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 O2RR2016FA0000372Rod End · corrodedDURING FLIGHT CONTROL ACTUATION NOTICED THAT RT INBOARD AILERON DIDN`T MOVE. FURTHER INVESTIGATION SHOWED INBD AILERON POWER CONTROL PACKAGE INSTALLATION PISTON ROD END SEPARATED FROM THE PISTON. CORROSION VISIBLE ON ROD END. SEE PHOTOS.Jun 24, 2016 · N199UA · Boeing 747422SDR AALA201605249003Control Servo · defectiveAIRCRAFT WAS GNDED. FLIGHT CREW REPORTED THAT THE LT OTBD AILERON WAS OSCILLATING & FLUTTERING RHYTHMICALLY DURING CRUISE & DECLARED AN EMER AS A PRECAUTIONARY MEASURE WHERE THE ACFT LANDED SAFELY WITHOUT FURTHER INCIDENT & TAXIED TO THE GATE UNDER ITS OWN POMay 21, 2016 · N277AY · Airbus A330323SDR A6WA201643909Aileron · stiffABNORMAL RESISTANCE WITH AILERON CONTROLS. FELT ON BOTH SIDES. GREATER STIFFNESS WHEN TURNING RT.May 19, 2016 · N466AW · Cndair CL6002B19SDR A6WA201643877Warning System · activatedON TAKEOFF AT 80 KNOTS, RECEIVED MASTER WARNING & CONFIG TRIM AURAL MSG. NOTICED AILERON TRIM FULL LT WING DOWN & RUDDER TRIM FULL NOSE RT. FLAPS INDICATE DASHES. RUDDER & AILERON TRIM WILL NOT MOVE. NO OTHER MSGS NOTED. RECEIVED FLAPS DEGRADED MSG AFTER May 11, 2016 · N435AW · Cndair CL6002B19SDR DALA2016051203887Bearing · wornFREEPLAY ON AILERON SECTOR BUSS AT LT WING. FREE PLAY ON AILERON SECTOR BUS WAS CORRECTED BY REPLACING BEARING ON BUS SECTOR IAW CMM 27-10-16. RII COMPLETED BY INSPECTION.May 11, 2016 · N919AT · Boeing 717200SDR 2016F00121Bearing · migratedCOPILOT AILERON CONTROL ROD FOUND DISCONNECTED FROM INTERCONNECT BELLCRANK, DUE TO BEARING MIGRATION FROM ROD END. INSTALLATION DID NOT HAVE LARGE DIAMETER WASHER INSTALLED, WHICH ACTS AS A FAIL-SAFE TO THIS OCCURRENCE. OPPOSITE SIDE WAS INSPECTED & SOME PLAMay 10, 2016 · N217B · Casa C212CDSDR HALA2016050200170Warning Message · false activationAILERON LOCKOUT ON EICAS ON DESCENT AT 240KTS. PERFORMED BITE CHECK ON LT & RT, SAM, NO DEFECT NOTED, SYSTEM OK IAW FIM TASK 27-11, FAULT TREE 804.May 2, 2016 · N581HA · Boeing 76733ASDR 2016FA0000176Bellcrank · wornTHE RT AND LT WING AILERON BELCRANK CLEVIS BOLTS, 2, AN23-9, AND, 2, AN23-10 WERE FOUND TO BE WORN, NOT EXCESSIVE OR UNSAFE, BUT DEFINITELY WORTH REPLACING. 1 OF THE ORIGINAL BOLTS APPEARED TO HAVE A MFG DEFECT. THESE ARE THE CLEVIS BOLTS THAT ATTACH THE AILApr 13, 2016 · N3164T · Cessna 177SDR A6WA201643754Link · crackedNUMBER 2 HYD SYS RT AILERON PCU LINK FOUND TO BE CRACKED OPEN 1/4 INCH ON THE TOP SIDE OF THE LINK, ON AILERON END. LINK ASSEMBLY WAS REPLACED & SISTER LINK REPLACED ALSO, LT SIDE LINKS INSPECTED. ACFT ALREADY WAS OUT OF SERVICE FOR RON MX.Apr 6, 2016 · N463AW · Cndair CL6002B19SDR T6FA20160330001Seal · frozenON CLIMB OUT, WE PASSED THROUGH 2 LAYERS OF CLOUDS. THE FIRST LAYER WAS FROM ABOUT 1500FT TO 5000FT. THE ANTI-ICE WAS TURNED ON BUT WE DID NOT GET AN, ICE DETECT, CAS. THE SECOND LAYER OF CLOUDS WERE FROM ABOUT 9000FT TO 10500FT. THE ANTI-ICE WAS AGAIN ON Mar 28, 2016 · N725BH · Lear 45LEARSDR UIEA2016032800219Bolt · corrodedDURING PFM OTBD AILERON PCA REPLACE FOUND BOTH PISTON ROD BOLTS CORROSION. IAW AMM 27-11-13-002-001 REV 85 STEP F E. REMOVED THE OTBD AILERON PCA PISTON ROD BOLTS AT OTHER SIDE. IAW AMM 27-11-13-402-012 REV 85 STEP G INSTALLED OTBD AILERON PCA PISTON ROD BMar 26, 2016 · N263SG · Boeing 747481SDR SWAA2016032850201Spring · defectiveDIVERSION, AILERON FEEL WAS UNUSUALLY LOW WHEN HAND FLYING. R & R SPRING ON AILERON & FEEL CENTERING UNIT IAW AMM 27-11-81.Mar 25, 2016 · N490WN · Boeing 7377H4SDR T6FA20160322001Seal · lack of lubeAIRCRAFT WAS CLIMBING THROUGH FL380, THE CREW GOT AN AMBER AP AIL MISTRIM CAS MSG. AUTOPILOT WAS DISENGAGED TO FIND THAT THEY HAD NO AILERON CONTROL. CONTROL WHEEL WOULD NOT MOVE FROM THE CTR POSITION. PERFORMED ROLL DISCONNECT, WAS ABLE TO CONTROL ACFT & LMar 20, 2016 · N90XR · Lear 45LEARSDR C77A20160322001Feel Unit · inoperativeDIFFICULT & EXCESSIVE CONTROL WHEEL FORCE REQUIRED WHEN ENTERING & ROLLING OUT OF RT TURN. FOUND BONDING STRAP BROKEN AT MID RT FUSELAGE. R & R BONDING STRAP IAW AMM 20-13-21. BONDING STRAP OK FOR SERVICE. FURTHER TROUBLESHOOTING REQUIRED. WORK ORDER REMAMar 19, 2016 · N616CZ · Emb ERJ170200LRSDR FDEA201603140928Control Unit · lack of lubeSTIFFNESS ON ROLL AXIS ON BOTH CAPTAIN & COPILOT CONTROLS. TROUBLE SHOT FOLLOWING TECH TIPS NR 15-0019 & FIM 27-11. INSPECTED & CLEANED ROD COMING TO LATERAL OVERRIDE QUADRANT & FEEL CENTERING & TRIM MECHANISM, NO DEFECTS FOUND. THEN INSPECTED LT, RT PCUS &Mar 14, 2016 · N915FD · Boeing 757236SDR UVVR2016031400040Cable · corrodedAILERON CABLE CORRODED.Mar 14, 2016 · N918JL · Raythn HAWKER900XPSDR UVVR2016031400039Cable · corrodedAILERON CABLE CORRODED.Mar 14, 2016 · N918JL · Raythn HAWKER900XPSDR UVVR2016031400038Cable · corrodedAILERON CABLE CORRODED.Mar 14, 2016 · N918JL · Raythn HAWKER900XPSDR UVVR2016031400037Cable · corrodedAILERON CABLES CORRODED.Mar 14, 2016 · N918JL · Raythn HAWKER900XPSDR SWIA201641939Servo · malfunctionedCO-PILOT ROLL CMD ADVISORY CONTROLS WERE CONTROLLABLE BUT SLUGGISH, DID NOT DISCONNECT AILERONS. NO UN-COMMANDED MOVEMENT. AP WAS ENGAGED WHEN THE MSG CAME ON. DISCONNECTED AP AND DIVERTED, EMERGENCY DECLARED. REPLACED THE AILERON SERVO, PERFORMED SPIN-DOWMar 7, 2016 · N941SW · Cndair CL6002B19SDR DJSR20160305001Circuit Breaker · trippedAILERON TRIM, FULL RT DEFLECTION, TRIPPED, TRIM ROLL, CIRCUIT BREAKER.Mar 5, 2016 · N481FL · Amd FALCON20SDR CA160221003Control Cable · frayed(CAN) BOTH AILERON DIRECT CABLES FRAYED AT PULLEYS. NORMAL WEAR.Feb 13, 2016 · Cessna 172NSDR CA160213001Bar · failed(CAN) TRAINING FLIGHT, STUDENT IN LH SEAT, INSTRUCTOR IN RH SEAT. THE INSTRUCTOR WAS VERBALLY COACHING THE STUDENT ON APPROACH TO RUNWAY 13 WIND 140/12KTS, 10 DEGREES FLAP. ALTITUDE WAS MAINTAINED AT 300` AGL CLOSE TO THRESHOLD. ENGINE POWER WAS THEN RETARDEDFeb 13, 2016 · Piper PA28140SDR QXEA2016021200141Control Chain · looseTHERE IS A TWO INCH FREE PLAY IN THE CAPTAIN'S SIDE YOKE, AILERON. EVIDENT EVEN WITH THE AUTOPILOT ON. PERFORMED OPS TEST OF AILERONS IAW AMM 27-10-00-710-801. NO DEFECTS. FOUND PILOTS CONTROL CHAIN VERY LOOSE. ADJUSTED CHAIN IAW AMM 27-31-01-820-801. SYSFeb 12, 2016 · N405QX · Bombdr DHC8402SDR UIEA2016020800078Unknown · malfunctionedEICAS MSG, AILERON LOCKOUT ON CLIMB OUT. FOUND CMC 27322 & 27001. REPLACED RT SRM IAW AMM 27-41-02.Feb 8, 2016 · N718BA · Boeing 7474H6SDR QXEA2016011900033Aileron Sys · malfunctionedEXCESSIVE RT WING DOWN AILERON TRIM REQUIRED AS AIRSPEED INCREASES AMOUNT OF RT AILERON ALSO INCREASES. DIVERTED AND ACCOMPLISHED A UNEVENTFUL LANDING. COMPLIED WITH FIM TASK 27-13-00-810-801, VERIFIED AILERON CABLE TENSIONS, VISUALY INSPECTED AILERON TRIM IJan 19, 2016 · N436QX · Bombdr DHC8402SDR AALA20160104003Bearing · bindingAILERONS BINDING DURING APPROACH & IMMEDIATELY AFTER LANDING IN BOTH DIRECTIONS, AFTER APPROX 10 DEGREES OF YOKE DEFLECTION. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMER WAS DECLARED. ACCOMPLISHED CONTROL WHEEL FORCE CHECK. R & R AILERON CENTERING CJan 1, 2016 · N833NN · Boeing 737823SDR YGJA201512290001Control Cable · wornWHILE PERFORMING A DOC 1 INSPECTION, 450 HR INTERVAL, THE RT LOWER INBD AILERON CABLE WAS FOUND WORN AT THE FAIRLEAD. THE WEAR WAS MORE THAN 50 PERCENT WHICH REQUIRES REPLACEMENT.Dec 29, 2015 · N417G · Cessna 510SDR AALA20151127007Mechanism · faultyCREW REPORTS AILERON LOCKOUT AT 300 KNOTS. AN EMER WAS DECLARED & THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. R & R RT AILERON LOCKOUT MECHANISM IAW MM 27-11-44, RIG & OPERATIONAL CHECKED GOOD. ACCOMPLISHED RT AILERON LOCKONov 24, 2015 · N352AA · Boeing 767323SDR AALA20151124005Actuator · faultyCREW REPORTS AILERON LOCKOUT AT 300 KNOTS. AN EMER WAS DECLARED & THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. R & R RT AILERON LOCKOUT ACTUATOR IAW MM 27-11-44, RIG & OPERATIONAL CHECK GOOD. ACCOMPLISHED RT AILERON LOCKOUT Nov 24, 2015 · N352AA · Boeing 767323SDR AALA20151121003Actuator · malfunctionedDURING CLIMB, PASSING APPROX 270 KTS, GOT EICAS MSG AILERON LOCKOUT WITH OVERHEAD LIGHT, ALSO, AIL-LOCK. FLIGHT CONTINUED, DECLARED EMER DURING APPROACH. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. ACFT REMOVED FROM SERVICE. R & R THE LT OTBD AILERON LOCKONov 21, 2015 · N352AA · Boeing 767323SDR COZA20151112063Pcu · leakingUPPER AILERON PCU LEAKING FLUID FROM OUTPUT SHAFT. REPLACED AILERON PCU & NO LEAKS FOUND.Nov 12, 2015 · N737KA · Boeing 7377BXSDR COZA20151112062Pcu · leakingLOWER AILERON PCU LEAKING FLUID FROM OUTPUT SHAFT. REPLACED AILERON PCU & NO LEAKS FOUND.Nov 12, 2015 · N737KA · Boeing 7377BXSDR CA151109002Control Cable · out of adjust(CAN) IT WAS REPORTED ON SEVERAL GCC ACFT, THAT THE NEUTRAL MARKS ON TENSION REGULATORS FOR THE WING AILERON CABLE CIRCUIT, AND THE FUSELAGE ELEVATOR CABLE CIRCUIT WERE OUT-OF-ALIGNMENT. TO DATE, THE CABLE TENSIONS OF THESE TENSION REGULATED CABLE CIRCUITS HNov 9, 2015 · Bombdr BD7001A10SDR RJEF20151105001Computer · malfunctionedDURING CLIMB, THE PILOT REPORTED FLIGHT CONTROL RT & LT AILERON FAULT, FLIGHT CONTROL ALTN LAW & HENCE THE ACFT WAS RETURNED, LANDING WITH NO INCIDENTS. ONCE ON GND THE ACFT, BOTH ELAC 1 & ELAC 2 WERE RESET IAW TSM 27-93-00-810-949-A. PERFORMED OPERATIONAL TNov 5, 2015 · N492TA · Airbus A320233SDR CA151106004Actuator · malfunctioned(CAN) A MAINTENANCE CHECK OF THE AILERON DISCONNECT SYSTEM REVEALED THAT THE AUTOPILOT ROLL SERVO CLUTCH WAS PERMANENTLY ENGAGED. THE ROLL ACTUATOR WAS REPLACED AND AILERON CONTROL CABLES WERE RIGGED BETWEEN AILERON SPLITTER QUADRANT AND AILERON TERMINAL QUADRNov 2, 2015 · Bombdr DHC8400SDR CA151102015Aileron · mismanufactured(CAN) PRODUCTION HAS REPORTED THAT THE HUB, FORK, AILERON OUTER WING, HAS BEEN MFG INCORRECTLY. IT HAS BEEN FOUND THAT HUBS WERE MISSING THE .03" X 45 CHAMFER AROUND THE .2495-.2505" DIAMETER HOLE. THE SHARP EDGE IS BROKEN, 0.005" TO 0.010", BUT THE CHAMFERNov 2, 2015 · Dhav DHC6*SDR CALA2015103000887Pcu · unserviceableAIR RETURN DUE TO STIFF AILERON MOVEMENT. REPLACED CAM FOLLOWER BEARING IAW MM 27-11-81-400-802 UP TO STEP C 6. REPLACED AILERON UPPER PCU IAW AMM 27-11-71. OPERATIONS NORMAL.Oct 30, 2015 · N18220 · Boeing 737824SDR 7GMB20151019005Actuator · failedTHE REPAIRED AILERON PCA WAS INSTALLED ON THE LT SIDE, BUT IT WOULDN'T KEEP THE LT AILERON NEUTRAL WHEN HYD POWER WAS REMOVED.Oct 15, 2015 · N286SJ · Emb EMB145XRSDR 7GMB20151019004Actuator · failedTHE REPAIRED AILERON PCA WAS INSTALLED ON THE LT SIDE, BUT IT WOULDN'T KEEP THE LEFT AILERON NEUTRAL WHEN HYD PRESS WAS REMOVED.Oct 15, 2015 · N286SJ · Emb EMB145XRSDR 7GMB20151019003Actuator · failedTHE REPAIR AILERON PCA WAS INSTALLED ON THE LT SIDE, BUT IT WOULDN'T KEEP LT AILERON NEUTRAL WHEN HYD PRESS IS REMOVED.Oct 15, 2015 · N286SJ · Emb EMB145XRSDR 7GMB20151019002Actuator · failedTHE REPAIRED AILERON PCA WAS INSTALLED ON THE LT SIDE, BUT WOULDN'T KEEP LT AILERON NEUTRAL WHEN HYD POWER WAS REMOVED.Oct 15, 2015 · N286SJ · Emb EMB145XRSDR 7GMB20151019001Actuator · failedDURING SCHEDULED INSPECTION, AILERON POWER CONTROL ACTUATOR PCA, FAILED AILERON ACTUATOR DAMPING COMPONENTS & MONITORING DEVICE FUNCTIONAL CHECK ON THE LT SIDE. REPLACED LT AILERON PCA, BUT IT WOULD NOT KEEP AILERON NEUTRAL WHEN HYD POWER WAS REMOVED. TROUBLOct 15, 2015 · N286SJ · Emb EMB145XRSDR A6WA201543078Link · wornFLIGHT 9368, AFTER TAKEOFF, ACCELERATED TO 200 KTS, AIRPLANE HAD A TENDENCY TO BANK RIGHT. ACCELERATED TO 250 KTS, ACFT TRIM PAST THE FIRST TRIM MARK ON AILERON TRIM INDICATOR WITH ZERO AILERON TRIM & NO PILOT INPUT, THE ACFT STARTED A CONTINUOUS ROLL TO THESep 21, 2015 · N466AW · Cndair CL6002B19SDR BGSR20150917004Control Cable · frayedDURING INSPECTION, FOUND LT AILERON CONTROL CABLE FRAYED AT PHENOLIC BLOCK. REPLACED WITH NEW CABLE.Sep 9, 2015 · N459J · Cessna 172SSDR A6WA201543029Aileron · tightAILERON CONTROL FEELS TIGHTER THAN USUAL ON FLIGHT CONTROLS. CHECK IN BOTH DIRECTIONS, FEELS EVEN TIGHTER TO THE RT, HYD PUMPS ON & OFF.Sep 3, 2015 · N462AW · Cndair CL6002B19SDR HALA2015090300183Warning Message · false activationRUDDER RATIO EICAS MESSAGE WITH RUDDER RATIO LIGHT ILLUMINATED. BOTH SAM'S SET "SAM" FAULT BALL IAW FIM 27-21, FAULT TREE 804, TEST IS GOOD FOR BOTH. BOTH RRCM AFTER FLIGHT CONTROL ELEC CB, ALL GOOD FOR RUD RATIO IAW FIM 27-21. OK FOR SERVICE.Sep 3, 2015 · N582HA · Boeing 76733ASDR CA150827003Actuator · malfunctioned(CAN) THE CREW REPORTED THAT THE ROLL CONTROL FEELS HEAVY WHILE PERFORMING CONTROL CHECKS. HYDRAULICS ON OR OFF. MAINTENANCE FOUND THE ROLL ACTUATOR NOT DISENGAGING. ROLL ACTUATOR REPLACED.Aug 24, 2015 · Bombdr DHC8400SDR CA150826007Actuator · malfunctioned(CAN) AFTER TAKEOFF PILOTS NOTICED AN UNUSUAL ROLL. OBSERVED ON THE PFCS THAT THE LH OUTBOARD SPOILER WAS DEPLOYED. BEFORE THEY COULD ACTION THE CHECKLIST, IT HAD RETRACTED. A/C RETURNED TO BASE. .T/S CARRIED OUT. WITH ROLL DISCONNECT PULLED & SYS 2 HYD ON, L/Jul 31, 2015 · Dhav DHC8311SDR SWIA201541379Aileron Sys · bindingAFTER DISCONNECTING AUTOPILOT, COULD NOT MOVE AILERONS. AFTER APPLYING SIGNIFICANT FORCE, AILERONS MOVED FREELY. LANDED WITH NO FURTHER PROBLEMS.Jul 28, 2015 · N967SW · Cndair CL6002B19
Back to JASC 2710