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 DL75A040945Control Cable · wornHMV-3 VISIT IN DFW. CABLE WORN, AILERON CABLE WORN AT LEFT WING OVERRIDE QUADRANT. CABLE FOUND TO BE IN POSITION A1B-4 AND PN BACC2C4AD06518FG. REPLACED CABLE PER OPN 2000 AND INSTALLED RECOMMENDED OPTIONAL CABLE PN BACC2C4CD06518FG ON RC 1388-1392 WITH RIISDR 0401789956Drain · cloggedAT CRUISE SPEED AND ALTITUDE, THE AIRCRAFT WOULD NOT TURN WITH AUTOPILOT. CREW CANCELLED AUTOPILOT AND WAS STILL UNABLE TO TURN THE CONTROL WHEEL BY HAND. COMPLIED WITH COM PROCEDURES AND AIRCRAFT DESCENDED TO A LOWER WARMER ALTITUDE. CREW FELT A SNAP AND TSDR DL76L040927Actuator · malfunctionedAILERON LOCKOUT IN FLIGHT AND C/B POPPED. A/C DIVERTED DUE TO WEATHER AND LT O/B AILERON LOCKED OUT. CLEANED LT O/B AILERON LOCKOUT ACT CONNECTOR AND SWAPPED LEFT AND RIGHT SAMS. ALL AILERONS OPERATIONAL. AS PRECAUTION PUT THE AILERON LOCKOUT SYS TO MCO 27SDR MV52004F00001Pulley · fodWHILE IN FLIGHT, PILOT EXPERIENCED SEVERE AILERON BINDING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. AFTER INSPECTION OF THE COMPLETE AILERON SYSTEM, IT IS SUSPECTED THAT FOD HAD COME IN CONTACT BETWEEN THE AFT AILERON PULLEY AND CASDR DL73S040904Mixing Valve · dirtyCONTROL YOKE HAS DEAD ZONE FEEL PLUS/MINUS SIX DEGREES OF CENTER WITH NO AILERON MOVEMENT. REMOVED DIRT AND DEBRIS FROM AILERON MIXING UNIT.SDR 04256621Warning Light · illuminatedCREW REPORT STATED TAKEOFF ROLL SET THRUST, ACCELERATED TO 40KTS OR SO AND TAKEOFF CONFIG AILERON WARNING ILLUMINATED. TRIMS WERE SET CORRECTLY AND TAKEOFF CONFIG WAS ON DURING INITIAL ROLL ON RUNWAY. THEN ABORTED TAKEOFF, CONTACTED MAINT AND DISPATCH AND PRSDR CA040913003Block · worn(CAN) AILERON SYSTEM CONTROL TUBE ASSEMBLY FORWARD SHAFT P/N 1260141-6/10 WAS WORN 25-30% DUE TO A FAILED CORRODED SUPPORT BEARING P/N 0760633-1. SOME NEEDLES FROM THE BEARING ASSEMBLY WERE MISSING.SDR 2004FA0000724Bearing · dislodgedIN FLIGHT, NOTICED THAT LOSS OF AILERON CONTROL INPUT HAD OCCURRED, AND UPON ADDED FORCE TO CONTROL YOKE, DETERMINED THAT TOTAL SEIZURE OF THE AILERONS HAD OCCURRED. LANDED WITH RUDDER CONTROL ONLY. REMOVED TUBE ASSY FROM FIREWALL AND FOUND SHAFT AND BEARINGSDR CA040830014Control Rod · cracked(CAN) ON INSPECTION, FOUND THE RT AILERON CONTROL ROD CRACKED ON THE OUTER THREADED PORTION OF THE ROD WHERE THE ROD END THREADS INTO THE ROD. THE CRACK WAS APPROXIMATLEY 1 INCH IN LENGTH LONGITUDINALY WITH THE ROD.SDR DHL2004366005Aileron · malfunctionedON DEPARTURE AFTER SLAT RETRACTION AND COMPLETION OF LT TURN, A/C REQUIRED 30 DEG LT AILERON TO MAINTAIN WINGS LEVEL. FCPI CONFIRMED PROPER CONTROL DEFLECTIONS. JETTISONED FUEL AND RETURNED. DEFERRED RT NR 3 ROLL SPOILER IAW MEL 27-62-01-1, CAT. (C) CONTSDR WLDA200488Warning Light · illuminatedAIR TURNBACK DUE TO AILERON DEFLECTED DISAGREE ALERT DISPLAYED AFTER TAKEOFF. DEACTIVATED TAKEOFF DEFLECTED AILERONS IAW MEL 27-13-2 CAT (C), ENTERED IN DMI M27AU1904-106.SDR CA040730011Bearing · loose(CAN) DURING 100 HR INSPECTION - LT IB AILERON CONTROL BELLCRANK WAS FOUND TO HAVE LOOSE FITTING BEARING. ALLOWING AILERON CONTROL ROD TO FLOAT UP AND DOWN, CONTACTING THE BELLCRANK ASSEMBLY. BEARING REMOVED, BELLCRANK AND CONTROL ROD CHECKED FOR DAMAGE, NONSDR CA040730010Bearing · loose(CAN) DURING 100 HR INSPECTION, RT AILERON OUTER PUSHROD WAS FOUND TO HAVE A LOOSE BEARING, ALLOWING ROD END TO FLOAT SIDEWAYS ON BEARING. BEARING REMOVED, ROD END INSPECTED FOR DAMAGE, NONE FOUND. NEW BEARING INSTALLED AND CHECKED SERVICABLE. PUSH ROD ASSYSDR WLDA200433Aileron · malfunctionedAIR TURNBACK DUE TO AILERON DEFLECTION DISAGREE LEVEL 2 ALERT ON FLAP/SLAT RETRACTION. DEFERRED ITEM TO DMI M27JL2404-122 IAW MEL 27-13-2 CAT (C). NOTE: NO EMERGENCY DECLARED AND NO FUEL DUMPED.SDR 04FDEA02045Structure · damagedCOMPLY WITH EA 1-5510-76669 HORIZONTAL STABILIZER BARREL NUTS REWORK PER SB MD11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000. HORIZONTAL STABILIZER BARREL NUTS REWORK PER SB MD11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000' HAS BEEN COMPLIED.SDR WLDA200431Actuator · defectiveLEVEL II ALERT AFTER SLAT RETRACTION, AILERON DEFLECTION DISAGREE AFTER T/O. A/C DIVERTED TO JFK. INSPECTED QUAD RINGS & ASSOCIATED LINKAGE, RAN FLIGHT CONTROLS. CHECKED FOR FLAIRING, PERFORMED RTS ON FCC 1&2 AILERON SYSTEM. ALL TESTS PASSED. DEFERRED AILSDR SWIA200413544Proximity Sensor · out of adjustON FFOD CHECKS NO TRIM AURAL WARNING. REPAIRED WIRING AT ELEVATOR TRIM PROX SENSORS AND ADJUSTED PER MM. OPERATIONAL CHECK GOOD.SDR AUS20040505Control Rod · bent(AUS) RT AILERON PUSH-PULL ROD BENT.SDR SWIA200413435Control Handle · mislocatedAILERON CONTROL DISENGAGE HANDLE WAS STICKING UP ABOUT .5 INCH WITH NO MAP LIGHTS ILLUMINATED. WHEN THE HANDLE WAS PUSHED IN, THE AILERON DISCONNECTED. RECONNECTED AILERON DISCONNECT PER MM 27-00-00. OPERATIONAL CHECK GOOD.SDR CA040618006Link Assy · crackedFOUND LEFT AND RIGHT LINK ASSY ON AILERON PUSH PULL TUBES CORRODED AND CRACKED ON ALL FOUR SIDES. PARTS WERE REMOVED AND A NEW LINK ASSY WERE INSTALLED.SDR SWIA200413397Arm · malfunctionedDURING PREFLIGHT NOTICE A SIGNIFICANT BINDING IN THE CONTROL WHEEL WHEN AILERONS ARE USED RIGHT AND LEFT AND IN ALL POSITIONS OF THE ELEVATOR. REMOVED AND REPLACED RIGHT AILERON RVDT AND ARM IAW EMB MM 31-30-11. OPERATIONAL CHECK GOOD. P/N: D370519, S/N OFFSDR AUS20040453Control Cable · worn(AUS) AILERON CABLE OUTER STRANDS BROKEN IN AREA LOCATED AT RT WING SPAR TRAILING EDGE AT WS 1110. SOME OUTER STRANDS WERE ALSO BROKEN IN AN AREA LOCATED FURTHER OB AT APPROXIMATELY WS 1195. SUSPECT CAUSED BY CABLE WEARING ON FAIRLEADS ALONG THE WING TRAILINSDR PCAA0405213Rod End · wornFLIGHT 4099 REPORTED A VIBRATION DURING CRUISE FLIGHT. THE VIBRATION DID NOT APPEAR TO BE ASSOCIATED WITH THE PROPELLERS. THE CREW DECIDED TO DIVERT TO MIDDLETOWN. MAINTENANCE FOUND THE INPUT CONTROL ROD AT THE RIGHT HAND AILERON WORN. BUSHING WAS INSTALLESDR SWIA200413323Trim Panel · damagedAILERON TRIM IS INTERMITTENT WHEN TRIMMING TO THE RT (LWR TRIM IS OKAY). REPLACED AILERON TRIM PANEL WITH SERVICEABLE UNIT. OPS CHECK GOOD. P/N: 601R51227-13.SDR CA040512003Control Cable · frayed(CAN) FRAYED AT WING ROOT PULLEY.SDR CA040512002Control Cable · frayed(CAN) FRAYED AT PULLEY WING ROOT, PULLEY NOT SEIZED.SDR 20040513Bearing · deterioratedDURING LOW SPEED FLIGHT, WHEN TURNING RIGHT, AS WHEEL PASSES 30-35 INDEX MARK, VIBRATION OCCURS. REMOVED AND REPLACED LT IB AILERON QUADRANT BEARINGS AND ADJUSTED AILERON SYSTEM IAW MM.SDR EIA2004033Connector · dirtyON CLIMBOUT WITH FLAPS UP, NOTICED IN LEFT TURN SLIGHT BUFFETING. UPON VISUAL FOUND LEFT OUTBOARD AILERON NOT LOCKED OUT. RETURNED TO PHIK. COULD NOT DUPLICATE. CLEANED AND FOUND OILY GRIME ON LEFT HAND OUTBOARD AILERON CANNON PLUG. CHECKED VOLTAGE WITH FSDR CA040428006Aileron · out of rigDURING TROUBLESHOOTING OF A PILOT REPORTED SNAG, THE CONTROL COLUMN IS BANKED SLIGHTLY TO THE LEFT IN ORDER FOR THE AIRCRAFT TO FLIGHT STRAIGHT AND LEVEL, CHECKED THE AILERON RIGGING AND FOUND THAT IF THE PROCEDURES FROM THE MM ARE FOLLOWED THE AIRCRAFT WILL BSDR 2004FA0000338Control Cable · brokenDURING ACCOMPLISHMENT OF THE AIRCRAFT'S FIRST PHASE 5 INSPECTION, FOUND ALL FOUR AILERON WING CABLES TO BE HEAVILY FLAT SPOTTED AT THE FAIRLEADS LOCATED AT WS 58.00, 103.43 AND 149.18. THE RT UPPER CABLE (P/N 6361002-7) HAD ONE BROKEN STRAND. THESE CABLES NOSDR PCAA0404187Actuator · inoperativeLGA REPORTED AILERON TRIM INOP. MAINTENANCE REPLACED THE AILERON TRIM ACTUATOR.SYSTEM CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.SDR PCAA0405187Actuator · inoperativeLGA REPORTED AILERON TRIM INOP.MAINTENANCE REPLACED THE AILERON TRIM ACTUATOR.SYSTEM CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.SDR DXTA200400287Aileron · vibrationAFTER TAKE OFF WITH GEAR UP ABOVE 180 KNOTS IAS, YOKE DEVELOPED AN AILERON SHIMMY/ VIBRATION OF APPROX. 1 TO 2 VIBRATIONS PER SECOND. INTENSITY INCREASED UP TO 300 KNOTS IAS, VIBRATIONS DECREASED ON DESCENT AND BELOW 170 KNOTS IAS. - PERFORMED FREE PLAY CHECK SDR ABXA040135Linkage · lack of lubeCOULD NOT MOVE AILERON TRIM WHEEL DURING DESCENT INTO ILN. LUBED AND INSPECTED LT, RT AND WHEEL WELL AILERON LINKAGES. OPERATED AILERON TRIM THROUGH NUMBEROUS TIMES. OPERATED NORMAL.SDR CA040512001Control Cable · frayed(CAN) CABLE FRAYED AT PULLEY, PULLEY NOT SEIZED.SDR QXEA200400230Trim Panel · failedSEA - FLIGHT 2181 - THE CREW REPORTED THAT THE AILERON TRIM WILL NOT TRIM OR MOVE TOWARDS RIGHT WING DOWN. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AILERON/RUDDER TRIM PANEL. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICSDR SO1450Rod · bentDURING PREFLIGHT, PILOT FOUND LT AILERON CONTROL ROD BENT AT AILERON SURFACE. AIRCRAFT GROUNDED AND TAKEN TO MAINTENANCE. REMOVED LT AILERON CONTROL ROD AND FOUND IT TO BE BENT APPROXIMATELY 25 DEGREES JUST AFT OF AFT ROD END BEARING. REPLACED WITH NEW ROD.SDR A6WA200440031Warning System · activatedABORTED TAKEOFF DUE TO AILERON MISCONFIGURATION WARNING MESSAGE ABOVE 80 KNOTS. BTMS READINGS 03, 03, 04, 06 REPORTED WEIGHT 52,000 LBS. COMPLIED WITH SPECIAL INSPECTION PROCEDURE IAW 5-51-27, ABORTED TAKEOFF. REMOVED AND REPLACED NR 3 AND NR 4 MLG TIRES. SDR CA040225012Actuator · stuck(CAN) EICAS MESAGE AILERON LOCKOUT, FOUND RT AILERON LOCK OUT ACTUATOR STUCK IN THE EXTEND POSITION, ACTUATOR REPLACED.SDR P5CA0401037Connector · inoperativeNO AILERON MOVEMENT INDICATION DURING FLIGHT CONTROL CHECK. CLEANED CONNECTOR ON AILERON INDICATOR IAW 27-10-00. OPS CK GOOD.SDR P5CA0401038Connector · looseNO AILERON MOVEMENT DURING FLT CONTROL CHECK. CLEANED AND RESECURED CONNECTOR D3296P AT J42-J-BOX. OPS CK OK, IAW MM 27-11-00.SDR GLBA20030564Idler Gear · stickingAILERON TRIM CATCHES AND STICKS, R&R IDLER GEAR ASSY. OPS CK GOODSDR P5CA0401036Circuit Card · looseOB AILERONS LOCKED OUT, CYCLED FLAPS TWICE AND RESET C/B. NO HELP. RESEATED A1 CARD IN FLAP CONTROL CK AND VISUAL, OPS NORMAL IAW MM 27-10-00.SDR GLBA20030560Control Cable · frayedLT AILERON CABLE FRAYED BETWEEN WS 124.58 AND 147.74 (LT WHEEL WELL), REMOVED AND REPLACED LT AILERON WING CABLE. OPS CK AND RIG CK GOOD.SDR U30A200400002Computer · faultyDURING PRE-FLIGHT OF FLT 718 DTW-ACA, THE CREW NOTED NR 1 SEC (SPOILER ELEVATOR COMPUTER) ON ECAM FAULTED AND ON OVERHEAD PUSHBUTTON SWITCH.MAINTENANCE SWAPPED THE NR 1 SEC AND THE NR 3 SEC. NR 3 SEC (S/N 5601) WAS DEFERRED PER MEL 27-94-01. ALL MAINTENEANCE PSDR AUS20040083Fitting · loose(AUS) LT AND RT AILERON CONTROL ROD ATTACHMENT FITTINGS, LOOSE.SDR CA040203003Control Chain · worn(CAN) DURING DECENT THE FLIGHT CREW NOTICED THE AILERONS BINDING AND VERY DIFFICULT TO MOVE. UPON SLOWING DOWN THE AIRCRAFT THE AILERON CONTROL RETURNED TO NORMAL. INVESTIGATION BY MAINTENANCE REVEALED THAT THE 27-71026-001 CONTROL CHAIN WAS SEIZED AND ALMOSSDR SO19200405477Aileron · inoperativeIAW L/P 23142 EXCESSIVE RT ROLL AFTER T/O RETURNED WITHOUT INCIDENT, PERFORMED TROUBLESHOOTING INSPECTED LUBRICATED AND CHECKED CABLE TENSION FOR THE AILERON SYS IAW MM. OPS CHECK GOOD. PERFORMED FUNCTIONAL CHECK FLIGHT AND RETURNED AIRCRAFT TO SERVICE WITHOSDR ARWA20040106Switch · inoperativeSTARTED TAKE-OFF ROLL, AILERON POWER LIGHT CAME ON. REMOVED AND REPLACED MANUAL CONTROL IND SWITCH IAW MM 27-11-14; OPERATIONAL CHECK NORMAL IAW MM 27-11-14 AND 27-11-0.SDR QXEA200400083Power Supply · failedSEA - FLIGHT 2462 - THE AILERON AND RUDDER TRIM INDICATORS SHOW VERY SLOW UNCOMMANDED TRIM MOTION. MAINTENANCE REPLACED THE RUDDER/AILERON TRIM POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
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