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 COMA0360421Control Quadrant · corrodedFLIGHT 5845 DURING TAXI CHECK, AILERON SYSTEM FAILED TEST, BINDING NOTICED IN THE AILERON SYSTEM. REPLACED THE RIGHT AILERON QUADRANT.Sep 21, 2003 · N926CA · Cndair CL6002B19SDR 2003UALA00697Fitting · crackedRT AND LT AILERON PCU, IB FITTINGS CRACKED ON INBOARD SIDE. BOEING HAS RELEASED SB 777-57-0047 TO REPLACE AILERON FITTINGS WITH IMPROVED PART. AILERONS REPLACED.Sep 18, 2003 · N775UA · Boeing 777222SDR SWIA200312438Mount · malfunctionedAILERON SYSTEM HAS BUMP. MOVEMENT NOT SMOOTH. INSTALLED SERVICEABLE MOUNT, CAPSTAN AND SERVO MOTOR FOR AILERON CONTROL IAW 27-20-00. P/N 622-5734-002 S/N OFF 6176.Sep 17, 2003 · N213SW · Emb EMB120ERSDR CA030911001Servo · jammed(CAN) DURING TAXI ,THE ECAM MESSAGE AILERON BLUE SYSTEM JAM CAME ON UPON THE FLIGHT CONTROL CHECK BY THE FLIGHT CREW. PROCEDURE PERFORMED AS PER CHECK LIST AND THE AIRCRAFT RETURNED TO THE GATE DUE TO HARD DEFLECTION OF CONTROL WHEEL AND UNABLE TO DETERMINE MSep 10, 2003 · Airbus A310300SDR SIMA200325307Selector · malfunctionedEVV - FLT 4010 - DURING APPROACH CREW REPORTED A FLAP FAIL MESSAGE. AFTER SELECTING FLAPS TO 45 DEGREES FLAPS STUCK AT 38 DEGREES EVEN WITH FLAP HANDLE AT 0 DEGREES. PERFORMED GO AROUND DURING WHICH AIRSPEED INCREASED TO APPROX 180KTS. PERFORMED FLAP FAIL PRSep 8, 2003 · N628AE · Emb EMB145LRSDR SWAA032016Spring · wornAILERONS SLUGGISH WHEN TURNING FROM EITHER DIRECTION. REMOVED AND REPLACED AILERON FEEL AND CENTERING MECHANISM SPRINGS PER MM.Sep 8, 2003 · N333SW · Boeing 7373H4SDR 2003FA0000888Control Cable · brokenRT AILERON OUTBOARD FORWARD CABLE WAS FOUND BROKEN AT OUTBOARD PULLEY LOCATION. PILOT NOTICED AIRCRAFT ROLLING TO RIGHT. LOOKED OUT WINDOW AND FOUND RT AILERON DEFLECTED UP APPROXIMATELY 2 INCHES FROM NEUTRAL POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. UPON VISep 8, 2003 · N651EJ · Cessna 650SDR ASOA03420Control Quadrant · dirtyDURING CLIMB-OUT FROM DFW-MOB, THE CREW EXPERIENCED THE AILERONS SHOWING SIGNS OF BINDING WHEN INITIATING LEFT TURNS. WITH SUFFICIENT INPUT THE AILERON POPPED FREE AND THE AIRCRAFT JERKED LEFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDSep 7, 2003 · N842AS · Cndair CL6002B19SDR AUS20030908Aileron · malfunctioned(AUS) AILERON CONTROL SYSTEM NOTCHY' WITH A CONSIDERABLE DEAD BAND IN THE CENTRE.Sep 5, 2003 · Boeing 737400SDR CA030918002Bearing · brinelled(CAN) SNAPPING NOISE HEARD WHEN AILERON MOVED. BEARING AREAS ON CONTROL TUBES FRONT OF FIREWALL FOUND SEVERELY BRINELLED.Aug 28, 2003 · Cessna 177SDR CA030930003Actuator · failed(CAN) DURING SCHEDULED MAINTENANCE AN OPERATIONAL CHECK OF THE ROLL SYSTEM DISCONNECT WAS PERFORMED IAW MFG MRB TASK 2760/02. IT WAS DISCOVERED THAT AILERON TRAVEL WAS RESTRICTED AT THE FULL LT WING DOWN SELECTION CAUSING THE ROLL SYSTEM DISCONNECT CLUTCH TO DAug 27, 2003 · Dhav DHC8*SDR DXTA200300094Bungee Cylinder · out of adjustAILERON CONTROL BINDING WORSE TO THE RIGHT, TAKES EXCESSIVE RIGHT WING DOWN TRIM AT HIGH SPEEDS. - ADJUSTED LT PCU ACTUATOR INPUT BUNGEE TO ELIMINATE FORCE FIGHT CONDITION. PERFORMED ADJUSTMENT IAW MFG 750 MM CHAPTER 27-10-00, OPS CHECKED GOOD.Aug 19, 2003 · N942QS · Cessna 750SDR 08010304Bearing · looseLDC873FT AILERON WAS REMOVED FOR OTHER MAINTENANCE. WITH THE AILERON REMOVED IT WAS DISCOVERED THAT THE BEARING MOUNTED IN THE ROLL TRIM MOTOR ASSY. (P/N-12546-001) WAS LOOSE. THIS BEARING IS INSTALLED WITH A LIQUID LOCKING PRODUCT AND SUBJECTED TO A LOAD TESAug 13, 2003 · N747C · Univar 1083SDR C1HA200381028Mount · crackedLT INBOARD AILERON TAB MOUNT, CENTER AND OUTBOARD FITTINGS CRACKED.Aug 13, 2003 · N681CA · Boeing 7272S7SDR ARWA20030803O-Ring · wornLOG PAGE 110832. DISCREPANCY: AT TOP OF DESCEND LOSS OF HYDRAULIC FLUID AND PRESSURE; COMPLETED ABNORMAL HYDRAULIC LANDING CHECKLIST. REMOVED AND REPLACED RT AILERON POWER ACTUATOR HYDRAULIC O-RINGS TO SWIVEL VALVE IAW DC8 MM 27-14-01. PERFORMED LEAK CHECKAug 13, 2003 · N8969U · Doug DC862SDR 2003FA0000850Bearing · bulgedDURING SPECIAL INSPECTION OF THE AIRCRAFT REVEALED THAT THE BEARING ON THE LT AILERON LEVER ASSY IS SHOWING SIGNS OF BULGING . PROBABLE CAUSE IS DESIGN OF LEVER ASSY. THE AMOUNT OF USE OF THIS SYSTEM. REDESIGN OR REPLACE BEARING OF A HIGHER QUALITY.Aug 11, 2003 · N865AF · Grob G120ASDR CA030817001Spring · broken(CAN) WHILE TOWING THE AIRCRAFT TO ITS PARKING SPOT, A BANG WAS HEARD. THE AILERONS DEFLECTED FULL SCALE LT. THE AILERON AND RUDDER WERE NO LONGER INTERCONNECTED. ONE OF THE SPRINGS WAS FOUND TO HAVE BROKEN OFF AT THE ATTACHMENT POINT. WHILE REPLACING THE SPAug 8, 2003 · Grob G115CSDR 2003FA0000917Control Cable · mismanufacturedNEW CABLE WAS .5 INCH TOO SHORT.Aug 6, 2003 · N110MH · Braero BAE125800ASDR CA030922002Pcu · jammed(CAN) DURING DESCENT, THE CREW RECEIVED A 'OB SPOILERON' CAUTION AND 'OB FLIGHT SPOILER' CAUTION MESSAGES.THE MDC REPORTED THE LT OUTBOARD MFS PCU JAM. CREW DECLARED AN EMERGENCY AND LANDED SAFELY WITH NO OTHER INCIDENTS REPORTED. FOLLOWING REPLACEMENT OF THAug 3, 2003 · Cndair CL6002C10SDR DL764030717Pcu · unserviceableRT INBOARD AILERON, OUTBOARD PCU BINDING. PCU BROKEN AT ROD END. AUTOPILOT LIGHT COMES ON DURING TURN AND DESENT. REPLACED PCUAug 3, 2003 · N845MH · Boeing 767432ERSDR QXEA200300877Warning System · activatedPDX-ON FLIGHT NUMBER 2437, CONFIG AILERON WARNING MESSAGE APPEARED. ABORTED TAKEOFF AND MESSAGE DISAPPEARED AFTER 1-2 SECONDS. MDC HAS NO REPORTS FOR AILERON TRIM SYSTEM. PERFORMED FAULT CONFIRM OF AILERON TRIM SYSTEM. OPERATIONAL TEST OF AILERON SYSTEM GOOD. Jul 24, 2003 · N614QX · Cndair CL6002C10SDR COMA0360329Aileron · bindingFLIGHT 5378 CREW REPORTED "AILERONS BINDING". COULD NOT DUPLICATE - NO AILERON BINDING NOTED - C/W COMAIR EO 27-075 FOR TROUBLESHOOTING.Jul 18, 2003 · N712CA · Cndair CL6002B19SDR SWIA200312197Seal · tornRIGHT AILERON IS UP INFLIGHT, REQUIRES 5 PERCENT LEFT RUDDER TRIM TO CENTER SLIP/SKID INDICATOR FOR STRAIGHT AND LEVEL FLIGHT. FOUND SEAL UNDER AILERON RT SIDE TO BE TORN. REPLACED TORN SEAL. OPS CHECKS GOOD.Jul 17, 2003 · N413SW · Cndair CL6002B19SDR 0301319862Control Cable · bindingCREW EXPERIENCED SIGNIFICANT BINDING OF THE AILERONS IMMEDIATELY AFTER TAKEOFF. AS AIRSPEED INCREASED, THE CONTROLLABILITY IMPROVED AND LESS FORCE WAS NEEDED TO MOVE THE CONTROL YOKE. FLIGHT RETURNED TO AN UNEVENTFUL LANDING BACK AT DTW. MAINTENANCE CONFJul 16, 2003 · N771NC · Doug DC951SDR CA030806008Actuator · malfunctioned(CAN) EICAS MSG, AILERON LOCKOUT. OCURRED AT 10,000 FT AT 250 KTS (APPROACH). RT OUTBOARD AILERON LOCKOUT ACTUATOR REPLACED AS PER MM CHECKS SERVICABLEJul 12, 2003 · Boeing 767233SDR AUS20030716Cable · misinstalled(AUS) AILERON CROSSOVER CABLE LOCATED IN RT WING WORN FLAT IN AREA WHERE CABLE RUNS ON FAIR LEAD. CABLE WAS INCORRECTLY ROUTED. PERSONNEL/MAINTENANCE ERROR.Jul 8, 2003 · Cessna 172RSDR IMJ2003F00000Actuator · restrictedCREW REPORTS ROLL CONTROL STIFF OR BINDING ON APPROACH. FOUND RIGHT AILERON ACTUATOR CAUSING PROBLEM. SYSTEM CHECKED FREE UNTIL HYDRAULIC PRESSURE APPLIED, THEN RESTRICTION NOTICED UPON QUICK APPLICATION OF INPUT. UNIT CURE DATE OF 4Q77, TNS/TSO UNK 15150.4Jul 3, 2003 · N33PJ · Gulstm G1159SDR USAASB03098Control Cable · brokenON CLIMB-OUT FROM ATL, EN ROUTE TO CLT, CREW REPORTED THE AIRCRAFT REQUIRED EXCESSIVE AILERON TRIM. CREW NEEDED ALMOST FULL LEFT AILERON CONTROL WHEEL DEFLECTION TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. FLIGHT RETURNED TO FIELD AT ATL AND LANDED WITHOUT FURTHEJul 2, 2003 · N383US · Boeing 7373B7SDR 2003FA0000783Barrel · damagedUPON INSPECTION FOUND TURN BARREL THAT HAS GROOVE FOR CLIPS SPLIT LOCATION UPPER RT ALIRON TURNBUCKLE ONLY FOUND THESE STYLE TURN BARRELS THAT DONT REQUIRE SAFETY WIRE ON LATER AIRCRAFT. FOUND THIS BEFORE AND COULD CAUSE LOSS OF AILRON CONTROL IF BROKEN.Jul 1, 2003 · N54182 · Piper PA18150SDR CA030627001Control Cable · chafed(CAN) DURING A ROUTINE MAINTENANCE INSPECTION, IT WAS OBSERVED THAT THE RT INBOARD AILERON CABLE ASSY WAS CHAFED AND WORN AT THE CABLE GUIDE. THE CABLE WAS REMOVED & NEW CABLE INSTALLED IAW MM 27-10-71. ADJUSTMENT AND FUNCTIONAL CHECK CARRIED OUT SERVICEABLE IJun 26, 2003 · Boeing 727225SDR IU62003F00031Manifold · crackedCRACKED MANIFOLD. OVER PRESSURIZED FILTER BOWL. (NR 178182)Jun 13, 2003 · Boeing 737*SDR COMA0360274Aileron · bindingFLIGHT 5523 AILERON BINDING IN FLIGHT. COULD NOT DUPLICATE, INSPECTED AILERON CONTROL PATH AND FOUND NO DEFECTS.Jun 12, 2003 · N708CA · Cndair CL6002B19SDR UPS03240919Buss Tie · corrodedINSPECTION TYPE: C&SI, RT I/B AILERON BUS QUADRANT CORRODED IN CABLE GROOVE. RIGHT I/B AILERON BUS QUADRANT REPLACED AS REQUIRED UP TO STEP D6 INCLUSIVE IAW MM 27-10-56.Jun 11, 2003 · N940UP · Boeing 727185CSDR DL76L030537Bearing · failedDURING TAXI OUT AILERONS WERE STIFF AND BINDING WOULD NOT RETURN TO CENTER WITH OUT EXTRA FORCE. DISC CTL RD AT CA DRUM-RT LCCA OUTPUT/RT LCCA TORQ TUBE.FIM 27-11-00 TBL10. T/S PER FIM 27-11-00 FIG 106 STEP 2. F/O CONT WHEEL STIFF. DISC UPPER/LWR INPUT ROJun 10, 2003 · N177DN · Boeing 767332SDR N3571YControl Wheel · strippedON ROUTINE SKYDIVING FLIGHT, THE APPROPRIATELY RATED AND QUALIFIED PILOT ENTERED A CROSS CONTROL MANEUVER TO CLOSE CABIN DOOR. UPON RETURNING TO NORMAL FLIGHT THE PIC EXPERIENCED LOSS OF AILERON CONTROL EXHIBITED BY CONTROL WHEEL ROTATING 360 DEGREES WITH NO Jun 10, 2003 · N3571Y · Cessna 182FSDR CA030611002Pcu · broken(CAN) DURING LANDING THROUGH APPROXIMATELY 60 KNOTS, AIRCRAFT EXPERIENCED A COMPLETE LOSS OF 'A' SYSTEM HYDRAULICS. (NOTE: 'A' PUMPS ON WITH LOW PRESSURE LIGHTS ILLUMINATED - MAX 1.5 MINUTES) MAINTENANCE INSPECTION REVEALED POSITION NR 1 LOWER AILERON PCU FILTJun 9, 2003 · Boeing 737281SDR SWAA031294Control Cable · wornNO DEFLECTION ON RT AILERON DURING CONTROL INPUT. REMOVED AND REPLACED (3 EA) AILERON BUS CABLES, ABSB-4, ABSA-3 AND ABSB-3 PER MM.Jun 8, 2003 · N620SW · Boeing 7373H4SDR 2003FA0000611Control Cable · frayedBROKEN STRANDS ON LEFT BALANCE CABLE WAS FOUND DURING NORMAL MAINTENANCE. CABLE HAS BROKEN STRANDS AT POINT WHERE CABLE WAS INBOARD PULLEY AT WING ROOT. PULLEYS SHOW NO SIGN OF WEAR AND TURN FREELY. THE TOTAL TIME ON THESE CABLES WERE FROM 1049 TO 2058. PROBAJun 5, 2003 · N772FT · Piper PA28R201SDR 2003F00530Balance Weight · detachedON DESCENT AT YIP, WITH TWO PAX ONBOARD, PILOTS EXPERIENCED DIFFICULTY IN TURNING A/C LATERALLY TO THE RT. PILOTS WERE ABLE TO CONTROL A/C AND MAKE A NORMAL LANDING. THE LOCAL AREA TECH REP FOR THE AIRFRAME MANUFACTURER WAS ABLE TO VERIFY THAT THE AILERON'S Jun 2, 2003 · N50KC · Gulstm GULFSTREAMGVSDR 6203N50KCBalance Weight · detachedON DESCENT, EXPERIENCED DIFFICULTY IN TURNING ACFT LATERALLY TO RIGHT. PILOTS WERE ABLE TO CONTROL ACFT AND MAKE A NORMAL LANDING. INITIAL INVESTIGATION BY PILOTS REVEALED A LOUD CLUNK WHEN LEFT AILERON WAS MOVED PHYSICALLY. T/R WAS ABLE TO VERIFY THAT AILEJun 2, 2003 · N50KC · Gulstm GULFSTREAMGVSDR CA030528009Cable · frayed(CAN) DURING AN EVENT NR 3 INSPECTION THE LT AILERON BALANCE CABLE WAS FOUND TO BE FRAYED WHERE IT CROSSES THE INBOARD PULLEY AT THE WING ROOT. THE PULLEY WAS REMOVED AND INSPECTED AND THE BEARING WAS FOUND TO BE IN GOOD WORKING ORDER, THE BEARING WAS LUBED May 27, 2003 · Piper PA44180SDR 2003FA0000651Control Cable · brokenBOTH LT AND RT FORWARD AILERON CABLES HAVE BROKEN WIRES. AT SPOT WHERE CABLE RIDES ON INBOARD PULLEY, NEAR WING ROOT. PULLEY TURNS FREELY. FOUND ON ROUTINE MAINTENANCE. PROBABLE CAUSE MISALIGNED PULLEY FROM FACTORY.May 22, 2003 · N880FT · Piper PA44180SDR CA030516001Controller · jammed(CAN) SHORTHLY AFTER TAKE OFF THRU FL250 THE AILERON SYSTEM JAMMED, FLIGHT CREW SUSPECTED ICE AS THERE WASHEAVY RAIN WHILE DEPARTING, THE FIRST OFFICER SIDE WAS AFFECTED, PILOTS SIDE WAS OK (AFTER CONTROL COLUMN DISCONNECT INVESTIGATION UNDERWAY,May 15, 2003 · Cndair CL6002B19SDR ASOA03201Link · wornFLT 4690 - DURING CLIMB-OUT FROM ATL-YUL, AT APPROXIMATELY 5,000 FEET THE CREW NOTICED A CYCLICAL VIBRATION IN THE AIRFRAME WITH THE AIRCRAFT VIBRATING ABOUT 45 TO 60 SECONDS EACH TIME, FOR ABOUT 1 TO 2 SECONDS, WHICH WAS VERY DEEP IN FREQUENCY. WHILE THE CREMay 13, 2003 · N829AS · Cndair CL6002B19SDR 2003FA0000477Control Cable · chafedDURING A ROUTINE INSPECTION, THE RIGHT AILERON BALANCE CABLE (P/N 0510105-362) WAS FOUND CHAFING ON A FAIRLEAD LOCATED MIDWAY THROUGH THE FLAP WELL AREA. THE CABLE IS EXTREMELY DIFFICULT TO EXAMINE THOROUGHLY WHILE INSTALLED. A BORESCOPE CAN AID IN VIEWING THEMay 13, 2003 · N472ER · Cessna 172RSDR 2003FA0000471Control Cable · chafedDURING A ROUTINE INSPECTION, THE LEFT AILERON BALANCE CABLE (P/N 0510105-364) WAS FOUND CHAFING ON A FAIRLEAD LOCATED MIDWAY THROUGH THE FLAP WELL AREA. THE CABLE IS EXTREMELY DIFFICULT TO EXAMINE THOROUGHLY WHILE INSTALLED. A BORESCOPE CAN AID IN VIEWING THE May 13, 2003 · N472ER · Cessna 172RSDR 2003FA0000472Control Cable · chafedDURING A ROUTINE INSPECTION, THE RIGHT AILERON BALANCE CABLE (P/N 0510105-365) WAS FOUND CHAFING ON A FAIRLEAD LOCATED MIDWAY THROUGH THE FLAP WELL AREA. THE CABLE IS EXTREMELY DIFFICULT TO EXAMINE THOROUGHLY WHILE INSTALLED. A BORESCOPE CAN AID IN VIEWING THEMay 13, 2003 · N441ER · Cessna 172RSDR 2003FA0000474Control Cable · chafedDURING A ROUTINE INSPECTION, THE RIGHT AILERON BALANCE CABLE WAS FOUND CHAFING ON A FAIRLEAD LOCATED MIDWAY THROUGH THE FLAP WELL AREA. THE CABLE IS EXTREMELY DIFFICULT TO EXAMINE THOROUGHLY WHILE INSTALLED. A BORESCOPE CAN AID IN VIEWING THE AREA MORE ACCURATMay 13, 2003 · N472ER · Cessna 172RSDR 2003FA0000473Control Cable · chafedDURING A ROUTINE INSPECTION, THE LEFT AILERON BALANCE CABLE WAS FOUND CHAFING ON A FAIRLEAD LOCATED MIDWAY THROUGH THE FLAP WELL AREA. THE CABLE IS EXTREMELY DIFFICULT TO EXAMINE THOROUGHLY WHILE INSTALLED. A BORESCOPE CAN AID IN VIEWING THE AREA MORE ACCURATEMay 13, 2003 · N441ER · Cessna 172RSDR 2003FA0000559Bearing · failedDURING INSPECTION OF AIRCRAFT, FOUND BEARING TO BE FAILING. RETAINING CLIP AND SEAL WERE BEING FORCED OUT OF BEARING.May 12, 2003 · N867AF · Grob G120A
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