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 96ZZZX2948Control Cable · wornALL FOUR AILERON CABLES CONTINUALLY WEAR RAPIDLY AT PULLEYS IN WING TRAILING EDGE. PULLEYS ACT AS FAIR LEADS, NO CABLE ANGLE CHANGE. SUBMITTER STATES AIRFLOW CAUSES CABLES TO VIBRATE ON PULLEYS AND WEAR THROUGH STRANDS.SDR 96ZZZX2947Control Cable · wornALL FOUR AILERON CABLES CONTINUALLY WEAR RAPIDLY AT PULLEYS IN WING TRAILING EDGE. PULLEYS ACT AS FAIR LEADS, NO CABLE ANGLE CHANGE. SUBMITTER STATES AIRFLOW CAUSES CABLES TO VIBRATE ON PULLEYS AND WEAR THROUGH STRANDS.SDR 96ZZZX2956Support · crackedSUPPORT WAS FOUND CRACKED AT THE FORWARD BOLT HOLE. LEFT AND RIGHT BELLCRANKS WERE NOT MAKING CONTACT WITH THE AFT STOPS. STOPS WERE APPROXIMATELY .50 INCH AWAY FROM THE BELLCRANKS. BOTH BELLCRANKS APPEAR TO BE IMPROPERLY RIGGED BECAUSE THE STOPS ARE ALMOSTSDR DLL12961205Actuator · failedON TAXI OUT, AFTER STARTING ENGINES THE A-SYSTEM HYD QUANTITY WENT TO .125 WITH LOW QTY LIGHT ON. SYSTEM PRESSURE WAS OK. DEPRESSURIZED SYSTEM AND RETURNED TO GATE. FOUND THE LEFT INBOARD AILERON THE OUTBOARD ACTUATOR HAD FAILED ALSO BREAKING ONE OF THE 3 HSDR P5CA9600229Control Cable · wornDURING PRE-DEPARTURE CHECK, FOUND RIGHT WING GEAR SHELF AREA AILERON CONTROL CABLE FORWARD OF HYDRAULIC RETURN FILTER WORN BEYOND LIMITS. REMOVED AND REPLACED AB-10 CABLE PER MM 20-11-03. SWAGED NEW TERMINALS, INSTALLED, SAFETIED AND TENSIONED IAW MM 27-11-0SDR COMA9630107Cam Lever Assy · bearing frozeAILERON CONTROLS ARE BINDING DURING FLIGHT. REPLACED THE RT AILERON CENTERING CAM LEVER ASSY. ACFT RETURNED TO SERVICE.SDR C2XA96IA119Bellcrank · rusted bearingIAH - DURING C-CHECK INSPECTION, THE LEFT AILERON TRANSITION BELLCRANK ABOVE THE TRIM ACTUATOR WAS FOUND TO HAVE A RUSTED BEARING. MAINTENANCE REMOVED AND REPLACED THE BELLCRANK AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR CA960522008Links · damaged(CAN) INSPECTION OF FLIGHT CONTROLS IN ACCORDANCE WITH SB A2/51. SPECIAL INSPECTION OF LINK STOP IN AILERON CONTROL CHAIN. LINKS #C2CF1197 AND C2CF1198 HAVE BEEN DAMAGED BY MAINTENANCE PERSONNEL, PROBABLY WITH VISE GRIP PLIERS. VERY DEEP SCRATCHES FOUND ON THESDR 96ZZZX2953Control Cable · misroutedDURING ANNUAL INSPECTION, LT AILERON CABLE WAS FOUND ROUTED OVER LIFT STRUT BRACKET. THESE CABLES ARE PART OF SB 12, BUT NOT LISTED FOR THIS MODEL AIRCRAFT. CABLE WAS REMOVED AND INSPECTED FOR DAMAGE. NONE WAS FOUND. CABLE HAD 84 HRS TIME SINCE REASSEMBLY SDR WWMA9600044Aileron Controls · lack of lubeCREW REPORTED, THAT THE ROLL CONTROL WAS ABNORMAL, AT LOWER AIRSPEEDS. ROLL TRIM CORRECTIONS VARYING LEFT TO RIGHT, BUT GENERAL TENDENCY IS A LEFT ROLL AS INDICATED AIRSPEED INCREASES. AILERONS FELL HEAVIER THAN NORMAL. QUICK SNAP INPUTS OF AILERON REQUIRED SDR AU960712Control Cable · worn(AUS) AILERON BALANCE CABLE FAULTY - CABLE WORN BEYOND LIMITS IAW AD/P68/23 AMDT2 - TURNBUCKLE NOT IN SAFETY (TOO SHORT) - SIX THREADS SHOWING EITHER SIDE OF TURNBUCKLE - PERSONNEL/MAINTENANCEERRORSDR 96ZZZX2957Support · crackedBELLCRANK SUPPORT FOUND CRACKED AT THE FORWARD BOLT HOLE. LEFT AND RIGHT BELLCRANKS WERE NOT MAKING CONTACT WITH THE AFT STOPS. STOPS WERE APPROXIMATELY .50 INCH AWAY FROM THE BELLCRANKS. BOTH BELLCRANKS APPEAR TO BE IMPROPERLY RIGGED BECAUSE THE STOPS ARE SDR 96ZZZX2950Support · crackedBELLCRANK SUPPORT WAS FOUND CRACKED AT THE FORWARD BOLT HOLE. LEFT AND RIGHT BELLCRANKS WERE NOT MAKING CONTACT WITH THE AFT STOPS. STOPS WERE APPROXIMATELY .50 INCH AWAY FROM THE BELLCRANKS. BOTH BELLCRANKS APPEAR TO BE IMPROPERLY RIGGED BECAUSE THE STOPS SDR P5CA9600219Actuator · inoperativeON TAXI OUT DURING CONTROL CHECK, RIGHT OUTBOARD AILERON WOULD NOT UNLOCK WITH FLAPS IN TAKEOFF RANGE. REMOVED AND REPLACED LOCK-OUT ACTUATOR IAW MM 27-11-16. OPS CHECK NORMAL.SDR 96ZZZX2835Control Cable · wornDURING A 1600-HOUR CONTROL CABLE INSPECTION, FOUND RIGHT WING UPPER AILERON CABLE, PN 120-27655-031, WORN WITH BROKEN STRANDS WHERE CABLE PASSES THROUGH NYLON GROMMET ON BOTH INBOARD AND OUTBOARD NACELLE STRUCTURE.SDR 96ZZZX2834Control Cable · wornDURING A 1600-HOUR CONTROL CABLE INSPECTION, FOUND LEFT WING LOWER AILERON CABLE, PN 120-27655-005, WORN WITH BROKEN STRANDS WHERE CABLE PASSES THROUGH NYLON GROMMET ON BOTH INBOARD AND OUTBOARD NACELLE STRUCTURE.SDR 96ZZZX2833Control Cable · wornDURING A 100-HOUR CONTROL CABLE INSPECTION, FOUND RIGHT WING LOWER AILERON CABLE, PN 120-27655-029, WORN WITH BROKEN STRANDS WHERE CABLE PASSES THROUGH NYLON GROMMET ON BOTH INBOARD AND OUTBOARD NACELLE STRUCTURE.SDR 96ZZZX2832Control Cable · wornDURING A 1600-HOUR CONTROL CABLE INSPECTION, FOUND LEFT WING LOWER AILERON CABLE, PN 120-27655-007, WORN WITH BROKEN STRANDS WHERE CABLE PASSES THROUGH NYLON GROMMET ON BOTH INBOARD AND OUTBOARD NACELLE STRUCTURE.SDR AU960568Cable · frayed(AUS) RH AILERON/RUDDER INTERCONNECT CABLE FRAYED DUE TO CHAFING ON EACH END OF THE STEEL TUBE COVERING THE CABLESDR AALA960655Casting · crackedTUL - FOUND INBOARD AILERON QUADRANT CASTING AND WEB AT CASTING CRACKED. REMOVED AND INSTALLED NEW WEB AND QUADRANT AND CASTING. (M)SDR 9609316613Actuator · iced upDURING CRUISE, THE AIRCRAFT WOULD NOT TURN, APPLIED A MODERATE AMOUNT OF PRESSURE TO FREE AILERONS. AIRCRAFT CONTINUED TO NRT AND LANDED WITHOUT INCIDENT. REMOVED ICE FROM THE CENTRAL CONTROL ACTUATOR LOAD LIMITER. REPLACED THE NR 2 PACK WATER SEPARATOR COASDR PLG41896G4Cable Assy · chafedDURING ROUTINE C-CHECK INSPECTION, CHAFING FOUND ON RIGHT FORWARD CONTROL CABLE IN AILERON CIRCUIT IN FUSELAGE. CABLE WAS REPLACED AND RIGGED IAW SAAB MM CHAPTER 27. (X)SDR 96ZZZX3116Control Cable · wornATW - RIGHT AILERON INTERCONNECT OUTBOARD CABLE WORN THROUGH TUBING. REMOVED AND REPLACED RIGHT AILERON INTERCONNECT OUTBOARD CABLE ASSY IAW MM 27-11-44.SDR 96ZZZX3115Control Cable · corrodedATW - LEFT AILERON INTERCONNECT OUTBOARD CABLE NEEDS TO BE REPLACED DUE TO CORROSION. REMOVED AND REPLACED LEFT AILERON INTERCONNECT OUTBOARD CABLE ASSY IAW 27-11-44.SDR 96ZZZX2932Cable Assy · broken strandsWHILE PERFORMING A 1,600 FLIGHT HOUR CABLE INSPECTION, FOUND LT WING UPPER AILERON CONTROL CABLE WORN AND WITH BROKEN STRANDS AT LT WS Y2902 AND WS Y3678 WHERE THE CABLE PASSES THROUGH THE INBOARD AND OUTBOARD NACELLE WALLS.SDR 96ZZZX2445Cable Assy · broken strandsWHIEL PERFORMING A 1,600 FLIGHT HOUR CABLE INSPECTION, FOUND LT WING AILERON LOWER WING CABLE HAD BROKEN STRANDS AT WS Y3678 WHERE CABLE PASSES THROUGH THE NACELLE.SDR 96ZZZX2444Cable Assy · broken strandsWHILE PERFORMING A 1,600 FLIGHT HOUR CABLE INSPECTION, FOUND RT WING AILERON LOWER WING CABLE WITH BROKEN STRANDS AT WS Y2902 WHERE THE CABLE PASSES THROUGH THE NACELLE.SDR DHL96708002Aileron Spring · wornLEFT CONTROL YOKE INPUTS BEYOND 30O YOKE BECOMES STIFF AND IF RELEASED AT MORE THAN 30O, LEFT YOKE WILL STAY AT THAT POSITION UNTIL MANUALLY RETURNED TO ZERO. PROBLEM DID NOT OCCUR BELOW 10,000 FT ON CLIMB OR DECENT. REPLACED AILERON QUADRANT CENTERING SPRINSDR 96ZZZX3105Control Cable · corrodedATW - AILERON INTERCONNECT CABLES ARE CORRODED AT WING ROOT PULLEYS. REMOVED AND REPLACED BOTH CENTER SECTION AILERON INTERCONNECT CABLES. REF W/C 2079 FOR FUNCTIONAL TEST OF AILERON CONTROLS.SDR DL767960829Actuator · failedDURING FLT CONTROL CHECK, AILERON AND ELEVATOR FELT VERY HEAVY. AIRCRAFT RETURNED TO BLOCK. REPLACED RT LCCA, RIGGED AND LEAK CHECKED, OPERATION NORMAL.SDR 96ZZZX2466Bolt · wedged aileronAILERON STOP BOLT NAS428-3-10 SECURED TO A NUTPLATE ON A BRACKET ASSSEMBLY PN 1221088-8 SECURED TO MAIN SPAR ASSEMBLY AND IS USED AS A STOP FOR UP-AILERON TRAVEL, FAILED TO STOP THE UP-TRAVEL OF THE RIGHT AILERON. BOLT DEFLECTED AND BOLT HEAD BECAME WEDGED ONSDR 96ZZZM764Cable · frayedDURING A 1600 HOUR CONTROL CABLE INSPECTION, FOUND LEFT WING LOWER AILERON CABLE, P/N 12027655-005, WORN WITH BROKEN STRANDS AT WING STATION Y2902 WHERE CABLE PASSES THROUGH NYLON GROMMET, P/N PE49068-505, AT OUTBOARD NACELLE STRUCTURE. IT APPEARS THAT THE CASDR CA960514101Control Cable · broken(CAN)WHILE CYCLING AILERON CONTROLS FOR INVESTIGATION OF A HYDRAULIC LEAK, THE CAPTAINS CONTROL WHEEL WOULD NOT RETURN TO THE CENTRE POSITION. FURTHER INVESTIGATION REVEALED THE AILERON DOWN CABLE RUN #7 BROKE INSIDE THE CONTROL COLUMN. AL SO THE AILERON "UPSDR C2XA96IA080Bearing · wornIAH - DURING C-CHECK INSPECTION, THE LEFT AILERON CONTROL SYSTEM BELLCRANK AT THE CENTER WING WAS FOUND TO HAVE A WORN AND RUSTED BEARING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR CA960327018Control Cable · frayed(CAN) DURING ROUTINE INSPECTION THE AILERON CABLE WAS FOUND FRAYED WHERE IT PASSES THROUGH THE PULLEY ASSEMBLY UNDER THE SCUFF PLATE AREA IN THE COCKPIT. THIS CABLE WAS FOR THE LEFT HAND AILERON. THE CABLE WAS REPLACED WITH A NEW ONE.SDR COMA9630079Ail Controls · lack of lubeAILERON CONTROLS ARE BINDING. BINDING IS MORE PRONOUNCED IN RT TURNS. CLEANED AND LUBRICATED AILERON SYSTEM, NO DEFECTS FOUND. FIGHT CHECK SATISFACTORY.SDR 96ZZZX2060Support · crackedDURING A ROUTINE ANNUAL INSPECTION, BOTH LOWER AILERON BELLCRANK BRACKETS WERE FOUND CRACKED BY THE FORWARD BOLT. SUBMITTER STATED THIS IS MOST LIKELY CAUSED BY EITHER IMPROPERLY ADJUSTED AILERON STOPS OR BY NOT 'TYING' THE CONTROLS WHILE THE AIRCRAFT IS PARKSDR 96ZZZX1989Control Cable · frayedDURING ROUTINE ANNUAL INSPECTION, THE AILERON BALANCE CABLE WAS FOUND FRAYED WITH APPROXIMATELY 50 PERCENT OF THE STRANDS BROKEN. LOCATION OF THIS DEFECT WAS WHERE THE CABLE PASSED BY THE THREE NYLON CABLE PULLEYS IN THE CENTER FUSELAGE AREA, ACCESSED THROUGHSDR 96ZZZM654Bearing · wornSTL - DURING APPROACH AIRCRAFT REQUIRED EXCESSIVE AILERON TRIM CHANGE WHEN POWER AND SPEED CHANGED, AND MORE POWER THAN NORMAL TO MAINTAIN PROPER SINK RATE. FOUND LEFT AILERON INBOARD HINGE EYEBOLT BEARING, MFG P/N DMD6-7E1-501, WORN. REPLACED HINGE EYEBOLT SDR CA960320010Bellcrank Assy · cracked(CAN)DURING A SCHEDULED 100 HOUR INSPECTION, MAINTENANCE PERSONNEL DISCOVERED A CRACK IN THE RIGHT AILERON BELLCRANK ASSEMBLY. PART NUMBER 40339-01, REFERENCE FIG. 96, ITEM #4 OF THE PIPER PA31-350 PARTS C ATALOGUE. P/N 761-487 REVISED MARCH 10, 1994. THE CRACSDR AU960366Control Cable · frayed(AUS) LH FORWARD AILERON CONTROL CABLE CONTAINED NUMEROUS BROKEN WIRES OVER A 100MM (4IN) LENGTH AT THE PULLEY LOCATED AT THE FIREWALLAREA AT FS 100.00SDR COMA9630045Bearing · seizedAILERON CONTROL MOVEMENT IS EXTREMELY STIFF ON GROUND AND IN FLIGHT. FOUND THE RT INBD AILERON BELL CRANK TO HAVE FROZEN BEARINGS. REPLACED THE CRANK ASSY.SDR 96ZZZX1282Support · elongated holesDURING ANNUAL INSPECTION, FOUND RT AILERON BELLCRANK BOLT HOLES ON THE SUPPORT CHANNELS TO BE ELONGATED. ONLY THE PIVOT HOLES WERE BAD, NOT THE STOP-PIN HOLES. SUSPECT CAUSED BY NOT INSTALLING CONTROL LOCK WHEN ACFT ON GROUND.SDR 96ZZZX1281Support · elongated holesDURING ANNUAL INSPECTION, FOUND RT AILERON BELLCRANK BOLT HOLES ON THE SUPPORT CHANNELS TO BE ELONGATED. ONLY THE PIVOT HOLES WERE BAD, NOT THE STOP-PIN HOLES. SUSPECT CAUSED BY NOT INSTALLING CONTROL LOCK WHEN ACFT ON GROUND.SDR MEJA960202Bellcrank · crackedDURING A ROUTINE INSPECTION, MAINTENANCE FOUND THE LT AILERON BELLCRANK CENTER HINGE HAD A SLIGHT CRACK. THE AIRCRAFT WAS REMOVED FROM SERVICE, INSPECTED AND FOUND SAFE FOR A ONE TIME FERRY FLIGHT FROM RAP TO SAT. UPON ARRIVAL AT SAT THE DEFECTIVE BELLCRANK SDR DL72S960367Bell Crank · wornPILOT REPORTS, AT 230 KTS A LOUD VIBRATION WAS HEARD FROM THE F/O WINDOW AREA DURING CLIMBOUT AND AT 220 KTS DURING DECEL THE VIBRATION STOPPED. REPLACED THE RIGHT HAND OUTBOARD AILERON TRIM TAB BELL CRANK, WHICH WAS FOUND TO HAVE OBLONGED MOUNT HOLES. RIG CSDR DLL10960403Flt Controls · lack of lubeAIRCRAFT HARD TO ROLL RIGHT, BUT ROLLS NORMAL BACK TO THE LEFT. TURNING OFF B-AILERON SERVO INBD, CAUSED UNCOMMANDED HARD LEFT ROLL. INSPECTION OF FLT CONTROL SYSTEM FOUND EXTREME BINDING IN LINKAGE BETWEEN LEFT INBD AILERON AND WHEEL WELL. LUBED LINKAGE BSDR CA960222038Panels · gouged(CAN)FOUND AS A RESULT OF SD ALERT AL-95-06 BOTH LEFT HAND (P/N 532DB) AND RIGHT HAND (P/N 632DB) PANELS GOUGED FROM LOWER JAM-SWITCH CLAMPS.SDR CA960222037Panel · gouged(CAN)FOUND AS A RESULT OF SD ALERT AL-95-O6 RIGHT HAND PANEL GOUGED FROM LOWER JAM-SWITCH CABLE CLAMP.SDR CA960222036Panel · gouged(CAN)FOUND AS A RESULT OF SD ALERT AL-95-06 RIGHT HAND PANEL GOUGED FROM LOWER JAM-SWITCH CABLE CLAMP.
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