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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UATA201910144210Bearing · failedBEARING IN AILERON CONTROL LEVER AT THE BOTTOM OF THE CO-PILOT'S YOKE TUBE FELL APART. REPLACED AILERON CONTROL LEVER WITH A SERVICEABLE UNIT.SDR UATA2019101424205Control Cable · frayedPILOTS OUTBOARD FORWARD AILERON CABLE FRAYED WITH BROKEN STRANDS. REPLACED CABLE WITH NEW.SDR UATA2019101400204Control Cable · frayedCOPILOT'S FWD INBOARD AILERON CABLE FRAYED WITH BROKEN STRANDS. REPLACED CABLE WITH NEW.SDR UATA2019101400203Control Cable · frayedCOPILOT'S OUTBOARD FWD AILERON CABLE IS FRAYED WITH BROKEN STRANDS. REPLACED CABLE WITH NEW.SDR SWIA2019101846525Control Cable · damagedWHILE PERFORMING TENSION CHECK OF THE ELEVATOR CONTROL CABLES FOUND THE LH ELEVATOR CONTROL CABLE CIRCUIT TO BE OUT OF LIMITS. AT 70 DEGREES THE MEASUREMENT IS 120, THE ALLOWABLE MEASUREMENT AT 70 DEGREES IS 125-135 (C-CHECK) RO: 10/16/2019 PERFORMED RIGGING OSDR SWIA2019101846524Control Cable · damagedWHILE PERFORMING TENSION CHECKS OF THE AILERON CONTROL CABLES FOUND THE LH TENSION REGULATOR TO BE OUT OF LIMITS AND REQUIRES ADJUSTMENT (C-CHECK) RO: 10/16/2019 PERFORMED ADJUSTMENT OF THE LH AILERON WING CIRCUIT IAW AMM.SDR SWIA2019101846523Control Cable · damagedWHILE PERFORMING TENSION CHECKS OF THE AILERON CONTROL CABLES FOUND THE RH TENSION REGULATOR TO BE OUT OF LIMITS AND REQUIRES ADJUSTMENT (C-CHECK) RO: 10/16/2019 PERFORMED RIGGING OF THE RH AILERON WING CIRCUIT IAW AMM.SDR SWIA2019101846522Control Cable · damagedWHILE PERFORMING TENSION CHECKS OF THE AILERON CONTROL CABLES FOUND THE RH O/B CONTROL COLUMN CABLE TO BE OUT OF LIMITS. THE MEASUREMENT IS 60 AT 80 DEGREES. THE ALLOWABLE MEASUREMENT AT 80 DEGREES IS 65-75 (C-CHECK) RO: 10/16/2019 PERFORMED TENSIONING OF THE SDR SWIA2019101846521Control Cable · damagedWHILE PERFORMING TENSION CHECKS OF THE AILERON CONTROL CABLES FOUND THE RH I/B CONTROL COLUMN CABLE TO BE OUT OF LIMITS. THE MEASUREMENT IS 60 AT 80 DEGREES. THE ALLOWABLE MEASUREMENT AT 80 DEGREES IS 65-75 (C-CHECK) RO: 10/16/2019 RH IB AND OB COLUMN CONTROL SDR SWIA2019101846520Control Cable · damagedWHILE PERFORMING TENSION CHECKS OF THE AILERON CONTROL CABLES FOUND THE LH O/B CONTROL COLUMN CABLE TO BE OUT OF LIMITS. THE MEASUREMENT IS 60 AT 80 DEGREES. THE ALLOWABLE MEASUREMENT AT 80 DEGREES IS 65-75 (C-CHECK) RO: 10/16/2019 ADJUSTED THE LH AILERON CONTSDR SWIA2019101846519Control Cable · damagedWHILE PERFORMING TENSION CHECKS OF THE AILERON CONTROL CABLES FOUND THE LH I/B CONTROL COLUMN CABLE TO BE OUT OF LIMITS. THE MEASUREMENT IS 55 AT 80 DEGREES. THE ALLOWABLE MEASUREMENT AT 80 DEGREES IS 65-75 (C-CHECK) RO: 10/16/2019 LH I/B AND O/B CONTROL COLUMSDR SWIA2019101846518Control Cable · damagedWHILE PERFORMING TENSION CHECK OF THE AILERON CONTROL CABLES FOUND THE R/H I/B FUSELAGE CABLE TO BE OUT OF LIMITS. THE MEASUREMENT IS 100 AT 80 DEGREES, THE ALLOWABLE MEASUREMENT IS 120-130 AT 80 DEGREES (C-CHECK) RO: 10/16/2019 PERFORMED RIGGING OF THE RH AILSDR SWIA2019101846517Control Cable · damagedWHILE PERFORMING TENSION CHECK OF THE AILERON CONTROL CABLES FOUND THE LH O/B FUSELAGE CABLE TO BE OUT OF LIMITS. THE MEASUREMENT IS 145 AT 80 DEGREES THE ALLOWABLE MEASUREMENT IS 120-130 AT 80 DEGREES. (C-CHECK) RO 10/16/2019 PERFORMED RIGGING OF THE LH FUSESDR AALA201909129007Nut · strippedAIRCRAFT WAS GROUNDED: DURING THE ACCOMPLSHMENT OF TASK CARD 12T21127001 THE LEFT WING INBOARD AILERON WAS NOT RESPONSIVE WHEN OPERATING THE CENTER HYDRAULIC SYSTEM. THE INBOARD AILERON ACTUATOR REACTION LINK ATTACH BOLT AND NUT NOT ATTACHED DUE TO THE NUT BEISDR 2019FA0000288Servo · corrodedDURING ROLL SERVO SLIP CLUTCH TORQUE FUNCTIONAL CHECK ROLL SERVO FAILS TEST, MAKES AUDIBLE GRINDING NOISE AND YOKE WAS JERKING LEFT TO RIGHT DURING FUNCTIONAL CHECK. REMOVED ROLL SERVO SLIP CLUTCH AND FOUND WATER AND OIL MIXED WITHIN SERVO MOTOR AND MOUNT. THESDR QXEA2019081300315Aileron Sys · malfunctionedDURING FLIGHT CONTROL CHECK AILERONS DID NOT CENTER . THEY REMAINED IN 30-45 DEG RIGHT TURN. REMOVED FROM SERVICE. ADJUSTED THE AILERON FEEL CENTERING CONTROLLER REF. 27-13-06-830-802. CHECKS NORMAL. FIRST CHECK FOUND AILERONS WERE TO THE RIGHT., ALSO FOUND THSDR CA190802005Bearing · seized(CAN) FLIGHT CREW REPORTED AILERON CONTROL HAD AN ODD FEELING IN FLIGHT, SOMEWHAT STIFF AND HEAVY. UPON AN UNEVENTFUL LANDING, MAINTENANCE PERSONNEL CARRIED OUT A FULL OPERATIONAL CHECK OF THE ROLL CONTROL SYSTEM I.A.W DH8 AMM 27-10-00-06 WHICH INCLUDED CHECKISDR CA190805005Pcu · failed(CAN) AILERON FAIL (C) POSTED IN-FLIGHT AILERON FAIL EICAS CAUTION MESSAGE GOT POSTED, QUICK REFERENCE HANDBOOK PROCEDURE WAS FOLLOWED AND THE AIRCRAFT DIVERTED. AIRCRAFT WAS DECLARED AOG. ONBOARD MAINTENANCE SYSTEM SHOWED FAULT CODE 2715F0006 - LEFT AILEROSDR CALA2019071801213O-Ring · brokenHYD QTY LOW L EICAS ADVISORY, LEFT HYDRAULIC SYSTEM RESERVOIR QUANTITY LOW. QTY < .40. LEAK CHK FOUND RT OUTBD AILERON OUTBD PCU CAP (IPC 27-11-11-11 ITEM 665) LEAK. INSPECTION FOUND LOCKWIRE BROKEN. CAP REMOVED FOUND O-RING BROKEN. O-RING (IPC 27-11-11-11 ITESDR CALA2019071501195Cap · leakingHYD PRESS SYS L EICAS CAUTION LOW LEFT HYDRAULIC SYSTEM PRESSURE. SYSTEM PRESSURE LESS THAN 12 00 PSI. LT HYD FLUID UPLITTED AND HYD PRESSURE SHOW NORMAL AS PER AMM 12-12-01.SDR 2020FA0000128Turnbuckle · crackedDURING ANNUAL INSPECTION DISCOVERED RT LOWER AILERON CONTROL CABLE TURNBUCKLE BARREL LOCATED UNDER AFT CABIN HEAT DUCT WAS CRACKED 3/4 INCHES LONGITUDINALLY FROM RT END. THE HEAT AIR DUCT ABOVE THIS TURNBUCKLE ASSEMBLY WAS IN A DECAYED CONDITION. RECOMMEND CSDR K11A2019063091502Unknown · malfunctionedAFTER TAKEOFF FLIGHT CONTROLS REQUIRED ABNORMAL AND EXCESSIVE AMOUNT OF RIGHT AILERON INPUT "UP" POSITION TO CONTROL AIRCRAFT.SDR K11A2019063091501Unknown · malfunctionedIMMEDIATELY FOLLOWING TAKEOFF, I NOTICED THAT PILOT WAS USING GREATER THAN NORMAL AILERON INPUT TO CONTROL AIRCRAFT. HE APPEARED TO BE FIGHTING THE PLANE. I ASKED HIM "IS THE PLANE FLYING OKAY"? HE RESPONDED "SHE'S FLYING FUNNY". THE DEPARTURE CLEARANCE WAS RUSDR KKVA20190701003Reu · failedCRUISING FL400 AND SPEED M.90 WITH AUTOPILOT ON, WE HAD “FCS MAINTENANCE REQUIRED” CAS MESSAGE. APPROXIMATELY 4 HOURS FROM TAKEOFF. QRH PROCEDURES FOLLOWED. THE AUTOPILOT DISCONNECTED AND THE AIRCRAFT SUDDENLY ROLLED TO RIGHT WHEN I PRESSED FLT CNTL RESET SW. SDR IPXA2019062543735Unknown · malfunctionedINSPECTION TYPE:NA DIVERSION -- AFTER T/O FLAP/SLAT RETRACTION LEVEL 2 AIL DEFLECT DISAG AC FT VERY DIFFICULT TO CONTROL REQUIRING ALMOST FULL RT AILERON AT TIMES QRH CHECK LIST NO HELP DECLARED EMERGENCY AND DIVERTED TO KCVG. DEFERRED PER MEL 27-13-2-0-1 DMPSDR CA190625001Lever · binding(CAN) WHILE CARRYING AILERON ROLL DISCONNECT, FOUND CLUNKING NOISE COMING FROM UNDERFLOOR QUADRANT. FOUND COPILOT AILERON PULLEY QUADRANT BEARING CAUSING THE NOISE. AILERON PULLEY QUADRANT LEVER AND BEARINGS REPLACED REFERENCE AMM 27-12-41. AILERON SYSTEM RIGGSDR CA190617004Pulley · seized(CAN) DURING CLIMB OUT CREW REPORTED STIFF ROLL CONTROL. FLIGHT RETURNED TO DEPARTURE AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING FOUND TWO BINDING PULLEYS IN THE RH AILERON CABLE CIRCUIT. PULLEYS REPLACED AND THE AIRCRAFT RETURNED TO SERVSDR 2019FA0000209Duct · crackedDURING THE ANNUAL INSPECTION, DUE TO A SAFETY RECOMMENDATION, THE SAFETY WIRE ON THE AILERON CABLE TURNBUCKLE WAS REMOVED TO INSPECT THE SWAGED END OF THE CROSSOVER CABLE. THE END NEAREST THE HEATER DUCT WAS FOUND TO HAVE A SIGNIFICANT CRACK. DUE TO THE AFFECTSDR CA190604023Coil · leaking(CAN) LOSS OF HYD FLUID IN SYS #3 PILOT REPORTED LOSS OF HYD FLUID IN SYSTEM #3 ON APPROACH HYD FLUID REPORTED FROM PILOTS AS COMING FROM RH ELEVATOR. PCU COIL ROBBED FIELD TEAM DEPLOYED. RH ELEVATOR HYD SYS #3 RETURN LINE COIL ASSY P/N C02041124-001 REPSDR FDEA201905291178O-Ring · cut"C HYD QTY" DURING FLIGHT. HAPPENED IN CRUISE AT FL340. FLUCTUATED DOWN TO .08 DURING DESCEN. PARKED AT GATE WITH .26 UPON FURTHER TROUBLESHOOTING, FOUND O-RING CUT UNDER AILERON ACTUATOR CHECK VALVE ACCESS PLUG. REMOVED RT I/B ACTUATOR TO FOM REF. 27-11-20-SDR CA190524024Aileron · stiff(CAN) THE BOMBARDIER FSR REPORTED THAT THE FLIGHT DIVERTED TO STUTTGART AND DECLARED AN EMERGENCY WHEN THE PILOT NOTED PROBLEMS WITH THE ROLL CONTROL OF THE AIRCRAFT. THE LANDING WAS UNEVENTFUL. THE POST FLIGHT INVESTIGATION SHOWED SIGNS OF DE-ICING FLUID MIXESDR 2019FA0000149Cable Assy · corrodedON AN ANNUAL INSPECTION OF THE AIRCRAFT, FOUND RIGHT AILERON CABLE BROKEN AT SWAGED PORTION ATTACHED TO TURNBUCKLE. THE CABLE WAS HELD TOGETHER ONLY BY THE SAFETY WIRE OF THE TURNBUCKLE. SOME CORROSION COULD BE SEEN ON THE SWAGED PORTION AFTER THE SAFETY WIRE SDR CA190503028Control Cable · damaged(CAN) DURING HMV CHECK, A DAMAGED CABLE WAS DISCOVERED. CABLE REPLACEMENT REVEALED AN ISSUE WITH BOTH THE ADOC MM AND THE ATR.DOC MM. AFTER CONSULTATION WITH ATR, THEY SUPPLIED THE CABLE LENGTH SPECS FOR ALLELEVATOR CABLES. ONE OF THE TWO LONG CABLES IN THE L/SDR FDEA2019041640793Aileron · stuckON TAXI OUT DURING FLIGHT CONTROL CHECK, LEFT AILERON INDICATOR STUCK IN FULL UP POSITION. SEVERAL MORE MOVEMENTS OF THE AILERON AND THE INDICATOR SHOWS FULL DOWN POSITION WHILE AILERONS CONTROL ARE IN THE NEUTRAL POSITION.SDR DGCA201904170006Control Unit · failedTCU SYSTEM FAILED DURING TAKE-OFF / CLIMB.SDR QXEA2019040800160Actuator · malfunctionedAFTER START FLIGHT CONTROL CHECK ROLL CONTROL FELT MORE HEAVY THAN NORMAL. NO OBVIOUS POINTS WHERE CONTROLS HUNGUP, IT WAS FULL TRAVEL JUST A MOVE HEAVY FEEL. AIRBORN NOTICED DEFINITE HEAVIER THEN NORMAL CONTROL FEEL IN ROLL CONTROL. HAND FLEW MOUTH OF 1 HOURSDR CA190409010Servo · damaged(CAN) THE CREW WERE CARRYING OUT PRE-FLIGHT CHECKS AND DURING THE AILERON CONTROL SWEEP FOUND THAT THEY COULD ONLY ACHIEVE ABOUT HALF DEFLECTION TO THE RIGHT (IT WAS BLOCKED), BUT FULL DEFLECTION TO THE LEFT. THEY TRIED TO MOVE THE AILERONS USING HEADING MODE SDR CA190403005Aileron Sys · flutter(CAN) ON FLIGHT OUT OF MAINTENANCE, FLIGHT CREW REPORTED THEY FELT A FLUTTER THRU THE AILERON CONTROL WHEEL WHEN TURNED AND PRESSURE MAINTAINED IN A STATIC POSITION. FLIGHT CREW STATED: `THE WHEEL FELT NOTCHY DURING TRANSITION . CONDITION MOST PROMINENT BETSDR CA190403002Computer · failed(CAN) RETURN TO GATE DUE TO GENERATOR 1 SMOKE INDICATION, SMOKE SMELL IN COCKPIT AND CABIN. RESOLUTION TSM 27-30-00-810-822-A CARRIED OUT, FOUND BURNING RESIDUAL AND SMELL FROM SPOILER ELEVATOR COMPUTER (SEC) #1 , SEC #1 REPLACED IAW AMM 27-94-34 PB 401.ELEVSDR FAUA20190325101Aileron · icedAT CRUISE ALTITUDE AILERONS WOULD NOT RESPOND, PILOT HAD TO PULL AILERON ROLL DISCONNECT FOUND THAT THE LT WOULD RESPOND AND RT STILL HAD NO RESPONSE PILOT DECLARED EMERGENCY AND ASK FOR A NEW DESTINATION TO KGJT UPON SHORT FINAL INTO KGJT PILOT REPORTED REGAISDR HALA2019031500128Control System · lack of lubeBINDING IN YOKE AT ABOUT 30 DEG. OF LEFT YOKE. ACCOMPLISHED FIM TASK 27-10-803 CLEANED AND LUBED AILERON TRANSITION SECTOR. AILERON CONTROL SYSTEM TEST OK.SDR 2GYR2019040500002Cable · misroutedLEFT AILERON CABLE NOT ROUTED CORRECTLY WHERE IT PASSES THROUGH LEFT WING ROOT, PASSES ON THE AFT SIDE OF THE BELLCRANK AND SHOULD BE ON THE FWD SIDE.SDR CA190318019Dcu · failed(CAN) CONFIG AILERON WARNING WHEN BRINGING POWER UP FOR TAKEOFF.SDR HNAA2019030100054Bolt · shearedLT AILERON DAMPER ROD END BOLT SHEARED. REMOVED AND REPLACED DAMPER AND AILERON.SDR VNAA2019021541101Unknown · malfunctionedON APPROACH, CREW REPORTED LEFT WING DOWN. THEY TRIMMED THE A/C AND REPORTED THE CONDITION WORSENED AND THE AUTOPILOT DISCONNECTED. THEY DECLARED AN EMERGENCY AND LANDED IN CLT. UPON LANDING THE CREW REPORTED THEY HAD TO HOLD THE CONTROL WHEEL TO THE RIGHT TO SDR AALA201902159008Bushing · wornLEFT ENGINE VIBRATION DURING CRUISE. EMERGENCY DECLARED, DIVERTED, AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. COMPLIED WITH AN INSPECTION AND FOUND THE RT AND LT ELEVATOR HINGE BEARINGS AND BUSHINGS OUT OF LIMITS. REMOVED AND REPLACED THE BUSDR CA190207012Guard · out of alignment(CAN) DURING SCHEDULED MAINTENANCE AND INSPECTION OF THE AILERON CABLE AND BELL CRANK IN ACCORDANCE WITH SL 1327 THE AILERON CABLE GUARD WAS OBSERVED TO BE BINDING ON THE AILERON CABLE AT THE BELL CRANK. THIS RESULTED IN DAMAGE TO THE CABLE AND BELL CRANK. PICSDR HNAA2019020100031Wheel · failedPDIS 655 27-12 2012781 31JAN19 PHL CLOSE
WITHOUT CREW INPUT AIRCRAFT EXPERIENCED AILERON
DISCONNECT ON SHORT FINAL AUDIBLE CLICK WAS HEARD JU
ST PREVIOUS TO DISCONNECT.
FACT 31JAN19 00:48 PHL
R&R AILERON DISCONNECSDR RAIA201901280001Support Fitting · crackedRH AILERON L/E PCA ROD END SUPPORT FITTING CRACKED- REMOVED RH AILERON PCA FITTING. INSTALLED RH AILERON PCA FITTING.SDR BIER201911519001Control Rod · dentedBOTH AILERON CONTROL RODS, P/N 2861101-4 WERE REMOVED FOR INSPECTION IN ACCORDANCE WITH AMM SECTION 5-10-00, TIME LIMITS & INSPECTIONS. BOTH CONTROL RODS HAVE DEFECTS, LT CONTROL ROD HAS A DENT 1.25" LONG BY .5" WIDE AND .031" DEEP, 79 INCHES FROM THE INBOARD
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