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.

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.Jul 30, 1998 · N905UP · Boeing 72751CSDR 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 ANDJul 29, 1998 · N15730 · Emb EMB120RTSDR AU980916Pushrod · loose(AUS) AILERON CONTROL SYSTEM PUSHROD LOWER END FITTING RIVETS LOOSE.Jul 28, 1998 · Piper PA60601PSDR 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 ACTUATORJul 16, 1998 · N345JW · Doug DC863SDR 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 SCOUNTJul 12, 1998 · N695AC · Bbavia 8GCBCSDR 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. SUBMITTEJul 11, 1998 · Dhav DHC8102SDR 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.Jul 9, 1998 · N721DH · Boeing 727228SDR 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)Jul 9, 1998 · N611AW · Bag BAE146300ASDR 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.Jul 7, 1998 · N721DH · Boeing 727228SDR 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 AJul 7, 1998 · N695AC · Bbavia 8GCBCSDR 98ZZZX2676Control Cable · wornAT ANNUAL INSPECTION, FOUND AILERON CABLE WORN BEYOND LIMITS. REPLACED AND RE-RIGGED AILERON CABLES.Jul 7, 1998 · N171M · Piper PA28R201SDR 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.Jul 6, 1998 · Dhav DHC8301SDR 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.Jul 1, 1998 · N9540R · Beech K35SDR 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.Jul 1, 1998 · N9540R · Beech K35SDR 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. Jun 24, 1998 · Dhav DHC8301SDR 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.Jun 23, 1998 · Dhav DHC8301SDR 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)Jun 19, 1998 · N612AW · Bag BAE146300ASDR VJ9800188Pcu · malfunctionedGOING TO RIGHT, AILERON APPEARS TO BE BINDING. FOUND B-SYSTEM HYDRAULICS MALFUNCTION IN AILERON PCU. REMOVED AND REPLACED PCU.Jun 7, 1998 · N737Q · Boeing 7372L9SDR 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 Jun 7, 1998 · N146SA · Dhav DHC6300SDR 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)Jun 5, 1998 · N612AW · Bag BAE146300ASDR 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)May 28, 1998 · N118RW · Boeing 7372Y5SDR 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 AILEMay 28, 1998 · N6182X · Beech A36SDR 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 May 23, 1998 · N584FE · Doug MD11SDR 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)May 21, 1998 · N857AW · Bag ATPSDR 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 OFMay 21, 1998 · Cessna 172RSDR 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 OFMay 21, 1998 · Cessna 172RSDR 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 OFMay 21, 1998 · Cessna 172RSDR 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 RMay 20, 1998 · N206PC · Cessna 750SDR 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 IMay 12, 1998 · N9598C · Chris A1SDR 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 IMay 12, 1998 · N9598C · Chris A1SDR CA980519004Pushrod · cracked(CAN) AILERON PUSH ROD AT SWAGED END FOUND CRACKED.May 5, 1998 · Swrngn SA226ATSDR 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 27-14-15-400May 1, 1998 · N924CA · Cndair CL6002B19SDR 98ZZZX2189Input Lever · crackedAILERON ACTUATOR INPUT LEVER FOUND CRACKED AT ATTACH BOLT HOLE. LEVER FOUND CRACKED AT ATTACHMENT BOLT HOLE.May 1, 1998 · N122DU · Gulstm G1159SDR CA980504018Turnbuckle · cracked(CAN) ONE INCH CRACK IN TURNBUCKLE BARREL STARTING FROM LT THREAD END. REPLACED.Apr 29, 1998 · Piper J3C65SDR 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 9701Apr 24, 1998 · N791AL · Doug DC862SDR 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 FACILITYApr 20, 1998 · N153UA · Boeing 747123SDR 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.Apr 17, 1998 · Dhav DHC8301SDR 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 Apr 17, 1998 · Dhav DHC8301SDR AU980453Control Cable · frayed(AUS) AILERON/RUDDER BALANCE CABLE FRAYED AT TERMINAL FITTING.Apr 17, 1998 · Piper PA31350SDR UPS98226433Hinge · crackedINSPECTION TYPE-C, RT OUTBD AILERON HINGE IS CRACKED, SECOND FROM INBD HINGE FITTING. REPLACED IAW 65-19275.Apr 15, 1998 · N930UP · Boeing 72722CSDR 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 FRAYIApr 8, 1998 · N62348 · Cessna 172PSDR 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 RApr 7, 1998 · N817CK · Doug DC861SDR UPS98226458Casting · corrodedINSPECTION TYPE-C, RT INBD AILERON TURNAROUND PULLEY CASTING HAS CORROSION ON LUG FOR TURNAROUND PULLEY. CASTING REPLACED IAW SRM 51-30-2.Apr 1, 1998 · N930UP · Boeing 72722CSDR 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.Apr 1, 1998 · N930UP · Boeing 72722CSDR 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 BRAApr 1, 1998 · N9729W · Piper PA28140SDR 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 BRAApr 1, 1998 · N9729W · Piper PA28140SDR 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.Mar 24, 1998 · Cndair CL2156B11415SDR 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 PMar 23, 1998 · N2148B · Piper PA32RT300TSDR 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.Mar 18, 1998 · N924UP · Boeing 72731CSDR 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)Mar 17, 1998 · N609AW · Bag BAE146200A
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