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 QXEA2015072600401Aileron Sys · malfunctionedAFTER PUSHBACK AND PRIOR TO TAXI, F/O NOTICED RESISTANCE TO AILERON WHEN DEFLECTED TO THE RT. SMOOTH DEFLECTION TO THE LT. RETURNED TO GATE. PERFORMED GVI OF LT AND RT WING AILERON CONTROL SYS AND GAP SEALS. NO DEFECTS NOTED. ACCOMPLISHED OPS TEST OF AILSDR CA150724004Control Cable · worn(CAN) DURING A SCHEDULED 3000 FH INSPECTION AN AILERON CONTROL CABLE IN THE L/H WING SHOWED WEAR BETWEEN RIBS 5 AND 6, THERE WAS NO VISIBLE CONTACT ON ADJACENT STRUCTURE.SDR CA150724003Control Cable · worn(CAN) DURING A SCHEDULED 333FH INSPECTION AN AILERON CONTROL CABLE IN THE R/H WING SHOWED WEAR BETWEEN RIBS 5 AND 6. THERE WAS NOT VISIBLE CONTACT ON ADJACENT STRUCTURE.SDR CA150710007Cable · corroded(CAN) AIRCRAFT HAS A HISTORY OF AUTOPILOT DISENGAGING ON ITS OWN WHILE IN FLIGHT. MDC LOGGED PITCH SERVO CIRCUIT. WHILE TROUBLESHOOTING THE PITCH SERVO CIRCUIT ISSUE, MX NOTICED THAT THE CONTROL WHEEL WAS NOT MOVING DURING THE CHECK OF THE AUTOPILOT AND THAT TSDR HALA2015060100124Aileron Sys · out of rigINBOUND AILERONS NOT DROOPING SYMETRTICALLY. RT DROOPING TOO FAR LT NOT DROOPING ENOUGH. POSSIBLE INDICATION, MALFUNCTION. TEST AILERONS, RESET FLIGHT CONTROL COMPUTERS. TRIMMED AILERONS TO ZERO. PERFORMED MCDP TESTS 1, 7, 30, 40, 66, 67. ACFT AILERONS CSDR COEA2015062807900Bellcrank · corrodedHEAVY CHECK. RIGHT AILERON TRIM TAB BELLCRANK HAS LEVEL 2 CORROSION. REPLACED BELLCRANK.SDR CA150624001Bearing · stiff(CAN) PILOT DEPARTED & DID A NORMAL CLIMB TO FL280. AROUND 1425Z HE HAD CAS CAUTION MSG AP HOLD LT WING DN. DISENGAGED THE AUTOPILOT & FOUND THAT THE AILERONS WERE BLOCKED IN NEUTRAL POSITION. REQUESTED A LOWER ALTITUDE & A RETURN STARTED DESCENT 1429Z GOINSDR CA150619002Actuator · binding(CAN) WHEN CONDUCTING THE AILERON CONTROL CHECK DURING TAXI, THE FLIGHT CREW DETECTED UNUSUALLY HIGH FORCE REQUIRED IN ROLL. CREW COULD ALSO HEAR A SERVO NOISE WHEN MOVING THE AILERONS. REPLACED THE AUTOPILOT ROLL ACTUATOR & THE SYS WAS TESTED SERVICEABLE. SDR QXEA2015061000321Trim Panel · malfunctionedAILERON TRIM RUNAWAY FULL DEFLECTION LT & RT. TRIM BUTTON WAS STICKING ON. RETURNED TO FIELD. LANDING UNEVENTFUL. R & R AILERON/RUDDER TRIM CONTROL PANEL, REF AMM TASKS 27-13-16-000-801 & 27-13-16-400-801. OPS CHECKS GOOD. RETURNED TO SERVICE.SDR QXEA2015061000319Trim Panel · malfunctionedAFTER TAKE OFF, EXPERIENCED A SUDDEN RWD ROLL INPUT THROUGH THE YOKE. HELD WINGS LEVEL MANUALLY. THEN NOTICED AILERON TRIM INDICATED FULL SCALE RWD. RETRIMMED TO NEUTRAL. AILERON TRIM SYS OPERATED NORMALLY FOR THE REST OF THE FLIGHT. REPLACED AILERON/RUDDESDR QXEA2015060900320Trim Panel · malfunctionedBOTH CONTROL YOKE DEFLECTION IS VERY HARD WHEN TURNING TO THE RT BOTH ON THE GROUND AND IN THE AIR. FEELS "RESTRICTED OR BOUND UP". AFTER PULLING ROLL DISCONNECT ON THE GROUND CAPTAINS YOKE TURNS FREELY, SPOILERS, BUT F/O'S YOKE, AILERONS FEELS VERY STIFF ANSDR AALA20150601005Actuator · faultyEMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH AILERONS UNLOCKED. R & R LT OTBD AILERON LOCKOUT ACTUATOR IAW AMM 27-11-44.SDR 2015FA0000252Aileron · crackedPERFORMED SB 1216B DISCOVERED CRACK AT AILERON ATTACH POINT ON BOTH THE LT AND RT AILERON.SDR 2GYR2015FA0000247Cable · displacedWHILE IN THE PROCESS OF PERFORMING AN INSPECTION ON ACFT. FOUND IN THE RT WING, AILERON WING SECTOR AREA, THE CABLE COMPLETELY OFF THE PULLEY. THE REFERENCE FOR THIS PULLEY IS 27-10-00, FG. 3, IT 50, PN S3504-4.5. LOW FRICTION PULLEY, RT.SDR WC73201506021988Control Cable · chafedDURING ROUTINE INSPECTION THE LT AILERON CABLE WAS FOUND CHAFED WHERE THE CABLE TRAVELS THROUGH THE INBD CLOSEOUT RIB FOR THE INBD L/E SECTION INBD OF WING BS BL54.85. THE AILERON CABLE HAD BEEN CHAFING OF THE ONBOARD EDGE OF THE WING SPAR HEAT SHIELD. A SIGSDR CA150515001Shaft · corroded(CAN) DURING HEAVY MX INSPECTION, THE MECHANIC SUSPECT CORROSION AT THE RT WING AILERON INPUT QUADRANT SHAFT AT THE BEARING. AFTER QUADRANT REMOVAL, THE SHAFT PN 82740083-101 WAS REMOVED FOR FURTHER INVESTIGATION, THE LEVER WAS ALSO REMOVED FROM THE ASSEMBLY SDR 2015FA0000186Control Cable · wornAILERON CABLES INSTALLED ALONG THE REAR WING SPAR PASS THROUGH THE WING RIBS WITH FAIR LEADS. EVERY 450 HOUR INSPECTION OF THE ACFT REVEAL THESE CABLES ARE WORN BEYOND LIMITS AND REQUIRE REPLACEMENT. THE CABLES ARE CHAFING ON THE FAIR LEADS DUE TO INSUFFICIENTSDR UG8A2015050501Unknown · malfunctionedUNCOMMANDED RIGHT ROLL TRIM RUNAWAY.SDR 39LA20150430134Control Quadrant · corrodedLEFT AILERON CABLE QUADRANT HAS AN AREA OF EXFOLIATION CORROSION APPROX 1.00 INCH BY .750 INCH BY .125 DEEP. REPLACED LT AILERON CABLE QUADRANT IAW AMM 27-11-02 P BLOCK 401.SDR AALA201504089016Control Servo · faultyUNCOMMANDED ROLL TO LT WITH SPOILER DEPLOYMENT, FLAPS 2. AUTOPILOT ON & OFF, AILERONS SHOWED CORRECTION TO RT. REPLACED LT GREEN AILERON SERVO CONTROL & BLUE AILERON SERVO CONTROL IAW AMM 27-14-51. ACCOMPLISHED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. SEESDR AALA201504089001Control Servo · malfunctionedUNCOMMANDED ROLL TO LEFT WITH SPOILER DEPLOYMENT, FLAPS 2. AUTOPILOT ON & OFF, AILERONS SHOWED CORRECTION TO RT. REPLACED LT GREEN AILERON SERVO CONTROL & BLUE AILERON SERVO CONTROL IAW AMM 27-14-51. ACCOMPLISHED OPERATIONAL CHECKS WITH NO DEFECTS NOTED.SDR BIGA20150406001Control Rod · wornDURING INSPECTION, THE AILERON CONTROL ROD WAS FOUND TO BE WORN APPROX 15% OF THE THICKNESS. THE ROD WAS WORN FROM THE AILERON GUST LOCK SYS & SEEMS ONLY WEAR ON THE PILOTS OTBD SIDE DUE TO A SLIGHT MISALIGNMENT OF THE GUST LOCK.SDR SWAA2015040638100Control Unit · faultyDIVERSION, SYS A ENG DRIVEN HYDRAULIC PUMP LOW PRESS LIGHT ILLUMINATED SYS A HYD QTY STABILIZED AT 1/4 FOR A LONG PERIOD THEN SLOWLY DECREASED TO NEAR ZERO. R & R A AILERON & ELEVATOR POWER CONTROL UNIT IAW MM.SDR 2015FA0000159Washer · missingRIGHT AILERON CONTROL PUSHROD FOUND MISSING WASHERS, ITEM 62 IN IPC PRINTOUT. THESE ACT AS SPACERS, AND WHEN MISSING CAUSE THE STRUCTURE TO SQUEEZE TOGETHER CAUSING AILERON SKIN WRINKLING AND POSSIBLE DAMAGE.SDR 29GA2015040100001Control Cable · out of adjustMCO AT 150KTS WITH FLAPS AT 15 DEGREES CONTROL YOKE VIBRATES AROUND LATERAL AXIS. PERFORMED LT AND RT AILERON TENSIONS, ADJUSTED LT AILERONS CABLE TENSIONS, OPS CHECK GOOD. FUNCTIONAL CHECK FLIGHT SATISFACTORY.SDR CA150312004Stop · cracked(CAN) WHILE DOING SCHEDULED INSPECTION TASKS ON "B" CHECK, A CRACK WAS FOUND IN THE RT AILERON UPPER TORQUE TUBE BEARING STOP. REPLACED WITH A NEW ONE.SDR CA150302013Actuator · cracked(CAN) THE LT OTBD ROLL SPOILER ACTUATOR VALVE BODY CRACKED AND CAUSED HYDRAULIC FLUID LOSS IN SYSTEM NR 2 IN FLIGHT.SDR SIMA20150225001Lug · gougedLEFT AILERON PCA ROD END MOUNT HAS 2 GOUGES. LT SIDE OF MOUNT GOUGE .0215 DEEP X .0730 H X .1645 L. RT SIDE OF MOUNT GOUGE .0160 X .140 H X .1825 L. ACCOMPLISHED PERMANENT REPAIR OF LT PCA ATTACH LUGS IAW ERS-EM-27MR-039.SDR HYIA20150220001BBolt · looseLEFT AILERON OTBD SHACKLE BOLT WAS FOUND LOOSE AFTER REPORTS OF SLIGHT VIBRATION IN FLIGHT FROM THE FLIGHT CREW. AILERON WAS R & R AT AN OUTSIDE VENDOR DURING 2014 HEAVY CHECK. SECURED & RE-TORQUED SHACKLE BOLT NUT IAW AMM JIC 20-21-12. NO FURTHER DEFECTS FSDR HYIA20150220001Bolt · looseLEFT AILERON OTBD SHACKLE BOLT WAS FOUND LOOSE AFTER REPORTS OF SLIGHT VIBRATION IN FLIGHT FROM THE FLIGHT CREW. SECURED & RE-TORQUED SHACKLE BOLT NUT IAW AMM JIC 20-21-12. NO FURTHER DEFECTS FOUND.SDR DXTA2015021705981Spring · failedAILERONS COMPLETELY FROZEN IN FLIGHT. DISCONNECTED AUTOPILOT, NO ROLL CONTROL. DESCENDED TO FL310 TO REGAIN CONTROL & ROLL BEGAN TO IMPROVE. REGAINED FULL CONTROL AT FL250. REMOVED AFU & INSTALLED A NEW UNIT. OPS CHECKED GOOD WITH NO DEFECTS NOTED IAW AMMSDR CA150216001Servo · failed(CAN) CREW RECEIVED FLIGHT CONTROL AILERON SERVO FAULT PLUS UNCOMMANDED 10-15 DEGREES BANK. EICAS SHOWING G IN AMBER UNDER R AILERON RESOLUTION R/H I/B AILERON PCU REPLACED AND TESTED IAW AMM 27-14-51.SDR CA150213011Aileron Sys · malfunctioned(CAN) INITIAL REPORT OF ROLL CONTROL STIFF DURING LEFT AND RIGHT TURNS. ON GOING TROUBLESHOOTING FOUND NUMEROUS ITEMS CONTRIBUTING TO THE STIFFNESS DETECTED IN THE ROLL CONTROL SYSTEM. REPLACED MULTIPLE PULLEYS CONTROL CABLES BEARINGS IN PILOTS CONTROL WHEEL CSDR CA150210008Pulley · corroded(CAN) WHILE UNDERGOING TROUBLESHOOTING FOR A FLAP FAULT, THE AILERON CABLE PULLEYS WERE OBSERVED TO HAVE RUST EMANATING FROM THEM, ONCE INSPECTED IT WAS DETERMINED THAT THEY WERE CORRODED AND HAVE BEEN REPLACED.SDR SWAA2015021236555Aileron · bindingBINDING FELT DURING AILERON OPERATION. COMPLIED WITH MT 727-10-00.SDR A6WA201542386Aileron · bindingAUTOPILOT ENGAGED, AILERON TRIM INDICATOR A, MANUALLY DISCONNECTED, AUTOPILOT HAD LT WING DOWN TENDENCY, BINDING AILERON & CLUNKING SOUND WHEN ACTUATEDSDR CA150204002Control Cable · frayed(CAN) DURING INSPECTION, CORROSION, WEAR & FRAYING OF THE AILERON CABLES WAS IDENTIFIED AT THE AFT INBD, WING AREA ABOVE THE MLG ASSEMBLIES WHERE THE CABLES ARE EXPOSED. SAME FINDINGS LT & RT, PN BA670-93210-29 & PN BA670-93210-31 CABLES, 4 REPLACED WITH NEW SDR BQVA20150129001Control Cable · chafedLEFT WING AILERON CABLE CHAFING AT OTBD BELL CRANK.SDR CA150128004Pulley · seized(CAN) AILERON CABLE PULLEYS BY GUST LOCK UNIT FOUND WITH WORN CENTRE BEARINGS FALLING OUT. AMM FIG201 ATA-27-12-00 PG 218 AT STATION Y.7.500 DETAIL N (REPORTED ON A-3 CHECK) PULLEYS REPLACED AS PER AMM 27-10-11 FUNCTION CHECK DUALS .SDR JZRR2015011200001Control Cable · frayedTHE FRAYED AILERON CONTROL CABLE WAS FOUND DURING A FINAL INSPECTION AFTER THE ACFT WAS STRIPPED & PAINTED. THE CABLE WAS LOCATED, VISUALLY, IN THE RT FLAP WELL INBD OF THE AILERON BELL-CRANK BETWEEN TWO RIBS, WS 133.29 & 151.04. THE FRAYED CABLE WAS IN PLAINSDR CA150207002Bearing · damaged(CAN) CREW REPORTED AILERONS STIFF. UPON FURTHER INSPECTION, MAINTENANCE FOUND UPPER BEARING REF IPC 27-11-07-06 ON LH FUSELAGE SECTOR TORQUE TUBE BEARING ASSY STIFF (METAL TO METAL CONTACT) REF IPC 27-11-07-01. MAINTENACE ALSO FOUND LH WING STUB AILERON FEEL SDR WRNA201501080028Control Unit · malfunctionedTHE CREW REPORTED TAKEOFF WAS SMOOTH AND UNEVENTFUL. NOTICED AN OUT OF TRIM AND OPPOSITE RUDDER TRIM. RT INBD AILERON DEFLECTED TO FULL DOWN POSITION DURING FLIGHT AND WAS UNABLE TO ENGAGE AUTOPILOT. DIVERTED AND DUMPED APPROXIMATELY 25 MINUTES OF FUEL PSDR AALA20141220005Pcu · leakingAIR INTERRUPT, RETURNED, & EMER DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE LT HYD SYS QTY BEGAN TO DECREASE SLOWLY. ON ARRIVAL FOUND RT OTBD AILERON POWER CONTROL UNIT LEAKING FROM PLUG. R & R RT OTBD POWER CONTROL UNIT IAW AMM 27-11SDR UIEA2014121900653Actuator · malfunctionedAT FL 400, ACFT OSCILLATED ON ROLL & YAW. COMPLIED WITH QRH 9.1. REPLACED RT OTBD AILERON LOCKOUT ACTUATOR & FUNCTIONAL CHECKS GOOD IAW MM 27-11-16 & 27-11-00.SDR CA141219006Control Cable · frayed(CAN) LEFT LOWER FORWARD AILERON CABLE, HAS MULTIPLE BROKEN STRANDS AT WING LOCATION Y -200.219. RIGHT UPPER FORWARD AILERON CABLE, PN 82742409-001 HAS MULTIPLE ROKEN STRANDS AT WING LOCATION Y -200.219. MAINTENANCE REPLACED THE LEFT & RIGHT WING LOWER FORWASDR CA141203008Control Cable · worn(CAN) DURING INSPECTION THE LT AND RT FWD AILERON CABLES LOCATED IN THE WING WERE DISCOVERED TO HAVE 40% BLENDING OF THE CABLE WHERE IT PASSES OVER THE PULLEYS.SDR UIEA2014112700609Control Cable · obstructedDURING FLIGHT CONTROL CHECK FIRST OFFICER`S YOKE BINDS AT 6 UNITS. FOUND HEAT SHRINK TYPE OF MATERIAL ON CABLE, MATERIAL BEING PULLED INTO PULLEY AT STATION 550LT SIDE WW. REMOVED MATERIAL FROM CABLE. OPERATIONS CHECKED FLIGHT CONTROL MM 27-00-00. OPERATIOSDR K5SR201411181912Cable Assy · frayedWHILE PERFORMING A WALK AROUND INSPECTION OF THE AIRCRAFT PRIOR TO MAINTENANCE, WAS CHECKING THE MOVEMENT OF THE AILERONS AND HEARD A STRANGE GRINDING NOISE. UPON FURTHER INSPECTION FOUND NOISE COMING FROM THE LT AILERON AREA. GAINED ACCESS TO THE LT AILERONSDR CA141119006Control Cable · out of tolerance(CAN) AFTER TAKEOFF THE CREW FELT THAT THERE WAS RESISTANCE IN THE ROLL CONTROLS, ESPECIALLY IN RIGHT TURNS. THE AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT AND LANDED UNEVENTFULLY. MAINTENANCE CARRIED OUT A DETAILED INSPECTION OF THE ENTIRE ROLL CONTROL SYSTEMSDR GLBA2014111700465Control Cable · brokenPILOT REPORTED THAT THE RUDDER AILERON INTERCONNECT CABLE BROKE. REPLACED THE AILERON RUDDER INTERCONNECT CABLE PN NAS323-13-0250 IAW MM 27-10-08.
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