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 WRNA200300004Aileron · delaminatedOn walk around found R/H I/B aileron to have damage. This damage is on the top trailing edge where a section of skin is peeling aft (approx. 4' width and 8" in length) exposing honeycomb.Corrective Action: Removed and replaced right wing in-board all speed ailSDR DHL2003367001Structure · vibrationCONTINUOUS MODERATE AIRFRAME VIBRATION WHEN ABOVE FLIGHT LEVEL 200 AND 250 KIAS. EMERGENCY DECLARED. RETURNED TO LAX. SUSPECT ALL-SPEED AILERONS. PERFORMED ADJUSTMENTS ON BOTH ALL-SPEED AILERONS IAW 27-10-00. GROUND OPS CHECKED GOOD AT THIS TIME. RT FUELSDR CA030212005Seal · leaking(CAN) EVIDENCE OF HYDRAULIC FLUID LEAKING FROM PCU SHAFT SEAL AREA.SUSPECT LEAKING IS WORSE AT ALTITUDE ORIN EXTREME COLD CONDITIONS.SDR AUS20030098Control Cable · worn(AUS) AILERON CABLES WORN AT FUSELAGE FAIRLEADS.SDR CA030117004Pcu · leaking(CAN) WHILE IN THE HANGAR, HYDRAULIC FLUID WAS NOTICED ON THE WING UNDERSIDE LEAKING FROM THE AILERON PCU DRAIN HOLES. DURING SUBSEQUENT LEAK CHECKS WITH THE PCU INSPECTION PANEL REMOVED NO SIGNIFICANT LEAKAGE NOTICED. DURING SHORT TURN AROUND FLIGHTS NO EVIDSDR 2003FA0000048Turnbuckle · brokenAILERON CABLE TURNBUCKLE FORWARD OF AFT SPAR BROKEN. SAFETY WIRE HOLDING CABLE TOGETHER, FOUND DURING ANNUAL INSPECTION. CABLE HAD BEEN CONTACTING AFT HEAT DUCT. APPEARS TO HAVE INTERNAL CORROSION FROM CONTACT WITH WIRE IN HEAT DUCT. FITTING SHOW NO SIGN OF WESDR HALA0300009Control Unit · malfunctionedOGG - EXPERIENCED AIRCRAFT CONTROL PROBLEMS IN ROLL AXIS PASSING 10,000 FEET QUICK 'JERK' AND AIRCRAFT MADE AN ABRUPT ROLL TO THE LEFT. SECURITY AND OPERATIONAL CHECKED FLIGHT CONTROL SYSTEM CHECK OK. REPLACED AILERON CONTROL UNIT PER MM. REPLACED TRIM PANESDR SWIA200311696Damper · malfunctionedLT AILERON FLUTTER DAMPER STATUS MESSAGE AND ICON ON FLIGHT CONTROL PAGE BETWEEN 160-200 KIAS, INTERMITTANTLY. REMOVED AND REPLACED LT AILERON FLUTTER DAMPER IAW MM 27-15-05. OPS CHECKS GOOD ON GROUND. FAILED FLIGHT TEST.SDR 2003FA0000025Aileron · jammedAILERON TRIM MOVED OVER 10 DEGREES IN FLIGHT WILL JAM, PILOT WILL NOT BE ABLE TO READJUST TO ZERO.SDR IXXA0200157OCylinder · leakingAFTER TAKEOFF FROM DEN, THE FLIGHT CREW NOTICED A DROP IN THE HYDRAULIC SYSTEM QUANTITY. THE FLIGHT CREW RETURNED TO DEN FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED A LEAK AROUND THE LEFT AILERON PACK. MAINTENANCE REPLACED TSDR 2003UALA00393Attach Fitting · cracked2 CRACKED ACTUATOR FITTINGS. REPLACED BOTH INBOARD AND OUTBOARD FITTINGSSDR 2002UALA01845Flaperon · malfunctionedAIRCRAFT EXPERIENCED FISHTAILING, LASTING 30 SECONDS. SYNOPTIC INDICATED INDEPENDENT CYCLING OF LT & RT FLAPERONS NEAR FULL UP DEFLECTION. AFTER 3-4 CYCLES OPS NORMAL. AUTOPILOT ENGAGED DURING ENCOUNTER, FL380. NO FMC DIRECTED TURNS.SDR AUS20021388Bearing · collapsed(AUS) LH AILERON YOKE BEARING COLLAPSED.SDR XNOA01092Regulator · failedDURING FLIGHT CONTROL CHECK AILERONS CONTROL VERY HEAVY. WILL NOT RETURN TO NEUTRAL. REMOVED & REPLACED LT CONTROL CABLE TENSION REGULATOR ASSY IAW A300 MM 27-11-17. PERFORMED OPERATIONAL AND FUNCTIONAL INSPECTION.SDR SWIA200211505Damper · malfunctionedLT AILERON FLUTTER DAMPER MESSAGE INTERMITTENT. REPLACED LT AILERON FLUTTER DAMPER IAW 27-15-05. OPS CHECK GOOD.SDR AUS20021333Cable · worn(AUS) AILERON CABLE FRAYED IN AREA OF FAIRLEAD LOCATED OUTBOARD OF LH NACELLE.SDR G1FR100Y1Control Unit · leakingELEVATOR ARTHUR FAILS RESISTANCE CHECKS. UNIT HAS STATIC LEAD MORE THAT 70 FEET/MINUTE. TSO UNKNOWN. UNIT REPLACED WITH OVERHAULED UNIT.SDR G1FR100YAControl Unit · leakingAILERON ARTHUR FAILS RESISTANCE CHECKS. STATIC LEAKS BEYOND LIMITS. TIME SINCE OVERHAUL UNKNOWN. UNIT REPACED WITH OVERHAULED UNIT.SDR CA021217006Bearing · broken(CAN) DURING 300-600 HOUR INSPECTION AILERON PCU OPERATION TEST. FOUND AILERON QUADRANT IN RT WHEEL WELL IS NOISY (SNAPPING). AFTER REMOVING RT AILERON QUADRANT ASS FOR INVESTIGATION, FOUND RT QUADRANT ITEM 57 PAGE 27-11-00 FGURE 3 IN IPC BEARING IS DAMAGE (RASDR CA021213002Actuator · malfunctioned(CAN) ENGINE INDICATION AND CREW ALERT SYSTEM MESSAGE APPEARED, AILERON LOCKOUT' CAPTION CAME ON DURING APPROACH. FAULTED LEFT ACTUATOR, ACTUATOR REPLACEDSDR CA021125002Bearing · broken(CAN) DURING 300-600 HOURS INSPECTION AILERON PCU OPERATION TEST, FOUND AILERON QUADRANT IN RT WHEEL WELL IS NOISY (SNAPPING).AFTER REMOVING RT/ AILERON QUADRANT ASSEMBLY FOR INVESTIGATION, FOUND RT/ QUADRANT, BEARING IS DAMAGED (RACES HALF WAY ROUND). CHANGESDR 2002FA0001313Tube · failedAT ANNUAL INSPECTION, A CLICKING NOISE WAS NOTED WHEN LANDING GEAR WAS RETRACTED. UPON INVESTIGATION, IT WAS DETERMINED THAT THE END FITTINGS RIVETED IN THE TUBE ASSEMBLY WERE WORKING. CATASTROPHIC FAILURE WAS PROBABLY NOT IMMINENT, HOWEVER IF LEFT UNATTENDESDR AUS20021293Bellcrank · damaged(AUS) LT AILERON BELLCRANK STOP BENT. DAMAGE ALSO TO PUSH-PULL ROD AND ATTACHMENT HARDWARE AS WELL AS TO THE AILERON CONTROL BRACKET AND SECURING RIVETS.SDR QXEA0201927Aileron · out of rigPDX - LEFT HAND AILERON WILL NOT MAKE PROPER UP TRAVEL. TENSIONED IAW DHC-8 200 MM 27-12-00, PARAGRAPH 3B, PAGE 503. REPAIRED IAW HORIZON AIR EA 2-27-70.SDR XNOA01084Aileron · stuckAILERONS BECAME LOCKED OUT TO THE RT DURING FLT CONTROL CHECK. PERFORMED AUTO PILOT ROLL SERVO CHECK, AUTO PILOT ROLL ENGAGMENT & DISENGAGMENT TEST, "AILERON CONTROL WHEEL OPERATION STIFF", ALL SPEED AILERON SERVO CONTROL OPS CHECK, AILERON CABLE VISUAL & SDR DFJ2002F00000Diode · defectiveLANDING GEAR WOULD NOT EXTEND UNTIL STARTING SYSTEM WITH HAND PUMP. FOUND DEFECTIVE DIODE IN DOWN SIDE OF GEAR SELECTOR SWITCH TO CONTACTOR. DIODE LOOKED NORMAL AND HAD NO EXTERNAL DAMAGE.SDR DHL2002741016Switch1) AILERON "B" SYSTEM LOW PRESSURE LIGHT ILLUMINATED ON FORWARD PANEL. RTO AT 20 KTS, SL, 174.3 K LBS, 27 DEGREE C. BEC NORMAL SEE DISCREPANCY 1P FOR RTO REASON.2) ENTERED ON DMI #10731 AS PER MEL 27-16 CAT "C". PLACARD INSTALLED. FOR INFORMATION ONLY.3) RSDR CA021017002Aileron · frozen(CAN) AILERONS BECAME VERY STIFF AND WOULD MOVE ONLY UNDER HIGH LOADING, SUSPECT FROZEN CONTROLS DESCENDING OUT OF 6000 FEET CONTROLS BECAME NORMAL. LT AND RT AILERON REAR QUADRANTS CLEANED AND SPRAY WITH WATER REPELLANT. OPERATIONAL TEST CARRIED OUT AS. UNSDR AUS20021153Sleeve · split(AUS) LH AILERON CONTROL ROD SLEEVE SPLIT THROUGH TAPER PIN HOLE.SDR XNOA01078Controller · malfunctionedDURING FLIGHT CONTROL CHECK RT L/S AILERON WOULD NOT DEFLECT FULL RANGE. MANUALLY DISCONNECTED, THEN RECONNECTED LSA SYSTEM. OPS CHECK NORMAL. NO DEFECT NOTED IAW A300 MM 27-10-00.SDR COMA0260570Control Cable · lack of lubeAILERON CONTROLS SEEMED STIFFENER THEN NORMAL. LUBRICATED THE LEFT AND RIGHT AILERON CONTROL ASSEMBLY PER EO 27-069RB.SDR SWIA200211305Trim Switch · inoperativeAILERON SWITCH INOP. REMOVED AND REPLACED AILERON TRIM SWITCH. OPERATED AILERON TRIM. OPS CHECK GOOD.SDR MASA200200009Warning Light · false activationABORTED TAKEOFF FOR AILERON MISS TRIM MSG. (TAKEOFF NO CONFIG) MX PERFORMED OPS CHECK OF AILERON SYSTEM. NO DEFECTS NOTED A/C RETURNED TO SERVICE.SDR COMA0260546Pulley · bindingAUTO PILOT LWD AND RWD CAUTION - AILERON CONTROL EXTREMELY DIFFICULT.REPLACED THE L/H AND R/H AILERON BELLCRANK ASSY IN MLG WHEEL WELLS.SDR IXXA0200075OPump · leakingENROUTE FROM TOL TO PDX, THE FLIGHT CREW NOTICED A DROP IN THE HYDRAULIC QUANTITY SYSTEM. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND PROCEDED TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT USING ALL PUMPS AND SYSTEMS AND FOUND NO DSDR WRLA200222Pin · backed outAILERON DEFLECT DISAGREE UPON FLAP RETRACTION, AIRCRAFT RETURNED TO DEPARTING STATION PANC. REPAIRED CONNECTOR PIN AT P1-1667. PIN E AND ALL FCC FLAP SYSTEMS PASSED RETURN TO SERVICE. (M)SDR CA020917005Rod End · broken(CAN) ON A SCHEDULED MAINTENANCE INSPECTION THE RT AILERON SWIVEL ROD END WAS FOUND STIFF. ON FURTHER INSPECTION THE BEARING RACE WAS FOUND BROKEN AND SOME OF THE BALL BEARINGS WERE MISSING.SDR UPS02239404Control Quadrant · corrodedINSPECTION TYPE:C LT I/B AILERON BUS QUADRANT FOUND TO HAVE CORROSION ON BEARING SEAT ON REMOVAL OF BEARINGS. REMOVED LOWER QUADRANT IAW MM 27-10-56, QUADRANT REPLACED IAW MM 27-10-56.SDR ABXA020149Bearing · brokenAILERONS WERE VERY DIFFICULT TO TURN TO THE LEFT WITH HYDRAULIC POWER ON. REPLACED THE RIGHT AILERON REVERSION MECHANISM BEARING ASSEMBLY FOR TAB LOCKOUT IAW DC-8 OVERHAUL MANUAL 27-6-2. PERFORMED TEST OF REVERSION MECHANISM IAW DC-8 MM 27-11-08. NO DISCREPSDR SIMA200224102Aileron · lightning strikeDFW - FLT 3473 - DURING CLIMB-OUT, AIRCRAFT WAS STRUCK BY LIGHTNING. AFTER INSPECTION REPLACED LEFT AILERON AND RIGHT ELEVATOR TRIM TAB. (M)SDR 2002FA0001101Hinge Pin · damagedDURING AN ANNUAL INSPECTION IT WAS FOUND THAT THE RIGHT OUTBOARD AILERON HINGE PIN HAD COME OUT OF THE HINGE ABOUT 5 INCHES. ONE COTTER PIN WAS STILL IN PLACE AND THE OTHER COTTER PIN WAS ONLY HALF THERE.SDR MALA020491CableON FLIGHT #2727, WHEN FLAPS SELECTED 15 DEGREES,CAPT AND FO'S YOKE VIBRATE UNTIL FLAPS SELECTED TO 20 DEGREES CAPT YOKE ALSO HAS RATTLE THAT ONLY STOPS WHEN HOLDING YOKE WITH PRESSURE. MAINTENANCE PERFORMED AILERON SYSTEM CABLE CHECK. NOTED LHOB AFT CABLE CISDR 042514Aileron · misriggedAFTER LANDING IN PANAMA CITY, FLORIDA ON FLIGHT 5466, THE CREW REPORTED THAT THE AILERON WAS RIGGED IMPROPERLY.MAINTENANCE IN PANAMA CITY FLORIDA, REINSTALLED THE CABLE DRUM AND THE CABLE TENSION. THE AIRCRAFT WAS THEN TEST FLOWN WITH SATISFACTORY RESULTS. NO SDR AUS20020952Cable · frayed(AUS) LH AILERON INTERCONNECT CABLE FRAYED IN AREA WHERE THE CABLEPASSES OVER THE CONTROL COLUMN UPPER PULLEY. PULLEY IS LOCATEDAPPROXIMATELY 200MM (8IN) BELOW THE CONTROL WHEEL.SDR SWAA021800Bearing · wornNOTICABLE BINDING IN AILERON CONTROL WHEEL. MX FERRY TO PHX. REMOVED AND REPLACED BEARINGS AT AILERON FEEL CENTERING UNIT AND F/O'S CONTROL YOKE ASSY PER MM.SDR CA020808001Pulley · frozen(CAN) FROZEN AILERONS AT FL280 CLIMBING TO FL300. A/C WAS STILL CONTROLLABLE BUT ONLY WITH A BANK ANGLE OF 5 DEG. DECIDED TO START A STRAIT DESCENT DOWN TO FL70 TO GET OUT OF FREEZING LEVEL. AT FL70 AILERON OPERATION WAS REGAINED. LANDING IN DUS WAS NORMAL.SDR VJ32002F00058Control Cable · frayedCABLE FRAYED WHERE IT PASSES THROUGH A PULLEY ASSEMBLY. CAUSE MAY BE DUE TO PULLEY NOT ROTATING WHEN CABLE IS EXERCISED. RECOMMEND TO INSTALL SEALED BEARING TYPE PULLEY IN THESE AREAS.SDR CA020827005Mixer Box · stiff(CAN) WHILE EN-ROUTE THE FLIGHT CREW EXPERIENCED AILERON CONTROL STIFFNESS & JAM. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT TOOK OFF IN HEAVY RAIN AND STANDING WATER ON THE RUNWAY. LT AILERON CABLE SYSTEM WAS INSPECTESDR CA020820002Mixer Box · damaged(CAN) WHILE ENROUTE, FLIGHT CREW EXPERIENCED AILERON CONTROL STIFFNESS AND JAM AT 25,000 FT. AUTO-PILOT DISSCONNECTED AND THE CREW WAS ABLE TO FREE THE JAM AND CONTINUED ON WITHOUT FURTHER INCIDENT. THE AIRCRAFT TOOK OFF IN HEAVY RAIN AND THERE WAS STANDING SDR CA020820001Mixer Box · contaminated(CAN) WHILE EN-ROUTE AT 29,000 FT, THE FLIGHT CREW EXPERIENCED AILERON CONTROL LOCKUP. A/P TRIM CAUTION MSG. AIRCRAFT DESCENDED TO 15,000 FT FOR 5 MIN. CONTROL RETURNED. AIRCRAFT CONTINUED TO DESTINATION WITHOUT INCIDENT. AIRCRAFT TOOK OFF IN HEAVY RAIN AND
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