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 2019FA0000033Control Cable · brokenDURING ANNUAL INSPECTION, FOUND RIGHT AILERON CABLE BROKEN AT SWAGED END BETWEEN SAFETY WIRE HOLE AND THREADED END. SAFETY WIRE WAS HOLDING IT TOGETHER.SDR DALA2018120306977Servo · flutterSHIP 3355 - DIV - DIVERTED TO NRT DUE TO REGULAR AND RHYTHMIC VIBRATION NOTED. LEFT OUTBOARD AILERON FLUTTER SHOWS CONSTANT MOVEMENT, MOST EVIDENT ABOVE 250 KIAS. CORRECTIVE ACTION: MAINTENANCE REPLACED BOTH OUTBOARD AILERON SERVOS AND THE #1 FLIGHT CONTROL SESDR CNMA201811210001Actuator · leakingCENTER HYDRAULIC QUANTITY EICAS IN FLIGHT DROPPED TO 0.33 WITH CENTER SYSTEM TURNED OFF . CORRECTIVE ACTION: FOUND RH INBOARD ELEVATOR PCA LEAKING. REMOVED AND REPLACED RH INBOARD ELEVATOR PCA IAW B767 AMM 27-31-05. OPS AND LEAK CHECK GOOD AT THIS TIME.SDR HALA2018111200578Warning Message · false activationETOPS SIGNIFICANT SYSTEM - AFTER LANDING WE HAD A STAB TRIM EICAS MSG.// PERFORMED TASKS PER FIM 27-48 FAULT TREE 806 NO FAULTS FOUND. OK FOR SERVICE.SDR 2018FA0000470Control Cable · corrodedDURING CRUSE ALTITUDE 7500FT, THERE WAS A LOSS OF AILERON CONTROL. THE AIRCRAFT DRIFTED TO THE RIGHT AND WAS CORRECTED BY ROLLING LEFT. THE PILOT THEN FELT SOMETHING BREAK AND THE RIGHT WING DROPPED. THE PILOT TURNED THE AILERON CONTROL YOKE TO THE LEFT, UNTISDR AALA201810249014Computer · faultedAN EMERGENCY WAS DECLARED. ECAM FOR A FLIGHT CONTROL ELAC 2 PITCH FAULT. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED TSM 27-90-00-810-803-A. REPLACED ELAC IAW AMM 27-93-34. OPS CHECKED GOOD. ACCOMPLISHED SUCCESSFUL LAND CAT 3 CAPABILITY TEST IAW JOB CARD 26T0SDR 2020FA0000053Control Cable · chafedRT WING, AILERON CONTROL CABLES, TWO EACH, CHAFED AT RUB-BLOCK INBOARD OF THE AUTOPILOT SERVO. CABLE STRANDS ARE NOT FRAYED, CANNOT DETECT CHAFE DAMAGE WITH RUNNING A RAG OVER THE DAMAGE. BUT STRANDS ARE DEFINITELY CHAFED BEYOND AN AMOUNT TO CAUSE CONCERN. SDR 9WGA20181012101Unknown · malfunctionedAIRCRAFT ROLLS LEFT WITH RUDDER & AILERON TRIM AT ZERO POSITION, ROLL RATE APPROX. 3 DEGREE/SEC.SDR CNMA2018101090001Pca · failedEXCESSIVE RIGHT RUDDER TRIM (5 UNITS) REQ'D TO MAINTAIN LEVEL YOKE DURING CLIMB OR ON APPROACH WITH FLAPS OUT. ON GROUND DURING INITIAL FLAP EXTENSION, R INBD AILERON WAS NOTED SIGNIFICANTLY LOWER THAN L INBD AILERON, BUT FLT CONTROL CHECK FELT & LOOKED OK. ISDR SIMA201809177001Control Panel · failedROLL TRIM ACTUATION JAMMED BUTTON DECLARED EMERGENCY. REMOVED AND REPLACED ROLL TRIM /BACK UP PITCH TRIM/YAW TRIM CTRL PANEL IAW MM 20-13-10 OPS/FUN CHECK OK IAW MM 27-14-00 27-40-00+27-24-00 RESPECTIVELY.SDR 2018FA0000353Control Cable · wornPREMATURE WEAR IN AILERON CONTROL CABLES. WEAR HAS OCCURRED IN TWO SEPARATE PLACES, BOTH DIRECT CABLES (P/N:0510105-260) AND THE CROSSOVER CABLE (P/N: 0510105-264) WORE AT THE PULLEYS IN THE CABIN OVERHEAD AND DIRECT CABLES P/N: 0510105-262 AND CROSSOVER CABLESDR FDEA2018082752185Pca · bindingAFTER PUSH BACK, DURING THE BEFORE TAKEOFF CHECKLIST, FIRST OFFICER NOTICED A BINDING IN THE LEFT AILERON DURING CHECK. RETURNED TO THE GATE. REMOVED AND REPLACED THE RT OTBD AILERON PCA IAW AMM 27-11-49, PERFORMED A LEAK AND OPS CHECK, CHECKED GOOD. ACSDR ASAA2018072325478Sensor · failedAC FAILS 30 DAY IN-USE CHECK DUE TO AILERON POS SENSOR FAILING TEST. MSG 22-11146 AND MSG 22-11145. GROUNDED - YES. REMOVED AND REPLACED AILERON POS SENSOR REF AMM 22-11-29. OPS NORMAL.SDR 2018FA0000212Control Cable · wornDURING PRE-FLIGHT INSPECTION, A ROUGHNESS WAS HEARD IN THE AILERON FLIGHT CONTROL CABLES. ON FURTHER INSPECTION THE AILERON CARRY THROUGH CABLE WAS FOUND EXCESSIVELY WORN WITH MULTIPLE BROKEN STRANDS AT THE FAIRLEAD RUB STRIP IN THE LEFT WING. THE REGION WHERESDR HALA2018062100294Aileron Sys · stickingAILERON TRIM WAS STICKING MULTIPLE TIMES WHEN MOVED LEFT WING DOWN. PERFORMED AN OPS CHECK OF AILERON TRIM. NO FAULTS NOTED. OK FOR SERVICE.SDR HALA2018062000291Control Cable · out of adjustROLL AXIS ON CONTROL YOKE HAS MUCH MORE THAN USUAL PLAY, CREATING A NULL CONTROL ZONE, ENOUGH TO MAKE THE AUTO PILOT DRIFT. AUTO PILOT DID NOT DISCONNECT. ACCOMPLISHED ADJUSTMENT OF THE AILERON BUSS CABLE SYSTEM IAW AMM 27-10-00. TEST FLIGHT, OPS CHECKED GOOSDR RAIA2018053180001Aileron Sys · malfunctionedAILERONS WILL NOT DEFLECT FULL TRAVEL. ONLY ABOUT 50%.LOCKED UP DURING CONTROL CHECK. PERFORMED F.I.M. TASK 27-12-00-810-8003-A. SYSTEM OPERATING NORMALLY. NO DEFECTS NOTED AND CYCLED AILERONS REPEATEDLY WITHOUT ISSUE.SDR 2018FA0000165Push-Pull Rod · corrodedAILERON AND SPOILER PUSH - PULL TUBES ARE ENCASED IN THE FIBERGLASS WING. THE WING STRUCTURE IS UNABLE TO BREATH, THE CORROSION IS BUILDING ON THE PUSH - PULL TUBES AND BELL CRANK BRACKETS WITH PITTING FORMING ON THE STRUCTURE. BOTH WINGS WERE EXAMINED USING ASDR SIMA20180504006Fitting · damagedLT AILERON DAMPER FITTING GOUGED INSIDE FITTING. REMOVED AND INSTALLED LT AILERON DAMPER FITTING IAW EO EM-27MR-112 REPAIR.SDR CALA2018042301187Control Cable · out of limitsFLIGHT CONTROLS BINDING, AILERONS COULD NOT MOVE PAST 11:00 O`CLOCK POSITION. HAPPENED AT 500AGL, FOUND THE FIRST OFFICER`S CONTROL YOKE CATCHES AT THE 11 OCLOCK POSITION WHEN MOVED FROM THE CENTER POSITION. COMPLETED A DETAILED INSPECTION IAW FIM. FOUND TSDR CA180404016Control Cable · chafed(CAN) DURING THE EMMA 2 INSPECTION IT WAS DISCOVERED THAT THE LEFT HAND AILERON CABLE WAS CHAFING ON THE STEERING CABLE AT THE BASE OF THE YOKE. THE CHAFING OCCURRED AS THE YOKE WAS PULLED BACK PAST LEVEL FLIGHT. CABLES WERE INSPECTED AND FOUND TO BE UNDAMASDR IPXA2018040428188Actuator · malfunctionedAIR TURN BACK AFTER TAKEOFF WHEN FLAPS WERE RETRACTED LEVEL 2 AILERON DEFLECT DISAGREE. QRH PROCEDURE DID NOT FIX THE ISSUE. REMOVED THE LT INBD AILERON DEFLECTION CONTROL ACTUATOR IAW MM 27-16-01, OPS CHECKED GOOD.SDR 2018FA0000122Turnbuckle · separatedAIRCRAFT LOST AILERON CONTROL IN FLIGHT, DECLARED EMERGENCY AND LANDED. AFTER SHUTDOWN THE SEPARATED CABLE FOR LEFT AILERON FROM TURNBUCKLE SWEDGED FITTING UNDER RIGHT SIDE OF COCKPIT PANEL WAS DISCOVERED. AIRCRAFT GROUNDED.SDR EPUA20180328001Cable Assy · frayedDURING SCHEDULED INSPECTION, THE RIGHT AILERON CABLE WAS SEVERELY FRAYED. THE CABLE WAS RUBBING ON THE FLOOR PANEL AT BS 180.SDR QXEA2018022800076Control Cable · out of rigAIRCRAFT REQUIRES SIGNIFICANT (EXCESSIVE) RIGHT AILERON TRIM (ALMOST 1 FULL TICK-MARK) AND RIGHT RUDDER TRIM TO FLY WINGS LEVEL TRIMMED ON CLIMB OUT AND CRUISE. REQUIRES 15 DEGREES RIGHT YOKE CONTROL TO LIFT OFF LEVEL ON TAKE OFF. ALL TRIM MUST BE REMOVED SSDR 2018FA0000063Control Cable · frayedDURING AN ANNUAL INSPECTION A RUBBING NOISE WAS HEARD DURING THE AILERON MOVEMENT. INSPECTION IN THE LEFT WING, WING STATION 70.85 (RIB OUTBOARD OF THE FLAP ACTUATOR ROD), THE AILERON CABLES TRAVEL THROUGH AN OPENING IN THE RIB. A PIECE OF PHENOLIC IS RIVETESDR A6WA2018022345640Link · out of adjustAIRCRAFT HAS EXCESSIVE RIGHT HAND ROLL TENDENCY DURING ROTATION AND CLIMB. BOTH AUTOPILOTS ON AND OFF. REQUIRES APPROX 1/2 LEFT HAND WING DOWN TRIM FOR STRAIGHT AND LEVEL FLIGHT. THRUST WAS MATCHED FOR N1. FLIGHT CONTROL PAGE INDICATES LEFT AILERON SLIGHTLY UPSDR A6WA2018022145640Link · out of adjustAIRCRAFT HAS EXCESSIVE RIGHT HAND ROLL TENDENCY DURING ROTATION AND CLIMB. BOTH AUTOPILOTS ON AND OFF. REQUIRES APPROX 1/2 LEFT HAND WING DOWN TRIM FOR STRAIGHT AND LEVEL FLIGHT. THRUST WAS MATCHED FOR N1. FLIGHT CONTROL PAGE INDICATES LEFT AILERON SLIGHTLY UPSDR HALA2018020600034Warning Message · false activationAILERON LOCKOUT EICAS CAUTION ILLUMINATED DURING CLIMB. THEN EXTINGUISHED. PERFORMED FIM 27-11 D.T. 804 BLOCK 1, 5, 10, 15. NO FAULTS SHOWN ON LEFT OR RIGHT SAM. PERFORMED LOCKOUT ACTUATOR AND MECHANISM TEST IAW AMM 27-11-44-422-016, STRP 3.I. TESTED OK.SDR EBVR20180201Casting · corrodedINSPECTION OF SECTOR REVEALED CORROSION ON BOTH THE ALUMINUM CASTING AND STEEL SHAFT. REPLACED SECTOR WITH NEW
ASSEMBLY P/N 6660303-18.SDR ANCF2018012802Controller · failedDURING INITIAL CLIMB, THE ECAM MASTER CAUITON F/CTL R AIL FAULT, 5 MINUTES LATER, F/CTL AIL SERVO FAULT. IAW AMM 27-14-51, PB 401. THE AILERON SERVO CONTROL WAS REPLACED .SDR 3SDR20180213005Spacer · chafedDURING LIFE EXTENSION INSPECTION IAW SB 04-009, FOUND CHAFE DAMAGE FROM AILERON CABLE CHAIN RUBBING THE CHAIN CONNECTING ROD AND ASSOCIATED SPACER. WITH AILERON CABLE TENSIONS SET IAW AMM, APPEARS TO BE EXCESSIVE SLACK IN CABLE CHAIN. ENGINEERING DOES NOT CSDR 3SDR20180212004Spacer · chafedDURING LIFE EXTENSION INSPECTION IAW SB 04-009, FOUND CHAFE DAMAGE FROM AILERON CABLE CHAIN RUBBING THE CHAIN CONNECTING ROD AND ASSOCIATED SPACER. WITH AILERON CABLE TENSIONS SET IAW AMM, APPEARS TO BE EXCESSIVE SLACK IN CABLE CHAIN. ENGINEERING DOES NOT CSDR HALA2018012600015Transducer · malfunctionedELEVATOR SERVO FAULT DURING CRUISE, FOLLOWED BY F/CTL PRIM 1 PITCH FAULT FOR 30 SEC, THEN CLEARED 1MIN, FOLLOWED BY F/CTR ELEVATOR SERVO FAULT SHOWING LT ELEV B & RT ELEV G AMBER BOXED ON F.CTLPG. REPLACED THE LT ELEVATOR POS TRANSDUCER IAW AMM 27-98--17, SDR ANCF2018010601Servo · failedLEFT AND RIGHT AILERON FAULT AFTER LIFT OFF, BOTH ACTUATOR IN BOTH WINGS WERE AMBER. IAW AMM 27-14-51-000-001-A, AND AMM 27-14-51-400-001-A THE AILERON SERVO CONTROL LT 33CE3 WAS REPLACED. .IAW AMM 27-94-34 PB 401,CONF 00 THE SEC N 2 REMOVED AND REPLACED. SDR SIMA20180103001Control Unit · failedFLIGHT CONTROL BINDING AT CRUISE ALTITUDE & ON DESCENT. CONTROL COLUMN RESTRICTED FROM RETURNING TO THE NEUTRAL POSITION. PERFORMED OPERATIONAL TEST OF AILERON SYSTEM IAW AMM 27-11-00, AND REMOVED AND REPLACED THE AILERON FEEL UNIT IAW 27-11-05 OPS CHECKED GOOSDR SCNA20171218319Control Cable · corrodedRT MLG WW RT AILERON CABLES CORRODED. REMOVED, REPLACED & OP CHECKED.SDR SCNA20171218316Control Cable · corrodedLEFT MLG WW LT AILERON CABLES HAS RUST COLORING INSIDE OF DUEL SET OF PULLIES. REMOVED & REPLACED & OPS CHECKED THE LT AILERON CONTROL CABLES.SDR 9WGA201711140001Aileron Sys · malfunctionedDURING CLIMB, THE AILERON DEFLECTION DISENGAGED. DUMPED FUEL, PERFORMED UNSCHEDULED LANDING.SDR HALA2017101700252Warning Message · illuminatedAILERON LOCKOUT EICAS AND OVERHEAD DISCRETE ILLUMINATED ON APP. WITH FLAPS 15, AND SLOWING THRU 180KTS. WARNINGS WENT OUT WITH LANDING GEAR DOWN, FLAPS 25. PERFORMED A BITE IAW FIM 27-11/804, TESTED OK, NO FAULTS. OK FOR CONTINUED SERVICE.SDR 2017FA0000525Control Cable · frayedNOTED UNUSUAL NOISE IN LEFT WING. INVESTIGATION REVEALED THE LEFT AILERON CABLE TO BE FRAYED WITH BROKEN STRANDS. THE AREA WHERE THE CABLE WAS FRAYED HAS NO ACCESS EXCEPT BY BORESCOPE. THE AREA AFFECTED HAS A RECOMMENDED SB11-27-05 WHICH INSTALLS AN INSPECTIONSDR GR422017101800511Aileron · malfunctionedDURING CRUISE AT FL450, AIRCRAFT ROLLED WITH CORRESPONDING AILERON RT FAIL CAS MESSAGE. RT AILERON DISPLACED IN UP POSITION. THREE ATTEMPTED FLIGHT CONTROL RESETS WITH NO EFFECT. CHECKED THE AIRCRAFT AND FOUND NO FAULTS.SDR 2017FA0000511Aileron Sys · malfunctionedDURING CRUISE, THE AIRCRAFT EXPERIENCED A SLIGHT ROLE TO THE COPILOT SIDE OF THE AIRCRAFT. ON BOARD COMPUTERS INDICATED AN AILERON ACTUATOR FAILURE FOR THE RIGHT AILERON. AIRCRAFT RETURNED TO DEPARTURE WITHOUT DECLARING AN EMERGENCY. THE COMPONENTS ARE BEISDR YENA201709260796Servo Valve · failedLIGHT AIRFRAME VIBRATION DURING CLIMB, FL190 TO FL230. FELT IN COCKPIT ONLY. STOPPED IN TURN, STARTED AGAIN AT WINGS LEVEL. SIMILAR ON DESCENT. DIVERTED, PERFORMED OPS TEST OF AILERON DAMPING IAW 27-10-00-810-828-A. DURING TEST FOUND LEFT AILERON SERVO GREEN HSDR YENA201709260795Servo · failedLIGHT AIRFRAME VIBRATION DURING CLIMB, FL190 TO FL230. FELT IN COCKPIT ONLY. STOPPED IN TURN, STARTED AGAIN AT WINGS LEVEL. SIMILAR ON DESCENT. DIVERTED, PERFORMED AN OPS TEST OF AILERON DAMPING IAW 27-10-00-810-828-A. DURING TEST FOUND LEFT AILERON SERVO GRSDR 2017FA0000499Spacer · looseWHEN INSPECTING THE AILERON CABLES THE INSPECTOR FOUND THAT THE SPACER LISTED BELOW HAD GAP IN IT CAUSING THE BOLT TO WOBBLE IN THE HOLE AND THE BELLCRANK TO DEFLECT. LOOKS LIKE THE SPACER USED MIGHT BE THE WRONG ONE AS THERE IS A GAP BETWEEN THE SPACER AND THSDR 2017FA0000498Spacer · looseWHEN INSPECTING THE AILERON CABLES INSPECTOR FOUND THAT THE SPACER (BELOW) USED HAD GAP IN IT CAUSING THE BOLT TO WOBBLE IN THE HOLE AND THE BELLCRANK TO DEFLECT. LOOKS LIKE THE SPACER USED MIGHT BE THE WRONG ONE.SDR COEA2017091306919Bellcrank · corrodedCORROSION FOUND ON THE RT AILERON BELL CRANK ASSY. REPLACED THE BELLCRANK.SDR UIEA2017091401665Control Rod · corrodedLEFT WING OTBD AILERON, BETWEEN OTBD AND INBD PCA, LEADING EDGE, CONTROL RODS HAVE SURFACE CORROSION. REMOVED AND REPLACED THE CONTROL RODS IAW AMM 20-11-00-910-802.SDR HNAA2017080200260Relay · malfunctionedSPOILER FAIL EICAS MESSAGE DISPLAYED AFTER RETRACTION. EXTINGUISHED DURING TAXI. PERFORMED SPOILER OPS CHECK. NO DEFECTS NOTED. R & R THE RELAYS K0030 AND K0031 FOR POSITIVE MAINTENANCE ACTION. OPS CHECKED GOOD. OKAY FOR SERVICE IAW MM 27-63-01.
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