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 UPS98227521Push Rod · corrosionINSPECTION TYPE-D, CORROSION ON LT O/B AILERON PUSH ROD ATTACH LUG. REPLACED PUSH ROD ATTACH WG CASTING IAW DRAWING NR 65-21766.SDR C2XA98IA289Control Cable · frayedSHV - FLT 3776 - THE PILOT REPORTED THE LEFT CONTROL YOKE HAD EXCESSIVE PLAY IN AILERON CONTROL. THE AIRCRAFT LANDED AT SHV WITHOUT INCIDENT WHERE MAINTENANCE FOUND THE LEFT AILERON CONTROL QUADRANT LOWER CABLE TO HAVE BROKEN STRANDS. MAINTENANCE REMOVED ANDSDR AU980916Pushrod · loose(AUS) AILERON CONTROL SYSTEM PUSHROD LOWER END FITTING RIVETS LOOSE.SDR ARWA980799Controls · wornLEFT AILERON VERY STIFF IN RIGHT TURN WHILE TROUBLESHOOTING AILERONS PROBLEMS. FOUND LT CABLE ROD END BEARING WORN, CRANK CRACKED AND SPOILER MIXER ROD END BEARING WORN. REMOVED AND REPLACED LATERAL SPOILER LT CONTROL CABLE IAW MM 20-17-0. REPLACED ACTUATORSDR 99ZZZM9Aileron · out of rigPILOT FLYING NEW AIRCRAFT FROM AMERICAN CHAMPION FACTORY TO ANCHORAGE,ALASKA, REPORTED THE AIRCRAFT FLEW 'HALF OF A BALL' OUT OF TRIM, AND WAS UNABLE TO CORRECT THE PROBLEM BY ADJUSTING THE RUDDER TRIM TAB. FLAPS AND AILERONS FOUND NOT TO BE RIGGED IAW SCOUNTSDR CA980721020Spring · weak(CAN) WHEN RIGHT WHEEL CONTACTED RUNWAY, THE AILERON ROLL SPOILER (RIGHT AND LEFT CONTROL WHEELS) SPLIT. RD 8-53-3620 ISSUE NR 2 HAD BEEN COMPLETED. SUSPECT A WEAK CLUTCH SPRING. GREASE ALSO FOUND ON AND IN CLUTCH MECHANISM-IT SHOULDN'T BE THERE. SUBMITTESDR DHL9872171DBracket · corrodedAT D-CHECK, RT I/B AILERON TURN AROUND PULLEY SUPPORT BRACKET ASSY HAS CORROSION PITTING AROUND PULLEY PIVOT BOLT HOLE LOWER SIDE AND LOWER O/B BOLT. REMOVED AND REPLACED BRACKET PER MM 27-10-1. N/R 2418.SDR 99ZZZM573Control Cable · corrodedBOTH CENTER AILERON INTERCONNECT CABLES ARE CORRODED. REMOVED AND REPLACED BOTH CENTER AILERON INTERCONNECT CABLES, GENERATED NEW WC FOR TRAVEL CHECKS AND FREEDOM OF MOVEMENT. (M)SDR DHL9872159DCasting · crackedAT D-CHECK, RT WING O/B AILERON GEARBOX SUPPORT CRACKED ON UPPER SIDE. REMOVED AND REPLACED CASTING PER SRM 51-10-1. N/R 2410.SDR 98ZZZX4095Bolt · improper partFORWARD LOWER CABIN DOOR HINGE BOLT IMPROPERLY DRILLED, INSTALLED SO THAT IT CONTACTED THE CABIN DOOR FRAME, KEEPING THE DOOR FROM CLOSING PROPERLY. FACTORY REPRESENTATIVES REPAIRED FIBERGLASS DOOR, REDRILLED, AND REINSTALLED CORRECTLY. BOLT ATTACHING LEFT ASDR 98ZZZX2676Control Cable · wornAT ANNUAL INSPECTION, FOUND AILERON CABLE WORN BEYOND LIMITS. REPLACED AND RE-RIGGED AILERON CABLES.SDR CA980714017Angle · failed(CAN) THE ANGLE BRACKET FOR THE AILERON SYSTEM HAD BEEN REWORKED PER RD8-53-3620, BUT ROLL DISCONNECT HAPPENED AGAIN. THE BRACKET WAS AGAIN REWORKED AND AGAIN ON TOUCHDOWN, THE ROLL DISCONNECT HAPPENED.SDR 98ZZZX3030Control Cable · frayedALL AILERON CABLES (4 EACH) WERE FOUND WORN AND FRAYED AT THE FAIRLEADS AT THE OUTBOARD END OF THE MAIN WHEEL WELLS. RECOMMEND AD NOTE REQUIRING CABLE REPLACEMENT AT REGULAR INTERVALS POSSIBLY 4,000 HOURS OR 20 YEARS WHICHEVER COMES FIRST.SDR 98ZZZX3029Control Cable · frayedALL AILERON CABLES (4 EACH) WERE FOUND WORN AND FRAYED AT THE FAIRLEADS AT THE OUTBOARD END OF THE MAIN WHEEL WELLS. RECOMMEND AD NOTE REQUIRING CABLE REPLACEMENT AT REGULAR INTERVALS POSSIBLY 4,000 HOURS OR 20 YEARS WHICHEVER COMES FIRST.SDR CA980714016Angle · interfering(CAN) ROLL DISCONNECT SOMETIMES GETS CAUGHT UP ON THE ANGLE BRACKET THAT MAKES UP THE SUPPORT BOX, WHICH HOLDS THE LEVER ASSY IN PLACE. IT CATCHES WHEN GOING FROM DISCONNECT TO CONNECT. IT CATCHES BETWEEN THE PLATE ASSY ON TOP AND THE EYE END OF THE CABLE. SDR CA980713013Clutch · malfunctioned(CAN) AT MAIN LANDING GEAR TOUCHDOWN, A ROLL DISCONNECT OCCURRED. ON ROLLOUT EVERYTHING BACK TO NORMAL, AND RE-ENGAGEMENT AND PROPER ROLL CONTROL OPERATION. SYSTEM CLEANED.SDR 99ZZZM544Control Cable · corrodedLEFT MAIN AILERON CONTROL CABLES ARE CORRODED AT PULLEY BETWEEN FUSELAGE FRAME NR 24 AND 25. REMOVED AND REPLACED LEFT MAIN AILERON CENTER CONTROL CABLES, TENSIONED AND SAFETIED. (M)SDR VJ9800188Pcu · malfunctionedGOING TO RIGHT, AILERON APPEARS TO BE BINDING. FOUND B-SYSTEM HYDRAULICS MALFUNCTION IN AILERON PCU. REMOVED AND REPLACED PCU.SDR 98ZZZM505Control Cable · damagedCREW REPORTED AILERON CONTROL 'STUCK' WHEN ROLLING TO THE RIGHT. AIRCRAFT MADE A SAFE LANDING AT GCN. MAINTENANCE FOUND A HOLLOW RIVET JAMMED IN CONTROL CABLE PULLEY AT FUSELAGE STATION 111.00. CABLE WAS DAMAGED REQUIRING REPLACEMENT. AREA UNDER LEFT CREW SDR 99ZZZM431Control Cable · corrodedTHE CENTER FUSELAGE INTERCONNECT CABLES ARE CORRODED AT RIGHT WING ROOT. REMOVED AND REPLACED BOTH CENTER FUSELAGE INTERCONNECT CABLES AND ADJUSTED IAW MM 27-11-00. W/CS GENERATED FOR FUNCTIONAL TEST OF AILERON CONTROLS AND DISCONNECT. (M)SDR W7NA9800001Control Cable · frayedEKO - FLT 9988 - AILERON BUS CABLE FRAYED. CABLE ROUTED WRONG AROUND CABLE GUARD. REMOVED AND REPLACED CABLE. ROUTED PROPERLY IAW MM 27-11-11, 27-11-101, AND 27-11-71. AILERON FUNCTIONALLY CHECKED GOOD. AIRCRAFT REUTRNED TO SERVICE. (X)SDR 98ZZZX2228Link · chafedAILERON AND RUDDER FORWARD BUNGEE SPRING INSTALLED IN SUCH A WAY THAT MADE THE AILERON CONTROL CABLE LINK P/N 35-524302 CHAFE UP AND DOWN THE AILERON CONTROL CABLE. BY REVERSING THE ATTACHMENT OF THE SPRING AT THE LINK END, THE LINK IS HELD AWAY FROM THE AILESDR 98FDEA00365Actuator · failedSTA-LAX: ALL DEFLECT DISAG ALERT ON SLAT RETRACTION. RETURNED TO LAX. AIRCRAFT RELEASED FOR SERVICE PER MEL/CDL 27-2. REMOVED ACTUATOR AND INSTALLED FIXED PUSHROD PER MEL MX PROCEDURE 27-2. REMOVED AND REPLACED RT OUTBOARD AILERON DEFLECTION ACTUATOR PER SDR UF6A980516Pin · failedORD - FLT 5708 - CSC CWP ILLUMINATED ON FINAL ALONG WITH AILERON SPLIT AND ENGAGED LIGHTS. MAINTENANCE REMOVED AND REPLACED AILERON SHEAR PIN. SYSTEM OPS CHECKED GOOD. ACFT TT: 12,683 HOURS. (X)SDR AU980558Control Cable · misinstalled(AUS) AILERON CABLE IN RT WING IS ROUTED OVER THE AUTOPILOT SERVO PULLEY AND OVER THE AILERON CABLE PULLEY RESULTING IN THE CABLE BEING PULLED OUT OF ALIGNMENT CAUSING A LARGE CABLE DEFLECTION THAT HAS THE CABLE RIDING ON THE COTTER PIN CABLE KEEPER INSTEAD OFSDR AU980554Control Cable · misinstalled(AUS) AILERON CABLE IN RT WING IS ROUTED OVER THE AUTOPILOT SERVO PULLEY AND OVER THE AILERON CABLE PULLEY RESULTING IN THE CABLE BEING PULLED OUT OF ALIGNMENT CAUSING A LARGE CABLE DEFLECTION THAT HAS THE CABLE RIDING ON THE COTTER PIN CABLE KEEPER INSTEAD OFSDR AU980550Control Cable · misinstalled(AUS) AILERON CABLE IN RT WING IS ROUTED OVER THE AUTOPILOT SERVO PULLEY AND OVER THE AILERON CABLE PULLEY RESULTING IN THE CABLE BEING PULLED OUT OF ALIGNMENT CAUSING A LARGE CABLE DEFLECTION THAT HAS THE CABLE RIDING ON THE COTTER PIN CABLE KEEPER INSTEAD OFSDR 98ZZZX2708Beam · looseDURING C/W SB 750-27-11, BOTH AILERON PCU'S WEEPING HYD FLUID. PCU'S REPLACED AND SB ACCOMPLISHED. ACFT RIGGED AND TESTED IAW CE750 MM. ON NEXT FLT, COCKPIT EICAS MESSAGES INDICATED AILERON PCU RIGGING INADEQUATE. HYD SERVICE UNIT RE-INSTALLED, RIGGING RSDR 98ZZZX2149Control Cable · wornDURING A 100-HOUR INSPECTION, FOUND A SLIGHTLY FLAT SPOT ON THE RT AILERON CABLE ADJACENT TO THE MOST INBOARD FAIRLEAD ON THE WING STRUT. FURTHER INVESTIGATION AND WIPING CABLE CLEAN WITH A RAG REVEALED A BROKEN STRAND AND SEVERAL MORE SOON TO BREAK. CLOSE ISDR 98ZZZX2135Control Cable · chafedDURING A 100-HOUR INSPECTION, FOUND A SLIGHTLY FLAT SPOT ON THE RT AILERON CABLE ADJACENT TO THE MOST INBOARD FAIRLEAD ON THE WING STRUT. FURTHER INVESTIGATION AND WIPING CABLE CLEAN WITH A RAG REVEALED A BROKEN STRAND AND SEVERAL MORE SOON TO BREAK. CLOSE ISDR CA980519004Pushrod · cracked(CAN) AILERON PUSH ROD AT SWAGED END FOUND CRACKED.SDR COMA9860094Link · crackedRIGHT AILERON WILL NOT TEST WITH SYSTEM 2 PRESSURE VERIFIED AT 2900 PSI. FOUND PCU OUTPUT LINK FOR SYSTEM 2 (INBOARD) BROKEN FORWARD OF AILERON ATTACH. REMOVED AND REPLACED OUTPUT LINK (P/N 27295-3) WITH SERVICEABLE (P/N 27295-5) IAW CANADAIR MM 27-14-15-400SDR 98ZZZX2189Input Lever · crackedAILERON ACTUATOR INPUT LEVER FOUND CRACKED AT ATTACH BOLT HOLE. LEVER FOUND CRACKED AT ATTACHMENT BOLT HOLE.SDR CA980504018Turnbuckle · cracked(CAN) ONE INCH CRACK IN TURNBUCKLE BARREL STARTING FROM LT THREAD END. REPLACED.SDR ARWA980463Cable Guide · brokenDURING D-CHECK, FOUND LEFT WING FRONT SPAR AT STATION XFS 422.0 HAS A PHENOLIC CABLE GUIDE BROKEN. FABRICATED REPAIR SPLICES AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-0705. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 9701SDR 98UAL900160Power Cont Unit · failedDURING OPERATIONAL CHECK OF AILERON CONTROL SYSTEM, LT INBOARD AILERON POWER CONTROL PACKAGE STARTED GUSHING HYDRAULIC FLUID. UPON EXAMINATION OF PCP AFTER REMOVAL, FOUND INNER ACTUATOR ROD SHEARED AT FORWARD END. AIRCRAFT WAS IN UAL-OMB MAINTENANCE FACILITYSDR CA980706016Ailerons · failed(CAN) ON LANDING IN LEFT CROSSWIND, THE AILERONS DISCONNECTED AT TOUCHDOWN WITH CAPTAIN FLYING. FIRST OFFICER'S AILERONS WERE STILL CONNECTED. CAPTAINS RECONNECTED ON ROLL-OUT. NO FAULTS FOUND. MOD 8/2376, SB 8-27-79 PREVIOUSLY ACCOMPLISHED.SDR CA980422006Clutch · disconnected(CAN) ON LANDING IN A LEFT CROSSWIND, THE AILERONS DISCONNECTED AT TOUCHDOWN. PILOT SIDE ONLY, COPILOT'S AILERONS STILL CONNECTED. CAPTAIN'S AILERONS RECONNECTED AT ROLLOUT. NO FAULT FOUND. HOWEVER, MOD. 8/2342--SB 8-27-79 WAS PREVIOUSLY ACCOMPLISHED, BUT SDR AU980453Control Cable · frayed(AUS) AILERON/RUDDER BALANCE CABLE FRAYED AT TERMINAL FITTING.SDR UPS98226433Hinge · crackedINSPECTION TYPE-C, RT OUTBD AILERON HINGE IS CRACKED, SECOND FROM INBD HINGE FITTING. REPLACED IAW 65-19275.SDR 98ZZZX1624Control Cable · frayedDURING INCORPORATION OF SK 172-149 KIT TO C/W SB 97-1, FOUND RT AILERON DIRECT CABLE FRAYED WHERE IT TRAVELS UNDER THE RT OUTBOARD PULLEY LOCATED AT THE LOWER AFT DOOR FRAME AREA. THIS IS A VERY DIFFICULT AREA TO INSPECT DURING ROUTINE INSPECTIONS. THE FRAYISDR CKSA98208Power Contl Vlv · failedMAN RUDDER AND AILERON LIGHTS CAME ON IN FLIGHT ALONG WITH RES PRESS LOW LIGHT HYD QTY DROPPED DOWN 1/3 FROM FULL. LOST ALL HYD PRESS. PERFORMED ABNORMAL HYDRAULICS THEN EMERGENCY HYDRAULIC CHECKLIST ACCORDING TO FOM. MADE 0 FLAP LANDING SFO. REMOVED AND RSDR UPS98226458Casting · corrodedINSPECTION TYPE-C, RT INBD AILERON TURNAROUND PULLEY CASTING HAS CORROSION ON LUG FOR TURNAROUND PULLEY. CASTING REPLACED IAW SRM 51-30-2.SDR UPS98226457Casting · corrodedINSPECTION TYPE-C, LT INBD AILERON TURNAROUND PULLEY CASTING HAS CORROSION ON LUG FOR TURNAROUND PULLEY. REPLACED CASTING WITH NEW ONE IAW SRM 51-30-2.SDR 98ZZZX1677Support · crackedAILERON BELLCRANK SUPPORTS BROKEN AT FORWARD ENDS OF SUPPORT. THE DAMAGE HAS TO BE FOUND WITH A MIRROR. THE BELLCRANK SUPPORTS LOOK SATISFACTORY LOOKING IN THE ACCESS HOLES ORIGINALLY INSTALLED BY PIPER. THE FRONT FLANGE OF THE AILERON BELLCRANK SUPPORT BRASDR 98ZZZX1676Support · crackedAILERON BELLCRANK SUPPORTS BROKEN AT FORWARD ENDS OF SUPPORT. THE DAMAGE HAS TO BE FOUND WITH A MIRROR. THE BELLCRANK SUPPORTS LOOK SATISFACTORY LOOKING IN THE ACCESS HOLES ORIGINALLY INSTALLED BY PIPER. THE FRONT FLANGE OF THE AILERON BELLCRANK SUPPORT BRASDR CA980331020Guard Pin · chafed(CAN) AILERON HAD BEEN ROUTED OVER ITS GUARD PIN. CABLE HAD CHAFED ITS WAY THROUGH THE PIN. ONCE PIN WAS REMOVED, THE CABLE TENSION DROPPED FROM 90 POUNDS TO 25 POUNDS. PIN IS LOCATED AT LT WS 462.SDR 98ZZZX1313Control Rod · brokenDURING ANNUAL INSPECTION, FOUND ROD END BEARINGS IN AILERON CONTROL ROD WORN. AFTER REMOVAL, FOUND INNER ROD END ACTUALLY BROKEN IN THREADED AREA. A SMALL HOLE WAS DRILLED THROUGH THE ROD ASSEMBLY ITSELF, AND THROUGH THE ROD END, AND THEN SECURED WITH ROLL PSDR UPS98226216Casting · corrodedINSPECTION TYPE-C, LT AILERON TURNAROUND PULLEY CASTING HAS CORROSION ON LOWER SUPPORT LUG FOR TAB PULLEY. CASTING REPLACED IAW OHM 27-12-00.SDR 99ZZZM491Pulley · seizedRIGHT WING LOWER AILERON TRIM CABLE PULLEY SEIZED OUTBOARD OF NR 4 FLAP TRACK. REMOVED AND REPLACED TRIM CABLE PULLEY'S AS NEEDED IAW MM. (M)
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