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 UALA2011032901492Actuator · faultyTHE "AIL LOCK" LIGHT ON AT LOW SPEED. EICAS MSG AILERON LOCKOUT DISPLAYED. OUTBD AILERONS DID NOT INDICATE NORMAL -LOCKED OUT- BOTH. CREW COMMENTS: AILERON LOCKOUT DISPLAYED AT 220 KNOTS FL140. REPLACED ACT PER MM.Mar 28, 2011 · N658UA · Boeing 767322SDR UALA2011032801486Servo Control · malfunctionedAIL SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. - F- CTL. TROUBLESHOOTING FAULTS R G AIL POS XDCR 33CES. DEACTIVATED RG AILERON SERVO 33CES. REPLACED RIGHT WING AIL, SERVO CONTROL 33CE2.Mar 27, 2011 · N492UA · Airbus A320232SDR MASA2011033002283Power Supply · faultyRUDDER/AILERON TRIM MOVE UNCOMMANDED. MX REMOVED AND REPLACED RUD/AIL TRIM PWR SUPPLY, OPS NORMAL.Mar 27, 2011 · N956LR · Cndair CL6002D24SDR UALA2011032801465Aileron Sys · bindingLEFT AILERON STUCK ALMOST JAMMED AT APPROX 2 TO 3 DEGREES DEFLECTION LF YOKE RT SIDE OK PER INBD CAPTAIN AILERON SLIGHTLY HEAVY IN LEFT TURN AT SLOW SPEED, LUBED FEEL AND CENTERING MECHANISM, ALL FORCES WITHIN LIMITS.Mar 26, 2011 · N676UA · Boeing 767322SDR UALA2011030901146Pca · malfunctionedRIGHT AILERON FLOATS WITH RT HYD SYSTEM DEPRESSURIZED. REPLACED AND OPS CHECKED THE RT INBD AILERON PCA PER MM. OPS CHECKED GOOD.Mar 8, 2011 · N658UA · Boeing 767322SDR UALA2011030801128Actuator · bindingAILERON LOCKOUT DESCENDING OUT OF 10000 240 KNOTS. RT OB AILERON LOCKOUT ACTUATOR PREVIOUSLY REPLACED. STILL FAULTING ACTUATOR. WORKING REPLACEMENT OF ACTUATOR. REPLACED RIGHT OTBD AILERON LOCKOUT ACTUATOR. CHECKED OK. AILERON LOCKOUT FAULT AND HYD PRESSURE Mar 8, 2011 · N647UA · Boeing 767322SDR UALA2011030901152Actuator · faultyAILERON LOCKOUT EICAS WITH ASSOCIATED OVERHEAD LIGHT ILLUMINATED ON ARRIVAL. REPLACED RIGHT OTBD AILERON LOCKOUT ACTUATOR PER MM.Mar 7, 2011 · N647UA · Boeing 767322SDR 2011FA0000141Control Cable · frayedTHE AILERON CABLE WAS FRAYED AND WORN SHOWING BROKEN STRANDS AT FUSELAGE STATION 65.33 WHERE THE CABLES PASS THOUGH THE 3 CEILING MOUNTED NYLON PULLEYS.Mar 1, 2011 · N375ER · Cessna 172SSDR IPXA1M64998Actuator · deactivatedAILERON DEFLECT DISAGREE ALERT ON TAKEOFF CLIMB. FOUND LT OTBD AILERON IS OUT OF LIMITS AT NEUTRAL POSITION. ADJUSTED LT OTBD DEFLECT ACTUATOR IAW AMM 27-16-02-4. CHECKS OK. PRECAUTIONARILY DEACTIVATE T/O DEFLECTED AILERON SYS IAW MEL. R & R INBD AILERON DFeb 27, 2011 · N273UP · Doug MD11FSDR J7SA20110225001Seal · dirtyCLIMBING THROUGH APPROX FL280 THE AMBER AP AIL MISTRIM CAS ILLUMINATED, DISENGAGED AUTOPILOT AND EXCESSIVE FORCE WAS REQUIRED TO MOVE AILERONS. THE EXCESSIVE FORCE DECREASED WHEN ALT DECREASED. R & R LT & RT AILERON BRUSH SEALS.Feb 25, 2011 · N438FX · Lear 45LEARSDR HALA2011022100117Actuator · malfunctionedETOPS SIGNIFICANT SYSTEM - AILERON LOCKOUT AT 310KTS LASTED FOR 2 MIN(CLIMB OUT). T/S PER FIM 27-11-00 FIG. 104.LEFT LOCKOUT ACTUATOR FAILED TWICE DURING CHECK. REMOVED AND REPLACED SAME PER AMM 27-11-44, SYS CHECKED OK.Feb 21, 2011 · N597HA · Boeing 767300SDR UIEA2011021100049Control Cable · wornFWD LT AILERON CONTROL CABLE AS-3 WORN OUT. REPAIRED IAW AMM 27-11-00 REV 70. ADJUSTMENT TEST.Feb 11, 2011 · N409MC · Boeing 74747UFSDR UIEA2011021100048Control Cable · wornFWD LT AILERON CONTROL CABLE AB-9 WORN OUT. (IAW AMM 27-11-00. ADJUSTMENT TEST.)Feb 11, 2011 · N409MC · Boeing 74747UFSDR UALA2011021000701Pcu · leakingLT INBD FLAPERON PCU LEAKING BEYOND LIMITS. REPLACED LT INBD FLAPERON POWER CONTROL UNIT IAW MM. UNIT WITHIN TOLERANCE.Feb 9, 2011 · N783UA · Boeing 777222SDR V0XR201102030017Control Cable · corrodedLEFT AILERON CONTROL CABLES ARE WORN BEYOND LIMITS. R & R CABLE.Feb 3, 2011 · N825HK · Emb EMB145LRSDR V0XR201102030016Control Cable · corrodedLEFT AILERON CONTROL CABLES ARE WORN BEYOND LIMITS. R & R CABLE.Feb 3, 2011 · N825HK · Emb EMB145LRSDR V0XR201102030015Control Cable · corrodedAILERON CONTROL CABLES ARE WORN BEYOND LIMITS. R & R CABLES.Feb 3, 2011 · N825HK · Emb EMB145LRSDR V0XR201102030014Control Cable · corrodedAILERON CONTROL CABLES ARE WORN BEYOND LIMITS. R & R CABLES.Feb 3, 2011 · N825HK · Emb EMB145LRSDR V0XR201102030013Control Cable · corrodedAILERON CONTROL CABLES ARE WORN BEYOND LIMITS. R & R CABLES.Feb 3, 2011 · N825HK · Emb EMB145LRSDR V0XR201102030012Control Cable · corrodedAILERON CONTROL CABLES ARE WORN BEYOND LIMITS. R & R CABLES.Feb 3, 2011 · N825HK · Emb EMB145LRSDR UALA2011012600424Roller · wornDURING FLT CONTROL CHECK AILERON STIFF AT MID ROLL. SOMETIMES LT SOMETIMES RT SIDE. FOUND AILERON CENTERING ROLLER WORN & FLATSPOTTED. REPLACED ROLLER IAW IPC. OPS CHECKED GOOD. CONTROL WHEEL SMOOTH FULL TRAVEL.Jan 25, 2011 · N676UA · Boeing 767322SDR UALA2011012500408Aileron Sys · out of rigACFT IN LEVEL FLT SYMMETRICAL EPR AND FUEL IS BALANCED. TRIM L2.5. FOUND ALL 4 AILERON NEUTRALS OUT OF LIMITS. ADJUSTED TO ALL 4 IAW MM. REMOVED FLIGHT DECK PINS, OPS CHECKED OK.Jan 23, 2011 · N851UA · Airbus A319131SDR 2ARF201101005Plate · brokenCAPTAIN REPORTED THAT DURING CRUISE, ACFT REQUIRED 4 GRADES OF AILERON COMPENSATOR TO MAINTAIN STRAIGHT AND LEVELED FLIGHT. DURING MX REVISION, THE SPIRAL DRIVE PLATE WAS DETECTED BROKEN; SO THE SPIRAL DRIVE PLATE WAS REPLACED IAW MM 27-10-07, TESTED CORRECT.Jan 15, 2011 · N583MD · Doug MD83SDR UALA2011011200202Control Unit · faultySTATUS MESSAGE FLIGHT CONTROL SYS SHOWING ON LOWER EICAS. REPLACED RIGHT WING OUTBOARD AILERON POWER CONTROL UNIT AS PER AMM. AFTER AILERON ADJUSTMENT (RIGGING), OPERATIONAL TEST AND RIGHT AILERON ACTUATOR CONFIDENCE TEST, NO FURTHER MESSAGES PRESENT. ALL TESJan 12, 2011 · N774UA · Boeing 777222SDR HALA2011010800024Actuator · failedETOPS SIGNIFICANT SYS - AILERON LOCKOUT EICAS CAME ON DURING DESCENT APPROX 10,OOO FT. T/S IAW FIM 27-11-00/101 NO FAULTS ON BOTH SAM IAW FIG 104A, CKD ALL CONNECTION FOUND NO FAULTS. DURING AILERON LOCKOUT TEST LT ACTUATOR APPEARS TO STALL. REPLACED SAME AJan 8, 2011 · N597HA · Boeing 767332SDR HALA2011010800022Warning Light · false activationETOPS SIGNIFICANT SYS - AIRLERON LOCKOUT EICAS MSG DISPLAYED AT 10000FT SPEED 250 KTS, EXTINGUISHED AT ABOUT 7000 FT AND 230 KTS. PERFORMED FIM 27-11-00/101, FIG 104 NO FAULTS OP'S CK GOOD.Jan 8, 2011 · N596HA · Boeing 767332SDR HALA2011010300005Warning Light · illuminatedETOPS SIGNIFICANT SYS - AILERON LOCKOUT EICAS ILLUMINATED DURING DESCENT THRU 10000 FT, SPEED 240 KTS, WENT OUT PASSING 4300 FT. T/S IAW FIM 21-11-00, FIG 104, RT SAM FAULTED RT ADC, RESET IAW BLOCK 25, FAULT CLEARED IAW BLOCK 57, SYS CKS OK, OK FOR SERVICE.Jan 3, 2011 · N597HA · Boeing 767332SDR CA101221012Disconnect Unit · failed(CAN) DURING A C CHECK INSPECTION ON THE AICRAFT, A FUNCTIONAL TEST OF THE AILERON DISCONNECT UNIT WAS PERFORMED. THE UNIT FAILED THE TEST. THE DEFECTIVE PART WAS REMOVED AND AN ACCESS PANEL ON THE UNIT WAS OPENED PER THE CMM AND FOUND BROKEN PIECES OF THE INTDec 20, 2010 · Dorner DO328300SDR DXTA2010122104370Switch · inoperativeROLL TRIM WORKED ON PRE FLIGHT AND POST FLIGHT, BUT DID NOT WORK IN FLIGHT. PERFORMED ROLL TRIM OPS TEST, NEUTRAL SWITCH CHECK - RT AND LT SIDES AND ROLL TRIM SEL SWITCH OPS CHECK. NO DISCREPANCIES NOTED. ALL WORK DONE IAW AMM 27-10-00.Dec 20, 2010 · N125QS · Raythn 400ARAYTHEONSDR BIGR12/15/10Control Cable · frayedDURING ANNUAL INSP THE LT AND RT AILERON CABLES (P/N MC0510105-262)WERE FOUND TO HAVE HALF OF THE WIRE STRANDS BROKEN AT A IDLER PULLEY INBD OF THE AILERON BELLCRANKS. BOTH CABLES WERE REPLACED AND ACFT WAS RERIGGED NO OTHER DEFECTS WERE NOTED.Dec 15, 2010 · N80CL · Cessna 172NSDR QXEA2010121600894Aileron Sys · out of rigLARGE AMOUNT OF LT WING DOWN AILERON TRIM TO MAINTAIN LEVEL FLIGHT, ALSO NOTED CONTROLS TURNED HARDER TO THE RT THAN THE LT. MX WAS UNABLE TO PIN RT TERMINAL QUADRANT WITHOUT PUSHING DOWN ON RT AILERON. FOUND RT AILERON SPLITTER TO AILERON TERMINAL QUADRANT Dec 12, 2010 · N414QX · Bombdr DHC8402SDR CA101202010Yoke · frozenACFT DEPARTED IN HEAVY PRECIPITATION ENROUTE. OAT 17 C AT DEPARTURE. APPROX 25 MIN AFTER TO AT 35,000 FT -60 OAT AP ENGAGED. CAS MESSAGE POSTED "AP TRIM IS RWD". TRIMMED ACFT TO LEVEL AT 41000 FT. PILOT DISCONNECTED AUTOPILOT AND MESSAGE CLEARED. USING NORMDec 1, 2010 · Bombdr BD7001A10SDR UALA2010111704261O-Ring · leakingLEFT WING INBOARD AILERON INBOARD POWER CONTROL ACTUATOR LEAKING HYD FLUID AT PRESSURE LINE UNION. REPLACED O-RING. PCA OP'S CHECK NORMAL AND NO LEAKS. CLEANED AS MUCH AS POSSIBLE HYD FLUID. MAY HAVE RESIDUAL FLUID AT NEXT LEG.Nov 16, 2010 · N672UA · Boeing 767322SDR 2010FA0001163Control Cable · frayed(U72S) DURING PASE III INSP FOUND RT AILERON CONTROL CABLES FRAYED AGAINST PN 0522647-10, FAIRLEAD ASSY, FWD OF AILERON AUTOPILOT SERVO. BOTH CABLES PN 0510105-362 AND 0510105-365 EFFECTED.Nov 9, 2010 · N5291W · Cessna 172SSDR 2010FA0001162Control Cable · frayed(U72S) DURING PHASE III INSP FOUND RT AILERON CONTROL CABLES FRAYED AGAINST PN 0522647-10 FAIRLEAD ASSY, FWD OF AILERON AUTOPILOT SERVO. BOTH CABLES PN 0510105-362 AND 0510105-365 EFFECTED.Nov 9, 2010 · N65956 · Cessna 172SSDR UALA2010110504104Actuator · leakingLT WING AFT OF PYLON SAIL TAIL AREA HAS EVIDENCE OF HYD LEAK. LEAK IS AT LT INBD AILERON INBD ACTUATOR ON ACT ROD SEAL. LEAK IS MEASURED AT 4 DROPS PER MIN. COMPLETED ACTUATOR REPLACEMENT.Nov 5, 2010 · N652UA · Boeing 767322SDR WRNA201000006Actuator · failedDURING CLIMB/CRUISE LEVEL 2 ALERT "AIL DEFLECTOR DISAGREE" ILLUMINATED. QRH (QUICK REF HANDBOOK) PROCEDURES FOLLOWED, LIGHT REMAINED ON. AIRCRAFT DUMPED APPROX. 48,400 LBS IF FUEL FOR APPROVED LANDING WEIGHT. A/C RETURNED TO FIELD. LANDING NORMAL. MX FOUNNov 2, 2010 · N950AR · Doug MD11FSDR UALA2010110104037Torque Tube · wornLEFT AILERON BINDS DURING FLT CONTROL CHECK WITH FLAPS 5 AROUND 6 UNIT. FOUND BEARING ON LEFT LATERAL CONTROL ACTUATOR INPUT CRANK WORN AND RUSTED. REMOVED LT LATERAL CENTRAL INPUT CRANK TORQUE TUBE ASSEMBLY. NOTE: CABLE GUIDE REMOVED UPPER BRKT. HANGING ON CNov 1, 2010 · N672UA · Boeing 767322SDR WRNA20100005Warning System · activatedAFTER T/O DURING CLIMBOUT FROM SKBO, LEVEL TWO (2) ALERT AFTER AILERON DEFLEC DISAGREEMENT LIGHT ON. AIR CREW FOLLOWED PROCEDURES AND DUMPED FUEL, APPROX. 46K LBS. AIRCRAFT RETURNED TO AIRFIELD, WITH NORMAL LANDING. MAINTENANCE INSPECTED AIRCRAFT, PLACED ITOct 26, 2010 · N950 · Doug MD11FSDR YENA20101018140Warning System · malfunctionedFLT 1784 BOG-MCO, AIR TURNBACK TO BOG DUE TO FLT CONTROL AIL 1 AND 2 FAULT ON ECAM. FLT CONTROL ALT LAW LOST. RESET ELAC 1 C/B B11 AND A01. PERFORMED OPS TEST REF AMM 27-14-00-710-001. AILERON HYD ACTUATION NO FAULTS FOUND. MCC VERIFIED ONE TIME OCCURENCE Oct 18, 2010 · N632JB · Airbus A320232SDR A6WA201040779Control Wheel · bindingON LANDING FELT AILERONS BINDING (HARD TO MOVE) AND DURING POST FLIGHT AILERON CHECK A MECHANICAL RATCHETING CAN BE FELT IN BOTH CONTROL WHEELS. R & R CAPTS CONTROL WHEEL SHAFT FWD AND AFT BEARINGS IAW AMM CH 27-11-01.Oct 17, 2010 · N432AW · Cndair CL6002B19SDR CA101013004Bolt · wrong partDURING A SERVICEABILITY CHECK, A RUBBING NOISE WAS NOTICED WHEN THE RT AILERON WAS MOVED TO IT`S FULL EXTENSION. FURTHER INVESTIGATION REVEALED THAT THE UPPER RT BOLT HOLDING THE ACTUATOR PLATE (PN 5565386-3) TO THE AILERON QUADRANT WAS RUBBING ON THE UPPER AIOct 12, 2010 · Cessna 550SDR CA101015003Actuator · failedDURING CRUISE, THE FLIGHT CREW NOTICED THAT THE AUTOPILOT COULDN`T KEEP THE ACFT LATERAL ATTITUDE LEVEL. THE AUTOPILOT WAS DISENGAGED AND THE PILOT IN COMMAND APPLIED PRESSURE ON THE CONTROL WHEEL AND THE SYS FREED UP. UPON ARRIVAL THE ACFT WAS REMOVED FROM Oct 7, 2010 · Cndair CL6002B19SDR MASA2010100601083Printed Ckt Board · defectiveAIL/RUD TRIM MOVES UNCOMMANDED. MX REMOVED & REPLACED POWER SUPPLY & PCB CARD AT JB10 JUNCTION BOX.Oct 4, 2010 · N514MJ · Cndair CL6002C10SDR CA100922003Control Cable · worn(CAN) DURANT UN INSPECTION DE TYPE C UN TECHNICIEN A DECOUVERT QUE DES CABLES D`AILERON ETAIENT USES PLUS QUE LA NORMALE DEUX DE CEUX -CI AVIENT ETE CHANGES L`AN DERNIER #215-92315-238 ET 215-92315-130 (TC# 20100922003)Sep 21, 2010 · Cndair CL2156B11215SDR UALA2010092103502Rod End · out of limitsAIRFRAME VIBRATION. ALL 4 ELEVATOR ROD ENDS ARE OUT OF LIMITS. LT ELEVATOR ROD ENDS INSTALLED. RT ROD ENDS INSTALLED. INSP ALL ELEV ROD ENDS FOR SAFETY AND SECURITY, OPS CHECKED ALL INDICATIONS NORMAL.Sep 21, 2010 · N823UA · Airbus A319131SDR UALA2010092003491Actuator · faulty"AIL LOCK" LT ON AT HIGH SPEED. EICAS MESSAGE "AILERON LOCKOUT" DISPLAYED. OTBD AILERONS INDICATED MOVEMENT, UNLOCKED, BOTH. LIGHT CAME ON FOR 5 MIN AND THEN WENT OUT. PERFORMED SAM BITE. NO FAULT BALL ON LT AND RT SAM. NO AILERON LOCKOUT STATUS MESSAGE ON Sep 19, 2010 · N658UA · Boeing 767322SDR HALA2010091700427Aileron Sys · malfunctionedETOPS SIGNIFICANT SYS - 2711XA09 - IN CRUISE, LT INBD AILERON INDICATES UPWARD DEFLECTION OF APPROX 2.5" RAIL IS NORMAL. ACFT TRIMMED ALL NORMAL (ZERO). VISUAL INSP CONFIRMED LT INBD AILERON DEFLECTED UPWARDS APPROX 2" AT OTBD EDGE, RT INBD AILERON FLUSH. PESep 17, 2010 · N593HA · Boeing 76733AERSDR SIMA201025603Unknown · malfunctionedON FLIGHT 3882 THE CREW REPORTED AN OCCASIONAL STICKING OR LAG/PLAY WITH AILERONS IN FLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE AND RELEASED ONLY FOR A FUNCTIONAL CHECK FLIGHT. THE FUNCTIONAL CHECK FLIGHT WAS SATISFACTORY. NO PARTS REMOVED OR REPLACED. Sep 11, 2010 · N526EA · Cndair CL6002C10SDR DXTA2010091304232Aileron Sys · bindingPLAY IN AILERON CONTROL & BINDING WHEN MOVING BOTH LT & RT OF NEUTRAL. BINDING NOTICABLE AT SPEEDS ABOVE 210 KIAS & BECAME WORSE AS SPEED INCREASED. AS SPEED DECREASED, BINDING & PLAY DECREASED. NOTHING ABNORMAL NOTICED DURING FLT CONTROL CHECK BEFORE & AFTESep 10, 2010 · N989 · Cessna 750
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