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 C2XA02CL158Damper · damagedDURING A 3A INSPECTION THE LEFT AILERON DAMPER ROD END BEARING WAS FOUND LOOSE. THIS ROD END CONNECTS TO THE AILERON FITTING. FURTHER INSPECTION REVEALED DAMAGE TO THE AILERON DAMPER FITTING. THE LEFT AILERON WAS REPLACED ALONG WITH THE AILERON DAMPER. OPESDR 02FDEA00526Pushrod · defectiveLEVEL 2 -AILERON DEFLECT DISAGREE- DURING FLAP RETRACTION AT 3300 FT. PERFORMED QRH PROCEDURES. THE LEFT AILERON REMAINED DEFLECTED AFTER FLAP RETRACTION. A/C ROLLS RIGHT. RELEASED FOR SERVICE PER MEL/CDL. INSTALLED FIXED PUSH-ROD IN LEFT OUTBOARD DEFLECTSDR 2002F00868Control Cable · damagedDURING AN A15 CHECK ON AIRCRAFT, NOTICED THAT CABLES WERE JUST WITHIN LIMITS. MAINTENANCE REMOVED AND REPLACED AILERON CABLES, PULLY, OUTBOARD ROLL SPOILER CABLE, RIGHT UPPER INBOARD AILERON CABLE, AN FCD WAS ISSUED TO INSPECT THE DHC8 FLEET. RESULTS PENDSDR AUS20020787Bolt · fractured(AUS) RT AILERON PCU RODEND BOLT HEAD BROKEN.SDR CA020809001Control Cable · frozen(CAN) PILOT REPORTED THAT THE AILERON TRIM MESSAGE WAS DISPLAYED ON EICAS WHILE IN CRUISE AND THAT AILERONS WERE VERY STIFF. AIRCRAFT DECENDED TO A LOWER ALTITUDE AND PROBLEM CLEARED. CREW REPORTED THAT THERE WAS HEAVY RAIN ON TAKE OFF. AIRCRAFT LANDED WITHOSDR SWAA021667Bearing · wornDURING SCHEDULED C4 CHECK, FOUND EXCESSIVE MOVEMENT AT RT OTBD AILERON QUADRANT PIVOT. REMOVED AND REPLACED AILERON QUADRANT BEARINGS PER MM.SDR GUUA07270207Bearing · wornINTERMITTENT VIBRATION FELT IN CONTROL WHEEL IN FLIGHTDETERMINED RIGHT YOKE BEARING TO BE WORN, BUT WITHIN LIMITS. REPLACED RIGHT AILERON YOKE BEARINGSDR SWAA021630Drum · out of adjustAILERON CONTROL RESPONDING ERRATIC WHEN TURNING LEFT AT SLOW SPEEDS. FOUND,UPPER BUS DRUM LUG, OUT OF ADJUSTMENT. ADJUSTED PER MM.SDR CA020801003Actuator · failed(CAN) RT AILERON LOCKED OUT DURING FLIGHT AFTER LEAVING YVR. RT LOCK OUT ACTUATOR REPLACED PER AMM 27-11-44 PG 1-12 OPERATION CHECKED SERVICEABLESDR 02FDEA00495Warning Light · illuminatedLEVEL 2 -AIL DEFECT DISAG- ALERT ILLUMINATED DURING FLAP/SLAT RETRACTION ON T/O. RECYCLED FLAPS IAW QRH. ALERT EXTINGUISHED MOMENTARY THEN REAPPEARED AFTER FLAP/SLAT RETRACTION.SDR QXEA0200957Servo · fouledPDX - AIRCRAFT RETURNED TO FIELD WHEN A SLIGHT BINDING WAS NOTED IN THE AILERON. MAINTENANCE INSPECTED THE AIRCRAFT AND REPOSITIONED THE SAFETY WIRE PIGTAILS ON THE AILERON SERVO. OPERATIONAL CHECK WAS PERFORMED AND WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVISDR ABXA020142Control Quadrant · damagedAILERON CONTROL QUADRANT ASSEMBLY, FOUND DAMAGE AT BEARING SEAT. REPAIRED AREA IAW REA B627-43542-MR.SDR WRLA200215Actuator · inoperativeAILERON DEFLECT DISAGREE LEVEL ALERT AFTER TAKE OFF AND AT SLAT RETRACT. SLATS AND FLAPS (15) RECYCLED WITH ALERT REMAINING. CONFIG. PAGE AND VISUAL SCAN CONFIRMED LEFT OUTBOARD AILERON WAS DEFLECTED. CHECK LIST PREFORMED AND RETURNED TO STATION. ENTERED ISDR ABXA020056Tube · wornLEFT LCCA CONTROL TUBE ASSEMBLY HAD WORN PIVOT BEARINGS. REPLACED LEFT LCCA TRUBE ASSEMBLY IAW B767 MM. OPS CHECKED GOOD.SDR ABXA020055Bearing · wornRT OUTBOARD AILERON, INBOARD PCA REACTION LINK BEARINGS WORN. REPLACED AILERON PCA IAW B767 MM. OPS CHECKED GOOD.SDR ABXA020054Bearing · wornRT OUTBOARD AILERON, OUTBOARD PCA REACTION LINK BEARINGS WORN. REPLACED AILERON PCA IAW B767 MM. OPS CHECKED GOOD.SDR ABXA020053Tube · wornRIGHT LCCA TUBE ASSEMBLY HAD WORN/RUSTED PIVOT BEARINGS. REPLACED LCCA TUBE ASSEMBLY IAW B767 MM. OPS CHECKED GOOD.SDR SWIA200211083Control Cable · corrodedRIGHT WING AILERON CABLES FROM THE TENSION REGULATOR INBOARD TO THE WHEEL WELL ARE CORRODED. RIGHT WING AILERON CABLES REPLACED IAW CRJ MM 27-00-00-960-802.SDR ABXA010912Bearing · seizedCAPTAIN'S AND FIRST OFFICER'S AILERON CONTROL WHEEL BINDING. COMPLIED WITH FIM 27A-11-00, FIG 106, BLOCK 1,2. FOUND BEARING ON LEFT WHEEL WELL QUADRANT CENTERING FORCE SEIZED. REPLACED BEARING IAW BOEING STANDARD OVERHAUL PRACTICES MANUAL 20-50-03. AILERONSDR COMA0260368AileronFLIGHT 5759 HEAVIER THAN NORMAL CONTROL FORCE REQUIRED FOR ROLL AND PITCH.INSPECTED FLIGHT CONTROLS AND CABLE TENSIONS. NO DEFECTS FOUND. FORCE CHECKS WITHIN LIMITS.SDR CA020610006Control Unit · lack of lube(CAN) AUTOPILOT TRIM RWD/LWD AFTER T/O AUTO PILOT DISCONNECTED AND FOUND DIFFICULT TO MOVE AILERONS.(L1255080) BOTH LT AND RT AILERON QUADRANTS LUBRICATED WITH BRAYCO NR 300 TO DISPLACE MOISTURE AND AILERON INSPECTION CHECK CARRIED OUT. OPS CHKS NORMAL SERVICESDR COMA0260359ShieldFLIGHT 6000 A/P LWD CAUTION MESSAGE. AILERON CONTROL FORCE VERY STIFF.ADJUSTED THE WHEEL BIN SPLASH GUARDS - NO OTHER DEFECTS NOTED.SDR XNOA01048Indicator · incorrectCOULD NOT GET FULL DEFLECTION LT AILERON. REMOVED & REPLACED SURFACE POSITION INDICATORS AS REQ IAW A300 MM REF 27-25-00. CONTROL SURFACES NORMAL. OPS CHECK GOOD ON GROUND.SDR COMA0260353Bellcrank · bindingFLIGHT 5296 A/P LWD CAUTION MESSAGE - AILERON CONTROLS ARE STIFF.REPLACED THE L/H AFT AILERON CONTROLS BELLCRANK ASSY.SDR DL76G020612Control Unit · malfunctionedIN CRUISE LOST LEFT SYMBOL GENERATOR FOLLOWED 5 MINS LATER BY RUDDER RATIO AND AILERON LOCKOUT EICAS MSGS AND LOSS OF ALL 3 AUTOPILOTS. FOUND LEFT SAM W/ FAULT BALL. WILL NOT RESET. CYCLED 1L AND 2LAC AND DC FLT CTL ELEC C/B'S. ALL FAULTS CLEARED. REPLACESDR CA020604001Aileron · jammed(CAN) AT FLIGHT LEVEL 310 AILERON SYSTEM PARTIALLY JAMMED RT AILERON 2 UNITS UP. REQUESTED LOWER ALTITUDE FLIGHT LEVEL 280 AND AILERON IMPROVED. AIRCRAFT FLOWN MANUALLY, APPROACH NORMAL (SUSPECT CABLE RUN HUMIDITY/FROZEN) AILERON REAR LT & RT QUADRANT LUBRISDR WRLA200211Actuator · inoperativeLEVEL 2 AILERON DEFLECT DISAGREE. (AIRCRAFT RETURNED TO DEPARTING STATION) TROUBLESHOOTING CARRIED OUT. GENERAL VISUAL INSPECTION OF ALL AILERON DEFLECTION ACTUATOR CONNECTORS AND PINS CARRIED OUT. NO DEFECTS NOTED. LEVEL 2 MESSAGE CLEARED. SYSTEM OK, OPSDR VJ32002F00039Rod · chafedAILERON ROD RUBBING AILERON BELL CRANK. REMOVED ROD AND INSTALLED NEW ROD. CONTROL ASSEMBLY WAS SHIMMED TO CORRECT THE PROBLEM.SDR SWIA200210899Bearing · ratchetingLEFT AILERON RATCHETS WHEN MOVED FULL UP AND DOWN. REPLACED LEFT AILERON WING QUADRANT BEARING, VERTICAL SWIVEL JOINT AND ACTUATING ARM WITH SERVICEABLE UNITS. OPS CHECK GOOD.SDR CA020523003Control Cable · dirty(CAN) CLIMBING THROUGH 23000 FT THE AILERONS BECAME STIFF AT -22C . AUTOPILOT MANUALLY DISCONNECTED . AILERON TRIM MOVED BUT YOKE DID NOT. CONTROL RETURNED AT 20000 FT AND +4C . AIRCRAFT LANDED WITHOUT INCIDENT. LT & RT TENSION REGULATORS INSPECTED FOR MOISTURSDR ACE0515021Yoke · crackedWHILE PERFORMING A SCHEDULED AILERON YOKE INSPECTION, FOUND THE RT AILERON YOKE CRACKED ON ONE SIDE OF THE TAPER PIN HOLE. ALONG THE GRAIN OF THE METAL. THIS COMPONENT WAS INSPECTED AT LEAST ONCE WITHIN THE PREVIOUS 2000 FLIGHT HOURS.SDR 02FDEA00331Actuator · failedON TAKEOFF AFTER SLATS RETRACTED LVL 2 AIL DEFLECT DISAGREE ALERT ILLUM'D. REMOVED AND REPLACED LT & RT INBOARD DEFLECT AILERON ACTUATORS PER MM 27-16-01-4. RIGGED, ADJUSTED AND TESTED OK.SDR COMA0260308Bellcrank · dirtyFLIGHT 5883 A/P TRIM LWD CAUTION MESSAGE. AILERONS VERY STIFF.COULD NOT DUPLICATE PROBLEM ON GROUND - AILERON AFT BELLCRANK ASSY WERE DETERMINED TO BE MOST PROBABLE CAUSE AND WERE REPLACED.SDR COMA0260307Bellcrank · dirtyFLIGHT 5261 - A/P TRIM LWD CAUTION MESSAGE. AILERON CONTROLS LOCKED UP.COULD NOT DUPLICATE PROBLEM ON GROUND - AILERON AFT BELLCRANK ASSY WERE DETERMINED TO BE MOST PROBABLE CAUSE AND WERE REPLACED.SDR COMA0260306Bellcrank · dirtyFLIGHT 5296 AILERON CONTROLS LOCKED UP, MINIMUM CONTROL AVIABLE. COULD NOT DUPLICATE PROBLEM ON GROUND - BOTH THE LT AND RT AILERON AFT CONTROL CABLE QUADRANTS WERE REPLACED AS THE MOST PROBABLE CAUSE OF DISCREPANCY.SDR F3LA200200136Control Cable · brokenFLIGHT CREW REPORTED SIGNIFICANT RT ROLL TENDENCY ON FINAL APPROACH AND LANDING. CORRECTED ON TOUCHDOWN. FOUND AILERON BUS CABLE BROKEN. REMOVED RT AILERON CABLE ABSB-4 AND FABRICATED, INSTALLED, ADJUSTED AND TESTED REPLACEMENT CABLE PER MM 27-11-0, 27-09-1SDR UPS02238313Hinge Fitting · crackedINSPECTION TYPE:C R/H O/B AILERON, 2ND HINGE FITTING FROM O/B HAS 2 SUSPECT CRACKS EMA NATING FROM BOTH UPPER FITTING FASTNER HOLES REPLACED R/H O/B AILERON FITTING IAW DRAWING 65-19259SDR SWAA020958Roller · wornBINDING IN AILERONS DURING FLAP MOVEMENT. REMOVED AND REPLACED CENTERING MECH CAM ROLLER PER MM.SDR 2002F00630Pulley Bracket · looseAT SCHEDULED THIRD 200 HOUR INSPECTION, DISCOVERED THE AILERON LEFT DOWN CONTROL CABLE TO BE FRAYED. DETERMINED CABLE FRAYING CAUSED BY INCOMPLETE INSTALLATION OF PULLEY MOUNTING BRACKET. SECURED BRACKET , AND REPLACED PULLEY AND CABLE. (M)SDR 2002FA0000629Control Cable · brokenALL FOUR CONTROL CABLES HAD STRANDS BROKEN. THE LEFT FORWARD CARRY THRU CONTROL CABLE HAD APPROXIMATELY 70 PERCENT OF ITS STRANDS BROKEN DUE TO CONTACT WITH PULLEY GUARD. THE OTHER PROBLEM IS WHERE CONTROL CABLES COME OUT OF FUSELAGE RUBBING ON PHENOLIC BLOCSDR 2002FA0000542Control Cable · brokenLEFT AILERON DIRECT CONTROL CABLE SEPARATED IN FLIGHT RESULTING IN A FATAL ACCIDENT. THE CABLE P/N 0510105-224 WAS VERY BADLY RUSTED AT THE POINT OF FAILURE LOCATED ABOVE THE RIGHT DOORPOST WHERE THE CONTROL CABLE RIDES OVER A PULLEY. THE PULLEY IN THIS AREASDR COMA0260268AileronFLIGHT 5375 ABORTED T/O DUE TO AILERON CONFIG WARNING.COULD NOT DUPLICATE. AILERON TRIM AND RIGGING FOUND SATISFACTORY.SDR DHL2002807545Aileron · crackedITEM: REF.: N/R 1754 LT. INBD. AILERON L/E UPPER SKIN CRACKED .250 @ STA. XA508.000CORR: PERFORMED MAJOR REPAIR IAW DHL EO020422, ED2893 , EO SEMANS 2002287SDR COMA0260259Hinge Fitting · oversizedTHE R/H AILERON HAS A SLIGHTLY OVERSIZE HOLE IN THE INBOARD HINGE FITTING AT STA 343.FABRICATED AN OVERSIZE BUSHING I/A/W WVAC EO 601R-57-3130 AND INSTALLED BUSHING I/A/W CRJ AMM 20-26-00910-803.SDR C8GA20020006Rod End · brokenFlight DAE001 from MIA to PTY. After takeoff during climb, crew could not keep aircraft level. Applied 5 units of trim and left rudder required to maintain level flight. Aircraft returned to MIA and landed without further incident. Upon landing found 2 rigSDR CA020410002Bellcrank · mismanufactured(CAN) DURING INSPECTION THAT REQUIRED REMOVAL IT WAS NOTICED THAT THE HOLE IN THE OUTPUT ARM (AILERON PUSHROD ATTACH POINT) HAD BEEN INCORRECTLY DRILLED TO 5/16 INCH INSTEAD OF 1/4 INCH. THIS ALLOWED LOST MOTION BETWEEN THE PUSHROD AND BELLCRANK. THE BORE SDR CA020502016Actuator · failed(CAN) AILERON LOCKOUT MESSAGE ON EICAS. REPLACED LEFT OUTBOARD LOCKOUT ACTUATOR.SDR DHL2002807544Aileron · crackedITEM: REF.: N/R 1756 LT. WING INBD AILERON UPPER SKIN CRACKED 1/2" @ STA. XW563.000CORR.: PERFORMED MAJOR REPAIR IAW E.O. DHL020320 , ED2861 , EO SEMANS 2002262. TRIMMED OUT CRACKED SKIN IAW EO DHL020320,ED2861,EO SEMANS 2002262. CLEANED , TREATED , PRIMED ARESDR ABXA010841Fitting · brokenLEFT INBOARD AILERON, INBOARD HINGE FITTING WAS BROKEN. INSTALLED NEW FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-21A, 51-3-0, 51-1-21, 51-1-24 AND 51-1-20D.SDR COMA0260239AileronFLIGHT 6066 AILERON CONFIG WARNING DURING T/O.COULD NOT DUPLICATE. INSPECTED AILERON SYSTEM - NO ABNORMALTY FOUND.
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