED WIRES WERE FOUND ON BOTH CABLES. THIS IS THE FOURTH SET OF CABLES WE HAVE FOUND CHAFING AT THIS SAME POINT ON ACFSDR SIMA20130313004Fitting · gougedDURING MAINTENANCE INSPECTION FOUND RIGHT AILERON PCA FITTING DAMAGED. THE AIRCRAFT WAS REMOVE FROM SERVICE. REMOVED AND INSTALLED PCA FITTING IAW EO EM-27MR-112. OPS CHECK GOOD FOUND. THE AIRCRAFT RETURN TO SERVICE.SDR WRLA20130308587Actuator · bypassingCREW REPORTED "AUTO PILOT 2 UNAVAILABLE IN FLIGHT. TURNING FINAL APPROACH AUTO PILOT 1 DISCONNECTED. ROLL CONTROL HAD RESISTANCE". DURING TROUBLESHOOTING MAINTENANCE FOUND, WITH ELECTRICAL POWER REMOVED FROM ACTUATOR AND WITH INPUT MECHANISM TO ACTUATOR DISCSDR SIMA20130304001Actuator · failedFLIGHT 9806. CREW REPORTED ACFT BANKS HARD TO RIGHT WITH AILERON TRIM AT ZERO. TO KEEP WINGS LEVEL 1/4 ROLL TRIM IS REQUIRED. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT AND RIGHT AILERON ACTUATORS IAW AMM 27-21-01. OPS AND & LEAK CHECKED GOODSDR IVLA20130209002Cartridge · bindingROLL TRIM CARTRIDGE CAUSED AILERON NOT TO RETURN TO NEUTRAL POSITION. FLIGHT CONTROL WAS STILL MOVEABLE. WAS FOUND ON PREFLIGHT. BELIEVE DIRT ON ACTUATION ARM CAUSED THE PROBLEM.SDR UALA2013021200840Servo · faultedAILERON DAMPING TEST DOES NOT PASS TEST EFCS NR 1 & 2 IN DOWN FACTOR IN THE LEFT AILERON. REPLACED LEFT AILERON SERVO IAW AMM. PERFORMED OPERATIONAL & DAMPING TEST OF SERVO'S WORKS OK, ACFT RETURNED TO SERVICE.SDR UALA2013021100803Actuator · faultedAILERON LOCKOUT EICAS. FOUND LEFT OUTBOARD LOCKOUT ATCUATOR AT FAULT. REPLACED ACTUATOR AS PER MM AND ACP TEST AS PER MM. ALL OPS OK AND INDICATIONS GOOD. CARRIED OUT INSPECTION OF REPLACEMENT OF LEFT AILERON LOCK OUT ACTUATOR, OBSERVED TEST ALL SATISFACTSDR SIMA20130207002Fitting · gougedDURING MAINTENANCE INSPECTION FOUND THE RIGHT AILERON PCA FITTING DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED PCA FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CA130206008Cable · damaged(CAN) OPERATOR HAS CARRIED OUT THE INSPECTIONS IAW SB V6/0022 AND HAS REPORTED THE CABLE IS DAMAGED WHERE IT CONTACTS THE FAIRLEAD, PN CSP135-2 LOCATED ON THE WING ROOT RIB. MFG ENGINEERING IS REVIEWING.SDR CA130206007Cable · damaged(CAN) OPERATOR HAS CARRIED OUT INSPECTION IAW SB V6/0022 AND REPORTED CABLE IS CONTACTING THE FAIRLEADS LOCATED ON THE WING ROOT RIB. ENGINEERING IS REVIEWING.SDR CA130206005Control Cable · chafed(CAN) AILERON CABLE FOUND CHAFED AT CONTACT POINT WITH FAIRLEAD PN CSP135-2 LOCATED ON WING ROOT RIB. ENGINEERING IS INVESTIGATING.SDR FDEA201302010248Bearing · failedON TAKEOFF ROLL AT 100-110 K, AILERON CONTROL WAS UNUSUALLY STIFF WIND WAS 290/19 NO GUST. REJECTED TAKEOFF, AND PERFORMED RTO CHECKLIST IN QRH. DURING TROUBLESHOOTING, FOUND BAD BEARING AT BOTH ENDS OF INBD PCA INPUT ROD SEIZED AND FALLING APART. REMOVED SDR SAJF20130201004Cable · broken(B-18715) ACFT PUSH BACK IN POSITION, FLAP DOWN, FOUND LT OTBD AILERON INOPERATIVE. THE ACFT WAS TOWED BACK TO HANGAR FOR MAINT. GROUND CK FOUND LT AILERON CONTROL CABLE AB13 BROKEN AND CABLE AA11 FRAYED. PFM INSPECTION OF AILERON CONTROL QUADRANT, CABLE DRSDR ASMF201303013Aileron Sys · out of adjustCAPTAIN REPORTED THAT DURING FLIGHT AND ON GROUND, THE AILERONS WERE HARD TO MOVE. MX PERSONNEL PERFORMED AILERON ADJUSTMENT AND TEST IAW AMM 27-11-00, ALL CORRECT.SDR HSYA2013011512Aileron Sys · frozenPILOT REPORTED THAT ON CLIMBOUT, NOTICED THE AILERON TRIM SEEMED TO BE FROZEN AND FELT LIKE IT WAS BINDING. WHEN TRYING TO ADJUST IT WOULD ONLY MOVE A LITTLE AND THEN SPRING BACK RIGHT AWAY. PILOT DECIDED TO RETURN TO DEPARTURE AND LANDED WITHOUT FURTHER INCSDR UALA2013010700075Actuator · faultyAILERON LOCKOUT. REPLACED LEFT AILERON LOCKOUT ACTUATOR PER MM, OPS TESTED GOOD. NO MESSAGES NOTED.SDR N6WA201301005001Control Cable · brokenCONTROL WHEEL (YOKE) DIFFICULT TO MOVE LEFT. FOUND AILERON SERVO CABLE BROKEN. REMOVED CABLE AND PERFORMED OP'S CHECK OF THE AILERON CONTROL SYS IAW AMM 27-11-00. NO FURTHER RESTRICTIONS OBSERVED. FOUND SAFE FOR A 1 TIME FERRY FLIGHT.SDR USAA2012121800025Control Cable · out of rigCREW REPORTED THAT EITHER A LEFT WING DIP OR A RIGHT WING RISE OCCURRED ON TAKEOFF OUT OF ORD. THIS HAD TO BE COUNTERED WITH A LARGE RIGHT AILERON INPUT. FLIGHT CONTINUED TO DESTINATION . QUICK CHECK OF SPOILER ACTUATORS FOR HISSING SOUNDS AND EXCESSIVE HEATSDR MTNA20121213001Aileron · lack of lubeAILERON, RUDDER AND ELEVATOR TRIM TOO STIFF, ELEVATOR TRIM SOMETIMES JAMS DURING FLIGHT. TROUBLESHOOT ALERON TRIM IAW C208 MM CH 27-10-02 PG 101 AND LUBED SYSTEM IAW MM 27-10-02 PG 601. TROUBLESHOOT RUDDER TRIM IAW MM 27-20-02 PG 102 AND LUBED FLEX SHAFT ASSSDR ASOA2012121202640Control Panel · unserviceableAILERON AND RUDDER TRIM UNCOMMANDED DEFLECTIONS. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE. R & R AILERON/RUDDER TRIM CONTROL PANEL IAW 700 27-12-10. PERFORMED OPS TEST OF AILERON/RUDDER TRIM IAW AMM 27-11-00-710-802 AND 27-22-00-710-801. NO FAULTS FSDR UALA2012111906691Warning System · activatedAIL SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. - F- CTLPROG TEXT: - ITEM ROLLED FORWARD. PFR FAULTING ELAC 1 & RT GREEN AIL MODE VLV. COMPLIED WITH MEL. PARTS: 482-9572 MR27935 AVL HMC RES/20NOV (644-9013) MR27145 SEE *F4649*.SDR A6WA201211204516Servo · defectiveIN CLIMB & CRUISE EXPIERINCED SLIGHT DUTCH ROLL MOVEMENT WITH ASSOCIATED LEFT WING DOWN AILIERON INDICATION. REF WO 193452 FOR ALL WORK PERFORMED REPLACED AILERON SERVO AND FCC # 2 AND ACCOMPLISHED FLIGHT CONTROL RIG AND OP CHECKS.SDR CA121114004Bearing · seized(CAN) 2 AILERON CIRCUIT PULLEYS IN THE RT SIDE OF THE CENTER WING AREA WERE FOUND TO HAVE SEIZED BEARINGS. DISCOVERED DURING AILERON CABLE REPLACEMENT. REPLACED WITH NEW.SDR CA121108005Bearing · seized(CAN) THE FLIGHT CREW REPORTED STIFF ROLL CONTROL. ON THE GROUND THEY DID A ROLL DISCONNECT AND FOUND THAT THE F/O CONTROL WHEEL WAS VERY STIFF TO OPERATE. MAINTENANCE INVESTIGATION FOUND THE LT WING AILERON QUADRANT CORRODED AND BEARINGS SEIZED. THE LT AILE
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