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 CA000713006Control Cable · frayed(CAN) DURING DISMANTLING REQUIRED BY AD CF-98-37, ALL CABLES WERE CHANGED AS PRECAUTIONARY MEASURE. HOWEVER, UPON REMOVAL, CABLE WAS FOUND WORN AND FRAYED AT LOWER RT DOOR BULKHEAD PULLEY. AREA IS DIFFICULT TO INSPECT AT ROUTINE INSPECTION. (X)SDR CA000714018Aileron · failed(CAN) ON CLIMB OUT OF HALIFAX AT FL250 RIGHT HAND AILERON INDICATED PLUS 1 DEGREE AND JAMMED, CONTROL WHEEL STIFF TO OPERATE. AUTOPILOT TRIM MESSAGE, AUTOPILOT DISCONNECTED. ON DESCENT AILERON RETURNED TO NORMAL. LUBRICATED ALL ACCESSIBLE PIVOT POINTS AT POWERSDR 2000UALA00320Control Cable · icedAT CRUISE, FL390, WITH AUTO THROTTLE AND AUTO PILOT ENGAGED, AUTO PILOT DISCONNECT LIGHT SHOWN & AURAL WARNING SOUNDED. PITCH-YAW DISENGAGED. AILERON MOVEMENT RESTRICTED. A-P DISCONNECT BAR USED. NO HELP. USED 15LBS PRESSURE TO DISENGAGE AILERONS. RE-OCCURREDSDR COMA0060478Aileron · sluggishA/P TRIM CAUTION MESSAGE. LITTLE TO NO CONTROL OF AILERONS. ELEVATORS ALSO EXTREMELY DIFFICULT TO MOVE. COULD NOT DUPLICATE. INSPECTED ALL FLIGHT CONTROLS AND CABLE RUNS. COMPLIED WITH FUNCTIONAL AND OPERATIONAL TEST OF AILERONS AND ELEVATORS. NO DEFECTSSDR 20000621SH001Bellcrank · fodPILOT WAS PERFORMING AEROBATICS WHEN, DURING A ROLL TO THE RIGHT, THE CONTROL STICK JAMMED DURING HIS ATTEMPT TO STOP THE ROLL. HE SLOWED/STOPPED THE ROLL USING ALL AVAILABLE AILERON INPUT USING FULL LEFT RUDDER. IN A HEAVY SLIP, HE WAS LOOKING AT AVAILABLE SDR C2XA00IA140Control Cable · misroutedDAL-IAH - FLT 4208 - DURING FLIGHT, THE CREW REPORTED A BINDING AND GRINDING DURING AILERON MOVEMENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE FOUND THE RIGHT UPPER AILERON CABLE TO BE MISROUTED. MAINTENANCE REMOVED AND REPLACED THE AFFESDR CA000519019Bearing · stuck(CAN) ON APPROACH, PILOT REPORTED THAT EXCESSIVE FORCE WAS REQUIRED TO MOVE AILERONS WITH AN INTERMITTENT LOSS OF ARTIFICIAL FEEL. INSPECTION REVEALED THE LEFT REAR QUADRANTS BEARING WAS STIFF. BOTH QUADRANTS REPLACED.SDR 20000523SH028Torque Tube · failedUPON ANNUAL INSPECTION, FOUND LT AILERON WITH EXCESSIVE PLAY. REMOVED TORQUE TUBE AND FOUND THREADED PORTION OF TUBE NOT THREADED TO THE TOP OF TUBE. TUBE REMOVED FROM SERVICE AND INSTALLED NEW TUBE. THE ROD ENDS WERE ALSO REPLACED WITH NEW. (X)SDR 00FDEA00345Actuator · inoperativeAIL DEFLECT DISAG LEVEL 2 CATUION DURING FLAPS RETRACTION. *S/D* REMOVED AND REPLACED AILERON ACTUATOR ASSY IAW MD 11, RIG AND ADJUSTMENT PER MD11 MM 27-16-02-4. OK FOR SERVICE.SDR 20000613SH007Pushrod Tube · failedLEFT WING AILERON PUSH ROD FOUND MISSING PLASTIC BEARING CAUSING RIVETS TO WEAR THROUGH PUSH ROD IN 2 PLACES. (X)SDR QXEA0001335Control Cable · chafedPDX- RIGHT HAND UPPER ANTI-UPFLOAT CABLE IS CHAFING ON THE NR 1 LIFTDUMPER OUT HYDRAULIC LINE B-NUT DIRECTLY ABOVE THE NR 2 MAIN LANDING GEAR. THE CABLE HAS APPROX 50 PERCENT WEAR. REPAIRED IAW FOKKER SRM 27-11-00 PAGE 512.SDR 2000UALA00234Compensator · leakingHYDRAULIC SYSTEM A FAILURE ON TAXI OUT PRIOR TO TAKEOFF. *S/D* FOUND ''A'' SYSTEM AILERON FLIGHT CONTROL MODULE COMPENSATOR CARTRIDGE LEAKING. REPLACED COMPENSATOR PER MAINTENANCE MANUAL. SERVICED HYDRAULIC SYSTEM. PRESSURIZED ''A'' SYSTEM, NO LEAKS NOTEDSDR AU000365Control Cable · worn(AUS) RIGHT AILERON CONTROL CABLES WORN BEYOND LIMITS IN THE AREA OF THE OUTER GUIDES.SDR CA000511041Bearing · rough(CAN) THE FLIGHT CREW REPORTED THAT THE AILERON MOVEMENT WAS ROUGH AND WAS MAKING A ROUGH SOUND. MAINTENANCE FOUND A ROUGH BEARING IN THE AILERON TORQUE TUBE HOUSING SUPPORT. THE BEARINGS WERE REPLACED WITH NEW.SDR CA000516019Rod · corroded(CAN) X-RAY INSPECTION OF AILERON PUSH ROD REVEALED SEVERE INTERNAL CORROSION.SDR COMA0060357Servo · failedTHE AILERON SERVO FAILED MOUNT CLUTCH TORQUE CHECK WHEN PERFORMING EO 05-08. REMOVED AND REPLACED AILERON SERVO MOUNT.SDR SIMA1103Rod · disconnectedDFW - FLT 3751 - RIGHT AILERON JAMMED ON FLIGHT CONTROL CHECKS. INTERCONNECT UNIT WAS OVERPOWERED. INSPECTED AILERON SYSTEM AND FOUND CONTROL ROD THAT ATTACHES TO POTENTIOMETER DETACHED FROM SHAFT. BOLT, NUT, AND COTTER PIN WERE STILL IN PLACE. CONTROL RODSDR CA000530023Rod · cracked(CAN) FLIGHT CONTROL ROD FROM BELLCRANK TO AILERON FOUND CRACKED. ROD REPLACED.SDR CA000519001Bracket · cracked(CAN) WHILE CONDUCTING CF-61-12, AILERON MASS BALANCE WT INSPECTION. A CRACK WAS FOUND IN SUPPORT BRACKET.SDR 20000424SH024Pin · brokenTHE AILERON PCU SUMMING LEVER WAS BINDING AND WAS NOT PROVIDING INPUT COMMANDS TO THE UNIT. FOUND PIN 3170314 IN 3 PIECES WHICH ALLOWED THE CRANK AND SLIDE TO BECOME DETACHED FROM THE SUMMING LEVER INPUT. ALSO, FOUND ONE BALL IN BEARING MB538 SPLIT IN TWO, BUSDR AWXA0000145Servo · malfunctionedAFTER TAKEOFF, LT AILERON HAD UPWARD DEFLECTION WITH NEUTRAL STICK, FLT CONT PAGE AND VISUAL CONFIRMED LT AILERON UP, RT AILERON NEUTRAL, MANUALLY FLEW A/C. COMPLIED WITH CRITICAL ALERT FUP. SECURITY, RIG, AND WIRING CHECKS COMPLETED. NO DEFECTS FOUND. RESDR MALA000187Panel · failedAT 300 FEET ABOVE THE GROUND, DURING LANDING PHASE. RECEIVED AN UNCOMMANDED LEFT AILERON TRIM RUN-A-WAY . TRIM INDICATOR FOR LEFT AILERON RAN CONTINOUSLY TO THE DOWN POSITION. BOTH AUTOPILOT AND YAW DAMPER WERE DISENGAGED SEVERAL MINUTES PRIOR. MAINTENANCESDR AU000312Control Cable · worn(AUS) RIGHT WING FORWARD INBOARD AILERON CABLE AND LEFT WING AFT INBOARD AILERON CABLE SEVERELY ERODED IN THE AREA WHERE THEY EXIT THE FUSELAGE.SDR UIEA0008Actuator · failedFLT 64 - AIRCRAFT DIVERTED TO ATL DUE ON CLIMB-OUT WITH AILERONS AND RUDDER TRIM SET TO ZERO, REQUIRED 3.5 UNITS OF LEFT AILERON TO MAINTAIN LEVEL FLIGHT AND 6 UNITS OF RUDDER TRIM TO NEUTRALIZE AILERONS. MAINTENANCE AT ATL FOUND TWO RIVETS SHEARED IN THE AILSDR 20000330SH010Control Cable · damagedDURING ANNUAL INSPECTION, FOUND CABLES DETERIORATED AND FRAYED AS WOULD BE FOUND IF INSPECTING SERIES AS AN AA1, AS SPECIFIED IN AD 72-6-2. AS THE REST OF THE GRUMMAN SINGLE ENGINE FLEET HAS SIMILAR CABLE RUNS AS THE AA1 SERIES AND THE EARLY AA5''''S WITH EARSDR 00FDEA00135Control Cable · twistedAILERON LOCKOUT SLAT INPUT CABLE 85B. REMOVED AND REPLACED AS PER MM 20-20-06. ADJ AND OPER CK CARRIED OUT PER MM 27-10-00, FOUND SATISFACTORY.SDR CA000307004Bearing · lack of lube(CAN) PILOTS REPORT THE AILERONS ARE STIFF IN FLIGHT. ROLL INPUT TO CONTROL AILERONS VERY STIFF. OK WITH ROLL DISCONNECT ENGAGED. SPOILER INPUT FORCE OK FOR TYPE. A/C LANDED WITHOUT INCIDENT. MAINT FOUND LEFT HAND LOWER AILERON BELLCRANK BEARING STIFF ANDSDR ABXA000132Trim Motor · contaminatedUNABLE TO MOVE AILERON TRIM KNOB IN CRUISE FLIGHT. INSPECTED AILERON TRIM TAIL SYSTEM. FOUND AFT ACTUATOR TO HAVE WATER CONTAMINATION. CLEANED, INSPECTED AND LUBED LEFT AND RIGHT TRIM ACTUATOR AS PER DC9 O/H MANUAL 27-10-6. PERFORMED AILERON TRIM CONTROL CSDR CA000306001Control Cable · frayed(CAN) DURING ROUTINE INSPECTION MAINTENANCE FOUND THE AILERON CABLE WAS FRAYED BEYOND LIMITS. LOCATION WAS ON FIRST PULLEY BELOW CONTROL YOKE IN COCKPIT PEDESTAL. ACCESS IS FROM BELLY PANEL IMMEDIATELY BEHIND NLG WHEELWELL.SDR DLM88000327Servo · failedDESCENDING FROM FL 350 TO FL 280 THE A/P TRIPPED OFF THE A/C WOULD NOT TURN TO THE RIGHT.(YOKE WOULD NOT GO PAST NUETRAL, LEFT TURN OK, A/C WOULD TURN RIGHT WITH RUDDER AND AILERON TRIM. AT APPROXIMATELY 18,000 FT THE CONTROLS BECAME EFFECTIVE. PRESSISDR MALA000153Vibration · detectedVIOLENT SHAKING OF A/C FELT BY ALL CREW MEMBERS AND PASSENGERS. OCCURRED IN TURNS A/S 160KTS ON CLIMBING OUT OF DTW 2ND PT INTO APN CLEAN CONFIG. MX INSPECTED A/C AND OPENED PANELS 152BB, 151DB, 631AT, 531AT, ALL CHECKS GOOD. REMOVED AND REINSTALLED RT AND SDR CA000224001Adc · failed(CAN) DURING INSPECTION, AILERION DISCONNECT UNIT FAILED TO RELEASE ON HANDLE OPERATION OR DIFFERENTIAL CHECK. UNIT REPLACED.SDR 20000407SH031Support Bracket · crackedDURING ROUTINE MAINTENANCE, FOUND LT AILERON BELLCRANK LOWER SUPPORT BRACKET CRACKED AT FORWARD BOLT HOLE. REPLACED BRACKET WITH NEW PART. LAST YEAR, THE SAME BRACKET ON THE RIGHT WING WAS ALSO CRACKED ALLOWING BRACKET TO FLEX ENOUGH TO CREATE SEVERAL INCHESSDR CA000218013Block · cracked(CAN) THE PHENOLIC CRACKED OUTBOARD OF THE FLOOR SUPPORT FRAME JUST MISSING THE AILERON BRIDAL CABLE ATTACK BLOCK. IF THE CABLE WERE TO VIBRATE FORE AND AFT, IT WOULD JAM ON THE BROKEN EDGE OF THE PHENOLIC. THE PHENOLIC CRACKED DUE TO HAVING TO BEND SHARPLY INSDR 2000UALA00084Pulley Bracket · wornTHE SPOILER CABLE PULLEY ASSEMBLY LOWER BRACKET COMPLETELY WORE THROUGH DUE TO A MISROUTED LEFT HAND AILERON CABLE. *S/D* THE AILERON CABLE WAS DEFLECTED APPROXIMATELY 2.25 INCH. REPLACED THE PULLEY BRACKET ASSEMBLY, PULLEY AND AILERON CABLE.SDR SWAA000229Spoiler Mixer · bindingAILERON STIFF AND FEELS BINDING WHEN MAKING LEFT ROLL. REMOVED AND REPLACED SPOILER MIXER, RATIO CHANGER AND AILERON BUS DRUM BEARING PER MM. OPS CHECK GOOD.SDR COMA0060136Bearing · bindingCREW NOTICED SLIGHT BINDING IN AILERON'S WHEN MOVING F/O'S CONTROL YOKE. INVESTIGATION FOUND THE CAUSE TO BE THE AILERON CONTROL AFT RIGHT QUADRANTS MOUNT BEARING. THE QUADRANT ASSEMBLY WAS REPLACED. AFTER REMOVAL, A CLOSER INSPECTION OF THE QUADRANT FOUND SDR AU000072Bearing · seized(AUS) RT OUTBOARD AILERON POWER CONTROL ACTUATOR INPUT LINK BEARING SEIZED.SDR CA000203011Control Cable · broken(CAN) WHILE CLEANING EXHAUST RESIDUE FROM THE RIGHT FLAP AREA, THE BOWDEN CABLE WAS FOUND BROKEN APPROXIMATELY 6 INCHES FORWARD OF THE FLAP CONNECTION. THE SUBMITTER STATED THE CABLE WAS FABRICATED FROM GALVANIZED MATERIAL AND HAD CORRODED IN THE PRESENCE OF ESDR 2000ZZZX405Pulley · separatedWHILE REPLACING AILERON PUSH/PULL ROD, SLACKNESS IN AILERON CABLE LED TO DISCOVERY THAT AILERON PULLEY, P/N S378-4 (LOCATED UPPER STARBOARD POSITION IN REAR DOORPOST BULKHEAD ASSY), WAS NO LONGER BOLTED IN POSITION. NUT HAD WORKED OFF BOLT, BOLT HAD BACKED OUSDR 99ZZZX4660Control Cable · looseDURING ROUTINE 100-HOUR ANNUAL, NOTED AILERON CABLE TENSION WAS SLACK ENOUGH THAT THE CABLES WERE RUBBING ON THE STRINGER WHERE THEY PASSED THROUGH (BELOW THE FLOOR UNDER THE COCKPIT). THE TENSION WAS SO LOW AS NOT TO READ ON THE TENSIONMETER. THE CABLES WERSDR 99ZZZX4659Control Cable · looseDURING ROUTINE 100-HOUR ANNUAL, NOTED AILERON CABLE TENSION WAS SLACK ENOUGH THAT THE CABLES WERE RUBBING ON THE STRINGER WHERE THEY PASSED THROUGH (BELOW THE FLOOR UNDER THE COCKPIT). THE TENSION WAS SO LOW AS NOT TO READ ON THE TENSIONMETER. THE CABLES WERSDR CA991229045Boot · loose(CAN) DURING PRE-FLIGHT WALK AROUND THE PILOT NOTICED THAT THE AILERON TRAVELS WERE NOT EQUAL ON THE LEFT AND RIGHT.IT WAS FOUND THAT THE BOOT AT THE BASE OF THE CONTROL STICK HAD MIGRATED DOWN AND SNAP FASTENERS AT THE TOP OF THE BOOT HAD LODGED BETWEEN THE SDR MZZA99235Control Cable · frayedTNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A FRAYED RIGHT WING INBOARD AILERON TAB CABLE WAS FOUND ON RT TE CAVITY BELOW NR 2 AND NR 3 ENGINE FUEL FEED LINE SHROUD. THE FRAYED CABLE WAS REMOVED AND REPLACED WITH A NEW ONE AND OPERATIONAL CHSDR CA991230015Screw · out of position(CAN) THE FLGHT CREW WAS REQUESTED TO TURN RIGHT BY ATC AND FOUND THE AILERON CONTROLS JAMMED. AFTER TRYING TO MANEUVER THE AIRCRAFT, THE CONTROLS RETURNED TO NORMAL WITH A LOUD SNAP. MAINTENANCE FOUND THE LOCK SCREW AND NUT ASSEMBLY, SECURING THE AILERON CABLSDR UPS99231126Aileron · delaminatedINSPECTION TYPE:SI LT O/B AILERON T/E WEDGE IS DELAMINATED AND SATURATED WITH OIL ON THE O/B AFT END. REMOVED A 1 HALF INCH AREA OF DELAMINATED SKIN AT O/B AFT CORNER UPPER AND LOWER SURFACES AND REMOVED CONTAMINATED POTTING COMPOUND. FABRICATED REPAIR PLUGSSDR 99ZZZX4312Pulley · separatedFOLLOWING WIND STORM, DISCOVERED BROKEN AILERON INPUT CONTROL ROD ON LT AILERON. FURTHER INSP REVEALED ZERO TENSION ON AILERON CONTROL CABLES. DISCOVERED RT UPPER AILERON PULLEY THRU-BOLT COMPLETELY BACKED OUT OF PULLEY. PULLEY, BOLT, NUT, AND BUSHING FELL SDR CA991104016Bellcrank · cracked(CAN) CRACK FOUND IN AILERON BELLCRANK. BELLCRANK REPLACED. SUBMITTER STATED THIS IS THE THIRD OCCURRENCE FOR THE SAME BELLCRANK.SDR 99ZZZX4315Pushrod · fracturedWHEN PILOT CHECKED CONTROLS AT RUN-UP, THE LT AILERON PUSHROD BROKE AT FIRST THREAD FLUSH WITH FACE OF ROD END JAM NUT. SUBMITTER NOT SURE IF CAUSE WAS INTERGRANULAR CORROSION OR A MFG DEFECT. BOTH LT AND RT PUSHRODS AS WELL AS STABILATOR PUSHROD (WHICH IS OSDR AU991047Rod End · seized(AUS) AILERON CONTROL ROD ROD END SEIZED AND BROKEN.
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