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 USAA2012110800012Servo Valve · faultyFLIGHT CREW REPORTED AILERON FLUTTER AFTER TAKEOFF. DECLARED AN EMERGENCY AND RETURNED TO PHX. MAINTENANCE REMOVED AND REPLACED RIGHT GREEN AILERON PCU SERVO VALVE IAW AIRBUS MAINTENANCE MANUAL 27-14-51.SDR SWIA201232154Aileron · out of adjustDURING DESCENT AIRCRAFT STARTED UNCOMMANDED LEFT TURN. UPON DISCONNECTING AUTOPILOT, AIRCRAFT CONTINUED LEFT TURN. (FLT 5615) INSPECTED ALL FLIGHT CONTROL CABLE ROUTING AND TENSIONS. ADJUSTED AILERON, AILERON TRIM TENSIONS. ALSO RT AILERON TAB WAS ADJUSTESDR T17A201210240001Aileron Sys · seizedABOUT 10 MILES OUT, FLAPS WERE EXTENDED TO 25, AILERONS FELT "HEAVY AND STIFF". WHEN THE FLAPS WENT TO 45 AT AROUND 1200AGL, FELT THE AILERONS LOCK UP IN CENTERED POSITION. COULD NOT MOVE THE AILERONS LEFT OR RIGHT. ATTEMPTED SOME QUICK SHARP FIRM "JABS" WSDR CALA2012101800681Pcu · leakingDURING CRUSE ENG 1 A HYD PUMP LOW PRESS LIGHT ILLUMINATED. FOLLOWED BY GRADUAL DEPLETION OF SYS A HYD. FLUID LEVEL, FOLLOWED B Y ELECT HYD A PUMP, PUMP LOW PRESSURE LIGHT. FOUND A SYS LOWER AILERON PCU LEAKING REMOVED & REPLACED SYS A AILERON PCU IN REF TO ASDR SWIA201232001Control Panel · failedJUST PRIOR TO 80KTS GOT T/O CAUTION WARNING WITH AILERON AND RUDDER TRIM WARNING MESSAGES. (FLT 5774) RESET CIRCUIT BREAKER 1L7. REPLACED AILERON RUDDER CONTROL PANEL IN REFERENCE TO AMM.SDR CA121017008Bearing · failed(CAN) AILERONS DIFFICULT TO MOVE IN FLIGHT. FOUND BEARING FAILED.SDR SIMA20121003008Fitting · scoredDURING MAINTENANCE INSPECTION FOUND THE RIGHT OVER AILERON BRACKET TO PCA HAS SCORING ON INSIDE DIAMETER TO WHICH HAT BUSHING IS INSTALLED INTO. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT AILERON PCA FITTING IAW EO EM-27MR-112. THE AISDR UALA2012100405632Actuator · failed"AIL LOCK" LT ON AT HIGH SPEED. EICAS MSG "AILERON LOCKOUT" DISPLAYED. OUTBOARD AILERONS INDICATED MOVEMENT - UNLOCKED, BOTH. CREW COMMENTS: 290 KNOTS AT 13,000FT,TEMP -8, THE RT SAM HAD AN ADC AND A LT AILERON LOCKOUT ACTUATOR FAULTBALL. BOTH DID RESET. SDR IPXA12M75578Aileron Sys · malfunctionedDURING CLIMB AT FLAP RETRATION LEVEL 1 AILERON DEFLECT INOP FOLLOWED BY LVL 2 AILERON DEFLECT DISAGREE. ACFT HAD UNCOMMANDED ROLL TO LEFT. RAN QRH CHECKLIST. NO RESOLUTION. DECLARED EMERGENCY, DIVERTED. ACCOMPLISHED FIM TROUBLESHOOTING 27-10-05, BLOCK 16SDR IPXA2M75578Warning Message · activatedDURING CLIMB AT FLAP RETRACTION LEVEL 1 AILERON DEFLECT INOPERATIVE FOLLOWED BY LEVEL 2 AILERON DEFLECT DISAGREE. ACFT HAD UNCOMMANDED ROLL TO LEFT. RAN QRH CHECKLIST. NO RESOLUTION. DECLARED EMERGENCY, DIVERTED. OPEN.SDR UALA2012092405419Pcu · faultyFLAPERON ACTUATOR STATUS MSG-REPEAT. REPLACE RIGHT INBOARD FLAPERON PCU PER AMM. SYSTEM OPS CHECK NORMAL.SDR UALA2012092405418Unknown · malfunctionedFLAPERON ACT STATUS: MSG 27-10302 ACTIVE & LATCHED. ACP'D FIM 27-11 TASK 816 STEP C. FOUND WIRE CHECKS GOOD. REF STEP C.(3), REPLACED ACE-L2 (M2712 2) PER MM27-02-02. LRU REPLACEMENT TEST CHECKS OK BUT FLAPERON POSITION SYSTEM TEST FAILS WITH MSG 27-16039,SDR UALA2012092105368Transmitter · faultyINBOARD AILERONS DO NOT EXTEND SYMMETRICALLY WHEN FLAPS ARE LOWERED; RT SIDE DROPS LOWER. FOLLOWED FIM 27-18-00 FIG 106 FOR INDICATOR FAILS TO RETURN TO ZERO WITH CONTROL WHEEL ZERO. FOLLOW "NO" ON DIAGRAM AND NEXT STEP STATES TO EXAMINE AILERON CABLE SYSTEM.SDR UALA2012092105353Actuator · faultyAILERON LOCKOUT. REPLACED RIGHT OUTBOARD AILERON LOCKOUT ACTUATOR PER MM AND RE-RACKED LEFT STAB TRIM RR MODULE. TEST OK PER MM 27-11-00, EICAS MSG CLEARED. REPLACE RIGHT OUTBOARD AILERON LOCKOUT ACT PER MM 27-11-16.SDR S9BA201209190002Bearing · failedLIMITED AILERON CONTROL AFTER TAKEOFF. R & R LT OTBD LOWER PULLEY RIGGED AILERON AND REMOVER RIGGING PIN IAW MM 27-00. BEARING ON PULLEY FAILED, PULLEY CAME OFF MOUNTING BRACKET.SDR SIMA20120912001Control Cable · out of adjustON FLIGHT 3737 THE CREW REPORTED THAT ON ARRIVAL, AILERON YOKE ON THE FIRST OFFICER’S SIDE FELT VERY HEAVY, AND OR BINDING. THE FIRST OFFICER FELT RATCHETING IN BOTH LEFT AND RIGHT ROLL. THIS PROBLEM ALSO WAS ACCOMPANIED WITH EICAS CAUTION MSG "AP TRIM IS LWSDR HALA2012090900204Warning Light · false activationDURING CLIMB OUT AND DESCENT EICAS MESSAGE "AILERON LOCKOUT. "ACCOMPLISHED FIM 27-11 FAULT TREE. NO DEFECTS NOTED. OK FOR SERVICE.SDR HALA2012090700203Warning Message · illuminatedDURING CLIMB AT APPROX 290 KTS RECEIVED AN AILERON LOCKOUT EICAS AND AILERON LOCK LIGHT. AFTER 10 MINS MESSAGE CLEARED. OPS NORMAL. PERFORMED FIM PROCEDURE 27-11 FAULT TREE 804 -NO FAULTS FOUND. ACFT OK FOR CONTINUED SERVICE.SDR UALA2012082704766Actuator · faultyAT 15000 270KTS TAKES 6 DEG LEFT RUDDER TO HOLD 2 DEG RT BANK RT INBD AILERON SHOWS UP. FOUND RT INBD CTR SYSTEM ACT INTERMITTENTLY BEING ABLE TO BE MOVED BY HAND THEN HYDRAULICALLY POWERED BACK TO NEUTRAL. VISUAL CONFIRM RT INBD AILERON FLOATING UP APPX 15 DSDR UALA2012082704773Actuator · faultyREMOVE RIGHT INBOARD AILERON ACTUATOR FOR LOG 2 AND LOG 3 RIGHT AILERON FLOATING. REMOVED ACTUATOR PER AMM 27-11-48 STEP1 THROUGH 2F7. P/N 282800.1009 S/N 2121.SDR REXA2012082401291Circuit Breaker · trippedAILERON TRIM DOESN'T WORK. FOUND AILERON TRIM CIRCUIT BREAKER TRIPPED FROM OVERNIGHT MAINTENANCE. CYCLED CIRCUIT BREAKER AND PERFORMED OPC ISA AMM 24-11-00. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.SDR UALA2012082404745Pcu · faultyFLAPERON MAINTENANCE MSG. REMOVED & REPLACED RIGHT INBOARD FLAPERON PCU PER AMM. COMPLETED UP TO AND INCLUDING STEP G3C PG 416. RESET ACE L2, PASSES LRU TEST BUT NOT FLAPERON POSITION TEST, RPL ACE L2, ACP LRU TEST-PASSED LRU TEST BUT FLAPERON STILL FAILS PSDR NX4R2012082000034Control Cable · frayedDURING A ROUTINE INSPECTION, THE AILERON PRIMARY CABLE WAS FOUND WORN AND FRAYED AT FS 65.33.SDR NX4R201208200033Control Cable · frayedDURING A ROUTINE INSPECTION, THE LT AILERON "DIRECT" CABLE WAS FOUND WORN WITH BROKEN STRANDS.SDR CA120820002Cable · frayed(CAN) DURING SCHEDULED INSPECTION OF THE EXPOSED AILERON CONTROL CABLES ALONG THE WING REAR SPAR TASK 000-27-900-705, A FRAYED CABLE WAS FOUND ON THE LT WING JUST OTBD OF BS YW-191.200. THE DAMAGE WAS FOUND TO BE BEYOND WEAR LIMITS. THE CABLE IS A .1250 DIAMSDR CA120821006Chain · faulted(CAN) THE AILERON SYS OF THE ACFT TEMPORARILY JAMMED IN FLIGHT. THE SYS WAS TROUBLESHOT AND THE JAM APPEARED TO BE IN THE COPILOT CONTROL WHEEL. AT FIRST IT WAS THOUGHT TO BE FAULTY BEARINGS SO THEY WERE REPLACED AND RE SHIMMED AS IAW THE MM. BUT FURTHER INVESDR USAA2012082000026Control Servo · faultyIN CRUISE, AILERON SERVO FAULT/ ELAC 1 PITCH FAULT AND AIRCRAFT ROLLED 5 DEGREES RIGHT PLUS SLIGHT PITCH UP. FLIGHT CONTROL SHOWS RIGHT AILERON GREEN SYSTEM IN AMBER. REMOVED AND REPLACED RIGHT GREEN AILERON SERVO CONTROL ACTUATOR PER AMM 27-14-51-400-001-A.SDR 9JLA2012101804510Actuator · failedTHE CREW REPORTED THE AILERON TRIM FREEZES UP IN FLIGHT. TROUBLESHOOTING SUSPECTED MOISTURE IN THE AILERON TRIM ACTUATOR. THE AILERON TRIM ACTUATOR WAS DISASSEMBLED CLEANED AND REGREASED, THE ACTUATOR WAS ASSEMBLED AND OPS CHECKS WERE SATISFACTORY IAW THE MM 2SDR CA120808002Rod End · sheared(CAN) DURING WALK AROUND, MAINTENANCE CREW FOUND AN EVIDENCE OF HYDRAULIC LEAK COMING FROM RT INBD AILERON POWER CONTROL PACKAGE. FURTHER INVESTIGATION SHOWN THAT THE HYDRAULIC WAS COMING FROM THE ACTUATOR. MAINTENANCE CREW DECIDED TO REMOVED THE DEFECTIVE PSDR CA120803006Pulley · seized(CAN) AILERON CONTROL PULLEY LOCATED AT LOWER RT CENTER WING, BS YW42.00, FOUND SEIZED DURING INSPECTION. REPLACED WITH NEW PULLEY.SDR UALA2012080204143Controller · oscillatesABNORMAL OSCILLATION IN AIRFRAME NOTED DURING CLIMB-OUT. FLIGHT DIVERTED. REPLACED AILERON SERVO CONTROL.SDR REXA2012073101209Unknown · unknownCREW REPORTED AILERONS FELT SLOPPY, OVER 1 INCH OF LATERAL PLAY AT YOKE. PERFORMED OPS TEST OF AILERON CONTROL SYSTEM NO DEFECTS NOTED. CREW REPORTED SLOP WITH TRIM OUT OF CENTER DETENT, NO DEFECTS NOTED IAW AMM 27-11-00-710-803.SDR CA120731003Control Cable · frayed(CAN) AFTER A SCHEDULED INSPECTION, 2 PRIMARY AILERON CABLES WERE FOUND FRAYED OUT OF LIMIT. INVESTIGATION ON THE REMAINING OF THE FLEET WAS DONE AND THE SAME PROBLEM WAS FOUND ON THE ACFT. LT, 82742407-001 AND RT 82742409-001, PRIMARY AILERON CABLES HAD TO BESDR CA120731002Control Cable · frayed(CAN) AFTER A SCHEDULED INSPECTION, TWO PRIMARY AILERON CABLES WERE FOUND FRAYED OUT OF LIMIT. INVESTIGATION ON THE REMAINING OF THE FLEET WAS DONE AND THE SAME PROBLEM WAS FOUND ON THE ACFT. LT 82742407-001 AND RT 82742409-001, PRIMARY AILERON CABLES HAD TO SDR CA120730001Control Cable · frayed(CAN) WHEN DOING A SCHEDULED INSPECTION, 2 AILERON CONTROL CABLES WERE FOUND FRAYED OUT OF LIMIT ON 1 ACFT. INSPECTION IS CURRENTLY BEING DONE ON THE REMAINING OF THE FLEET, AND 2 OTHER ACFT SO FAR WERE IDENTIFIED WITH OUT OF LIMIT FRAYED CABLES.SDR DALA12004056303Control Cable · damagedDURING WALKAROUND INSPECTION, FOUND THE LEFT OUTBOARD AILERON SURFACE STICKS AT UPWARD (SMALL AMOUNT). MAINTENANCE PERFORMED OPS CHECKS FOR AILERONS, FOUND INBOARD AND OUTBOARD AILERONS SURFACE WON'T MOVE, NO STATUS AND CMC MESSAGES FOUND PER AMM 27-11. PERFSDR UALA2012072303995Computer · malfunctionedAILERON SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS: F-CTL AIL SERVO FAULT SAMC TEXT: CFDS FAULTING ELAC2. IF DF WILL NEED TO SWAP WITH ELAC 1 TO DF ELAC1. REMOVED AND REPLACED ELAC PER AMM.SDR REXA2012071801169Unknown · unknownAILERON TRIM DOESN'T APPEAR TO BE WORKING. TRIM IS HARD TO CENTER. FULL DEFLECTION ON TRIM DOESN'T MOVE YOKES OR CONTROL SURFACES. PERFORMED OPERATIONAL TEST OF AILERON TRIM SYSTEM IAW AMM 27-11-00. ALL CHECKED GOOD.SDR 2012FA0000515Shutoff Valve · failedWHILE PERFORMING THE AILERON HARDOVER PREVENTION SYSTEM OPERATIONAL CHECK (HOPS), LEFT AILERON HYDRAULIC S/O (PILOT-C4) CIRCUIT BREAKER WOULD POP AND HYDRAULIC PRESSURE WAS NOT REMOVED FROM THE AILERON ACTUATOR. SHUTOFF VALVE WAS FOUND ELECTRICALLY SHORTED. SDR EBTR20120712006Control Cable · brokenON APPROACH PILOT SELECTED FULL FLAPS, HEARD LOUD POP AIRCRAFT WANTED TO ROLL RIGHT. CORRECTED WITH AILERON, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENCE. INSPECTED AIRCRAFT FOUND THAT A FLOOR PANEL CLIP NUT HAD BECOME CAUGHT IN FLAP DRIVE GEAR/CHAIN CAUSSDR UALA2012070903654Actuator · failedAIRFRAME VIBRATION, RTFL. WORSE IN AFT PART OF AIRCRAFT. BOTH LEFT AILERON ACTUATORS REPLACED.SDR REXA2012070601051Pcu · out of adjustRIGHT AILERON OUT OF CENTER BY APPROXIMATELY 1/2 INCH FROM WING AND TRAILING EDGE OF OUTBOARD FLAP. RIGGED RIGHT INBOARD AND OUTBOARD AILERON PCU'S PER AMM 27-11-00. OPS CHECKED NORMAL, AIRCRAFT OK FOR SERVICE.SDR YENA20120702549Computer · failedFLT 221 DCA-MCO, AT 190KTS FLAPS 1 WITH HALF SPEED BRAKES ON AUTOPILOT FLAPS 2 SELECTED A/C ROLLED 15 DEGREES BANK LEFT FOR 3 SECONDS THEN CORRECTED WHEN SPEED BRAKES RETRACTED. A/C AGAIN ROLLED LEFT 1 MINUTE LATER WITH NO CHANGES TO CONFIG AUTO PILOT DISCONNSDR USAA2012070200023Mechanism · faultyEN ROUTE FROM EWR TO CLT, CREW REPORTED WHEN MOVING AILERON TO THE LEFT, THERE SEEMS TO BE A "CATCH" AT ABOUT 4 UNITS ON THE AILERON TRIM INDICATOR. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AILERON ARTIFICIAL CENTERING ANDSDR UALA2012062903444Computer · faultedCREW REPORTS ACFT REQUIRED SIGNIFICANT AILERON TRIM INPUT, FOUND LEFT FLAPERON DRIFTING UP. REACHED POINT TO AFFECT ACFT STABILITY AND SNAPPED BACK DOWN. ON GROUND HAD LEFT PFC LANE FAULT AND ACE L2 FAILED GROUND TEST. REPLACED LEFT PFC AS PER AMM, ALL TEST SDR HNAA2012062200834Aileron · out of adjustCONTROL COLUMN IS 10-15 DEGREES RT OF CENTER ON TAKEOFF. LARGE CONTROL INPUTS REQUIRED AT 150 TO MAINTAIN LEVEL FLIGHT. ADJUSTED LT AILERON IAW MM 27-13-00. ACFT RELEASED FOR EVALUATION FLIGHT.SDR SIMA20120620012Feel Unit · malfunctionedON FLIGHT 9801 THE CREW REPORTED THE FLIGHT CONTROL COLUMN HAD A "BINDING" FEEL DURING TURNS WHEN HAND FLYING. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FEEL UNIT QUADRANT IAW CRJ-700 AMM 27-SDR CA120615001Pulley · seized(CAN) DURING HEAVY MAINTENANCE INSPECTION A DEFECT WAS RECORDED THAT THE AILERON PULLEYS, 2 IN THE AFT RT CENTER WING WOULD NOT ROTATE THROUGH FULL RANGE AND THAT BEARINGS WERE ROUGH, IPC 27-12-00, FIG 30, ITEM 450. PULLEYS REPLACED IAW AMM. AF TSN: 54670, CSNSDR CA120614005Pulley · seized(CAN) ROLL CONTROL WAS VERY STIFF AT ALL SPEEDS IN FLIGHT. DURING TROUBLESHOOTING, THE RT SIDE MOST OTBD AILERON PULLEY ASSEMBLIES WERE FOUND TO BE SEIZED. BOTH PULLEY ASSEMBLIES WERE REPLACED WITH SERVICEABLE UNITS. FRICTION TEST WAS CARRIED OUT.SDR 2012FA0000423Control Cable · wornLT AILERON CROSSOVER AND AILERON DIRECT CABLE AT WS 71.125 ARE WORN AND FRAYING AFTER MAKING CONTACT WITH THE RIB ANTI-RUB BLOCK. AILERON CONTROL CABLE TENSION WAS MEASURED AND FOUND TO BE WITHIN LIMITS.
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