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 96UAL900928Rod · bindingRIGHT HAND OUTBOARD AILERON WILL NOT ALIGN WITH CONTROL WHEEL CENTERED. *S/D* AILERON ACTUATOR SPRING CARTRIDGE INPUT ROD FOUND BINDING. REPLACED ROD.SDR CA970109029Actuator · failed(CAN) EICAS (ENGINE INDICATION AND CREW ALERTING SYSTEM) MESSAGE AILERON LOCKOUT. RH AILERON LOCKOUT CYLINDER REPLACED.SDR 97ZZZM403Trim Chain · corrodedLEFT AILERON TRIM SCREWJACK CHAIN APPEARS TO BE CORRODED. LEFT TRIM CABLE TURNBUCKLES LOOSE. REMOVED AND REPLACED LEFT AILERON TRIM CHAIN IAW 27-12-17. A DJUSTED CABLES AND COMPLIED WITH FUNCTION TEST IAW 27-12-00. CHECKS OK. (M)SDR 9627549950Control Mech · lack of lubeCONTROL WHEEL REQUIRED ABOVE NORMAL FORCE TO BANK AIRCRAFT TO THE LEFT. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE LUBED ALL PULLEYS, FAIRLEADS, AND AILERON SECTORS. NO BINDING OR FLAT SPOTS WERE NOTED. ALSO, CLEANED GRIT FROM RIGHT WHSDR 96UAL900883Control Syst · out of adjustAILERON CONTROL WHEEL FORCES HAVE EXCESSIVE DEAD BAND OR LACK OF FEEL EITHER SIDE OF NEUTRAL IN LANDING CONFIGURATION. ESPECIALLY NOTICEABLE, ALSO STIFF. *S/D* AILERON SYSTEM RERIGGED. AIRCRAFT TEST FLOWN AND THERE WAS NO EVIDENCE OF A DEAD BAND OR STIFFNESSDR ABXA9700482Override Mech · failedOVERRIDE MECHANISM SHAFT AND BEARING FAILED DAMAGING LOWER SKIN, GUSSETT AND HINGE WEB FITTING. REPAIRED PER DC8 MM.SDR 97ZZZM386Cables · corrodedPERFORMED AILERON INTERCONNECT CABLE CHECK. FOUND AILERON INTERCONNECT CABLES CORRODED AT WING ROOT PULLEYS. REMOVED AND REPLACED IAW AMM GENERATED W/C FOR FUNCTIONAL CHECK.SDR 97ZZZM385Cables · corrodedLEFT AND RIGHT AILERON INTERCONNECT CABLES COVER SLEEVES ARE WORN IN TWO AT CABLE GUIDES. REMOVED AND REPLACED LEFT AND RIGHT AILERON INTERCONNECT CABLES IAW AMM W/C GENERATED FOR FUNCTIONAL CHECKS. REF W/C 2365. (M)SDR C2XA96BT013Drive Cable · brokenBTV - INBOUND FLIGHT 3682, CAPTAIN REPORTED 'YOKE MOVEMENT FEELS RESTRICTED. CAN'T GET FULL DEFLECTION OF RIGHT AILERON'. AIRCRAFT LANDED WITHOUT PROBLEM. UPON INSPECTION FOUND THE AILERON TRIM SERVO DRIVE CABLES BROKEN AND SERVO DRIVE BINDING. REMOVED ANDSDR 96ZZZX5732Aft Manifold · crackedAS DETERMINED BY NDI, AILERON PCU MANIFOLD IS CRACKED IN FILTER PORT ADJACENT CHECK VALVE AND INLET PORTS. SUBMITTER STATED THIS IS A CONTINUING DEFECT WITH THIS PART.SDR 96ZZZX5731Fwd Manifold · crackedAS DETERMINED BY NDI, AILERON PCU MANIFOLD IS CRACKED IN FILTER PORT ADJACENT CHECK VALVE AND INLET PORTS. SUBMITTER STATES THIS IS A CONTINUING DEFECT WITH THIS PART.SDR SIMA962971Interconnect · crackedDFW - DURIGN COMPLIANCE OF EO E9-2700-001 (AD 93-22-10) REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM. THE FLAP INTERCONNECT ROD APPEARED TO HAVE SEVERAL CRACKS JUST INBOARD OF BEARING SLEEVES. THE INTERCONNECT ROD WAS REPLACED AS A PRECAUTIONARY STEP. FUSDR 97ZZZM379Cables · rustedRIGHT AILERON CONTROL CABLES ARE RUSTED AT WING ROOT CABLE PULLEYS. INSTALLED RIGHT AILERON CONTROL CABLES IAW AMM W/C GENERATED FOR REQUIRED CHECKS AND SAFTIES.SDR C2XA96IA255Bellcrank · rustyIAH - DURING 3C-CHECK INSPECTION, ROUTINE INSPECTION OF THE AILERON CONTROL SYSTEM FOUND A CONTROL ROD BELLCRANK TO HAVE RUSTY BEARINGS. THE LEFT WING AILERON CONTROL SYSTEM BELLCRANK AT RIB NR 23 WAS REMOVED AND REPLACED AND THE AIRCRAFT WAS APPROVED FOR RETSDR 96ZZZX5631Aileron · rivets looseDURING ANNUAL INSPECTION, FOUND BOTH AILERONS TO HAVE CONTROL LOOSENESS INTERNALLY. REMOVED AILERON ASSYS AND FOUND BOTH TO HAVE LOOSE RIVETS AT TORQUE TUBE TO AILERON ATTACHMENT. SUSPECT AIRCRAFT EXPERIENCED HIGH WINDS FROM REAR WHILE PARKED. GUST LOCKS ONSDR 96ZZZX5630Aileron · rivets looseDURING ANNUAL INSPECTION, FOUND BOTH AILERONS TO HAVE CONTROL LOOSENESS INTERNALLY. REMOVED AILERON ASSYS AND FOUND BOTH TO HAVE LOOSE RIVETS AT TORQUE TUBE TO AILERON ATTACHMENT. SUSPECT AIRCRAFT EXPERIENCED HIGH WINDS FROM REAR WHILE PARKED. GUST LOCKS ONSDR CA961120001Bearing · rough(CAN) DURING CLIMB AILERON SEIZED. AIRCRAFT RETURNED NO INCIDENT. BEARINGS IN ROLLER FOUND ROUGH AND REPLACED.SDR 97ZZZX173Bolt · fell outDURING AN ANNUAL INSPECTION IT WAS FOUND THAT THE AN 4-10A BOLT CONNECTING THE PUSH/PULL ROD TO THE LEFT AILERON HORN HAD BACKED OUT TO THE POINT THAT BY MOVING THE AILERON BY HAND, THE BOLT FELL OUT COMPLETELY. THE BOLT WAS NOT SAFTIED. FURTHER INSPECTION OFSDR 96DHL802005Aileron Ctl Vlv · bypassingAFTER TAKEOFF, AIRCRAFT ROLLED TO THE RIGHT IN LEVEL FLIGHT AND FELT AS IF IT WAS OPERATING IN MANUAL REVERSION MODE. THERE WERE NO OTHER INDICATIONS OF THE A/C OPERATING IN MANUAL REVERSION. REMOVED AND REPLACED AILERON CONTROL VALVE CYLINDER AND AILERON TASDR 96ZZZX5034Control Cable · frayedCABLE WAS INSTALLED TO AIRCRAFT. PRE-TENSIONED TO 200 FEET/POUNDS (PER MM) WHILE AILERON CONTROLS WERE RUN THROUGH WHILE CABLE WAS UNDER TENSION AT 200 POUNDS, A SMALL 'BULGE' WAS NOTED AT APPROIXMATELY MID-CABLE LENGTH. AN INTERNAL CABLE STRAND HAD BROKEN (SDR CA961001008Control Cable · worn(CAN) AILERON CABLE FOUND WEARING INTO FLOOR BOARD NEAR THE COCKPIT FIREWALL. FLOORBOARD HAD BEEN INCORRECTLY INSTALLED AND SCREW HOLES WERE ELONGATED.SDR 96FDEA01382Fitting · corrodedNR0360 AND 027, CORROSION (C57-581-01-1) LT WING O/B AILERON CONTROL ROD FITTING ON AILERON IS CORRODED. *S/D* REMOVED AND REPLACED LT WING O/B AILERON CONTROL ROD FITTING ON AILERON IAW FEDEX SRM 51-30-2.SDR P5CA9601202Housing · corrodedCORROSION LT INBOARD AILERON POWER CONTROL PACKAGE HOUSING SURFACE. CORROSION REMOVED FROM SURFACE PER SRM 51-10-01.SDR ASOA96032Aileron Contl · roll rightFLT NR 7259 - OUTBOUND ATL-BQK, CAPTAIN EXPERIENCED A STRONG RIGHT ROLL TENDENCY IN THE AILERONS WITH AUTOPILOT OFF. CREW ELECTED TO RETURN TO ATL AND REQUESTED EQUIPMENT TO MEET THE AIRCRAFT. LANDING WAS MADE SAFELY IN ATL WITHOUT FURTHER INCIDENT. EXTENSISDR VTZA96285Servo · malfunctionFLT NR 6266 - IAD- BTV - DURING CRUISE, MADE A UNSCHEDULED LANDING DUE TO UNCOMMANDED INPUT FROM THE AILERONS. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED SERVO, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETUSDR P5CA9600470Control Cable · failedRIGHT WHEEL WELL FORWARD BULKHEAD BS 1283 CABLE FOUND LOOSE. UPON INVESTIGATION FOUND CABLE BIRD CAGED BY PULLEY AT BS 410 RBL 90 WL 210. REPLACED CONTROL CABLE PER BOEING MAINTENANCE MANUAL 20-11-03 AND 27-11-00.SDR P5CA9600469Control Cable · frayedLEFT WHEEL WELL AILERON CONTROL CABLE AA-9 HAS BROKEN STRAND AT REAR SPAR WS 435. REPLACED CABLE PER BOEING MAINTENANCE MANUAL 20-11-03 AND 27-11-00.SDR IXXA96138Bus Links · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT INBOARD AILERON, INBOARD BUS LINKS WERE FOUND TO BE CRACKED. THE BUS LINKS WERE REPLACED IAW THE DOUGLAS SRM AND MM. (M)SDR AU961100Control Cable · frayed(AUS) AILERON CABLE AB13 LOCATED IN AREA OF LH REAR SPAR HAD SIX OF SEVEN STRAND BROKEN AT CABLE DRUM AT WS 776.98 - CABLE AA11 ALSO DAMAGED WITH NUMEROUS BROKEN STRANDS - SUSPECT CAUSED BY INCORRECT INSTALLATION AND ALIGNMENT WITH BOTH CABLES BEING IN THE SASDR 96UAL900565Servo Control · leakingLANDED UNDER AMBER ALERT AT IAD DUE TO LOSS OF HYDRAULIC PRESSURE. *S/D* FOUND LEFT OUTBOARD AILERON SERVO CONTROL LEAKING. REPLACED SERVO CONTROL AND OPERATIONALLY CHECKED NORMAL.SDR 97ZZZX317Cables · rustedBOTH UPPER AND LOWER AILERON CONTROL CABLES RT WING ROOT ARE RUSTED AND NEED REPLACED. CORRECTIVE ACTION: REMOVED AND REPLACED UPPER AND LOWER RT AILERON CONTROL CABLES IAW A.M.M. SEE WORK CARD NR 2069 FOR FUNCTION CHECKS.SDR CA960715004Quadrant · cracked(CAN) DURING ROUTINE INSPECTION, THE LT AILERON QUADRANT WAS SUSPECTED TO BE CRACKED. AS A PRECAUTION, THE RT QUADRANT WAS INSPECTED AS WELL. THE LT QUADRANT WAS REPLACED AND RT WAS CHECKED BY EDDY CURRENT AND FOUND TO BE SERVICEABLE. PART TC: 18,996.SDR 96ZZZX3827Control System · corrosionINSPECTION FOUND AILERON CONTROL SYSTEM, LT AND RT, CORROSION.SDR CA960722006Panel · jams aileron(CAN) ON PREFLIGHT CREW FOUND AILERONS JAMMED. INVESTIGATION FOUND THAT THE RIGHT HAND BELLY PANEL (PANEL 612) THAT COVERS THE AILERON PUSH PULL RODS AND THE FLAP INTERCONNECT WAS BULGED INWARDS AND WAS FOULING THE AILERON SWING LINK. A HOLE HAD DEVELOPED IN TSDR CA960717002Spring · malfunction(CAN) AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL DISCONNECT ON LANDING. ROLL DISCONNECT SYSTEM INSPECTED AND NO FAULT FOUND. MANUFACTURER NOTIFIED. AWAITING APPROVAL OF DEHAVILLAND SB 8-27-79 REINSTALLATION AND REPOSITION OF MODIFIED DISCONNECT SPRING.SDR 96ZZZX3680Control Cable · frayedLEFT AILERON BALANCE CABLE FOUND FRAYED AT WS 56.87 ON CABLE SUPPORT BLOCK. THIS AIRCRAFT WAS ON 100-HOUR INSPECTION AND ONCE CABLE STARTED FRAYING, CONDITION MUST HAVE ACCELERATED, CABLE WAS 50 PERCENT THROUGH.SDR 96ZZZX3818Pcu Link · defectiveCREW REPORTED A HIGH PITCH NOISE COMING FROM THE RIGHT AILERON. INVESTIGATION PROVED THE AILERON PCU TO AILERON LINK WAS CHATTERING ON THE AILERON BOLT BUSHING. SPECIFICALLY, THE ANTI-ROTATION TABS OF THE LINK. THE BUSHINGS WERE REPLACED AS WELL AS THE LINKSDR 96ZZZX4168Control Cable · frayedDURING PHASE 12 INSPECTION, FOUND LOWER INBOARD AILERON CABLE WITH BROKEN WIRES. THIS WEAR/DAMAGE OCCURS AT FAIRLEADS P/N S338-1. INSPECTION FOUND TEFLON FAIRLEAD DAMAGES THIS CABLE ABOUT 75 PERCENT OF THE TIME. SUBMITTER STATED SOMETHING NEEDS TO BE DONE ASDR IXXA96120Control Cable · brokenON TAXI OUT AND FLIGHT CONTROL CHECKS AT ATL, AILERONS FELT STIFF WITH VERY LITTLE SPOILER PRESSURE DROP. THE AIRCRAFT RETURNED TO RAMP. MAINTENANCE INSPECTED THE FLIGHT CONTROL CABLES AND FOUND THE LEFT AILERON BUS CABLE BROKEN. MAINTENANCE REPLACED THE BRSDR DL76L961651Control Cable · severedDURING CLIMB, FLIGHT CREW HEARD A CRACK FOLLOWED BY A/C ROLL TO THE LEFT. TEMPORARILY LOST LEFT IDG BUT QUICKLY RETURNED. FOUND AILERON CONTROL CABLE A2B-3 SEVERED AND RIGHT GENERATOR FEEDER CABLE WORN JUST FORWARD AND RIGHT OF THE FORWARD CARGO COMPARTMENT SDR DL76L961525Control Cable · brokenON CLIMBOUT THROUGH 5000 FT, LOST RIGHT GENERATOR. NO EICAS MESSAGES. ALMOST CONCURRENT WITH GEN LOSS, EXPERIENCED LEFT AILERON HARD OVER WITH NO ASSOCIATED EICAS CAUTION OR STATUS MESSAGE. REPLACED A2B-3 AILERON CONTROL CABLE.SDR C2XA96IA147Lever Assy · bearings badIAH - DURING C-CHECK INSPECTION, THE AILERON INTERCONNECT ROD WAS FOUND TO HAVE STIFF BEARINGS ON THE LEFT END. MX REMOVED AND REPLACED THE LEFT LEVER ASSEMBLY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR C2XA96IA146Bearing · rusted bearingIAH - DURING C-CHECK INSPECTION, THE LEFT AILERON BELLCRANK INSIDE PANEL 544AB WAS FOUND TO HAVE A RUSTED AFT BEARING. MX REMOVED AND REPLACED THE BELLCRANK AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR 96ZZZX3214Control Cable · defectiveDURING ANNUAL INSPECTION, SERVICE BULLETINS WERE BEING REVIEWED. DURING REVIEW OF THESE BULLETINS, THERE WERE NUMEROUS REFERENCES TO PROBLEMS WITH PULLEYS AND CABLES IN THE AILERON SYSTEM. UPON INSPECTION OF THE AILERON CABLES, THERE WAS A CABLE FOUND TO BE SDR P5CA9600242Actuator · malfunctionedAFTER PUSHBACK, DURING FLIGHT CONTROL CHECK, FLIGHT CREW OBSERVED THAT LEFTHAND OUTBOARD AILERON DID NOT MOVE WITH FLAPS DOWN, RETURNED TO BLOCKS. CLEANED ELECTRICAL PLUG ON AILERON LOCKOUT ACTUATOR, OPERATIONAL CHECK SATISFACTORY PER MM 27-00-00.SDR 96ZZZX3433Control Cable · chafedDURING A 100-HOUR INSPECTION, THE FOLLOWING DEFECTS WERE FOUND: THE AILERON CONTROL CABLE WAS SCRAPING THE PRIMER LINE(S) LOCATED IN THE FIREWALL AND A CRACK IN THE CONTROL CABLE SUPPORT BETWEEN THE INSTRUMENT PANEL AND THE FIREWALL ON THE PILOT'S SIDE.SDR CA960723536Actuator · malfunction(CAN) DURING FLIGHT AILERON LOCKOUT MESAGE ON EICAS. RH AILERON LOCKOUT ACTUATOR REPLACED.SDR CA960606003Linkage · cracked(CAN) AILERON LINKAGE ASSEMBLY FOUND CRACKED. IT IS SUSPECTED THAT LINKAGE HAD FILLED WITH FLUIDS AND THEN FROZE CAUSING IT SWELL AND CRACK. DRAIN HOLE FOUND FILLED WITH UNKNOWN SEALANT.SDR UPS96220549Pulley Fittings · corrodedINSPECTION TYPE SI, L/W I/B AILERON TURN AROUND PULLEY FITTING IS CORRODED ON LOWER SURFACE. REMOVED CORRODED FITTING WHICH WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-40, INSTALLED NEW FITTING IAW SRM 51-30-2, MM 27-10-00 MM 27-61-00.SDR 97ZZZX284Cables · out of adjustATW - AILERON INTERCONNECT CABLES WORN AT THE RIGHT SIDE FUSELAGE PRESSURE SEALS. CORRECTIVE ACTION: REMOVED AND REPLACED AND ADJUSTED INTERCONNECT CABLES IAW BAE MM 27-11-44 AND 00. GENERATED W/C TO C/W AILERON CONTROLS CK.
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