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 CA141114002Control Cable · broken(CAN) DURING FULL AND FREE FLIGHT CONTROL MOVEMENT CHECKS, THE PILOT NOTED THAT THE SPOILERS WERE NOT ACHIEVING FULL TRAVEL. WHEN MAINTENANCE DID A FUNCTIONAL CHECK THEY NOTED THAT THE AILERON WAS NOT MOVING IN THE UP POSITION, ONLY IN THE DOWN. WHEN CHECKED TSDR SIMA20141027005Support · brokenEXCESSIVE RESISTANCE ON YOLK WHEN PULLED AFT, LAST 1/3. TRANSFERRED TO NRWC 618-DFW-02203. IAW TO NRWC 618-DFW-02205 FOUND AILERON SUPPORT BROKEN & SUPPORT SEMI GROMMET DAMAGED AT STATION 5418.0 & 5833.0 IAW NRWC 618-DFW-02206. PERFORMED ELEVATOR CONTROL CASDR FDEA201410183314Actuator · malfunctionedAIRCRAFT TAKES AT LEAST 3.5 DEGREES OF LT DOWN AILERON TRIM FOR LEVEL FLIGHT. REMOVED AND REPLACED LT IBD AILERON ACTUATOR IAW MM.SDR IPXA2014092984450Actuator · out of adjustDURING CLIMB, SLATS RET RECEIVED LVL 2 AIL DEFLECT DISAGREE ALERT, RAN QRH CK LIST. DEFFERRED IAW DMP 27-13-2-0-1. ASSIGNED DI 538403. T/S C/O IAW FIM 28-08-05-00, REV 78.00, 07-22-14, FOUND AFSC AT FAULT. R & R SAME IAW AMM 28-08-03, REV 80.01, 09-23-14 OPSDR IPXA2014092684410Control Rod · damagedINSPECTION N, LEVEL 2 AILERON DEFLECT DISAGREE. TROUBLESHOT IAW FIM27-10-05 BLK 1,2,3,4,5,6. SYS FOUND NORMAL. UNABLE TO DUPLICATE FAULT. PERFORMED FCC-1 & -2 R-T-S TEST. ALL TEST PASSED. REMOVED LT OTBD AILERON DEFLECTION CONTROL ROD IAW AMM 27-16-02-0SDR CA140917008Pulley · seized(CAN) DURING HEAVY MAINTENANCE INSPECTION, AILERON CONTROL PULLEYS FOUND SEIZED AT WING STATION 242 LT AND RT. PULLEYS REPLACED WITH NEW.SDR N6WA2014091613Control Cable · corrodedBOTH RT AILERON CABLES AT WS 148.019 SHOW CORROSION. CLEANED & TREATED BOTH RT AILERON CABLES IAW AMM 20-70-00.SDR CA140912006Control Cable · frayed(CAN) LH OB AILERON CABLE IS BLENDED AND HAS SEVERAL BROKEN STRANDS. LH AILERON CABLE FROM LH NACELLE TO AILERON TERMINAL QUADRANT WAS REPLACED IAW AMM TASK#27-10-00-400-802. PICTURES ATTACHED.SDR CA140908020Cable · worn(CAN) FOUND RT AILERON CARRY THROUGH CABLE WEARING ON PHENOLIC WEAR STRIP NEAR FLAP CONTROL ROD. CABLE HAD WEAR THAT CAUSED BROKEN STRANDS.SDR CA140910008Control System · frozen(CAN) FLIGHT LEVEL 27,000 FT ,OAT -45 .THE AUTO PILOT DIS- ENGAGED AT THIS TIME THE PILOT TOOK CONTROL OF THE AIRCRAFT AND FOUND THE AILERON CONTROLS WERE FROZEN. THE PILOT DESENDED TO 15,000 FEET AT THIS POINT THE CONTROLS STARTED TO FREE UP AND AS THE AIRCRASDR CA140825003Spring · misinstalled(CAN) FOUND AILERON INTERCONNECT SPRING, RT, OF FUSELAGE ON WRONG SIDE OF BRACKET. PLACED SPRING ON CORRECT SIDE. FUNCTION CHECK CARRIED OUT. CHECK OK.SDR FDEA201408182202Control Cable · brokenCAC COMPARTMENT SLAT TO AILERON LOCK OUT CONTROL CABLE BROKEN. R & R SLAT TO AILERON LOCKOUT CONTROL CABLE IAW MM 27-11-04-2. ADJUSTED AILERON LOCKOUT & OPERATIONS CHECKED GOOD IAW AMM 27-10-00-5.SDR CA140815004Control Cable · worn(CAN) FOUND LEFT HAND AILERON CARRY THROUGH CABLES WEARING ON PHENOLIC WEAR STRIP NEAR FLAP CONTROL ROD.SDR ASOA2014080711026Control Panel · intermittentINBOUND, RECEIVED AN UNCOMMANDED LT FULL AILERON TRIM AND LT FULL RUDDER TRIM INDICATIONS. NORMAL CENTRAL FEEL WITH AP DISENGAGED. AP WOULD NOT REENGAGE. EMERGENCY ACTIONS, AILERON TRIM SYSTEM, REMOVED AND RE-INSTALLED AILERON/RUDDER CONTROL PANEL. PERFORSDR CA140805005Pulley · seized(CAN) THE FLIGHT CREW REPORTED THAT THE ROLL CONTROL WAS STIFF IN FLIGHT FOR BOTH LT AND RT TURNS. MAINTENANCE INVESTIGATION FOUND A SEIZED PULLEY IN THE AILERON CIRCUIT AT THE LT WING ROOT. THE PULLEY WAS REPLACED AND SYSTEM TESTED SERVICEABLE.SDR QXEA2014073100642Actuator · malfunctionedAILERONS, WHEN TURNING RIGHT REQUIRES STRAINED PRESSURE AND SOME RESISTANCE SPEEDS ABOVE 200 KTS VERY NOTICEABLE. AILERON CABLE RUN INSPECTION, TENSION, AND RIGGING. FUNCTIONAL TEST OF ROLL SPOILERS AND TIGHTENING OF LEAKING B-NUT ON THE RT OTBD SPOILER. TESDR SIMA20140722001Switch · inoperativeAILERON SYS 1 INOPERATIVE IN FLIGHT. R & R AIL SYS NR 1 PUSH BUTTON IAW AMM 20-13-08. OPERATIONS CHECKED GOOD AT THIS TIME.SDR ASOA20140714097Disconnect Unit · malfunctionedTHE CREW REPORTED THAT ON ARRIVAL WHEN THE AUTOPILOT WAS DISCONNECTED, THE CAPTAIN LOST TOTAL CONTROL OF THE AILERONS DURING SHORT FINAL. F/O'S SIDE HAD MINIMAL INPUT. LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE AILERON DISCONNECT UNIT, AND AS A PRECAUTSDR SIMA20140713006Actuator · failedON TAKEOFF FELT A SLIGHT UNCOMMANDED ROLL. R & R ROLL TRIM ACTUATOR IAW AMM 27-14-00. OPERATIONS CHECKED GOOD.SDR FDEA201406281576Pulley · defectiveON DEPARTURE CLIMB WITH AUTO PILOT NR 2 ON WHEN THE SLATS WERE RETRACTED THE ACFT GAVE VERY HARD TO THE RT. THE AILERONS COMPENSATED BY GOING LT 6 UNITS. AT THIS POINT WE CHECKED THE FLIGHT CONTROL POS PAGE & SPOILERS 7, 6 & 5 ON THE LT WING WERE UP. AFTERSDR CA140627001Mechanism · stiff(CAN) PILOT REPORTED: F/O YOKE FEELS STIFF DURING CONTROL CHECK. ONLY STIFF WITH LT AILERON, F/O SIDE. FOUND STIFFNESS AND NOISE EMANATING FROM AILERON TRANSFER CONTROL MECHANISM ASSY. MECHANISM ASSEMBLY REPLACED.SDR USAA2014062700003Control Servo · faultyEN ROUTE AN ABRUPT MOMENTARY UNCOMMANDED AILERON ROLL IN CRUISE FLIGHT. FLIGHT CONTROL AILERON SERVO FAULT ILLUMINATED ON ECAM. AMBER B SYS FAULT INDICATED ON E & W DISPLAY. LT OTBD B AILERON CONTROL SERVO, FIN 33CE3 IAW AMM 27-14-51-000-001A. SYS OPS CHECSDR UIEA2014061200233Control Cable · out of adjustLEFT AILERON FLIGHT CONTROL CHECK. PRONOUNCED BUMP COMING BACK TO NEUTRAL. FOUND LOST MOTION DRUM OUT OF RIG. AILERON BUS CABLES ACBA & ACBB ADJUSTED IAW MM 27-11-00. AILERON SYS FUNCTIONAL CHECK OK IAW MM 27-11-00.SDR CALA2014060991250Aileron · malfunctionedRIGHT AILERON DEFLECTED DOWN 2 - 3 SCALE WITH ASSOCIATED ROLL OBSERVED.SDR CALA2014060991237O-Ring · damagedHYDRAULIC QTY DECREASED TO 047. QTY STABLE WITH PUMPS OFF RT SYS FIM 29-11-00 FIG 107. REPLACED O RING ON LT AILERON ACTUATOR PLUG FOUND LEAKING.SDR YENA20140525100Servo Control · leakingDURING CRUISE, FLT 390, WITH AUTOPILOT ON, EXPERIENCED SUDDEN FIVE DEGREE ROLL OR DIP TO LT WITH IMMEDIATE RECOVERY. AT SAME TIME FLIGHT CONTROL AILERON SERVO FAULT ECAM APPEARED ON FLIGHT CONTROL PAGE LT AILERON "B" HAS AMBER BOX DISPLAYED. ECAM & QRH COMPSDR USAA2014052200012Control Servo · unserviceableAIRCRAFT EXPERIENCED SLIGHT ROLL OSCILLATIONS, LEFT DURING CRUISE CLIMB AT .78 265 KIAS FOLLOWED IMMEDIATELY BY FLIGHT CONTROL AILERON SERVO FAULT ECAM. FLIGHT CONTROL STATUS PAGE DISPLAYED G AILERON SERVO INOPERATIVE SYMBOLOGY. ALTITUDE FL310 CLIMBING. ROLLSDR CA140515006Boot · unsecure(CAN) LT AND RT CONTROL BOOTS FOR AILERON CONTROL RODS CAME LOOSE, UNGLUED IN WING CENTER SECTION.SDR CA140516002Bolt · interference(CAN) BALANCE CABLE TO LT AILERON BELLCRANK ATTACH BOLT FOUND TO BE INTERFERING WITH AILERON PUSHROD AT FULL TRAVEL.SDR CA140505014Control Cable · misrouted(CAN) WHILE PERFORMING A VISUAL INSPECTION IN THE FLIGHT COMPARTMENT UNDER FLOOR, AME TECH NOTICED MISROUTED CABLES BETWEEN AILERON AUTO-PILOT SERVO AND AILERON CABLES, BOTH SYS CABLES WERE MAKING CONTACT BETWEEN EACH OTHER, CHAFING. WHEN PERFORMING SUCH MAINSDR CA140502006Servo · failed(CAN) DURING CLIMB, WHILE THE ACFT WAS EXECUTING A LT BANK TURN WITH THE AUTOPILOT ENGAGED, FLIGHT CREW RECEIVED A BOXED "A" YELLOW INDICATION ON THE PRIMARY FLIGHT DISPLAY (PFD) INDICATING A SIGNIFICANT MISTRIM CONDITION ASSOCIATED WITH AN AP TRIM IS LWD CAUTSDR A6WA201441460Aileron · stiffWITH AUTOPILOT OFF, AILERONS VERY STIFF TO MOVE IN BOTH DIRECTIONS. ON APPROACH FIRST OFFICER COULD ONLY ROLL AILERONS 1/2 TRAVEL TO THE RIGHT.SDR CHQA20140423137Fitting · damagedDURING INSPECTION, THE LT AILERON ACTUATOR ATTACH LUG OTBD HAT BUSHING WAS FOUND TO BE MIGRATING AWAY FROM THE LUG. THE LT AILERON PCA FITTING WAS REPLACED IAW SRM 51-20-01 & SRM 51-40-02.SDR SIMA20140410014Control Cable · frayedRIGHT AILERON CABLE IN WW AREA THAT CONNECTS TO AILERON SERVO MOUNT IS FRAYED. R & R CABLE IAW AMM 27-11-00-400-804 & E379813 FOR CABLE TENSION CHECK.SDR SWAA2014032626545Pcu · leakingDIVERSION A SYS LEAKED FOLLOWED BY TOTAL A SYS FAILURE. R & R AILERON PCU IAW MM.SDR CA140320003Control Cable · frayed(CAN) THIS IS A 2005 172S AIRPLANE WITH 1300 HOURS TOTAL TIME & THE ACFT HAS BEEN HUNGERED MOSTLY THAT WE ARE IMPORTING. DUE TO PAST EXPERIENCE OF FINDING FRAYED AILERON CABLES IN THESE MODELS, THE AILERON CABLES IN THE WINGS WERE REMOVED FOR DETAILED INSPECTSDR CA140514005Feel Unit · interference(CAN) INTERFERENCE WAS FOUND BETWEEN LT WHEEL WELL STRUCTURE, FR52 AND AILERON FEEL UNIT WHEN FULLY TRIM RT WING DOWN. INTERFERENCE BETWEEN STRUCTURE & AILERON FEEL UNIT PERMANENTLY REPAIRED IAW ETD 2014-190-023347 & ERJ190-53-53144. HFEC C/O AT BLENDED AREASDR 7GMB1159032020141Pca · failedCREW REPORTED AILERON CONTROL STIFFER THAN NORMAL IN FLIGHT. THE ACFT LANDED SAFELY AT THE DESTINATION. MAINTENACE TROUBLESHOT AND FOUND LT AILERON PCA, POWER CONTROL ACTUATOR, FAILED DAMPING COMPONENT AND MONITORING DEVICE FUNCTIONAL CHECK. SPECIAL FLIGHT PESDR CA140310010Control Cable · misinstalledCABLE, PN 6560141-6, ORDERED FOR REPLACEMENT DURING PHASE 5 INSPECTION. PRIOR TO INSTALLATION AME NOTICED THE BALL END WAS SWAGED ON BACKWARDS. THE SHANK END OF THE BALL SWAGE THAT IS TO PROTRUDE THROUGH THE FORK WAS FACING THE WRONG WAY. A CABLE WAS RE-ORDSDR J7SA0228201401Control System · stiffON CLIMB OUT POSITIONING FROM KPDX TO KSJC CREW REPORTED BOTH PILOTS & COPILOTS AILERON CONTROLS WERE STIFF. CREW DIVERTED TO KSMF. CREW DECLARED AN EMERGENCY, AILERONS RETURNED TO NORMAL AT APPROXIMATELY 10K & ACFT LANDED SAFELY.SDR SWIA201436411Trim Panel · faultyCONFIGURE TRIM WARNING. NOTICED AILERON & RUDDER TRIM INDICATIONS FULLY DEFLECTED. IN FLIGHT SLOWLY RETURNED TO CTR. RUDDER REMAINED, AILERON CONTINUED ROLL DEFLECTION IN OPPOSITE DIRECTION. AIRCRAFT OPERATED NORMALLY OTHERWISE. IN FLIGHT CAUTION AP TRIM SDR 2014FA0000076Cable · frayedLEFT AILERON CABLE WOULD WEAR ON CABLE FAIRLEAD BLOCKS CAUSING CABLE TO FRAY. FAIRLEAD BLOCKS WERE A REPLACEMENT FOR A PULLEY. FAIRLEADS LOCATED ABOVE PASSENGERS HEADLINER.SDR SIMA20140216007Support · corrodedAILERON FWD TORQUE TUBE RT SUPPORT CORRODED. R & R AILERON FWD TORQUE TUBE RT SUPPORT IAW SRM 51-40-02.SDR OG5S2014FA0000072Control Cable · frayedALL THREE AILERON CABLES FRAYED WHERE THE CABLES RUN THROUGH THE 3 FAIR-LEADS MOUNTED ABOVE THE OVERHEAD CABIN PANEL. THE FAIR-LEADS, PN 0560100-3 WERE A REPLACEMENTS FOR PULLEYS, PN S394 MOUNTED IN THE SAME LOCATION.SDR CA140211004Aileron Sys · jammed(CAN) EVENT PILOT HAND FLEW THROUGH FL200, THEN AUTOPILOT WAS ENGAGED, ALL SYSTEMS NORMAL. CLIMBING THROUGH 280 AMBER CAS, AP HOLDING LW DOWN, APPEARS. FUEL WAS BALANCED WITHIN 20 LBS, AILERON TRIM IS NEUTRAL. PILOT DISENGAGES AP, TRIMS TO RELIEVE RESS, APPSDR SWIA201436250Unknown · malfunctionedA/C REQUIRES RWD AILERON TRIM UNTIL FLAPS ARE EXTENDED FOR LANDING. THEN REQUIRING CONSIDERABLE LWD AILERON TRIM. YOKE WAS BINDING DURING ROLLS TO THE LT & RT IN THE LANDING CONFIGURATION. FLT 6378 COMPLETED DETAILED INSPECTION OF THE AILERON & AILERON AUTOSDR CA140115004Control Cable · frayed(CAN) RIGHT AILERON CONTROL CABLE WAS REMOVED TO INSPECT THE CONDITION OF THE CABLE DUE TO PREVIOUS ISSUES WITH STAINLESS STEEL CABLES FRAYING ON THE RUB STRIP. FRAYING WAS AGAIN FOUND ON THE CABLE WHERE THE CABLE CONTACTS THE RUB STRIPS IN THE WING.SDR CALA2014011390135Actuator · faultyAILERON LOCKOUT EICAS ADVISORY MESSAGE DISPLAYED. EITHER OR BOTH AILERON LOCKOUT ACTUATOR UNLOCKED WHEN IT SHOULD BE LOCKED, OR LOCKED WHEN IT SHOULD BE UNLOCKED OR FAILED. AIRCRAFT SEEMS TO FLY NORMALLY. REPLACED LT OTBD AILERON LOCKOUT ACTUATOR IAW AMM27-SDR USAA2014010600020Transducer · faultyEN ROUTE FROM PHL TO UVF, CREW REPORTED AN ECAM. F/CTL AILERON SERVO FAULT. FLIGHT RETURNED TO FIELD AT PHL & LANDED WITHOUT INCIDENT. RECEIVED CFDS POST FLIGHT REPORTS. LAST LEG, ELAC 1 OR INPUT OF LT PEDALS TRANSDUCER UNIT 25CE1 FAULTS. TROUBLESHOOTING SDR CA140103014Aileron Sys · stiff(CAN) DURING DESCENT, CREW DISCONNECTED THE AUTOPILOT, AT WHICH TIME THEY NOTICED THE AILERON AND ROLL CONTROL WERE VERY STIFF, CREW STATED THAT THE ACFT REMAINED LEVEL BUT VERY DIFFICULT. EXCESSIVE CLEAN OFF AILERON ARTIFICAL FEEL UNIT INPUT SHAFT-LT WHEEL W
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