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.

SDR DXTA2009032303560Bolt · wornWHILE TURNING THE YOKE TO THE RIGHT, THE CONTROLS "BIND" UP AROUND HALF DEFLECTION. REMOVED AND REPLACED CORRODED SPOILER INBD AND OTBD BUNGEES. REMOVED AND REPLACED SPOILER MIXER INPUT PULLEY SPRING TENSIONER IAW MFG DWG 6760260 MADE REQUIRED ADJUSTMENT. REMMar 11, 2009 · N943QS · Cessna 750SDR IPXA09M54970Actuator · inoperativeINSPECTION TYPE:N/A AIR TURNBACK. AIL DEF DISAGREE DISPLAYED. RIGHT AIL DEF REQUIRED TO MAINTAIN LEVEL FLIGHT. REMOVED AND REPLACED RT INBOARD AILERON DROOP ACTUATOR IAW MM 27-16-00-05, OPS CHECK NORMAL P/N ON ARH7054-517, S/N J0570, P/N OFF 4083935-901, S/Mar 9, 2009 · N288UP · Doug MD11FSDR CVGA20090228001Seal · frozenDURING CLIMB WITH AUTOPILOT ENGAGED PASSING FL340 THE PFD INDICATED AN AILERON MISTRIM ANNUNCIATION. AFTER DISCONNECTING THE A/P, THE CREW NOTED THAT THE AILERONS FELT STIFF. THE CREW STOPPED THE CLIMB AT FL350, RAN THE APPROPRIATE CHECKLISTS, AND DECLARED AFeb 28, 2009 · N95AG · Lear 60LEARSDR UALA2009031000653Actuator · out of rigA/C FLIES WITH LT WING DOWN, WITH 1.5 UNITS LT RUDDER TRIM REQUIRED. WHILE TROUBLESHOOTNG FOUND RT OUTBOARD B AIL ACTUATOR BUSHINGS AND ROD ENDS OUT OF RIG. BOTH BLUE AND GREEN RT AIL SERVO ACT WERE REPLACED.Feb 25, 2009 · N404UA · Airbus A320232SDR UALA2009022500653Actuator · wornA/C FLIES WITH LT WING DOWN WITH 1.5 UNITS LT RUDDER TRIM REQUIRED. WHILE TROUBLESHOOTNG FOUND RT OTBOARD B AIL ACTUATOR BUSHINGS AND ROD ENDS. BOTH BLUE AND GREEN RT AIL SERVO ACT WERE REPLACED.Feb 25, 2009 · N404UA · Airbus A320232SDR ASOA200900242Unknown · activatedREFF AFDL 440826 ITEM 2 - RUDDER AND AILERON TRIM RUNAWAY ON CLIMBOUT. EMERGENCY DECLARED. A/C RETURNED TO ATL AFTER T/O. FLT 5418 DEL 131 MINS.Feb 25, 2009 · N885AS · Cndair CL6002B19SDR 2009FA0000227Guide · chafedDURING 100 HR INSP, FOUND LT AND RT AILERON CABLES WORN THROUGH SEVERAL STRANDS AT WING STA 71. THERE IS A CABLE RUB BLOCK INSTALLED ON THE RIB AT THIS STATION. IT IS CAUSING EXCESSIVE WEAR TO THE CABLES. REPLACED BOTH CABLES IN LT AND RT WINGS. P/N 051010Feb 20, 2009 · N21706 · Cessna 172SSDR HALA2009021800053Actuator · malfunctionedETOPS SIGNIFICANT SYSTEM FRM 27110200, EICAS MSG "AILERON LOCKOUT" DISPLAYED WITH "AILERON LOCK " DISCREET LIGHT CAME ON AT LOW SPEED APPROX 250 KTS THEN EXTINGUISHED AT APPROX 245KTS. REPLACED LEFT AILERON LOCKOUT ACTUATOR IAW B767 AMM 27-11-44 SYSTEM OK.Feb 18, 2009 · N592HA · Boeing 7673CBSDR CA090220002Control Tube · bent(CAN) ACFT, AFTER COMPLETING REF/A/B, MX NOTICED BOTH THE LT AND RT AILERON TORQUE TUBE ASSEMBLIES WERE BENT. CABLES FOUND LOOSE UPON ARRIVAL. ALL AILERON CABLES TIGHTENED ACCORDING TO REF/A/AND/B/AND. DUE TO CURVATURE OF TUBES, CABLES ARE NOW SITTING LOWFeb 17, 2009 · Emb ERJ190100LRSDR DL777090199Aileron Sys · malfunctionedRTB DUE ON TAXI OUT DURING FLT CONTROL TEST GOT FLT CONTROL MSG/C MAT FAULTED LEFT AILERON FAULT CODE 270-001-00 27-10222 RESET PER FIM TASK 27-41-00-810-814. 0 CURRENT MSGS.Feb 14, 2009 · N861DA · Boeing 777232SDR GLBA20090212ATurnbuckle · obstructedIN FLIGHT AILERON WOULD STICK AND POP LOOSE WHEN TURNING FLIGHT CONTROLS BOTH DIRECTIONS. MAINTENANCE INSPECTED AILERON SYSTEM IAW MM 27-10-02 . FOUND TURNBUCKLE RUBBING ON LIGHTNING HOLE ANTI-CHAFE PROTECTION. REPAIRED PROTECTION AS REQUIRED. MAINTENANCE CFeb 12, 2009 · N122UX · Beech 1900DSDR J4PA4438Trim Motor · shortedAT 1656 LOCAL DEPARTED FROM KCUB TO KIGX WITH 2 PAXS, CRUISE TO 5,000 FT. AUTOPILOT WAS PULLING TO RIGHT. AFTER RESETTING OF THE AP SMOKE WAS SEEN FROM THE RIGHT SIDE OF THE CENTER AVIONICS RACK. THE AUTOPILOT WAS DISCONNECTED AND THE SMOKE STOPPED. AFTER LFeb 11, 2009 · N509SR · Cirrus SR22SDR UALA2009020900429Pcu · faultyFLT CONTROL SYS CMC MSG AND LEFT OUTBOARD AILERON MSG -2710201. REPLACED THE LT OUTBOARD AILERON POWER CONTROL UNIT. INSPECTED FOR SAFETY, SECURITY AND CORRECT OPERATION.Feb 8, 2009 · N780UA · Boeing 777222SDR SWAA090885Pcu · leakingLOSS OF A-SYSTEM HYDRAULIC QUANTITY FOLLOWED BY LOSS OF A-SYSTEM HYDRAULICS (ENGINE AND ELECTRIC PUMPS TURNED OFF AT FIRST LOW PRESS LIGHT INDICATION 1/4 TANK QUANTITY). FOUND A-SYSTEM AILERON PCU LEAKING. REMOVED AND REPLACED PCU PER MM.Feb 6, 2009 · N376SW · Boeing 7373H4SDR CA090206001Control Cable · wornFOUND DURING AN INSPECTION THAT THE AILERON BALANCE CONTROL CABLE WAS WORN AT STATION 71.125.Feb 5, 2009 · Cessna 172SSDR SWAA090641Pcu · leakingDIVERSION, A-SYSTEM HYDRAULIC QUANTITY DROPPED TO 1/4. REMOVED AND REPLACED A-AILERON PCU PER MM.Jan 29, 2009 · N607SW · Boeing 7373H4SDR Z5FA011909N605CS1Control Wheel · bindsAFTER A MODERATE CROSS-WIND TAKEOFF FROM MYEF WITH 20 PERCENT LEFT AILERON APPLIED, THE CREW WAS UNABLE TO RETURN THE CONTROL WHEEL BACK TO A NEUTRAL POSITION. AFTER 2 TO 3 FORCEFUL CLOCKWISE MOVEMENT ATTEMPTS, THE CONTROL WHEEL BECAME FREE. WHEN THE AIRCRAFJan 19, 2009 · N605CS · Cessna 680SOVSDR Z5FA02009119001Control Column · unknownAFTER A MODERATE CROSS-WIND TAKEOFF WITH 20 PERCENT LT AILERON APPLIED, THE CREW WAS UNABLE TO RETURN THE CONTROL WHEEL BACK TO A NEUTRAL POSITION. AFTER 2 TO 3 FORCEFUL CLOCKWISE MOVEMENT ATTEMPTS, THE CONTROL WHEEL BECAME FREE. WHEN THE ACFT WAS AT 5000 FT Jan 19, 2009 · N605CS · Cessna 680SOVSDR UALA2009012000224Actuator · failedAILERON LOCKOUT LIGHT IS ON. REPLACED RT OUTBOARD AILERON LOCKOUT ACTUATOR.Jan 19, 2009 · N642UA · Boeing 767322SDR CA090119007Aileron · stuck(CAN) AS THE FLIGHT CREW COMPLETED THEIR FLIGHT CONTROL CHECK, DURING TAXI OUT FROM THE GATE, THE CREW DETERMINED THAT THE AILERONS WERE JAMMED. THE ACFT TAXIED BACK TO THE GATE FOR MX ACTION.Jan 16, 2009 · Emb ERJ170200SUSDR A6WA200940013Pcu · out of rigDURING FLT AN ABNORMAL AMOUNT OF LT AILERON TRIM WAS REQUIRED F/O WINGS LEVEL FLIGHT, FLT CTL POS IND, LT AILERON UP AND RT AILERON CTR. FOUND LT AILERON PCU OUT OF RIG. RIGGED LT AILERON PCU IAW AMM 27-11-00. OPS CHECK GOOD AT THIS TIME. (K)Jan 11, 2009 · N441ZW · Cndair CL6002B19SDR UALA2009011200128Pcu · failedFLIGHT CONTROL SYS ANY CONDITION OF THE FLIGHT CONTROL SYS OR IT'S SYS INTERFACES WHICH WOULD PREVENT DISPATCH. FLIGHT CONTROLS SYS BELOW MINIMUM DISPATCH REQUIREMENTS. STATUS MSG01- LATCHED CRUISE MODE DEPENDENT; FLAPERON PWR CONTROL UNIT (LT OTBD) DOES NOT FJan 11, 2009 · N221UA · Boeing 777222SDR CA090112012Control System · malfunctioned(CAN) AIRCRAFT AILERONS BINDING, MUST OVER CORRECT TO MOVE AILERONS, TO MUCH FORCE NEEDED. AILERON CONTROL SYSTEM ADJUSTMENT/TEST DONE IAW AMM 27-12-00. FUSELAGE AND WING CABLE TENSIONS FOUND TO BE HIGH, ADJUSTED AS PER FIG 201 SHEETS 344. 2. REPLACED RT AIJan 9, 2009 · Dhav DHC8102SDR HALA2009010700007Circuit Card · faultyETOPS SIGNIFICANT SYSTEM - EICAS AILERON LOCKOUT LIGHT ILLUMINATED @ 300KTS IND.3. R&R LT & RT YSM ON CUST CARD NR 39 AVIONICS 5001 AND PERFORMED FUNCTIONAL TEST OF AILERON LOCKOUT SYSTEM IAW MM 27-11-00-735-524. FUNCTIONAL TEST GOOD.Jan 7, 2009 · N587HA · Boeing 767300SDR 2009FA0000001Rod End · lack of lubeACFT HAD AN ISSUE WITH THE AILERON CONTROL ON A FLT IN THE PATTERN. THE AILERON CONTROL BECAME VERY STIFF DURING FLT ALTHOUGH ALL APPEARED NORMAL ON THE PREFLIGHT AND RUNUP . INSPECTED ACFT, FOUND THAT IT WAS VERY STIFF. FOUND THE ISSUE TO BE THE LT AILERON Jan 5, 2009 · N507BW · Quartz 11ESDR CA090112005Control Cable · out of rig(CAN) AILERON CONTROLS VERY STIFF (ARE LOCKING IN THE WINGS LEVEL POSITION). RECTIFICATION, AILERON CONTROL SYSTEM CABLES RIGGED IAW AMM 27-12-00-02. (TC NR 20090112005)Jan 3, 2009 · Dhav DHC8102SDR UALA2008123007048Actuator · leakingRT AILERON HAS EXCESSIVE FLUID RUNNING OUT OF IT. REPLACED RT INBD AILERON PCA. OPS AND LEAK CHKS GOOD.Dec 28, 2008 · N548UA · Boeing 757222SDR UALA2008122206946Actuator · faultyAILERON LOCKOUT EICAS AND OVERHEAD LIGHT CAME ON AROUND 300 KTS. CREW ADVISED BOTH O/B AILERONS APPEAR TO BE LOCKED OUT IN CRUISE. RT AIL LOCKOUT MODULE FAULT BALL DISPLAYED, RT AIL LOCKOUT ACTUATOR REPLACED.Dec 20, 2008 · N655UA · Boeing 767322SDR UALA2008121706912Actuator · faultyTHE "AIL LOCK" LT ON AT LOW SPEED. EICAS MSG AILERON LOCKOUT DISPLAYED. REPLACED RIGHT WING AILERON LOCKOUT ACTUATOR. REPLACED RT WING AILERON LOCKOUT ACTUATOR. TESTED NORMAL. RECEIVED SAME EICAS SEVERAL FLIGHT SEGMENTS LATER. REPLACED RIGHT SAM AND RT ADec 16, 2008 · N652UA · Boeing 767322SDR 2008FA0000882Bellcrank · misrepairedEXCESSIVE AILERONS T/E FREE PLAY. SUSPECTED AIL SYS CUMULATIVE WEAR. UPON FURTHER CLOSE VISUAL INSP, FOUND AILERONS BELLCRANK ASSY, PIVOT BRG HSG SECURED TO BELLCRANK PLATE WITH (3 EACH) BLIND FASTENERS. PROTRUDING HEAD FASTENERS WERE FOUND LOOSE AND EXHIBITINDec 9, 2008 · N1420J · Gulstm 112ASDR CA081204003Sensor · unserviceable(CAN) FDR CORRELATION CHECK REVEALED LT AILERON ROLL SENSOR UNSERVICEABLE. SENSOR INSPECTED. OPERATING CABLE FRAYED AND BINDING. SENSOR REPLACED.Dec 4, 2008 · Aerosp ATR42300SDR CA081203011Bracket · cracked(CAN) LT AILERON INPUT BRACKET FOUND CRACKED. LT AILERON QUADRANT BRACKET REMOVED P/N 85711569-001. POST S/B 8-57-27 QUADRANT BRACKET TO BE INSTALLED. NEW BRACKET IS IN SHEET METAL SHOP. REMOVED AND REPLACED NEW LT AILERON QUADRANT BRACKET IAW SB 8-57-27. Dec 2, 2008 · Dhav DHC8301SDR 2008FA0000926Control Cable · frayedTT ON CABLES UNKNOWN SUSPECT ORIGINAL. FOUND LT AFT AILERON CABLE FRAYED AT WING STA 59 THE PULLEY WAS FROZEN. INSPECTED REST OF SYSTEM NO DEFECTS FOUND. ON REPLACEMENT OF CABLE FOUND WAS ALSO FRAYED AT WING STA 87.29. THE PULLEYS AT THIS STATION WERE TURNINGDec 1, 2008 · Cessna 421BSDR 2008FA0000924Control Cable · frayedTT ON CABLES UNKNOWN SUSPECT ORIGINAL. FOUND LT AFT AILERON CABLE FRAYED AT WING STATION 58.94 THE PULLEY WAS FROZEN. INSPECTED REST OF SYSTEM NO DEFECTS FOUND. ON REPLACEMENT OF CABLE FOUND WAS ALSO FRAYED AT WING STA 87.29. THE PULLEYS AT THIS STATION WEDec 1, 2008 · Cessna 421BSDR DLM88081602Control Cable · fodWHEN SLATS/FLAPS WERE EXTENDED FROM CLEAN POSITION, THE AIRCRAFT ROLLED APPROXIMATELY 20-30 DEGREES UNCOMMANDED. INSPECTED AIRCRAFT, FOUND SCREWDRIVER STUCK IN CONTROL CABLES ABOVE E/E DOOR AT STA 116. REMOVED TOOL. RAN FLIGHT CONTROLS, FLAPS/SLATS, AILERONov 19, 2008 · N952DL · Doug MD88SDR SWIA200820461Support · bentFLT 5790 - AILERONS BINDING. REPLACED BENT RVDT ROD SUPPORT ON AILERON BELLCRANK.Nov 17, 2008 · N271YV · Emb EMB120ERSDR JRA2008F00000Spring Assy · stretchedAILERON CONTROL CABLES BINDING TO THE RIGHT FROM FULL LEFT POSITION. INSPECTION OF AILERON CONTROL CABLES REVEALED STRETCHED SPRING AT RUDDER INTERCONNECT. REMOVED AND REPLACED SPRING IAW 440 MM, SEC 8-2, PAGE 26. OPS CHECK OK. (K)Nov 14, 2008 · N587CA · Cvac STC440SDR DXTA200811093347Proximity Switch · inoperativeAFTER LEVELING OFF AT 10,000, ACFT WAS SEVERELY OUT OF TRIM. IMMEDIATELY AFTER TRIMMING, AILERON RATIO LOW MESSAGE APPEARED. MESSAGE REMAINED ON UNTIL APU SHUTDOWN PRIOR TO LANDING. CONFIRMED DISCREPANCY, AILERON LOW RATIO ON W/ HYD POWER APPLIED TO ACFT. RNov 9, 2008 · N999QS · Cessna 750SDR SWIA200820673Link · corrodedC-CHECK, LEFT FLUTTER DAMPER SHEAR LINK ASSEMBLY CORRODED. REPLACED PER AMM.Nov 8, 2008 · N445SW · Cndair CL6002B19SDR 2008UALA06456Actuator · faultyTHE "AIL LOCK" LT ON AT LOW SPEED. EICAS MSG AILERON LOCKOUT DISPLAYED. RECEIVED AILERON LOCKOUT MSG. REPLACED LEFT AILERON LOCKOUT ACTUATOR. MESSAGE CLEARED.Nov 7, 2008 · N660UA · Boeing 767322SDR SWIA200820349Aileron · obstructedFLT 5450 - ON APPROACH, AILERONS JAMMED. REMOVED DEBRIS BELOW TORQUE TUBE.Nov 2, 2008 · N216SW · Emb EMB120SDR CA081031004Roll Pin · missing(CAN) LT WING AILERON PUSHROD ASSY FOUND TO BE MISSING ONE ROLL PIN THAT RETAINS THE INBD END ROD END BEARING. THIS IS A DEFECT FROM THE FACTORY (INSIDE OF HOLE IS PAINTED). ALL OTHER ROD ENDS INSPECTED NO OTHER DEFECTS FOUND, ARROW SHOWS MISSING PIN HOLE.Oct 31, 2008 · Airtrc AT802ASDR UALA2008111306257Control Unit · faultyRUDDER AND AILERON TRIM EXCESSIVE WITH AILERON DEFLECTED. SUSPECT LEFT INBD AILERON STUCK IN UP POSITION, AS IND ON EICAS FLT CONT, IS DEFLECTED APPX HALF UP AND NOT RESPONDING TO INPUT. RUDDER AND AIL TRIM IS EXCESSIVE. AILERON FOR 6 HRS WAS ABOUT HALF DEFOct 24, 2008 · N663UA · Boeing 767322SDR CA081023001Bearing · seized(CAN) DURING FLAP INSP, AN ENGINEER FOUND AN AILERON PULLEY INSIDE THE WING BOX SEIZED. FURTHER INVESTIGATION REVEALED THE ADJACENT PULLEY WAS ALSO CORRODED. BOTH PULLEYS WERE REPLACED AND THE ACFT RETURNED TO SERVICE. 1915 HRS WERE REMAINING BEFORE COMPLETIOct 23, 2008 · Dhav DHC8102SDR CA081022008Clevis Bolt · worn(CAN) DURING AN AILERON CABLE (IN WING) REPLACEMENT THE CLEVIS BOLTS WERE FOUND TO BE WORN MORE THAT 30 PERCENT, REPLACED WITH NEW AN 24-12 CLEVIS BOLTS.Oct 21, 2008 · Dhav DHC2MKISDR 22AA20081003Mechanism · lack of lubeUPON RETRACTING FLAPS 2 1/2 UNITS OF AILERON TRIM TO THE RT MUST BE USED TO KEEP WINGS LEVEL. PERFORMED AILERONS SYSTEM TEST IN ACCORDANCE WITH M/M 27-10-00. FOUND NORMAL, FLAP SYSTEM TEST IN ACCORDANCE WITH M/M 27-50-00. FOUND NORMAL SPOILER SYSTEM OPERATIOct 19, 2008 · N140WE · Doug DC1040FSDR CHQA200800204Trim Panel · faultyFLIGHT 5601, IAH TO JAX. DURING CLIMB, THE FLIGHT CREW EXPERIENCED AN AILERON TRIM RUN-AWAY. THE QRH WAS FOLLOWED AND THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AILERON/RUDDER TRIM PANEL AND THE AILERON TRIM SYSTEM OPOct 18, 2008 · N702BR · Cndair CL6002B19SDR 2008FA0000769Control Cable · wornDURING ANNUAL INSP, THE RT AILERON RETURN CABLE WAS FOUND WORN BEYOND LIMITS BY THE WHITE PLASTIC PULLEY NEAR THE LEADING EDGE AT THE WING ROOT. (K)Oct 10, 2008 · N6523N · Cessna 210NSDR AALA200802708Actuator · failedJFK INFLIGHT ORD TO BRU - BOTH AILERON FLOATING IN FLIGHT. RIGHT INBOARD AILERON WOULD NOT GO BELOW NEUTRAL. LEFT INBOARD AILERON OVER COMPENSATING FOR THE RIGHT SIDE. DIVERTED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED LEFT AND RIGHT INBOARD AND OUTBOAROct 9, 2008 · N350AN · Boeing 767323SDR QXEA200801110Control Panel · malfunctionedPDX FLIGHT 9850. RT AILERON TRIM SWITCH STUCK WHEN APPLYING TRIM. TRIM RAN AWAY TO THE RT. WAS ABLE TO NEUTRALIZE TRIM BY APPLYING LT AILERON TRIM FIRMLY. THE SWITCH APPEARED TO BE STUCK. MX R&R THE AILERON/RUDDER TRIM CONTROL-PANEL PER Q400AMM TASKS 27-1Oct 6, 2008 · N407QX · Bombdr DHC8402
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