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 SWIA200719112Bearing · corrodedRIGHT AILERON INBOARD PCU OUTPUT LINK ASSEMBLY HAS CORRODED BEARING, FOUND AT C-CHECK. REPLACED RIGHT AILERON PCU LINK ASSEMBLY PER CRJ200 AMM 27-14-15-000-801.Sep 15, 2007 · N982SW · Cndair CL6002B19SDR FDKA200709471Control Cable · damagedFDM RON MCO - FLIGHT CONTROL YOKE BOTH SIDES HARD TO MOVE WITH GRINDING. MX INSPECTED CABLES AND PULLEYS. MX REMOVED AND REPLACED PULLEYS IN CARGO COMPARTMENT.Sep 15, 2007 · N853MJ · Emb EMB145LRSDR SIMA200725703Control Cable · out of adjustCREW NOTIFIED IN FLIGHT THAT FLIGHT CONTROLS STIFF AND AIRCRAFT FLY’S TAIL HEAVY DURING FLIGHT CONTROL CHECKS FOR BEFORE TAKEOFF FOUND PITCH AND ROLL TO BE STIFFENER THAN NORMAL. WITH PITCH TRIM PROPERLY SET FOR TAKEOFF (17 PAX AND 348 CARGO) AIRCRAFT WANTED Sep 13, 2007 · N724AE · Emb EMB135LRSDR DXTA200702465Servo · out of adjustAIRCRAFT WILL NOT FLY STRAIGHT WITH A/P AT FL360. AILERON TRIM FULL R. RUDDER TRIM .1250 L, SLIGHT LT TURN, FUEL BALANCED, .79M / FL240 A TRIM FULL R - RUD TRIM .1250 L, NO TURNS, FUEL BALANCED, 290 KTS / 10,000 FT A TRIM .5 R - RUD TRIM .1250 L, NO TURNSep 10, 2007 · N338QS · Cessna 680CESDR FDKA200709442Control Panel · inoperativeAILERON SYSTEM 1 CUT OUT SWITCH INOP. MX REPLACED FLIGHT CONTROL PANEL.Sep 4, 2007 · N828MJ · Emb EMB145LRSDR 2007UALA03616Rod End · wornLOW HUM WITH ASSOCIATED LOW VIBRATION ON C-P FLOOR IN CLIMB AND CRUISE. WORN SERVO ROD OF AILERON CONTROL SYSTEM. REPLACED L OUTBOARD AILERON SERVO ROD END. NO REPEATS SINCE ORIGINAL.Sep 3, 2007 · N432UA · Airbus A320232SDR COMA0760543Unknown · malfunctionedFLIGHT 5113 - ON CLIMB, BOX A ON PFD FLASHED 2-3 SECONDS, FOLLOWED BY AUTO-PILOT DISCONNECT. NOTICED STIFFNESS IN CONTROLS WHEN TURNING LEFT. RETURNED TO ATL. LANDED WITHOUT INCIDENT. PERFORMED EO-27-075, AILERON CONTROL PATH INSPECTION. NO FURTHER DEFECTAug 26, 2007 · N812CA · Cndair CL6002B19SDR 2007FA0000720Control Cable · frayedDURING A ROUTINE INSPECTION, THE AILERON BALANCE CABLE WAS FOUND BADLY WORN IN THE LT WING AT STATION 71.125. THE CABLE IS DIRECTED OVER A FAIRLEAD AT THIS LOCATION AND TYPICALLY WEARS VERY BADLY AT THIS CONTACT POINT. BECAUSE THE WEAR PATTER IS OVER A STRAIGHAug 21, 2007 · N454ER · Cessna 172SSDR DL76S071102Control Cable · brokenLEFT OUTBOARD AILERON LOCKED IN DOWN POSITION. FOUND CABLE A3B-3 FOR LT O/B AIL BROKEN JUST O/B OF THE LT O DROOP QUADRANT. REMOVED BROKEN CABLE RECEIVED NEW CABLE FROM BOEING P/N BACC2C4C04961FG. REPLACED CABLE A3B PER OPN 2000 CABLE REPLACEMENT AND RIGGEDAug 20, 2007 · N136DL · Boeing 767332SDR CA070821002Link Assy · failed(CAN) WHILE MAINTENANCE WAS DOING A OVERNIGHT CHECK TO THE AIRCRAFT, THEY OBSERVED THE LINK-ASSY AILERON LVDT WAS HANGING DOWN. THE ROD LINK HAD BROKEN AT THE AILERON END. (TC NR 20070821002)Aug 15, 2007 · Bombdr DHC8402SDR ASMF200708001Plate · brokenCAPTAIN REPORTED THAT DURING CRUISE THE AILERON GOT STUCK WHEN THE COMPENSATOR KNOB IS TURNED TO THE RT SIDE. DURING CHECK, A SCREW WAS DAMAGED AND PLATE SPIRAL DRIVE BROKEN. THEY WERE REPLACED AND TRIM WAS PERFORMED TO CONTROL MECHANISM IAW MM 27-10-07, TESTEAug 2, 2007 · N754RA · Doug DC987SDR VNAA0708001Trim System · out of limitsCREW REPORTED ON TAKEOFF ROLL, RECEIVED A RED WARNING MESSAGE INDICATING A TAKEOFF CONFIGURATION. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE AILERON TRIM OUT OF LIMITS FOR TAKEOFF CONFIGURATION. MAug 1, 2007 · N259PS · Cndair CL6002B19SDR AWXA200700951Servo Valve · leakingDFW - PHX - EL - LOG 7827212 - CREW REPORTED, DURING CRUISE THEY RECEIVED A GREEN HYD RESERVOIR LOW LEVEL ECAM MESSAGE. THE CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENFUL. MX REPLACED THE LEFT AILERON SERVO VALVE DUE TO IT LEAKING. OPERATIONAL/LEAK Jul 31, 2007 · N620AW · Airbus A320231SDR MWEA070160Motor · inoperativePRIMARY TRIM IS WORKING INTERMITTENTLY. REMOVED AND REPLACED PRIMARY TRIM MOTOR.Jul 20, 2007 · N916ME · Boeing 717200SDR 2007FA0000646Pushrod · bentAILERON PUSHROD WAS FOUND BENT DURING PREFLIGHT. REMOVED PUSHROD AND WENT TO INSTALL NEW ROD AND FOUND THAT ALL FOUR RODS IN STOCK HAD BAD THREADS- PD WAS OVERSIZED.Jul 19, 2007 · N2277T · Cessna 172SSDR SWIA200718602Control Cable · corrodedLEFT LOWER AILERON CABLE CORRODED AT PULLEY, DISCOVERED AT C-CHECK. REPLACED LEFT LOWER AILERON CABLE IAW AMM 27-00-01.Jul 18, 2007 · N580SW · Emb EMB120ERSDR SWIA200718487Rvdt · bindingON TAXI CHECK, YOKE ONLY DEFLECTS APPROX 1/3 OF THE WAY TO FULL RIGHT AILERON. REPLACED NR 1 AILERON RVDT AND ALIGNED IAW MM 31-30-00.Jul 9, 2007 · N580SW · Emb EMB120ERSDR SIMA200719003Control Unit · failedCAUTION PITCH FEEL MESSAGE, DECLARED EMERGENCY. REMOVED AND REPLACED SPOILER STABILIZER CONTROL UNIT IAW CRJ AMM 27-61-05. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.Jul 8, 2007 · N500AE · Cndair CL6002C10SDR 2007UALA02473Cable · misroutedRIGHT AILERON CABLE MISROUTED ABOVE CONTROL QUADRANT CASTING DAMAGE TO CABLE AND AILERON QUADRANT ATTACH HARDWARE. [07-31-07] REMOVED AND REPLACED MISROUTED CABLE.Jul 6, 2007 · N369UA · Boeing 737322SDR WRNA200700044Unknown · sparksON TAXI OUT, DURING FLIGHT CONTROL CHECK, CREW IN AIRCRAFT FOLLOWING BEHIND REPORTED SPARKS COMING FROM RT AILERONS, RETURNED TO BLOCKS. RAN NR 3 AND NR 4 ENGINES IAW 71-00-00, ACCOMPLISHED OPERATION CHECK OF GENERATORS IAW 24-21-01 PG 601. OPENING AND CLOSIJul 5, 2007 · N526UP · Boeing 747212BSDR HALA0700274Transmitter · out of adjustETOPS SIGNIFICANT SYSTEM, BTB, INBOARD AILERON DISPLAY ON EICAS DOES NOT SHOW CORRECT CONTROL CHECK. ON ARRIVAL BACK INTO GATE FOUND RT IB AILERON NOT FAIRING. ADJUSTED INBOARD AILERON TRANSMITTER PER AMM 27-18-00-501 AND ADJUSTED INBOARD AILERON PCA INPUT RJul 3, 2007 · N597HA · Boeing 767332SDR HALA0700270Unknown · unknownETOPS SIGNIFICANT SYSTEM, ON CLIMB-OUT RT I/B AILERON APPEARED ON STATUS PAGE TO BE IN EXTENDED UP POSITION THIS CAUSED LEFT RUDDER TRIM USE OF 4 UNITS. IN CRUISE LOOK AT BOTH I/B AIL BOTH APPEARED TO BE BELOW NORMAL WHILE STATUS PG DEPICTED THEM ABOVE NORMALJun 28, 2007 · N587HA · Boeing 76733ASDR SWIA200718426Bellcrank · wornFLT 5788 - THE YOKE FEELS AS THOUGH IT FALLS INTO A DETENT IN THE CENTER POSITION. REPLACED LEFT AILERON BELLCRANK AND AILERON SPIGOT BEARING IAW EMB 120 MM 27-11-05.Jun 28, 2007 · N295SW · Emb EMB120ERSDR 2007UALA02304Actuator · malfunctionedLEFT AILERON LOCKOUT ACTUATOR -NO RESPONSE- (SRM-R) MESSAGE 27321 HARD FAULT LAST FOUR LEGS. [07-24-07] REPLACED LT AILERON LOCK OUT ACTUATOR. COMPLETED INSTALLATION & TEST PER MM 27-11-16. ALL TESTS NORMAL PER PROCEDURE NR 4. AIRCRAFT OK FOR SERVICE.Jun 28, 2007 · N104UA · Boeing 747422SDR FDKA200706291Trim Panel · faultyFDM 6201 FLL-MCO (0336 PHX LCL). ROLL TRIM INOP. MX REMOVED AND REPLACED ROLL TRIM PANEL, OPS CHECK GOOD.Jun 21, 2007 · N843MJ · Emb EMB145LRSDR SWIA200718463Counterweight · migratedLEFT AILERON OUTBOARD LEAD WEIGHT HAS MIGRATED OUT DUE TO CORROSION AND IS RUBBING ON BEARING SUPPORT, DISCOVERED AT C-CHECK. REPLACED LEFT AILERON LEAD WEIGHT IAW EMB 120 MM 27-00-00 AND 51-61-01.Jun 18, 2007 · N271YV · Emb EMB120ERSDR SWIA200718345Bearing · roughNOTCH IS FELT ON FIRST OFFICERS YOKE WHEN TURNED TO THE LEFT OR RIGHT. REPLACED AILERON TORQUE TUBE RIGHT BEARING IAW AMM 20-26-00.Jun 15, 2007 · N423SW · Cndair CL6002B19SDR FDKA200706272Connector · looseFDM 5982 MCO-FLL (0510 PHX LCL). PITCH TRIM FAIL IN FLIGHT. MX RESET THE CONNECTOR ON HORIZONTAL CONTROL UNIT, OPS CHECK GOOD.Jun 14, 2007 · N825MJ · Emb EMB145LRSDR HNAA0700210Control Cable · wornRIGHT AILERON INBOARD AND OUTBOARD WING REAR SPAR WORN TO LIMITS. RIGHT INBOARD AND OUTBOARD AILERON CABLES REMOVED AND REPLACED IAW 27-12-00.Jun 9, 2007 · N907HA · Dhav DHC8102SDR HNAA0700208Control Cable · wornLEFT AILERON INBOARD AND OUTBOARD WING REAR SPAR CABLES (UPPER AND LOWER) WORN TO LIMITS. LEFT WING INBOARD AND OUTBOARD AILERON CABLES UPPER AND LOWER REMOVED AND REPLACED PER SRM 27-12-00.Jun 9, 2007 · N907HA · Dhav DHC8102SDR HNAA070028Control Cable · wornLEFT AILERON INBOARD AND OUTBOARD WING REAR SPAR CABLES (UPPER AND LOWER) WORN TO LIMITS. LEFT WING INBOARD AND OUTBOARD AILERON CABLES UPPER AND LOWER REMOVED AND REPLACED PER SRM 27-12-00.Jun 9, 2007 · N907HA · Dhav DHC8102SDR ARWA20070602Bypass Valve · brokenAILERON MANUAL REVERSER LIGHT STAYS ON WHILE AILERON IS POWERED AND CONTROL CHECK UNSATISFACTORY. REMOVED AND REPLACED BROKEN BYPASS VALVE TURNBUCKLE AND ADJUSTED AILERON POWER TO MANUAL REVERSION MECHANISM IN ACCORDANCE WITH DC-8 M/M 27-11-8; OPERATIONAL CHEJun 5, 2007 · N441J · Doug DC863FSDR COMA0760417Spring · out of rigFLIGHT 5503 - LEFT AND RIGHT AILERON MORE STIFF THAN NORMAL. -A- ON PFD WITH AUTO-PILOT ON, IN TURNS. HYD PUMP 1A SQUEALING. AILERONS FELT NORMAL WHEN DISCONNECTED. FOUND BOTH CENTERING MECHANISMS FORCE TOO HIGH. RIGGED LEFT AND RIGHT AILERON CENTERING MEMay 31, 2007 · N709CA · Cndair CL6002B19SDR DXTA200702214Servo · inoperativeFL410, AIRCRAFT STARTED LT BANK (YOKE MOVED ABOUT 60 FT TO THE LT) CASS MESSAGE RETRIM LT WING DOWN CAME ON. LIGHT WENT OUT AFTER ABOUT 5 MINS. REPLACED AILERON SERVO IAW MM CH 22-10-01. OP'S CHECK GOOD.May 23, 2007 · N944QS · Cessna 750SDR SWIA200718252Bushing · noisySIGNIFICANT SQUEAKING NOISE FROM LEFT AILERON IN BOTH DIRECTIONS. REPLACED LEFT AILERON HINGE BUSHINGS AND HARDWARE IAW MM 27-14-15.May 21, 2007 · N905SW · Cndair CL6002B19SDR CA070524005Link Assy · broken(CAN) WHEN DOING WP8 INSPECTION TASK 000-057-640-500 GVI OF THE (RT) AILERON ASSY. MAINTENANCE FOUND LINK ASSY P/N 82740162-001 FROM THE RT AILERON LVDT BROKEN. (TC NR 20070524005)May 19, 2007SDR FDKA200705201Unknown · unknownAILERON SYSTEM 1 DOES NOT SHUT OFF DURING FLIGHT CONTROL TEST. MX RESET AIRCRAFT POWER OPS GOOD.May 11, 2007 · N835MJ · Emb EMB145LRSDR CA070427008Guard · worn(CAN) FLIGHT CREW REPORTED ROLL CONTROL INPUTS SEEMED STIFF, ESPECIALLY LT TO RT IN-FLIGHT. ON GROUND NO INDICATION OF STIFFNESS AND NOTHING ADVERSE WITH ROLL DISCONNECT. MAINTENANCE INSPECTION FOUND LT OB AILERON CABLE ROUTED AROUND WRONG SIDE OF CABLE GUARD.Apr 25, 2007 · Dhav DHC8311SDR NSVA20070111Centering Mech · malfunctionedCONTROL PRESSURE FOR ROLL IS AT LEAST 2X HIGHER THAN ANY OTHER ACFT PILOT HAS FLOWN. PITCH AND YAW OK. "AIL" FLASHING INTERMITTENTLY. NOTED MORE DURING TURNS. "AIL" WILL STILL FLASH INTERMITTENTLY EVEN IF AILERON TRIM IS NEUTRALIZED. CHECKED PULLEYS UNDERApr 23, 2007 · N239CJ · Saab 340BSDR CA070502010Control Cable · frayed(CAN) DURING INSPECTION RT WING AILERON CONTROL CABLES FOUND TO BE FRAYED WITH BROKEN STRANDS AT WING STATION 100 WHERE CABLES TRAVEL ON TOP OF FAIRLEAD PN 0522647-10 CABLES WERE REPLACED WITH NEW UNITS FROM MFG. (TC NR 20070502010)Apr 18, 2007 · Cessna 172SSDR 2007FA0000337Control System · out of rigDURING INSPECTION, FOUND AILERON RUDDER INTECONNECT OUT OF RIG AND CAUSING INTERFERENCE BETWEEN RUDDER AND AILERON. THIS IS THE FOURTH AIRCRAFT WE'VE FOUND WITH THIS PROBLEM AND ONE ACTUALLY HAD THE RUDDER AND AILERON LOCK IN FULL OPPOSITE DEFLECTIONS JUST PRIApr 18, 2007 · N636ST · Cirrus SR22SDR SWIA200718098Pulley · wornAILERON CONTROLS BIND IN CENTERED POSITION. REPLACED OUTBOARD AILERON PULLEYS ON LEFT AND RIGHT WINGS IAW MM 27-00-00.Apr 10, 2007 · N218SW · Emb EMB120ERSDR COMA0760308Link · fracturedDURING A HMV5 INSPECTION, THE LEFT AILERON OUTBOARD PCU LINK WAS FOUND TO BE FRACTURED. REPLACED PCU LINK AND ACCOMPLISHED SB601R-27-130.Apr 9, 2007 · N708CA · Cndair CL6002B19SDR GUUA04070701Unknown · unknownFLIGHT: 0253, DURING FINAL APPROACH FLIGHT CONTROLS WILL NOT PERMIT RT AILERON INPUT. INSPECTED LT AILERON CONTROL SURFACE REMOVED PANELS AND INSPECTED CABLES, PULLEYS, BEARING ATTACHMENTS ALSO INSPECTED AILERON CONTROL QUADRANTS UNDER THE FLOOR FOR LOOSE ITEApr 7, 2007 · N280AS · Emb EMB120ERSDR DXTA200702058Control Cable · out of adjustAIRCRAFT WILL NOT FLY LEVEL IN FLIGHT AFTER AILERON RIGGING WITH CONTROLS CENTERED. ADJUSTED AILERON WING AND FAIRING CABLE TENSION AND RIG IAW 560XL MM 27-10-00. OPS CHECK OK.Mar 31, 2007 · N604QS · Cessna 560XLSDR 2007FA0000270Control Cable · worn(REF MODEL 35 SERIES IPC FIG. 27) LT AILERON CABLE FOUND RIDING ON PROP CONTROL CABLE SHEATH, ABOUT 2 INCHES AFT OF FIREWALL. AILERON CABLE WAS WORN ABOUT HALF THROUGH, AND THE PROP CABLE WAS WORN THROUGH THE SHEATH TO THE INNER STEEL CABLE. (VERY DIFFICULT Mar 26, 2007 · N1363Z · Beech N35SDR SWAA071573Control Rod · wornDURING SCHEDULED 14Y CHECK, LEFT AILERON FAILED THE FREEPLAY CHECK. REMOVED AND REPLACED LEFT AILERON CONTROL ROD ASSY.Mar 25, 2007 · N358SW · Boeing 7373H4SDR DL76G070202Actuator · malfunctionedON CLIMB-OUT WITH A/P ON NOTICED CONTROL WHEEL DEFECTED 2 DEGREES RIGHT WITH A/P OFF RUDDER TRIM PLACED 7 DEGREES RIGHT TO CENTER WHEEL. REMOVED LEFT INBD AIL PCA OUTBD PCA LT SYS OK TO INSTALL PCA S/N 3666. INSTALLED LEFT INBD AIL OUTBD PCA INSTALLATION OK. Mar 11, 2007 · N1613B · Boeing 767332SDR HALA0700097Actuator · unknownETOPS SIGNIFICANT SYSTEM, "AILERON LOCKOUT" DISPLAYED ON EICAS. T/S PER FIM 27-11-00, FIG 104 AND THE RIGHT SAM FAULTED "R AIL LOCK ACT". PER FIM BLOCK 35, RESET AND FAULT DID NOT RETURN. FOR PRECAUTIONARY T/S, REMOVED AND REPLACED RIGHT AILERON LOCK-OUT ACMar 9, 2007 · N583HA · Boeing 76733ASDR DXTA200701974Pcu · inoperativeON LANDING A "FLIGHT CONTROL FAULT" MESSAGE APPEARED AND THE 'AILERON FLIGHT CONTROL SHUTOFF LIGHT BLINKED. REPLACED "B" PCU (AILERON) , ADJUSTMENT & OPS. IAW. CE 750. M/M CE750. 27-11-05.Feb 28, 2007 · N948QS · Cessna 750
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