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 CALA2017080802511Mount · brokenFLT CONTROL YOKE LOCKED IN FULL LEFT POSITION DURING CHECK, NO RETURN TO CENTER. LATERAL TRIM CONTROL ACTUATOR MOUNTING BOSS ON AIRFRAME BROKEN OFF CAUSING THE LATERAL FEEL, CENTERING AND TRIM MECHANISM DRUM ASSEMBLY TO BIND. THE LATERAL CONTROL SUPPORT BOX CSDR SOKF20170721007Warning Message · illuminatedDURING FLIGHT, THE AIRCRAFT RETURN TO DEPARTURE DUE TO AN ECAM WARNING MESSAGE FOR FLT CONTROL LT AILERON FAULT. INCLUDED IN THE MEL 27-14-01. THE AIRCRAFT RETURNED TO NORMAL OPERATION.SDR DBCA2017062300001Proximity Switch · failedNO TAKEOFF CAS MESSAGE - ROLL SYSTEM CAS IN NO TAKEOFF PAGE NOTED WHILE TAXIING. CREW RETURNED TO HOME BASE. REMOVED AND REPLACED AILERON RATIO ACTUATOR PROXIMITY SWITCH. OPERATIONS CHECKED GOOD.SDR QXEA2016062300430Control Cable · looseON GROUND, YOKE CANTED 10-15 DEG TO THE RIGHT. IN FLIGHT DURING CLIMBOUT REQUIRES 10-15 DEG RT WING DOWN (YOKE) AND SUBSTANTIAL RIGHT RUDDER TRIM / RIGHT AILERON TRIM TO MAINTAIN WINGS LEVEL FLIGHT. LANDING UNEVENTFUL. AIRCRAFT REMOVED FROM SERVICE. PERFORMEDSDR HALA2017062300164Warning Light · false activationAILERON LOCKOUT ILLUMINATED MOMENTARILY DURING CLIMB OUT, AT 290 KTS TO 300 KTS AT 4000 FT. PERFORMED FIM 27-11 FAULT TREE 804, NO FAULTS NOTED, SYSTEM OK OK FOR SERVICE.SDR FDEA201706201711Yoke · damagedLATERAL PLAY IN YOKE FOR AILERON INPUT.SDR JGVR20170614002Shaft · corrodedAILERON AFT SECTOR SHAFT ASSEMBLY HAS CORROSION. REMOVED AND REPLACED THE AILERON AFT SECTOR SHAFT IAW MM 27-10-03.SDR AALA20170531002Control Panel · failedTHE AIRCRAFT WAS GROUNDED. CREW REPORTS AFTER TAKEOFF CAPTAIN’S YOKE HAD VIBRATION AND GRINDING FEEL AT ALL TIMES. CMD A AUTOPILOT WOULD NOT ENGAGE. YOKE HAS SLOP TOO. NOTICED SLOP IN LEFT TURN ABOVE 1500" COPILOT FELT A LITTLE VIBRATION GRINDING IN HIS YOSDR 2017FA0000225Cable · wornFOUND LEFT AILERON LOWER WING CABLE RUBBING NEAR WS 273 FAIRLEAD. REPLACED THE LEFT AILERON LOWER WING CABLE IAW MM 27-10-00.SDR 2017FA0000224Cable · wornFOUND LEFT AILERON LOWER WING CABLE RUBBING NEAR WS 273 FAIRLEAD. REPLACED THE LEFT AILERON LOWER WING CABLE FROM OUTBOARD SECTOR TO TURNBUCKLE IAW MM 27-10-00.SDR HALA2017053000133Warning Message · false activationAILERON LOCKOUT EICAS MESSAGE ILLUMINATED FOR 30 SECONDS, THEN EXTINGUISHED. PERFORMED FIM TASK 27-11 FAULT TREE 804,NO DEFECTS NOTED, OK FOR SVC.SDR SAJF201705230001Rod End · crackedLATERAL CONTROL PROBLEM IN FLT. LOSS OF INBOARD AILERON (RIGHT) IN FLT IS SUSPECTED. GROUND CHECK FOUND RT I/B AILERON ACTUATOR ROD END CRACK. REPLACE ACTUATOR ON MAY 8, RETURN MAY 8, AFTERNOON.SDR A6WA201744985Aileron · malfunctionedDURING FINAL APPROACH WITH FLAPS SET AT 45 DEG AND GEAR DOWN WITH AP OFF FO REPORTED AN AILERON JAM AT ABOUT 2500 FT AGL. AILERONS WOULD NOT MOVE TO THE LEFT. FO MADE A 2ND ATTEMPT AND OVERCAME THE RESTRICTION TO MOVEMENT. LANDED WITHOUT INCIDENT. AFTER LANDINSDR QXEA2017042400323Panel · out of positionAILERONS BINDING & HARD TO MOVE TO THE LEFT AND RIGHT. AFT F/A REPORTS GRINDING NOISE DURING YOKE MOVEMENT. FOUND GRINDING NOISE TO BE CABLE RUN UNDER PANEL 245DZ, CUTTING INTO PANEL'S AFT MIDDLE AREA, REPOSITIONED PANEL, NOW NO GRINDING NOISE HEARD WHILE MOVISDR HALA2017041400097Aileron · malfunctionedDURING CHECK FLIGHT, FOUND LEFT INBD AILERON DOES NOT DROOP CORRECTLY WITH FLAPS DEPLOYED.SDR IPXA2017041416130Warning Message · activatedLEVEL 2 ALERT. AILERON DEFLECT DISAGREE. DIVERTED.SDR HALA2017033000091Warning Message · false activationOUTBOARD AILERON LOCKOUT EICAS MESSAGE DISPLAYED MOMENTARILY AT 285KTS, NO AILERON MOVEMENT OBSERVED. UNABLE TO DUPLICATE. NO EICAS MESSAGE NOTED ON ARRIVAL. PERFORMED AILERON POSITION INDICATING SYSTEM TEST IAW AMM 27-18-00 & 501, NO ISSUES.SDR HALA2017032600081Warning Message · illuminatedAILERON LOCKOUT ADVISORY EICAS MESSAGE DISPLAYED & LOCK AMBER OVERHEAD LIGHT ILLUMINATED WHILE CLIMBING THRU FL 220 & REMAINED ON FOR DURATION OF THE FLT. TROUBLESHOT IAW FIM 27-11, FAULT TREE 804, R SAM BOX HAD FAULT RT AILERON LOCK OUT. RESET IAW FIM. NO FASDR HALA2017032600079Module · malfunctionedETOPS SIGNIFICANT SYSTEM, AILERON LOCKOUT EICAS CAME ON DURING DESCENT ABOVE 270 KTS. PERFORMED FIM TASK 27-11 FAULT TREE 804. FOUND FCC FAULT TO BE PRESENT ON SAM LEFT HAND SIDE. NEED TO REPLACE LEFT SAM. REMOVED AND REPLACED STABILIZER TRIM AND AILERON LOCKOSDR DALA2017032802473Control Cable · out of adjustAILERONS AND ELEVATOR STIFF-DIFFICULT TO MOVE IN FLIGHT. FOUND AILERON CABLES 7&8 TENSION OUT OF LIMITS (TOO LOW) ADJUSTED CABLES IN REF TO AILERON CABLES 7&8 TENSION ADJUSTMENTS & SAFETIES PER AMM 27-10. LUBED LATERAL CONTROL MIXER IN REF TO AIM 12-21. FOUND SDR FDEA201703150918Transducer · out of adjustYOKE BECAME LOCKED IN POSITION DURING PRE TAKEOFF FLIGHT CONTROL CHECK. ADJUSTED PLATE ON CENTRAL WHEEL FORCE TRANSDUCER IAW MM 27-11-08-4-0. AILERON AND FLAPERON CONTROL SYSTEM TEST PERFORMED IAW MM 27-11-00-5-0. TEST PASSED.SDR YENA201703100182Bearing · dirtyAFTER TAKEOFF, IT WAS NOTICED THAT THE FLIGHT CONTROLS IN THE ROLL MODE WERE STICKING. THE AIRCRAFT WAS HAND FLOWN. THE STICKING OF THE CONTROLS GOT WORSE THE HIGHER THE AIRCRAFT WENT. AUTO PILOT WORKED WELL. NO NOTICE OF ONLY ISSUES OF FL280 OF 290 - 310 KTSSDR T17A201702158017Bushing · missingDURING DECENT AT 29000 FT AND 290 KTS, PILOT EXPERIENCED A VIOLENT SHAKE IN THE YOKE. SLOWED TO 250 KTS AND SHAKE WENT AWAY. MAINTENANCE FOUND THE LEFT AILERON CENTER MOUNT UPPER BUSHING MISSING.SDR QXEA2017021300052Aileron · icedAFTER ENGINE START, RELEASED THE CONTROL LOCK AND PERFORMED A CONTROL CHECK IAW NORMAL PROCEDURES, DISCOVERED A ROLL CONTROL BIND. PULLED THE ROLL DISCONNECT AND DISCOVERED THE CAPTAIN'S CONTROLS ARE FREE BUT THE FO'S CONTROLS ARE STILL BINDING. ON ARRIVASDR 8LFA2016020601Bearing · contaminatedDURING CLIMB, PILOT NOTICED BINDING IN AILERON CONTROLS. RETURNED TO DEPARTING AIRPORT. UPON INSPECTION FOUND RT AILERON BELL CRANK BEARING WAS FULL OF WATER. SUSPECTED WATER FROZE AT ALTITUDE AND CAUSED BINDING.SDR QXEA2017010800044Aileron · out of rigAIRCRAFT ROLLS TO THE LEFT WITH CONTROL YOKES NEUTRAL FUEL WAS BALANCED AND TRIM NEUTRAL THIS OCCURRED WITH AP ON AND OFF. LANDING UNEVENTFUL. RIGGED AILERON SYSTEM IAW AMM 27-10-00-830-805. RETURNED TO SERVICE.SDR A6WA2017020744784Aileron · bindingAILERON CONTROL BINDING AND CLICKING DURING FLIGHT CONTROL CHECK, ON FO'S SIDE, NO BINDING FELT ON CAPT SIDESDR AWKA20170202Pcu · malfunctionedAFTER APPROXIMATELY 4.5 HOURS INTO CRUISE FLIGHT, THE FLIGHT CREW RECEIVED A “RE-TRIM R WING LOW” AMBER CAS MESSAGE. CREW TRANSFERRED FUEL TO THE LEFT WING AND MADE MINOR ADJUSTMENTS TO THE AILERON AND RUDDER TRIM; THE CAS MESSAGE EXTINGUISHED. DURING DESCENT,SDR FJTA17012201Bellcrank · lack of lubeAIRCRAFT DEPARTED AND CREW DETERMINED THAT TURNS TO THE RIGHT PRODUCE A STIFF CONTROL YOKE. RETURNED AND LANDED WITH NO FURTHER ISSUES. MAINTENANCE VERIFIED THE DISCREPANCY. MAINTENANCE LUBRICATED AILERON CENTERING MECHANISM BELLCRANK HARDWARE, ROLLER LEVERSDR DALA2017011300305Cam · contaminatedAILERONS BINDING DURING FLIGHT CONTROL CHECK. FOUND SAND AND DEBRIS STUCK TO CAM FOLLOWER PLAT ON TOP OF MIXER. CLEANED. OPERATION CHECKS GOOD. (LP# 9461644)SDR FDEA201701050830Actuator · faultyON DEPARTURE TRIED TO ENGAGE AUTOPILOT, COULD NOT GET AUTO PILOT NR 1 TO ENGAGE. RETURNED. PERFORMED FCC-1 AFS R-T-S TEST. TEST FAIL AT AILERON SYSTEM, PER FIM 22-12-17 CHECKED FROM FCC-1 RECEPTACLE FOUND RAM LVDT B-6G & B-6H OPEN CIRCUIT NO READING. ON FCCSDR T6FA201701037044Seal · frozenFLEW TO KLUK ABOUT 0700. A/C SAT ON THE RAMP UNTIL ABOUT 1530, ABOUT WHICH TIME WE DEPARTED FOR KGRR. APPROX 10 MINUTES INTO OUR FLIGHT APPROACHING FL250 WITH A CLEARANCE TO CLIMB HIGHER. ABOUT THIS TIME AND ALTITUDE, WE RECEIVED AN AMBER AP AIL MISTRIM EICSDR ECQ2017F00000Bellcrank · mismanufacturedDURING A 100 HR INSPECTION, THE LT AILERON HAD EXCESSIVE UP AND DOWN MOVEMENT. FURTHER INSPECTION LED TO IN BOARD BELLCRANK BEARING. WHEN THE BELLCRANK WAS REMOVED IT WAS NOTICED THAT AT SOME POINT BELLCRANK HAD BEEN WELDED. DURING NORMAL INSPECTION THIS ARSDR VNAA2016112200031Control Panel · failedAILERON TRIM INOPERATIVE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED AILERON/RUDDER CONTROL PANEL IAW AMM. OPS CHECKED GOOD, THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR EBVR20161102001Control Cable · brokenBROKEN STRANDS ON AILERON AFT CABLES (RT AND LT) AT APPROXIMATE WS 533. CABLE STRANDS CONSISTENTLY FOUND BROKEN ON MULTIPLE AIRCRAFT OF SAME MODEL AND WITH APPROXIMATELY THE SAME HOURS AND CYCLES. THE BROKEN STRANDS ARE FOUND ON THE AFT CABLE (BOTH LH AND RHSDR IPXA2016102109681Actuator · inoperativeRECEIVED A LEVEL 2 AILERON DEFLECT DISAGREE. RAN CHECKLIST, NO HELP. REPLACED THE RT WING AILERON DEFLECTION ACTUATOR IAW AMM 27-16-01-401 REV 86.02. OPS TESTED IAW AMM 27-16-00-700-801 REV 86.02. TESTED GOOD. OSDR VNAA2016091800023Control System · stiffAILERONS ARE HARD TO MOVE, FEEL INDENTS. MECHANICS TROUBLESHOT LEFT AND RIGHT HAND FORWARD FUEL QUADRANTS, NO DEFECTS NOTED. INSPECTED RIGHT HAND REAR FUEL QUADREANT AND FOUND BUSHING OUT OF ROUND AT APPROX 45 DEGREES FULL RIGHT AILERON MOVEMENT. TECHNICIANSSDR HALA2016091300349Actuator · malfunctionedAILERON LOCKOUT DURING CLIMB ON EICAS. FOUND RT AILERON LOCK FAULT BALL ON LEFT SAM. REPLACED THE LEFT SAM IAW AMM 27-09-00. PERFORMED SAM TEST PER B767 AMM 27-09-00. CHECKED GOOD.SDR HALA2016091200348Actuator · warning messageRT WING LOCKOUT ACTUATOR AILERON HAD A MESSAGE INFLIGHT. REMOVED AND REPLACED RT WING AILERON LOCKOUT ACTUATOR. FUNCTIONAL TESTED GOOD IAW AMM 27-11-44.SDR UIEA2016091000756Aileron · oscillatesMULTIPLE ITEMS: AILERON OSCILLATED UNCONTROLLABLY WITH AUTOPILOT ENGAGED IN FLIGHT. EFIS DISPLAY BLACKED OUT INTERMITTENTLY WHILE IN HOLDING WITH AUTOPILOT ON AND AILERONS WOULD JERK LT THEN RT UNCOMMANDED. GLARE SHIELD LIGHTS FLICKERED ALSO. TCAS RA COMMANSDR IPXA2016091208177Skin · gougedINSPECTION TYPE: PR/H, INBD AILERON HAS NUMEROUS DEEP GOUGES ON L/E SKIN. REMOVED AND REPLACED THE AILERON IAW AMM 27-11-01-004-001 AND 27-11-01-404-008.SDR IPXA2016091208176Skin · gougedINSPECTION TYPE: PL/H, INBD AILERON HAS NUMEROUS DEEP GOUGES ON L/E SKIN. REMOVED AND REPLACED THE LT AILERON IAW AMM 27-11-01-004-001 AND 27-11-01-404-008.SDR HALA2016090200340Warning System · false activationETOPS SIGNIFICANT SYS, ACCELERATING THROUGH AT 270 KTS AILERON LOCKOUT MESSAGE ON EICAS. MESSAGE EXTINGUISHED AT 1 MINUTE LATER REVIEWED ORH PROCEDURE. PERFORMED BITE AND RESET ON AILERON LOCKOUT UNITS IAW FIM 27-11, FAULT TREE 804, OK FOR SERVICE.SDR SIMA20160827001Grommet · detachedAFTER TAKEOFF WHILE HAND FLYING, THE TURN TO THE RIGHT FELT A BIT LOOSE IN THE YOKE. WHEN RETURNING TO CENTER THERE WAS A DISTINCT CLUNK FEELING. THIS WAS CONSISTENTLY FELT BY BOTH PILOTS. ON THE PREVIOUS FLIGHT THE AILERON BOX WAS DISPLAYED AND THE RT WINSDR HALA2016082200332Aileron Sys · malfunctionedAILERON LOCKOUT DISPLAYED UNDER 270 KNOTS ON DESCENT. PERFORMED FIM 27-11 FAULT TREE 804. DID STEP 1,21,23, AND 55 SYSTEM OK. NO 30 DAYS HISTORY.SDR HALA2016082200331Aileron Sys · malfunctionedAILERON LOCKOUT MESSAGE CAME ON AT 12,000FT AND 250KTS. EXTINGUISHED ON GROUND. PERFORMED FIM 27-11 TREE 804. NO FAULTS NOTED. OK FOR SERVICE.SDR AALA201608059013O-Ring · leakingFLIGHT CREW REPORTED LOSS OF YELLOW HYDRAULIC SYSTEM FLUID AFTER RECIEVING ECAM MESSAGES FOR HYDRAULIC YELLOW RESERVOIR LOW LEVEL, HYDRAULIC ENGINE 2 PUMP LOW PRESSURE AND HYDRAULIC YELLOW SYSTEM LOW PRESSURE APROXIMATELY 250 MILES FROM CLT. THE FLIGHT CREW COSDR HALA2016072100292Warning Message · false activationAILERON LOCKOUT ON EICAS, DURING DESCENT THROUGH 10000 FT AT 240 KTS. EXTINGUISHED ABOUT 2 MINUTES LATER. ACCOMPLISHED FIM 27-11 TREE 804. NO FAULTS. OPS CHECKED OK.SDR HALA201607210291Warning System · false activationETOPS SIGNIFICANT SYSTEM, AILERON LOCKOUT ON EICAS ON DESCENT THROUGH 10,000 FT AT 240 KTS EXTINGUISHED ABOUT 2 MIN LATER. ACCOMPLISHED FIM 27-11 TREE 804 NO FAULTS, OPS CK OK. OK TO CONTINUE.SDR VNAA2016070200003Pcu · faultyON APPROACH, AILERONS REQUIRED EXCESSIVE ROLL. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT AILERON NR 1 POWER CONTROL UNIT AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED
Back to JASC 2710