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 MASA200600928Warning Light · illuminatedASH 6428 MCI, AIRCRAFT HAD GLD NOT ARMED CAUTION MESSAGE. MAINTENANCE RESET THE SYSTEM.SDR SWIA200616493Pulley · bindingPILOT REPORTED SLIGHT DETENT WHEN MOVING AILERONS THROUGH CENTER POSITION. REPLACED RIGHT AILERON WING BOX LOWER PULLEY IAW 27-00-01. REMOVED AILERON AUTOPILOT SERVO AND INSP CLUTCH FOR FREEDOM OF MOVEMENT FOUND GOOD. INSTALLED SERVO, CYCLED AILERONS THROUGSDR MASA200600905Dcu · malfunctionedASH 7353 IAD - ELEVATOR SPLIT CAUTION MESSAGE. AIRCRAFT FERRIED TO CLT FOR WHERE MAINTENANCE REPLACED BOTH DCU'S AND POS SENSOR 2.SDR MASA200600897Aileron · malfunctionedASH 6235 LAS, AILERON JAM WOULD RELEASE WHEN OVER POWERED. OPS NORMAL. VISUALLY INSPECTED QUADERANTS. PERFORMED ROLL AXIS TEST AND TESTED EACH SIDE. NO FAULTS NOTED, NO LEAKS AT PCU'S.SDR F06037Control Cable · failedDURING AN AILERON CHECK ON GROUND, THE CREW HEARD A BINDING SOUND. MAINTENANCE WENT OUT TO INSPECT AND FOUND THAT THE AILERON CABLE SNAPPED IN THE AILERON QUADRANT AREA. MAINTENANCE REMOVED AND REPLACED CABLE.SDR WRLA2006010Control Cable · damagedAILERON BECAME JAMMED DURING CRUISE FLIGHT. FOUND RIGHT INBOARD AILERON TRIM CABLE DAMAGED SECTION 206 AND PULLEY DAMAGED. REMOVED TRIM CABLE AND PULLEY PER MM 27-10-00. INSTALLED NEW TRIM CABLE AND PULLEY, ADJUSTED TRIM CABLE PER MM 27-10-00. OPS CHECK GOSDR HALA0700096Unknown · unknownETOPS SIGNIFICANT SYSTEM, AILERON LOCK LEFT ILLUMINATED AT ALL SPEEDS. EICAS MSG AILERON LOCKOUT DISPLAYED. PERFORMED FIM 27-11-00 FIG 104 SHEET 3 ITEM 10 "R AIL LOCK ACT/PSEU" FAULT BALL ON LEFT SAM. FAULT BALL CLEARED AND DID NOT RETURN NR 67 SYSTEM IS OKSDR 2006FA0000259Casting · bentINCOMING INSPECTION FOUND AILERON DRIVE YOKE ATTACH CASTING BENT. UPON FURTHER INSPECTION IT WAS DISCOVERED THE DRIVE YOKE UPPER OR LOWER SHIMS WERE NOT INSTALLED. DRIVE YOKE ATTACH BOLT WAS INSTALLED CAUSING THE CASTING TO BE BENT AND REQUIRES REPLACEMENT BSDR CWQR2006001Turnbuckle · mismanufacturedDURING A CABLE CHANGE ON THE AILERON SYSTEM, THE PROPER CABLE TENSION COULD NOT BE BROUGHT UP. UPON INSPECTION FOUND NEW CABLE ASSEMBLY TERMINAL END WAS NOT PROPERLY MACHINED. BECAUSE THE NECK (AREA BETWEEN THREADS AND TOOL HOLE) WAS NOT REDUCED THE TURNBARRSDR 2006FA0000371Control Cable · frayedWHILE CONDUCTING AN ANNUAL INSPECTION PRIOR TO PLACING THE AIRCRAFT ON LINE AFTER PURCHASING IT FROM A LOCAL OPERATOR THE LT FORWARD AILERON BALANCE CABLE WAS FOUND TO BE BADLY WORN AND FRAYED. RESEARCH OF THE MAINTENANCE RECORDS SHOWED THAT THE PREVIOUS OWNESDR 2006FA0000370Control Cable · frayedWHILE CONDUCTING AN ANNUAL INSPECTION PRIOR TO PLACING THE AIRCRAFT ONLINE AFTER PURCHASING IT FROM A LOCAL OPERATOR THE RT AILERON BALANCE CABLE WAS FOUND TO BE BADLY WORN AND FRAYED WITH ONLY 1 STRAND LEFT HOLDING IT TOGETHER. THE LOCATION OF THE FRAYING WASDR 2006FA0000369Control Cable · frayedWHILE CONDUCTING AN ANNUAL INSPECTION PRIOR TO PLACING THE AIRCRAFT ONLINE AFTER PURCHASING IT FROM A LOCAL OPERATOR THE LT AILERON BALANCE CABLE WAS FOUND TO BE BADLY WORN AND FRAYED. THE LOCATION OF THE FRAYING WAS AT THE 1ST IB PULLEY IN THE WING ROOT. THSDR DXTA200601274Pcu · failedWHILE AT FL 400 IN CRUISE " FLT CONTROL FAULT " CAS MSG ILLUMINATED WITH VIOLENT RT ROLL/YAW OF A/C. DISENGAGED A/P, CHG,D FC COMPUTER AND NOTED LIGHT ON RIGHT REAR FLT CONTROL SHUT OFF SWITCH, RT ELEV SHUT OFF. LIGHTED SWITCH WITH NON-COMMANDED ROLLS OCCURED SDR WRLA2006007Actuator · malfunctionedAFTER TAKEOFF FROM SNN AND DURING CLIMB, WHEN FLAPS/SLATS WERE RETRACTED, A DEFLECTED AILERON DISAGREE ALERT MESSAGE WAS DISPLAYED ON THE SD ALONG WITH LEFT OUTBOARD AILERON INDICATING DEFLECTED. FLIGHT CREW FOLLOWED PROCEDURES AND RETURNED TO SNN, WHERE THE SDR MASA200600586Switch · dirtyASH 7391 MDT - MACH TRIM WILL NOT ENGAGE. CREW COMPLIED WITH MEL PROCEDURES. MX CLEANED SWITCH.SDR CA060224008Turnbuckle · chafedDURING A SCHEDULED PHASE 5 INSPECTION ON CESSNA 650 C-FIMO, THE TECHNICIAN DISCOVERED THAT THE LT AND RT AILERON OUTBOARD AFT CABLE CHAFED THROUGH THE LOKCLAD AND THE TURNBUCKLE WAS DAMAGED.SDR MASA200600532Warning Message · illuminatedASH 6240 PHX, PITCH FEEL CAUTION MESSAGE AT DEPATURE TIME. MAINTENANCE RESET THE SYSTEM.SDR CA060221011Bracket · crackedDURING CRUISE FLIGHT, CREW REPORTED AILERON CONTROL SEEMED STIFF. AFTER NORMAL LANDING MAINTENANCE INSPECTION FOUND RT AILERON SUPPORT BRACKET FOR AILERON INPUT QUADRANT CRACKED. CAUSING OUTBOARD AILERON QUADRANT TO RUB ON BRACKET. THIS AIRCRAFT IS PRE MOD SDR MASA200600476Actuator · malfunctionedASH 7072 DRO, CAPTAIN REPORTED AILERON TRIM WILL NOT MOVE. MAINTENANCE REMOVED AND REPLACED AILERON TRIM ACTUATOR.SDR IXXA06SMN064SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RT INBD AILERON SHOWS SEVERAL SPOTS OF CORROSION AND NON STANDARD REPAIR ON LWR PLATING, STA XA 550.000. PERFORMED MAJOR REPAIR. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED EXISTING PANEL PLATING (CORRODED) + REPAIR NOSDR MASA200600383Actuator · out of adjustASH 7056 COD, AILERON TRIM STUCK IN FULL LT POSITION. MAINTENANCE R&R POTENTIOMETER AND ADJUSTED ACTUATOR.SDR CA060214003Control Cable · broken(CAN) DURING ROUTINE MAINTAENANCE INSPECTION, SEVERAL WIRES FOUND BROKEN ON RT AILERON CONTROL CABLE AS IT PASSES AROUND CABLE PULLEY AT FRAME 4. PULLEY FOUND SEIZED TO BOLT. CABLE, PULLEY AND BOLTS REPLACED. (TC NR 20060214003)SDR MASA200600320Control Panel · malfunctionedASH 6579 TUS - MACH TRIM BUTTON FLASHES AND MACH TRIM WILL NOT ENGAGE. MAINTENANCE R&R PANEL.SDR COMA0560827Servo · malfunctionedFLIGHT 5657 - FLIGHT CONTROLS STUCK DURING LANDING APPROACH. REPLACED THE AILERON SERVO.SDR SWAA060250Mechanism · bindingAILERONS BINDING. FOUND LT AILERON TOWERSHAFT BINDING. REMOVED AND REPLACED LT AILERON TOWERSHAFT FEEL & CENTERING MECHANISM PER MM.SDR CA060125003Control Cable · damaged(CAN) DURING NORMAL INSPECTION IT WAS FOUND THAT ONE OF THE AILERON WING LOOP CABLES WAS WEARING INTO THE SIDE OF THE LIGHTNING HOLE OF THE FIRST WING RIB ON THE LT WING. THE CABLE WAS DAMAGED AS WELL. THE AIRCRAFT WAS GROUNDED UNTIL THE CABLE WAS REPLACED, SDR CA060303007Control Cable · brokenLT AILERON CONTROL YOKE CROSSOVER CABLE BROKEN STRANDS. THIS WAS FOUND AT PHASE 5 INSPECTION AND IS A COMMON FINDING AT 1200 HOURS.SDR CA060303006Control Cable · brokenRT AILERON CONTROL YOKE CROSSOVER CABLE BROKEN STRANDS. THIS WAS FOUND ON PHASE 5 INSPECTION AND IS A COMMON FINDING AT 1200 HOURS OF USE.SDR MASA200600048Sensor · malfunctionedASH 7253 IAD - RT AILERON ON FLIGHT CONTROL PAGE DOES NOT SHOW FULL TRAVEL. MAINTENANCE REMOVED AND REPLACED RT AILERON POSITION SENSOR.SDR SWIA200616112Transmitter · out of adjustRT AILERON POSITION INDICATES 2 DEGREES UP ON EICAS WHEN AILERON IS IN NEUTRAL. ADJUSTED POSITION TRANSMITTER IAW CRJ 700MM 27-15-15-820-801-A0.SDR SWIA200516055Flutter Damper · leakingINTERMITTENT FLUTTER DAMPER STATUS MESSAGE. REPLACED RT AILERON FLUTTER DAMPER IAW MM 27-15-05. OPERATIONAL CHECK GOOD.SDR 2005UALA01510Servo Valve · oscillatesRETURNED TO FIELD DUE TO AILERON VIBRATION. RT GREEN AILERON SERVOCONTROL SERVO VALVE WAS FOUND OSCILLATING, THUS CAUSING INFLIGHT AILERON VIBRATION. REPLACEMENT OF THE SERVOVALVE RESOLVED THE PROBLEM. NO FURTHER ANOMALY WAS REPORTED.SDR SWIA200516026Linkage · obstructedWHEN CHECKING FLIGHT CONTROLS, YOKE HANGS UP HALF WAY TO THE RIGHT. REPLACED LT AILERON RIVET TO QUADRANT LINKAGE IAW MM 31-30-11. OPERATIONAL CHECK GOOD.SDR QXEA200600288Bushing · unknownYYC - C3 RIGHT AILERON OUTBOARD PCU INBOARD LUG BUSHING FOUND NON CONFORM. REPLACED BUSHING IAW HORIZON AIR EA R-27-218.SDR QXEA200600287Unknown · unknownYYC - C3 RIGHT AILERON FAILS BACKLASH TEST ON NR 3 HYDRAULIC SYSTEM. REPAIRED IAW CRJ700 SRM 27-11-00-710-001-A01.SDR AU510002053Pulley · seized(AUS) AILERON SYSTEM SLIGHTLY STIFF. LT TRIM ACTUATOR CHANGED BUT DEFECT REMAINED. INVESTIGATION FOUND A SEIZED PULLEY IN AILERON CONTROL SYSTEM. PULLEY LOCATED AT LT AB CABLE RUN AT STN 380 WL 283. (CASA NR 510002053)SDR AU510001742Control Cable · wornRT AILERON CARRY THROUGH CABLE WORN TO LIMITS. CABLE WAS WORN BY THE PHENOLIC RUB BLOCK LOCATED AT WS 71.125.SDR AU510001456Actuator · failed(AUS) RT OUTBOARD AILERON LOCKOUT ACTUATOR FAILED IN PARTLY EXTENDED POSITION. WORKSHOP INVESTIGATION OF THE ACTUATOR FOUND INTERNAL CORROSION. SEE ATTACHMENT FOR INVESTIGATION DETAILS. (OTHER CAUSE: MATERIAL - AGE - ENVIRONMENT ) (CASA# 510001456)SDR XN0A1282Connector · disconnectedLT LOW SPEED AILERON WILL NOT CONNECT FOR TAKE-OFF AND THE RT LOW SPEED AILERON IS CONNECTED. CONNECTED THE LT LOW SPEED AILERON CONNECTOR PLUG, SYSTEM OPS CHECKS GOOD IAW AMM 27-11-01.THIS CLEARS DMI NR 5967.(STATUS:ORIG/CLOSED)SDR 2005FA0001615Control Cable · corrodedAILERON CABLE RUNNING FROM LT WHEEL WELL AREA LOWER REAR SPAR THRU CABIN UNDER FLOOR TO PEDESTAL AND CONTROL SPROCKET WAS FOUND SEVERELY RUSTED AND ABOUT HALF THE WIRE STRANDS HAD FAILED IN THE AREA WHERE THE CABLE MET THE SWAGED TERMINAL END. AREA IS VERY HARSDR 2005FA0001614Control Cable · corrodedAILERON CABLE RUNNING FROM LT WHEEL WELL AREA LOWER REAR SPAR THRU CABIN UNDER FLOOR TO PEDESTAL AND CONTROL SPROCKET WAS FOUND SEVERELY RUSTED AND ABOUT HALF THE WIRE STRANDS HAD FAILED IN THE AREA WHERE THE CABLE MET THE SWAGED TERMINAL END. AREA IS VERY HARSDR 2005FA0001596Control Cable · failedAILERON CABLE RUNNING FROM LT WHEEL WELL AREA LOWER REAR SPAR THRU CABIN UNDER FLOOR TO PEDESTAL AND CONTROL SPROCKET WAS FOUND SEVERELY RUSTED AND ABOUT HALF THE WIRE STRANDS HAD FAILED IN THE AREA WHERE THE CABLE MET THE SWAGED TERMINAL END. AREA IS VERY HARSDR 2005FA0001595Control Cable · damagedAILERON CABLE RUNNING FROM LT WHEEL WELL AREA LOWER REAR SPAR THRU CABIN UNDER FLOOR TO PEDESTAL AND CONTROL SPROCKET WAS FOUND SEVERELY RUSTED AND ABOUT HALF THE WIRE STRANDS HAD FAILED IN THE AREA WHERE THE CABLE MET THE SWAGED TERMINAL END. AREA IS VERY HASDR 2005FA0001598Control Cable · failedAILERON CABLE RUNNING FROM LT WHEEL WELL AREA LOWER REAR SPAR THRU CABIN UNDERFLOOR TO PEDESTAL AND CONTROL SPROCKET WAS FOUND SEVERELY RUSTED AND ABOUT HALF THE WIRE STRANDS HAD FAILED IN THE AREA WHERE THE CABLE MET THE SWAGED TERMINAL END. AREA IS VERY HARDSDR 2005FA0001613Control Cable · corrodedAILERON CABLE RUNNING FROM LT WHEEL WELL AREA LOWER REAR SPAR THRU CABIN UNDER FLOOR TO PEDESTAL AND CONTROL SPROCKET WAS FOUND SEVERELY RUSTED AND ABOUT HALF THE WIRE STRANDS HAD FAILED IN THE AREA WHERE THE CABLE MET THE SWAGED TERMINAL END. AREA IS VERY HARSDR A6WA200540335Control Cable · frayedSPOILERON FAULT, AILERON FEELS ROUGH WHEN TURNED TO THE RIGHT. AC HAS FRAYED AILERON CABLES DUE TO INCORRECT INSTALLATION, REPLACED CABLES.SDR A6WA200540327Aileron · unknownREQUEST INSPECTION OF RT AND LT AILERONS. THAWED ICE FROM AILERON, INSPECTED SURFACE MOVEMENT AND SURFACES. NO DEFECTS NOTED. (K)SDR CA051129002Spring · fracturedDURING TAXI, THE FLIGHT CREW NOTICED A FULL LEFT BIAS DEFLECTION IN THE AILERON SYSTEM. MAINTENANCE FOUND ONE OF THE AILERON INTERCONNECT SPRINGS HAD FRACTURED AT THE END RING THAT PROVIDES CONNECTION TO THE BRIDLE. IT IS FELT THAT THE ISSUE MAY HAVE BEEN INSDR SWIA200515813Control Cable · out of rigAILERONS HAVE A CATCH/CLICK FEEL AFTER NEAR NEUTRAL POSITION WHEN YOKE IS TURNED LEFT AND RIGHT. CHECKED CABLE CIRCUITS. RERIGGED RIGHT AILERON FUSELAGE WING CABLES AND RETENSIONED SAME CABLES IAW 27-11-00.SDR QXEA200501391Flt Controls · stiffDEN - FLIGHT CONTROLS FEEL STIFF ON PITCH AND ROLL ON YOKE. MAINTENANCE INSPECTED BOTH CONTROL YOKES FOR STIFFNESS AND FOUND NO OBSTRUCTIONS. OPERATE NORMALLY. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
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