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"

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SDR C2XA10CL122Recovery Unit · out of adjustCLE FLT 2578 THE CREW REPORTED THE AIRCRAFT REQUIRED A SIGNIFICANT AMOUNT OF LEFT TRIM TO COUNTER A DISTINCT RIGHT ROLL. MAINTENANCE INSPECTED AND ADJUSTED THE LEFT AND RIGHT AILERON NEUTRAL RECOVERY UNIT. OPERATIONAL CHECKS WERE GOOD.Jul 30, 2010 · N14977 · Emb EMB145LRSDR RYNA2010007020023Indication Sys · malfunctionedWHILE PERFORMING CONTROL WHEEL SURFACE CHECKS, LEFT O/B AILERON SHOWED NO MOVEMENT ON LOWER EICAS SCREEN. SWAPPED RT & LT STAB TRIM/AILERON LOCKOUT MODULES FOR TROUBLESHOOTING. CHECKS GOOD PER FIM 27-09-00, NO HELP. SWAPPED BACK, BOTH CHECK GOOD. TRANSFERRJul 22, 2010 · N120DL · Boeing 767332SDR HALA2010071600301Control Cable · brokenLEFT AILERON CONTROL CABLE (7F) HAS BROKEN STRANDS. REPLACED LEFT AILERON TAB CONTROL CABLE (7F) IAW M/M 20-00-02 & 27-10-00. OPERATION & RIG CHECK GOOD.Jul 14, 2010 · N476HA · Boeing 717200SDR SWIA201024539Control Panel · defectiveRUDDER RUN AWAY TO RIGHT INFLIGHT, UNCOMMANDED. (FLT 591) REPLACED AILERON/RUDDER TRIM CONTROL PANEL.Jul 9, 2010 · N755SK · Cndair CL6002C10SDR UALA2010070102350Actuator · failedAILERON LOCKOUT EICAS. CONFIRMED BOTH CB C17 LT AILERON LOCKOUT AND C18 R AILERON LOCKOUT POPS WITH OR WITHOUT PERFORMING AILERON LOCKOUT TEST. IT POPS WITHIN 30 TO 60 SECS AFTER RESET. REF SSM 27-10-02, WDM 27-11-12, 27-11-22 SHOWS SYSTEMS ARE INDEPENDENT ANJul 1, 2010 · N664UA · Boeing 767322SDR ASAA1058015Bearing · lack of lubeDURING MANEUVERING FOR LANDING ON SHORT FINAL WHILE APPLYING AILERON TO ROLL LEFT YOKE MOMENTARY LOCKED AND REQUIRED EXCESSIVE FORCE TO OBTAIN DESIRED ROLL INPUT F/O HAND FLYING DURING FAULT. ISOLATION/TROUBLESHOOTING FOUND SIGNIFICANT NOISE CLICKING COMING FJun 28, 2010 · N546AS · Boeing 737890SDR SWAA103782Shaft · corrodedDURING SCHEDULED 16Y CHECK, FOUND CORROSION ON SHAFT OF AILERON BODY QUADRANT. REMOVED AND REPLACED SHAFT PER MM.Jun 27, 2010 · N380SW · Boeing 7373H4SDR UALA2010062302210Shutoff Valve · faultyON TAXI COULD ONLY GET 2040 PSI FROM LT ELEC HYD PUMP ALONG WITH EICAS MESSAGE AND AUDIO. LT ELEC HYD PMP PSI AT 2200. LT ELEC PUMP, ELCU REPLACED, NO HELP. SUSPECT INTERNAL COMPONENT BYPASSING. WILL NEED TO ACP CHECKS. WITH REF TO LOW PRESSURE ON LT ACMP, FJun 22, 2010 · N655UA · Boeing 767322SDR CA100617007Pulley · seized(CAN) AILERON CONTROL REPORTED AS STIFF. RECTIFICATION, WITH ROLL CONTROL DISCONNECTED FOUND THE PILOTS SIDE TO BE STIFF. FOUND CAPT CONTROL COLUMN HAND WHEEL BEARING TO BE ROUGH. HAND WHEEL REMOVED AS PER 27-32-17 AND BEARINGS (P/N- MS27641-10) REPLACED. Jun 15, 2010 · Dhav DHC8102SDR SWIA201024716Rod End · corrodedLEFT AILERON TRIM TAB ROD ENDS CORRODED. (C-CHECK) REPLACED LEFT AILERON TRIM TAB ROD ENDS.Jun 7, 2010 · N221SW · Emb EMB120ERSDR NSVA201093Control Cable · chafedDURING A SCHEDULED 4A CHECK WHILE PERFORMING WC 27-900-705 DETAILED VISUAL INSPECTION OF THE EXPOSED AILERON WING CABLES, THE LEFT FORWARD INBOARD CABLE WAS FOUND SEVERELY CHAFED, APPROX 40-50 PERCENT THROUGH, AT WING STATION Y-194.219 AND APPROX STATION Y-200Jun 7, 2010 · N202WQ · Bombdr DHC8402SDR UALA2010060701971Control Cable · misroutedFLIGHT CONTROLS STIFF IN PITCH AND ROLL ON GROUND AND IN AIR. HEAVY CONTROLS FELT ON BOTH CONTROL COLUMNS, AP'S DISENGAGED, HYD'S PRESS AND QTY'S NORMAL. CHECKED LT AND RIGHT AILERON PCU. COMPLETED SYSTEM TEST. SYSTEM WILL INCREASE WHEEL FORCE. HAD TO FLY APPJun 6, 2010 · N589UA · Boeing 757222SDR DXTA2010061104120Bearing · wornRUBBING HEARD/FELT IN YOKE & FLOOR DURING FORE & AFT MOVEMENT OF YOKE ONLY WHEN AIRBORNE & AT ALL AIRSPEEDS & CONFIGURATIONS. NO RUBBING INDICATED WITH LT/RT MOVEMENT OF YOKE. RUBBING HEARD/FELT ON BOTH SIDES YOKE & FLOOR OF COCKPIT WITH EACH PILOT CALLING RJun 6, 2010 · N670QS · Cessna 560XLSDR SWIA201024351Flap · defectiveAIRCRAFT ROLLS WHEN FLAPS SELECTED TO 45 DEGREES. (FLT 1005) REMOVED EXCESSIVE PAINT BUILDUP ON FLAPS LEADING EDGE.Jun 6, 2010 · N593ML · Cndair CL6002B19SDR CA100608008Control Cable · obstructedWHEN ELEVATOR CONTROL PULLED ALL THE WAY BACK THE AILERONS WERE LOCKED UP. HOSE CLAMP WAS HOLDING STRUCTURE CLOSER TO CONTROL COLUMN SHAFT. WHEN CONTROL COLUMN WAS PULLED OUT, A ROLLER ADJUSTMENT SCREW CONTACTED THE STRUCTURE, BINDING. THE AILERONS, AS HOSE CJun 1, 2010 · Piper PA60600SDR UALA2010060101893Actuator · faultyRT AILERON LOCK OUT ACTUATOR. NEED TO REPLACE RT AILERON LOCK OUT ACTUATOR. IT DID HIT AGAIN. REPLACED RT AILERON LOCKOUT ACTUATOR. OPS CHECKED GOOD.May 30, 2010 · N648UA · Boeing 767322SDR 2010FA0000507Control Cable · frayedDURING INSPECTION THE AILERON CABLES ARE INSPECTED WITH MAGNIFICATION WHERE KNOWN WEAR/FRAYING IS COMMON. THIS CABLE, P/N-0510105-360 WAS FOUND WORN AT F.S.: 65.53. THERE WERE BROKEN STRANDS AND THE AREA IS EXTREMELY SHINY. THIS IS A COMMON DISCREPANCY FOR May 25, 2010 · N442ER · Cessna 172SSDR UALA2010052501799Actuator · faultyLT & RT AILERON LOCKOUT MSGS. DUE TO REPEAT WRITE UP OF AILERON LOCKOUT NEED TO REPLACE THE RT & LT AILERON LOCKOUT ACTUATORS. REPLACED THE RT & LT AILERON LOCKOUT ACTUATORS. FUNCTION TESTS OK.May 24, 2010 · N648UA · Boeing 767322SDR DXTA2010052404097Control Unit · bindingON APPROACH AFTER DISENGAGING THE AUTO PILOT/YAW DAMP AT 180KTS THE ACFT WOULD ONLY ROLL (5) DEGREES TO THE RT. BOTH THE CAPTAIN AND COPILOTS CONTROLS SEEMED JAMMED. ONCE ON THE GROUND WE ARE ABLE UNJAM THE CONTROLS WITH FULL MOVEMENT. REPLACED AILERON AFU.May 22, 2010 · N723QS · Gulstm 200SDR 2010FA0000498Control Cable · wornDURING A PREFLIGHT INSPECTION WITH THE AILERON UP, EXCESSIVE WEAR OF THE FORWARD OUTBOARD AILERON CABLE WAS NOTED AT THE RBS 189 FAIRLEAD. THE PHENOLIC PROTECTOR WAS IN GOOD CONDITION EVEN THOUGH THE CABLE HAD BEEN RUBBING ON IT. MANY STRANDS WERE WORN THROUGHMay 20, 2010 · N105TB · Gulstm G1159SDR A6WA201040365Actuator · bindingDURING APPR F/O FELT BINDING IN AILERONS (BOTH LT AND RT) UPON LANDING, PERFORMED AILERON CHECK AND FELT BINDIING IN BOTH DIRECTIONS ON BOTH SIDES. R & R AILERON TRIM ACTUATOR IAW AMM 27-12-01. OPS TEST GOOD.May 19, 2010 · N432AW · Cndair CL6002B19SDR 2010FA0000492Control Cable · frayedDURING INSPECTION THE AILERON CABLES ARE INSPECTED WITH MAGNIFICATION WHERE KNOWN WEAR/FRAYING IS COMMON. THIS CABLE, CESSNA P/N-0510105-364 WAS FOUND WORN AT W.S.: 71.125. THERE WERE BROKEN STRANDS AND THE AREA IS EXTREMELY SHINY. THIS IS A COMMON DISCREPANCYMay 19, 2010 · N442ER · Cessna 172SSDR 2010FA0000491Control Cable · frayedDURING INSPECTION THE AILERON CABLES ARE INSPECTED WITH MAGNIFICATION WHERE KNOWN WEAR/FRAYING IS COMMON. THIS CABLE, CESSNA P/N-0510105-364 WAS FOUND WORN AT FS 65.33. THERE WERE BROKEN STRANDS AND THE AREA IS EXTREMELY SHINY. THIS IS A COMMON DISCREPANCY FORMay 19, 2010 · N442ER · Cessna 172SSDR 2010FA0000490Control Cable · frayedDURING INSPECTION THE AILERON CABLES ARE INSPECTED WITH MAGNIFICATION WHERE KNOWN WEAR/FRAYING IS COMMON. THIS CABLE, P/N-0510105-360 WAS FOUND WORN AT F.S.: 65.53. THERE WERE BROKEN STRANDS AND THE AREA IS EXTREEMLY SHINY. THIS IS A COMMON DISCREPANCY FOR THIMay 19, 2010 · N442ER · Cessna 172SSDR MASA2010050900475Warning System · activatedCONFIG TRIM MASTER WARNING ON T/O ROLL. RTG; PERFORMED AILERON EXCESSIVE BACKLASH CHECK PER AMM.May 9, 2010 · N37178 · Cndair CL6002B19SDR UALA2010050301477Servo · out of toleranceAIRFRAME VIBES. GOES AWAY WITH ROLL INPUTS. VIBRATION REPORT CHECKLIST COMPLETE. FLIGHT CRE W REPORT STATES, SLOWING TO 300 KIAS AT FL280 IN CLIMB, ALL VIBES WENT AWAY. DEFINITELY SPEED RELATED, MEDIUM FREQUENCY FELT LIKE ELEVATOR OR AILERON FLUTTER, BUT INTEMay 3, 2010 · N809UA · Airbus A319131SDR 2010FA0000411Control Cable · frayedDURING A ROUTINE INSP, THIS CABLE WAS FOUND WORN WITH BROKEN STRANDS. IT IS VERY DIFFICULT TO SEE WITHOUT MAGNIFICATION AND APPEARS ONLY AS A SHINY SPOT ON THE CABLE. THIS CABLE AND (2) OTHERS PASS ACROSS THE CEILING THROUGH 3 PULLEYS JUST ABOVE THE REAR SEAT Apr 23, 2010 · N464ER · Cessna 172SSDR N6WA20100406Aileron · bindingAILERONS JAMMED IN FLIGHT. INSPECTED AILERON CONTROL CABLES IN PRESSURIZED AND UNPRESSURIZED ZONES, AVIONICS BAY, WHEEL WELL, UNDER SPOILER PANELS FOR DAMAGE OR FOD, NO DAMAGE NOTED IAW AMM 27-11-00. NO DAMAGE ON AILERONS FOUND AT THIS TIME.Apr 18, 2010 · Cndair CL6002C10SDR UALA2010041901292Bearing · bindingAILERONS BIND DURING FLIGHT CONTROL CHECK. FOUND ROD END BEARINGS WORN ON CONTROL ROD BETWEEN THE RT LCCA TORQUE TUBE AND THE AILERON CONTROL OVERRIDE MECHANISM. VERIFIED ROD ENDS REPLACED ON BENCH COMPARITOR. ROD LENGTH AT ORIGINAL CONFIG. REPLACED ROD ENDApr 18, 2010 · N675UA · Boeing 767322SDR MYWA100068Actuator · leakingETOPS SIGNIFICANT ITEM - UPPER AILERON POWER CONTROL UNIT IS LEAKING FROM ACTUATOR PISTON.Apr 13, 2010 · N753MA · Boeing 73748ESDR A6WA201040277Feel Sensor · out of adjustHIGHER THAN NORMAL CONTROL FORCE REQUIRED WHEN APPLYING AND NEUTRALIZING RT ROLL INPUTS FROM CTR OS ON BOTH YOKES IN FLIGHT. INSPECTED RIGGING OF AILERON FEEL AND SENSORY MECHANISM ON BOTH SIDES. ADJUSTED IAW AMM 27-11-00. OPS CHECK GOOD.Apr 2, 2010 · N458AW · Cndair CL6002B19SDR HALA2010032900140Bearing · bindingETOPS SIGNIFICANT SYS - "IAW FLIGHT CREW" BINDING IN AILERONS WHEN DOING FULL TRAVEL CHECKS, LT TURNS ONLY, RT TURNS OK. REPLACED AILERON CONTROL FEEL BEARING. - OPS CHECK OK, REF CMM 27-11-23-701-3D (9).Mar 29, 2010 · N584HA · Boeing 76733ASDR 22AA201000067AControl Cable · brokenACFT ROLLS WHEN SPEED BRAKE IS EXTENDED. DIFFERENCE SHOWS ON SPI. DURING INSP FOUND RT/LT INBD AILERONS OUT OF RIGGING. ALSO ON PRE/FLT FOUND LT WING GROUND SPOILERS NOT DEPLOYING FULLY & SPOILER HANDLE NOT RETRACTING AUTOMATICALLY. ALSO SPOILER PANEL 1 & 2 NOMar 28, 2010 · N524MD · Doug DC1030SDR UALA2010032200943Servo Control · faultyLT AILERON ISSUE, FLIGHT DIVERTED. AILERON JERK HAPPENED WITH A-P ON, AP WASN'T DISENGAGED AND DID NOT KICK OFF. SPOILERS DIDN’T DEPLOY OR MOVE TO CAUSE ANY ROLL. AILERON FLOATED UNTIL AN INPUT WAS MADE THEN AILERON JERKED INTO COMMANDED POSITION. UNCOMMANMar 21, 2010 · N811UA · Airbus A319131SDR HALA2010031900131Seal · out of positionETOPS SIGNIFICANT SYSTEM - LEFT AILERON BINDS. FOUND RIGHT INBOARD AILERON OUTBOARD LOWER SEAL AT LEADING EDGE STICKING OUT FOUR INCHES. RE-SECURED SEAL, SECURITY AND OPS CHECK OK REF FIM 27-11-00 FIG 107.Mar 19, 2010 · N584HA · Boeing 7673G5SDR 2010FA0000230Cable · brokenRT AILERON BUS CABLE PN 3763151-501 BROKEN JUST OTBD OF THE RT INBD AILERON. FOUND LT AILERON WAS INOPERATIVE; THEREFORE PLACING HIGH TENSION ON THE BUS CABLE. WE ARE QUARANTINING THE ACTUATOR AND CABLE ASSY UNTIL FURTHER INVESTIGATION.Mar 16, 2010 · N802DH · Doug DC873SDR SIMA201006704Fitting · wornDURING THE MAINTENANCE BASE VISIT THE LEFT AILERON ACTUATOR FITTINGS WERE FOUND TO BE LOOSE IN BORES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT AILERON FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.Mar 5, 2010 · N618AE · Emb EMB145LRSDR 2010F00054Cable · brokenRT AILERON BUS CABLE PN 3763151-501 BROKEN JUST OTBD OF THE RT INBD AILERON. FOUND LT AILERON ACTUATOR WAS INOPERATIVE THEREFORE PLACING HIGH TENSION ON THE BUS CABLE. QUARANTINED THE ACTUATOR AND CABLE ASSY UNTIL FURTHER INVESTIGATION.Feb 27, 2010 · N802DH · Doug DC873SDR UALA2010030100734Control Rod · bindingCAPT FELT BINDING ON AILERON ON APPROACH AFTER LANDING ON GROUND. FLT CONTROL BINDING AILERON DISCONNECTED AND CONNECTED CONTROL RODS. OPS CHECKS NORMAL. NO BINDING FOUND IN SYS. RII INSPECTION METHOD NR 1 OF REMOVED AILERON CONTROL RODS AS CALLED OUT IN FIM.Feb 26, 2010 · N670UA · Boeing 767322SDR 2010FA0000215Control Cable · frayedDURING A PRE-PURCHASE INSPECTION, FOUND CONTROL YOKE BINDING WHEN TURNED TO THE LT AT APPROX 45 DEGREES. INSPECTED AILERON CNTRL SYS AND FOUND SCREW LODGED IN PULLEY GROOVE AND DAMAGED CABLE. ACFT HAD FLOWN 2.0 HRS SINCE LAST ANNUAL INSPECTION. THE SCREW APFeb 18, 2010 · N315W · Beech A36SDR SWIA201023689Pcu · out of rigUNCOMMANDED RIGHT ROLL WHEN FLAPS EXTENDED TO 45 DEGREES. (FLT 6016) RIGGED LEFT AILERON PCU AND RIGHT FLAP BPSU.Feb 18, 2010 · N943SW · Cndair CL6002B19SDR SWIA201023697Aileron · out of rigAIRCRAFT ROLLS TO THE RIGHT WHEN FLAPS ARE SELECTED PAST 30°. (FLT 4556) ADJUSTED LEFT AILERON RIG AND CLEANED WINGS.Feb 16, 2010 · N413SW · Cndair CL6002B19SDR UALA2010021100521Bearing · wornCREW REPORTS ON FLT CONTROL CHECK FOR AILERON, THE CONTROL WHEELS (CAPTS AND FO'S) FEEL AN UNUSUAL HARD SPOT AT ABOUT THREE-QUARTERS TRAVEL LT WING DOWN. LT AIL LCCA UPR & LWR TORQUE TUBE SUPPORT BEARINGS (3EA) FOUND WORN & CORRODED AT LWR LINK ARM FOR FEEL, Feb 11, 2010 · N647UA · Boeing 767322SDR SWIA201023646Pcu · out of adjustUNCOMMANDED LEFT ROLL WITH FLAPS SELECTED FOR LANDING. (FLT 4731) RIGGED RIGHT AND LEFT AILERON PCU'S.Feb 10, 2010 · N438SW · Cndair CL6002B19SDR CLCA02092010.1Warning System · activatedAFTER TAKEOFF (SBKP) LEVEL 2 DEFLECT AILERON DISAGREEMENT WARNING APPEARED ON EAD. PERFORMED CHECKLIST, WARNING REMAINED, RETURNED TO AIRPORT (SBKP). ENTERED ON DEFERRED MAINTENANCE ITEM (DMI) PER MEL 27-13-2, CAT "C", PLACARD INSTALLED, AIRCRAFT RELEASE BACFeb 9, 2010 · N701GC · Doug MD11FSDR SIMA201003502Fitting · damagedDURING MAINTENANCE BASE INSPECTION FOUND RIGHT AILERON ACTUATOR FITTING TO BE DAMAGED BEYOND LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED AILERON ACTUATOR FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.Feb 3, 2010 · N614AE · Emb EMB145LRSDR CLCA01282010.1Warning System · activatedAFTER TAKEOFF (SBKP) EAD INDICATES LEVEL 2 AILERON DEFLECT DISAGREE. PERFORMED QRH CHECKLIST AND INDICATION STILL PRESENT. RETURNED TO AIRPORT. ENTERED ON DEFERRED MAINTENANCE ITEM (DMI) PER MEL 27-13-2, CAT "C", PLACARD INSTALLED, AIRCRAFT RELEASE BACK TO Jan 28, 2010 · N701GC · Doug MD11FSDR CA100121001Control Cable · worn(CAN) THE AILERON CABLES ON LAKE ACFT, MODELS, LA-4, -200, -250 HAVE BEEN FOUND WEARING AT FUS STA 117 0N LA-4, 200`S AND FUS STA 176 ON LA-250 WRE THE CABLE CONTACTS THE PHENOLIC FAIRLEAD. THE WEAR OF THESE CABLES IS DEPICTED IN AC43.13-1B, CHAP. 7, PG7-36, FJan 21, 2010 · Conaer LA4200SDR UALA2010011500187Aileron Sys · malfunctionedAILERON CONTROL ISSUE, FLIGHT DIVERTED. INSPECTED CABLES AND PULLEYS FROM WHEEL WELL TO AILERON PCU'S BOTH LT AND RT WING. ALSO CHECKED AILERON QUADRANTS AND COLD SOAKED QUADRANT BRGS IN WHEEL WELLS AND DAMPER UNDER COCKPIT PIT FLOOR FOR TROUBLESHOOTING. NOJan 14, 2010 · N589UA · Boeing 757222SDR ANCF09123000056AController · malfunctionedAIR TURN BACK. LT AND RT AILERON FAULT WAS PRESENTED AFTER TAKE OFF. IAW TSM 27-95-00-810-802 FAILURE OF THE FCDC 2 WAS PERFORMED AND TEST OK AND AMM 27-96-00-740-0021 THE BITE TEST OF THE EFCS GROUND SCANING WAS PERFORMED AND SATISFACTORY.Jan 12, 2010 · N664AV · Airbus A320214
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