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 RRXA98069Controls · malfunctionedIN FLIGHT THERE WAS A LARGE DEAD SPOT IN THE AILERONS IN THE CENTER/NEUTRAL POSITION. IN FLIGHT THE AIRPLANE ROLLS LEFT AND RIGHT. TO STOP OR CONTROL THE ROLL YOU HAVE TO DO A DUTCH ROLL TYPE OF MANUVER TO CONTROL THE ROLL. INSPECTED CONTROL SURFACES, CABLEMar 13, 1998 · N8084U · Doug DC871FSDR 99ZZZM510Control Cable · corrodedLEFT CLAD INTERCONNECT CABLE FOR AILERONS SHOWS EVIDENCE OF CORROSION AT DIFFERENTIAL SECTOR BETWEEN RIBS 14/15. REMOVED AND REPLACED LEFT CLAD INTERCONNECT CABLE (AILERON) IAW BAE MM. GENERATED W/C TO PERFORM AILERON FUNCTIONAL CHECKS AND PRIORITY 2 WC TO RMar 10, 1998 · N609AW · Bag BAE146200ASDR 99ZZZM508Control Cable · corrodedRIGHT WING AILERON INTERCONNECT CABLES AT WING ROOT PULLEY CORRODED. REMOVED AND REPLACED FUSELAGE INTERCONNECT CABLES (AILERON) IAW BAE MM. GENERATED WC TO PERFORM AILERON FUNCTIONAL CHECK AND PRI 2 WC TO RE-CHECK TENSION AT 4000 FLT INTERVAL. (M)Mar 10, 1998 · N609AW · Bag BAE146200ASDR 99ZZZM506Cable Guard · seizedRIGHT WING ROOT, OUTBOARD CABLE GAURD SEIZED AND BOTH PULLEYS WORN FOR CENTER SECTION AILERON INTERCONNECT CABLES. REMOVED AND REPLACED PULLEYS EXTRACTED SEIZED GUARD AND REPLACED WITH NEW GUARD, RIGHT WING ROOT. (M)Mar 10, 1998 · N609AW · Bag BAE146200ASDR MZZA98101Control Cable · misinstalledKUL - RT AILERON BODY CABLE SYSTEM, AFT QUADRANT ABOVE RT WHEEL WELL FOUND TO HAVE CABLES INSTALLED ON WRONG GROOVES IAW MM 27-61-11, PARA 71 PLS NOTE THAT RETAINERS STILL HAD ORIGINAL BOEING TAMPER PROOF SEALANT. CABLES SWAPPED IN GROOVES IAW MM 27-62-11, BOMar 2, 1998 · N623DH · Boeing 727264SDR ARWA980207Bolt · shearedUNABLE TO MOVE AILERONS IN MANUAL TO RIGHT. UNABLE TO MOVE RIGHT RUDDER PEDAL UPON FURTHER INSPECTION FOUND SHEARED BOLT AT LT MANUAL REVERSION MECHANISM LINKAGE JAMMING LINKAGE. REMOVED AND REPLACED BOLT, AILERON REVERSION SYSTEM OPS. CHECKED NORMAL IN MANFeb 24, 1998 · N1804 · Doug DC862SDR MZZA98102Drum · crackedKUL - LOST MOTION DEVICE UPPR CABLE DRUM FOUND CRACKED AT CABLE RETAINER SLOT. DRUM REPLACED IN LOST MOTION DEVICE IAW OHM 27-10-03. (M)Feb 20, 1998 · N623DH · Boeing 727264SDR COMA9960081Link · wornRIGHT AILERON FAILS BACKLASH CHECK. REPLACED BOTH PCU LINKS.Feb 19, 1998 · N958CA · Cndair CL6002B19SDR CA980309011Actuator · malfunctioned(CAN) SHORTLY AFTER TAKEOFF CLIMBING THROUGH 3500 FEET IN LEFT TURN RUDDER RATIO AND AILERON LOCK OUT MESSAGE APPEARED ON ENGINE INDICATION AND CREW ALERTING SYSTEM AND OVERHEAD PANEL. REPLACED STAB TRIM AND AILERON LOCKOUT MODULE.Feb 18, 1998 · Boeing 767233SDR AU980417Control Arm · misrigged(AUS) AILERON CONTROL SYSTEM RIGGED INCORRECTLY. THE AILERON BELLCRANKS WERE NOT HITTING THE STOPS AND THE AILERONS WERE SHORT OF TRAVEL BY FIVE DEGREES. PERSONNEL/MAINTENANCE ERROR.Feb 18, 1998 · Beech 58SDR AU980174Aileron · misrigged(AUS) AILERON CONTROL SYSTEM INCORRECTLY RIGGED.Feb 18, 1998 · Beech 58SDR DLL14980391Actuator · brokenHYD SYS-A FLUID LEVEL DROPPED TO 1/4 DURING CRUISE FLT. UNLATCHED ENG PUMP S/O SWITCH FOR HYD SYS-A AND FLUID LOSS STOPPED. FOUND LT OUTBD ACTUATOR OF INBD AILERON BROKEN AND HYD LINE AT ACT BROKEN. REPLACED SAME PER MM, ALL CKS OK. CKD A-PUMP HYD FILTERS Feb 15, 1998 · N740DA · Lkheed 1011385115SDR MZZA98076Pcu Cover · crackedKUL - Q-CHECK - DURING REASSEMBLY OF AILERON PCU LINKAGE ASSEMBLY, LOWER COVER WAS FOUND CRACKED AT LOWER RIG PIN HOLE. REPAIR TO LOWER COVER CUT-OUT IAW ECRA 5270C072. PLEASE REFER TO ROUTINE CARD NR 552 FOR REASSEMBLY OF PCU LINKAGES. (X)Feb 9, 1998 · N622DH · Boeing 727264SDR MZZA98075Bracket · damagedKUL - Q-CHECK - DURING REPLACEMENT OF RT AILERON BUS CABLE, FOUND RT AILERON BUS CABLE TURNAROUND PULLEY BRACKET DAMAGED. PLATES FABRICATED AND INSTALLED IAW BOEING DRAWING 69-25882. REFER HNRC 869821 FOR CABLE REPLACEMENT. (X)Feb 9, 1998 · N622DH · Boeing 727264SDR MALA975949Centering Mech · malfunctionedWHILE IN FLIGHT, THE AILERONS WOULD BIND UP AND RELEASE WHEN TURNED TO THE LEFT. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE LEFT AILERON CENTERING MECHANISM ASSEMBLY. ALL CHECKS GOOD.Feb 2, 1998 · N46XJ · Saab SF340ASDR UPS98225650Casting · corrodedINSPECTION TYPE-D, LT I/B AILERON TURNAROUND FITTING HAS CORROSION AROUND LOWER PULLEY MOUNT HOLE. CASTING REPLACED IAW SRM 51-10-1 AND MM 20-80-1.Jan 29, 1998 · N943UP · Boeing 72722CSDR UPS98225631Fitting · corrodedINSPECTION TYPE-D, RT I/B AILERON TURNAROUND FITTING HAS CORROSION AROUND LOWER PULLEY MOUNT HOLE. RT I/B AILERON TURNAROUND FITTING REPLACED IAW SRM 51-10-1 ADN MM20 -80-1.Jan 26, 1998 · N943UP · Boeing 72722CSDR 98ZZZX1698Control Rod · rustedDURING ANNUAL INSPECTION NOTED AILERON ROD RUSTY. UPON FURTHER INSPECTION, FOUND ROD RUSTED TO THE EXTENT IT COULD BE SEPARATED IN TWO WITH LIGHT HAND PRESSURE. SUBMITTER RECOMMENDED INSPECTING AT EACH ANNUAL.Jan 15, 1998 · N261CB · Mooney M20KSDR CALA9800018Control Module · leakingTHE A-SYSTEM HYDRAULIC OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF WHILE CLIMBING THROUGH 6000 FEET. A MINUTE LATER, THE A-HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. THE HYDRAULIC FAILURE CHECKLIST WAS PERFORMED, FUEL WAS DUMPED, AND THE AIRCRAFT WAS RETURNED TO IJan 12, 1998 · N32725 · Boeing 727224SDR 98ZZZX311Support Assy · crackedINSPECTION FOUND THE AILERON CONTROL REVERSION ASSEMBLY HAS A CRACK ON BOTH SIDES OF THE SUPPORT ASSEMBLY.Jan 9, 1998 · Doug DC8*SDR 98ZZZX287Support Assy · crackedTHE AILERON CONTROL REVERSION ASSEMBLY HAS A CRACK ON BOTH SIDES OF THE SUPPORT ASSEMBLIES.Jan 9, 1998 · Doug DC8*SDR 98ZZZX705Control Cable · wornRIGHT WING AILERON CABLE (OUTBOARD, AFT) WORN THROUGH CLAD. FOUND DURING OPERATION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE CHANGE, ALL PRIMARY CONTROL SURFACES.Jan 5, 1998 · N650Z · Cessna 650SDR 98ZZZX704Control Cable · frayedRIGHT WING AILERON CABLE, (INBOARD, FORWARD) HAS BROKEN WIRES IN SEVERAL STRANDS AT CABLE PULLEYS WS 88.00. FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE HCANGE, ALL PRIMARY CONTROL SJan 5, 1998 · N650Z · Cessna 650SDR 98ZZZX703Control Cable · frayedRIGHT WING AILERON CABLE (INBOARD FORWARD), HAS BROKEN WIRES IN ONE STRAND AT CABLE PULLEYS WS 88.00. FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE CHANGE, ALL PRIMARY CONTROL SURFACEJan 5, 1998 · N175J · Cessna 650SDR 98ZZZX702Control Cable · frayedRIGHT WING AILERON CABLE, (OUTBOARD, FORWARD), HAS BROKEN WIRES IN STRAND AT CABLE PULLEY WS 175.63 (PLUS OR MINUS). FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE CHANGE, ALL PRIMARYJan 5, 1998 · N175J · Cessna 650SDR 98ZZZX701Control Cable · frayedRIGHT WING AILERON CABLE, (OUTBOARD, AFT) HAS BROKEN WIRES IN STRAND AT CABLE PULLEY WS 175.63 (PLUS OR MINUS). FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE CHANGE, ALL PRIMARY CONTRJan 5, 1998 · N175J · Cessna 650SDR 98ZZZX700Control Cable · frayedRIGHT AILERON CABLE, (OUTBOARD FORWARD) AT CABLE PULLEYS WS 175.63 (PLUS OR MINUS) HAS BROKEN WIRES IN STRAND. FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HR CABLE CHANGE, ALL PRIMARY CONTROL Jan 5, 1998 · N150F · Cessna 650SDR 98ZZZX699Control Cable · frayedRIGHT AILERON CABLE (INBOARD FOWARD) AT CABLE PULLEYS WS 88.00. BROKEN WIRES IN THREE STRANDS. FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800 HOUR CABLE CHANGE, ALL PRIMARY SURFACES.Jan 5, 1998 · N150F · Cessna 650SDR 98ZZZX698Control Cable · frayedRIGHT WING AILERON CABLE, OUTBOARD, AFT HAS BROKEN WIRES IN STRAND AT CABLE PULLEY WS 175.63 (PLUS OR MINUS). FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE CHANGE, ALL PRIMARY CONTROLJan 5, 1998 · N150F · Cessna 650SDR 98ZZZX2768Control Cable · corrodedATW - RIGHT CLAD COVERED AILERON INTERCONNECT CABLE IS CORRODED AT OUTBOARD PULLEY. REMOVED AND REPLACED RIGHT OUTBOARD AILERON INTERCONNECT CABLE AND ADJUSTED IAW MM 27-11-00. W/C 5023 GENERATED FOR FUNCTIONAL CHECK.Jan 2, 1998 · N156TR · Bag BAE146200ASDR 98ZZZX2761Cable · corrodedATW - LEFT WING CLAD AILERON INTERCONNECT CABLE IS CORRODED AND NEEDS CHANGING. REMOVED AND REPLACED LT OUTBOARD AILERON INTERCONNECT CABLE AND ADJUSTED IAW MM 27-11-00. W/C 5023 GENERATED FOR FUNCTIONAL CHECK.Jan 2, 1998 · N156TR · Bag BAE146200ASDR 98ZZZX2733Control Cable · corrodedAILERON INTERCONNECT CABLES ARE CORRODED AT LR WING ROOT PULLEYS. REMOVED AND REPLACED BOTH CENTER SECTIONS OF THE AILERON INTERCONNECT CABLE CIRCUIT AND ADJUSTED IAW MM 27-11-00. W/C 5023 GENERATED FOR FUNCTIONAL CHECK.Jan 2, 1998 · N156TR · Bag BAE146200ASDR AU980026Control Cable · frayed(AUS) LH UPPER AILERON CABLE FRAYED IN AREA WHERE THE CABLE PASSES THROUGH THE INBOARD ENGINE NACELLEJan 1, 1998 · Emb EMB120SDR CA980113015Control Cable · chafed(CAN) AILERON BALANCE CABLE CHAFING ON FLOOR SKIN AND HYD LINE. CABLE REPLACED, HYL LINE RECLAMPED AND FLOOR SKIN MOVED.Dec 22, 1997 · Piper PA23250SDR 98ZZZX113Bolt · wrong partDURING A CUSTOMER REQUESTED AILERON RIGGING CHECK, DISCOVERED THE AFT BOLTS ON BOTH AILERON BELLCRANKS WERE CHAFING ON THE AILERON CONTROL ROD AS AILERONS WERE MOVED. ALL 4 BOLTS CONNECTING THE AILERON CABLES TO THE BELLCRANKS WERE AN23-12. AN EXAMINATION OFDec 19, 1997 · N4511F · Piper PA28181SDR 98ZZZX168Control Cable · misinstalledDURING 100-HOUR INSPECTION, FOUND LEFT AILERON DIRECT CABLE TURNBUCKLE NOT SAFETIED. THE TURNBUCKLE IS NOT VISIBLE WITH THE HEADLINER INSTALLED. IT WOULD HAVE BEEN UNABLE TO DETECT HAD THE HEADLINER NOT BEEN REMOVED TO REPLACE DAMAGED AILERON CABLE. RECOMMEDec 17, 1997 · N361ES · Cessna 172RSDR AU971565Control Cable · broken(AUS) DURING TAXI AFTER LANDING, THE AILERON CONTROLS ROLLED LEFT AND DIDN'T ROLL BACK WITH RUDDER INPUT. AILERONS STILL HAD FULL AND FREE MOVEMENT BUT WITH A BIAS OF SLIGHT SPRING PRESSURE TO THE LEFT CONTROL DOWN. INVESTIGATION FOUND THE LH AILERON/RUDDER INDec 15, 1997 · Piper PA31350SDR 98ZZZX167Control Cable · frayedWHILE PERFORMING A 100-HOUR INSPECTION, FOUND THE RIGHT HAND AILERON CABLE FRAYED/TANGLED AS IF SOMETHING MIGHT HAVE GOT BETWEEN IT AND THE PULLEY IN THE SAME AREA AS THE PULLEY. ALSO, FOUND A ROUND FILE APPROXIMATELY .1875 INCH DIAMETER. IT IS UNCLEAR IF THDec 12, 1997 · N361ES · Cessna 172RSDR EIAA970210Control Cable · out of adjJFK - RIGHT AILERON REQUIRES EXTRA PRESSURE FOR RIGHT TURNS. RIGGED AILERON LOST MOTION PER MM 27-11-00, OPS CHECK OK. (M)Dec 10, 1997 · N471EV · Boeing 747273CSDR QXEA9700892Gap Seals · wornDURING FLIGHT AIRCRAFT REQUIRED SOME AILERON AND RUDDER TRIM TO FLY COORDINATED. THIS CAUSED THE AIRCRAFT TO BE HARD TO TURN LEFT, WORSE AT HIGHER SPEEDS. CHECKED AILERON RIGGING AND TRAVEL CHECKED GOOD. COMPLIED WITH EA 9-57-320, INSTALLED AILERON GAP SEALDec 5, 1997 · N811PH · Dhav DHC8102SDR M8XA328MXC1Control Cable · frayedCOS - DURING THE COURSE OF THE C-CHECK INSPECTION, MAINTENANCE DISCOVERED THAT BOTH AUTO-PILOT AILERON AND ELEVATOR CONTROL CABLES WERE FRAYED. MAINTENANCE REPLACED BOTH CABLES IAW AMM 27-11-03. OPERATIONAL CHECK SATISFACTORY. (M)Dec 5, 1997 · N328MX · Dorner DO328100SDR 98ZZZM112Hyd Line · failedON CAC - FLT 148 - MGGT-KMIA - UTILITY HYD FAILURE OCCURRED AT 1802Z. PERFORMED A/E HYD SYSTEM LEAK ON LOSS CHECKLIST. AFTER CLEARING RUNWAY BRAKE SYSTEM PRESS DECREASED. BRAKE BOTTLE WAS USED. RT MAIN ALSO FAILED TO EXTEND MANUALLY. EXTENDED RIGHT MAIN WDec 2, 1997 · N707HE · Boeing 707330CSDR HNAA9791798Bushings · failedFLT EN69 - BWI-ORF - EXPERIENCED A ROLL CONTROL DISCONNECT ON LANDING, AFTER TOUCHDOWN AT ORF. REMOVED AND REPLACED THE ROLL CONTROL DISCONNECT CLUTCH BUSHINGS PER FCD8-27-291. ALSO, REMOVED AND REPLACED THE CLUTCH SPRING. (M)Dec 1, 1997 · N917HA · Dhav DHC8102SDR 98ZZZM178Clutch Spring · failedFLT EN69 - BWI-ORF - EXPERIENCED A ROLL CONTROL DISCONNECT ON LANDING, AFTER TOUCHDOWN AT ORF. REMOVED AND REPLACED THE ROLL CONTROL DISCONNECT CLUTCH BUSHINGS PER FCD8-27-291. ALSO, REMOVED AND REPLACED THE CLUTCH SPRING. (M)Dec 1, 1997 · N917HA · Dhav DHC8102SDR GLBA97214Bolt · looseLEFT WING VIBRATES AND SHAKES VISIBLY IN FLIGHT. LEFT AILERON TO BELLCRANK BOLT LOOSE. (M)Nov 30, 1997 · N267UE · Emb EMB120RTSDR HNAA9790697Clutch Plate · failedFLT 3315 - PIT-CHO - ON LANDING, IN TURBULENCE, AILERON CHANNEL DISCONNECTED AND RECONNECTED WITH NORMAL YOKE MOVEMENT. NO ASSOCIATED CAUTION LIGHTS ILLUMINATED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE LEVER AND CLUTCH PLATE, SPROCKET ANDNov 27, 1997 · N906HA · Dhav DHC8102SDR 98ZZZM180Spring Pin · failedFLT 3315 - PIT-CHO - ON LANDING, IN TURBULENCE, AILERON CHANNEL DISCONNECTED AND RECONNECTED WITH NORMAL YOKE MOVEMENT. NO ASSOCIATED CAUTION LIGHTS ILLUMINATED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE LEVER AND CLUTCH PLATE, SPROCKET ANDNov 27, 1997 · N906HA · Dhav DHC8102SDR 98ZZZM179Sprocket · failedFLT 3315 - PIT-CHO - ON LANDING, IN TURBULENCE, AILERON CHANNEL DISCONNECTED AND RECONNECTED WITH NORMAL YOKE MOVEMENT. NO ASSOCIATED CAUTION LIGHTS ILLUMINATED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE LEVER AND CLUTCH PLATE, SPROCKET ANDNov 27, 1997 · N906HA · Dhav DHC8102SDR 97ZZZX5211Control Link · brokenIN-FLIGHT FAILURE. OWNER-PILOT NOTICED SLOPPY AILERON RESPONSE, SAW RT AILERON 'VIBRATING', NOT RESPONDING TO CONTROL INPUT. RIGHT CONTROL LINK ROD ASSEMBLY LOCATED AT BELLCRANK BELOW CABIN FLOOR HAD BROKEN ALONG FACTORY WELD THEN THROUGH THE TUBING WALL. TNov 19, 1997 · N201ZU · Mooney M20JSDR 9721639912Control System · malfunctionedDURING DESCENT, THE FLIGHT CREW DISCOVERED THAT THE AILERON INPUT WAS STUCK TO THE RIGHT WHEN TURNING FROM DOWN WIND TO BASE-LEG. THE CREW SUCCESS FULLY GAINED FULL FLIGHT CONTROL FUNCTIONS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE FLIGHT CONTRONov 17, 1997 · N962N · Doug DC931
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