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 HALA0700071Unknown · unknownETOPS SIGNIFICANT SYSTEM - "AILERON LOCKOUT" EICAS MESSAGE ILLUMINATED AT HIGH SPEED, MOMENTARILY DURING CLIMB A/C >=290KIAS. T/S PER FIM 27-11-00/101 FIG 104 BLKS 1-5-10-15. SYS IS OK.Feb 28, 2007 · N583HA · Boeing 76733ASDR 2007UALA00492Control Cable · misroutedLT WING AFT AILERON BUS CABLE CONTACTING MLG BEAM APPROX RSS 268 ON OUTBD SIDE OF GEAR BEAM. AILERON CABLES MIS-ROUTED. IMPROPER ROUTING OF CABLES. REROUTED CABLES CORRECLTY.Feb 18, 2007 · N904UA · Boeing 737522SDR 200702121Aileron · frozenFLIGHT 7549 IAD TO ROC DURING CRUISE THE AUTOPILOT DISCONNECTED. THE CREW BEGAN TO HAND FLY THE A/C AND FOUND THE AILERONS FROZEN. WITHIN 2-3 SECONDS THE CONTROLS MOVED FREELY AGAIN, WITH SLIGHTLY -HEAVY- FEEL. THIS REOCCURRED ON TWO OTHER OCCASIONS DURING Feb 8, 2007 · N631R · Emb ERJ170100SESDR SIMA200703805Control Cable · wornFOUND LEFT INBOARD AILERON CABLE WORN AT FRAME 25 FAIRLEAD. REMOVED AND REPLACED AILERON CABLE IAW EMB AMM 27-11-01. OPERATIONAL CHECK GOOD, RETURNED TO SERVICE.Feb 6, 2007 · N655AE · Emb EMB145LRSDR SIMA200703808Control Cable · wornFOUND LEFT OUTBOARD AILERON CABLE WORN AT FRAME 35 FAIRLEAD. REMOVED AND REPLACED AILERON CABLE IAW EMB AMM 27-11-01. OPERATIONAL CHECKED GOOD - RETURNED AIRCRAFT TO SERVICE.Feb 6, 2007 · N655AE · Emb EMB145LRSDR SIMA200703804Control Cable · wornFOUND RIGHT OUTBOARD AILERON CABLE WORN AT FRAME 35 FAIRLEAD. REMOVED AND REPLACED AILERON CABLE IAW EMB AMM 27-11-01. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.Feb 6, 2007 · N655AE · Emb EMB145LRSDR 2007FA0000104Control Cable · frayedDURING A ROUTINE INSPECTION THE AILERON CONTROL DIRECT CABLE WAS FOUND SERIOUSLY WORN IN THE CABIN OVERHEAD AREA. THE AILERON BALANCE AND DIRECT CABLES ARE SEPARATED AND GUIDED BY 3 PULLIES, P/N-S394, INDEX NR 30, CHAPTER 27-10-00, FIG 3 IN THE CESSNA PARTS MAFeb 1, 2007 · N5275S · Cessna 172SSDR CA070201005Washer · split(CAN) THE CREW OBSERVED BINDING IN THE AILERON SYSTEM WHILE EXECUTING A RT TURN DURING DEPARTURE. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT FURTHER PROBLEM. POST FLIGHT INSPECTION DETECTED A LOCATION IN THE SYSTEM WHICH EXHIBITED AN INCREASED RESISTAJan 30, 2007 · Aerosp ATR42300SDR DHL2007760003Line · leakingA ENG 1/2 HYDRAULIC PUMP LOW PRESS LIGHTS ILLUMINATED IN FLT LOSS OF ALL A PRESS AND QUANTITY PERFORMED HYDRAULIC SYSTEM A FAILED ABNORMAL CHECKLIST. FOUND FLEX LINE AT ELEVATOR POWER CONTROL PACKAGE WITH HOLE IN IT REPLACED LINE WITH TEMP (17114-4CR-0240). Jan 24, 2007 · N760AT · Boeing 7272B7SDR SWAA070216Bearing · bindingAILERONS BIND BEYOND 10 TO 15 DEGREES OF TRAVEL IN BOTH DIRECTIONS. ELEVATOR TRAVEL NORMAL. REMOVED AND REPLACED FEEL CENTERING SPRING CAM ROLLER BEARING PER MM.Jan 16, 2007 · N655WN · Boeing 7373H4SDR A8J2007F00001Circuit Board · faultyON 1/10-07 AT 1900, AIRCRAFT EXPERIENCED AN AILERON BOOST FAILURE. PILOT DECLEARED AN EMERGENCY AND LANDED AT ITS SCHEDULE DETINATION WITHOUT ANY COMPLICATIONS. AILERON BOOST CIRCUIT BOARD WAS REPLACED AND THE SYSTEM CHECKED GOOD. (K)Jan 10, 2007 · N777XS · Cessna 650SDR TRAX200700056Control Cable · frayedAILERON SERVO AUTO PILOT CABLE FRAYING AND SERVO ACTUATOR DRUM DAMAGED. REFER TO EXELTECH WORK PACKAGE YUL000164 NRTC AILERON AUTO PILOT ROLL ACTUATOR AND CABLES REMOVED IAW JIC 22-13-71 RAI 10000, AILERON SERVO AUTO PILOT CABLE AND SERVO ACTUATOR REPLACED IJan 9, 2007 · N635AS · Aerosp ATR72212SDR A6WA200740008Aileron · ratchetingNOTICEABLE HANGUP/LATCH IN AILERON ROLL CONTROL ON BOTH YOKES NEAR NEUTRAL POSITION, NOTICED IN FLIGHT, 6000-7000 FT WHILE HAND FLYING. (M)Jan 9, 2007 · N414ZW · Cndair CL6002B19SDR 2007UALA00004Aileron · flutterRTFL DUE TO UNCONTROLLABLE AILERON FLUTTER. BLEED GREEN SYSTEM HYDRAULICS. AILERONS MOVED SMOOTHLY DURING OPS TEST.Dec 31, 2006 · N453UA · Airbus A320232SDR DXTA200601820Proximity Switch · malfunctionedUPON SETTING THROTTLES FOR TAKE OFF, (NO TAKEOFF) WARNING CAME ON. THE WARNING WAS GENERATED FROM A (ROLL SYSTEM) FAULT. SHUT OFF ALL ELECTRICAL POWER TO SEE IF MESSAGE WOULD CLEAR, BUT THE FAULT COMES BACK WHEN RT AILERON IS PUT IN (CONTROL YOKE MOVED RT). Dec 27, 2006 · N350QS · Cessna 680CESDR 2006UALA02422Servo Valve · faultyNO LAND 3 MESSAGE DUE TO RT AILERON SERVO FAULT. NO LAND 3 CAME ON A FEW TIMES. FAILED ON EACH OF THE LAST 12 LEGS WITH MESSAGE: NO LAND 3 AIL SRVO-FCCR. REPLACED R FLT CNTRL COMPUTER. NO HELP REINSTALLED ORIGINAL. SUSPECT AILERON SERVO VALVE NEEDS REPLADec 22, 2006 · N667UA · Boeing 767322SDR CA061218018Rod · misinstalled(CAN) DURING C-CHECK, A INSPECTOR FOUND THE AILERON INPUT ROD NOT PROPERLY INSTALLED ON BOTH SIDE LT AND RT AILERON. THE ROD END WAS FABRICATED WITH A CUT OUT FOR AVOID THE CONTACT BETWEEN THE ROD END AND THE QUADRANT SHAFT. ON THE SAME A/C, WE FOUND THE BOTDec 18, 2006 · Dhav DHC8102SDR DXTA200601774Spring · bindingWHEN AIRBORNE, THE AILERONS BIND DURING A LT OR RT TURN WHEN THE CONTROL WHEEL IS MOVED APPROXIMATELY 5 TO 10 DEGREES FROM NEUTRAL (PILOT FLYING FROM LT SEAT). (M2B)- REPLACED SPRING ON SPOILER MIXER INPUT. C/W IAW MM 27-12-02 RIG + OPS CHK GOOD IAW MM 27-1Dec 3, 2006 · N989QS · Cessna 750SDR CA061201001Control Cable · worn(CAN) LT AILERON CONTROL CABLE WORNED IN FAIRLEAD, ACCESS PANEL 740-2 (RT SIDE). CABLE NEEDS REPLACEMENT. THIS CABLE HAS BEEN REPLACED ON 2005-11-22 AND CUMULATED 151 HOURS FLYING TIME.Dec 1, 2006 · Cndair CL2151A10SDR 2007FA0000098Support Bracket · crackedCRACKS IN AILERON BELLCRANK LOWER SUPPORTS BOTH LT AND RT. LOOK REAL CLOSE ON INSPECTION BECAUSE NUT AND WASHER COVER AREAS. (K)Nov 30, 2006 · N4509X · Piper PA28R200SDR NOCA21406Spring · corrodedLEFT WING INBOARD AILERON OUTBOARD DROOP QUADRANT SPRINGS ARE CORRORED INTERNALLY. REMOVED AND REPLACED SPRINGS, RIGGED SPRINGS PER AMM 27-11-38-404-046. INSTALLED QUADRANT PER AMM, RIGGED CHECKED GOOD, OPS CHECKED GOOD.Nov 30, 2006 · N760NA · Boeing 767383SDR NOCA21306Rod End Bearing · corrodedRIGHT WING AILERON OUTPUT QUADRANT UPPER CONTROL ROD (TO OUTPUT QUADRANT) ROD ENDS RUSTY. REMOVED CONTROL ROD, REPLACED ROD END BEARINGS, INSTALLED RIGHT AILERON OUTPUT QUADRANT UPPER CONTROL ROD PER MM RIG CHECKED GOOD, OPS CHECKED GOOD.Nov 29, 2006 · N760NA · Boeing 76739HSDR NOCA21206Spring · corrodedRIGHT WING AILERON OUTPUT QUADRANT SPRINGS RUSTED. INSTALLED NEW SPRINGS PER MM ON OUTPUT QUADRANT. RIG CHECK GOOD, OPS CHECKED GOOD.Nov 29, 2006 · N760NA · Boeing 76739HSDR NOCA21006Spring · corrodedRIGHT WING AILERON BREAKOVER MECHANISM SPRINGS RUSTED. BLOCKED CABLE, REMOVED RIGHT WING AILERON OVERRIDE QUADRANT, REMOVED & REPLACED SPRINGS & OVERRIDE BEARINGS PER MM. INSTALLED OVERRIDE QUADRANT. RIG CHECKED GOOD, OPS CHECKED GOOD. P\N OF BEARING 567349Nov 29, 2006 · N760NA · Boeing 76739HSDR CA061129003Master Link · defective(CAN) DURING FIGHT ID 2C3-30 THE MASTER LINK (N025) FELL OFF THE COPILOT’S AILERON CHAIN CAUSING A LOSS OF AILERON CONTROL FROM THE COPILOT’S SIDE. THE FLIGHT TEST ENGINEER WAS ABLE TO COLLECT ALL THE PIECES FROM THE MASTER LINK DURING THE FLIGHT HOLD AND THE Nov 24, 2006 · Found FBA2CSDR 4519711182006Control Quadrant · bindingCREW REPORTS AILERON BINDS WHEN MOVING LT OR RT FROM CENTER AND POPS WHEN IT FINALLY MOVES. MAINTENANCE PERFORMED A SPRING FORCE CHECK AND FOUND NO DEFECTS. IAW INFO SERVICE LETTER, SUSPECT THE UPPER AILERON QUADRANT DETENT IS ALLOWING THE SWEDGE BALL TO POP,Nov 18, 2006 · N432FX · Lear 45LEARSDR DXTA200601752Servo Control · bindingCONTROL WHEEL RATCHETING. LT CONTROL WHEEL THE RATCHETING IS MORE DEFINED. REMOVED AND REPLACED AFT AILERON SECTOR PCU IAW MM CHPT. 27-10-01.Nov 12, 2006 · N951QS · Cessna 750SDR NOCA18906Spring · corrodedSPRING CORRODED ON AILERON CENTERING UNIT ON WING T/E FWD OF INBOARD. REMOVED AND REPLACED OUTBOARD DROP QUADRANT SPRINGS IAW 767 AMM 27-11-39. AILERON RIG OK. OPS CHECKED OK.Nov 7, 2006 · N767NA · Boeing 767324SDR NOCA18806Control Cable · corrodedAILERON CABLE RUSTY AROUND SECTOR ABOVE ANGLE TORQUE TUBE BOX FWD OF INBOARD AILERON. INSTALLED RIGHT WING INBOARD CABLE A4B & INSTALLED COTTER PIN AFTER BLOCKING CABLE AT INBOARD SECTION OF WING. RIGGED AIRCRAFT PER MM 27-11-00-5, OPS CHECKS OK.Nov 7, 2006 · N767NA · Boeing 767324SDR DXTA200601715Mixer Box · wornCONTROL WHEEL FEELS LIKE THERE IS A DETENT AS YOU TURN EACH DIRECTION. PRIOR TO THAT POINT FROM CENTER (NEUTRAL) POSITION, TURN RATE IS SLOW. AFTER THE DETENT THE TURN RATE INCREASES. A/C DIVERTED TO SERVICE CENTER. REMOVED ROLL SPOILER MIXER BACK ASSEMBLYNov 6, 2006 · N951QS · Cessna 750SDR CA061026002Bearing · jammed(CAN) DURING THE C CHECK INSPECTION, NR 5 BEARING ON 8 IN A WING AILERONS SYSTEME CABLE FAIRLEADS WAS FOUND JAMMED AND FLAT SPOTTED. ALL CABLES PASSING THRU THE FAIRLEAD HAVE TO BE REPLACE DUE TO THE CHAFFING IN THE BEARING, THE WORSE ONE WAS THE CABLE P/N:827Oct 26, 2006 · Dhav DHC8102SDR DXTA200601687Bungee · wornTHE AILERON TRIM IS CALIBRATED WITH THE NO TAKEOFF MESSAGE HOWEVER IN LEVEL FLIGHT, FUEL BALANCED RECEIVED AN AMBER L WING DOWN TRIM. WHICH YOU TRIM TO EXTINGUISH MESSAGE. THE ROLL TRIM INDICATOR IS BEYOND HALF TRAVEL. REPLACED AILERON FEEL BUNGEE WITH NEW Oct 26, 2006 · N941QS · Cessna 750SDR UPS06M48338Control System · inoperativeATB - AILERON DEFLECT DISAGREE MESSAGE. TAKEOFF DEFLECTED AILERON SYSTEM INOP. ITEM TRANSFERRED TO DMI M336464 PER MEL 27-13-2-0-1. DMP 27-13-2 C/W. PLACARD INSTALLED. REMOVED AND REPLACED WIRES 24-18 BL & 24-18 RD PER AMM 20-30-09-2. CHECKS GOOD PER AMM Oct 26, 2006 · N283UP · Doug MD11FSDR CA061025003Cable · broken(CAN) FINDINGS DURING C-CHECK INSPECTION IN AREA WING STA 171, AFT SPAR, LT AND RT REVEALED HEAVILY CHAFED AILERON CABLES IN PULLEY AREA AT WING BS 171. ON RT SIDE THE CABLE WAS SEVERELY DAMAGED AND ONLY A PART OF ONE STRAND WAS LEFT INTACT. THE CABLE IS OF TYOct 20, 2006 · Dhav DHC8301SDR UPS06M48240Warning Message · illuminatedATB - LEVEL 2 "AILERON DEFLECT DISAGREE" UPON CLEAN UP AFTER T/O. FOLLOWED CHECKLIST PROCEDURES AND WHEN COMPLETED, THE LEVEL 2 ALERT RETURNED. FUEL WAS DUMPED AND A/C RETURNED TO ANC. DEFERRED PER MEL 27-13-2-01-1, PLACARD INSTALLED, M335539. DMP 27-13-2 Oct 12, 2006 · N281UP · Doug MD11FSDR 2006UALA01951Motor · faulted"AIL LOCK" LIGHT WITH ASSOCIATED "AILERON LOCKOUT" EICAS ADVISORY LEVEL MESSAGE DISPLAYED DURING HIGH SPEED FLIGHT. CONFIRMED RT AILERON LOCKOUT ACTUATOR BAD. REPLACED PER MM27-11-44. FINAL CHECK GOOD. RETURN AC TO SERVICE. DAMAGED ACTUATOR MOTOR. SUSPECOct 4, 2006 · N648UA · Boeing 767322SDR NSVA200600166Control Cable · out of adjustLIGHT TO MODERATE VIBRATION IN FLIGHT CONTROLS (YOKE) WHEN FLAPS 15 SELECTED. FOUND AILERON CABLE TENSIONS TO BE LOW AND READJUSTED CABLE TENSIONS IAW MM 27-11-00-2. PERFORMED RANGE OF MOVEMENT CHECK IAW MM 27-10-00.Oct 3, 2006 · N252CJ · Saab 340BSDR DL76L060788Mechanism · malfunctionedDURING FLIGHT CONTROL CHECK AILERONS APPEARED STIFF RETURNED TO GATE FOR REPAIRS. EXAMINED ALL BEARINGS IN THE AILERONS AND WHEEL WELLS INBOARD AND OUTBOARD AILERON DROOP MECHANISM FEEL MECHANISM TORQUE CONTROL RODS AILERON LOCKOUT MECHANISM AILERON OVERRRIDESep 27, 2006 · N190DN · Boeing 767332SDR IXXA06SMN319SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD AILERON LEADING EDGE SKIN CRACKED AT STATION XD525.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFACE. APPLIED SEALANT TO FAYING SURFACESep 25, 2006 · N825BX · Doug DC871FSDR RAIA00609019Control Cable · wornDURING A FLEET WIDE INSPECTION OF THE AILERON CONTROL CABLES, ONE OF THE RT AILERON CONTROL CABLES WAS FOUND TO BE WORN AT THE RT PRESSURE SEAL. MAINTENANCE REMOVED AND REPLACED THE CABLE.Sep 13, 2006 · N802HK · Emb EMB145SDR RAIA00609020Control Cable · wornDURING A FLEET WIDE INSPECTION OF THE AILERON CONTROL CABLES, THE RT AILERON CONTROL CABLE WAS FOUND TO BE WORN AT THE POINT WHERE IT TRANSITIONS FROM THE PRESSURIZED VESSEL TO THE WING ROOT (PRESSURE SEAL). MAINTENANCE REMOVED AND REPLACED THE CABLE.Sep 13, 2006 · N809HK · Emb EMB145SDR RAIA00609018Control Cable · frayedDURING UNASSOCIATED MAINTENANCE, LT AILERON CONTROL CABLE WAS FOUND TO BE FRAYED WERE CABLE TRANSITIONS THROUGH THE PRESSURIZED VESSEL. MAINTENANCE REMOVED AND REPLACED THE CABLE.Sep 12, 2006 · N802HK · Emb EMB145SDR QXEA200602417Aileron · bindingSEA FLIGHT NR 2212 - AILERONS BINDING. MAINTENANCE REPLACED LEFT AILERON. OPERATIONAL CHECK FLIGHT GOOD. AIRCRAFT RETURNED TO SERVICE.Sep 11, 2006 · N364PH · Dhav DHC8202SDR HALA0600692Warning System · malfunctionedETOPS SIGNIFICANT SYSTEM - ON CLIMB-OUT AILERON LOCKOUT LT ILLUMINATED AT 300KTS. REMAINED ON REST OF THE FLT. ACCOMPLISHED FIM 27-11-00, FIG 104. ALL PASS, NO DEFECTS NOTED. OK FOR SERVICE.Sep 9, 2006 · N583HA · Boeing 767300SDR SWIA200618238Link · corrodedRIGHT AILERON FLUTTER DAMPNER SHEAR LINK IS CORRODED. REPLACED RIGHT AILERON FLUTTER DAMPNER SHEAR LINK IAW CRJ MM 27-15-05-400-802-A01.Sep 7, 2006 · N609SK · Cndair CL6002C10SDR FDKA200609251Control System · malfunctionedFDM 6113 PNS. AILERON SYSTEM 2 INOPERATIVE EICAS MESSAGE. MX RESET WITH THE CREW AND MESSAGE CLEARED.Sep 7, 2006 · N847MJ · Emb EMB145LRSDR 2006FA0001072Shaft · failedTHE HOLE IN THE SHAFT WAS MISDRILLED WHERE THE TAPER PIN ATTACHES IT TO THE SPROCKET, WHICH IS PART OF THE AILERON CONTROL SYSTEM. THE MISDRILLED HOLE ALLOWED THE PIN TO BREAK FREE OF THE SHAFT. THIS FAILURE CAUSED THE SEPARATION OF THE RT CONTROL WHEEL FROMSep 4, 2006 · N4112R · Piper PA32300SDR MASA200602203Unknown · malfunctionedASH 6132 CLT - GLD NOT ARMED CAUTION ON FINAL. MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.Aug 30, 2006 · N905J · Cndair CL6002D24SDR HALA0600640Control Module · unknownAILERON TRIM IS INTERMITTENT TO THE RIGHT-TRIM GETS STUCK OCCASIONALLY. REMOVED AND REPLACED CAPT AILERON/RUDDER TRIM CONTROL MODULE IAW AMM 27-10-07. OPS CHECK GOOD.Aug 29, 2006 · N475HA · Boeing 717200SDR CA060823001Pulley · seized(CAN) DURING A PHASE CHECK THE LT AILERON CABLE PULLEY WAS FOUND TO HAVE A SEIZED BEARING AND A WORN PULLEY. PULLEY AND BEARING REPLACED. A FLEET CAMPAIGN WILL BE INIATED TO CHECK ALL AILERON PULLEYS FOR FREEDOM OF MOVEMENT AND BEARING CHECK. TIMES: 36,972Aug 23, 2006 · Boeing 737522
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