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 MASA200602155Torque Tube · out of adjustASH 7078 DEN - ROLL CONTROL DIFFICULT UNDER LOAD IN FLIGHT. MX ADJUSTED RT AILERON TORQUE TUBE AND BALANCED BOTH AILERONS.SDR CA060822005Pulley · corroded(CAN) DURING A PHASE CHECK, A GRINDING NOISE WAS HEARD WHEN THE AILERON WAS MOVED BY HAND TO CHECK FOR FREEDOM OF MOVEMENT. UPON FURTHER INVESTIGATION,THE BOLT HOLDING THE PULLEY IN PLACE WAS REMOVED AND THE BEARING FELL APART. BEARING WAS SEVERELY CORRODED ASDR ABXA060230Control Wheel · bindingCAPTAIN AND FIRST OFFICER'S AILERON CONTROL WHEEL BINDS. LUBRICATED LOAD FEEL AND CENTERING MECHANISM. AILERONS OPS CHECKED GOOD IAW B767 AMM 27-11-00-5.SDR MASA200602070Warning System · malfunctionedASH 7275 IAD - A/C ABORTED TAKEOFF DUE TO A AILERON CONFIG MESSAGE. MX COULD NOT DUPLICATE.SDR 06FDEA02849Support · corrodedTHE RT INBD AILERON SUPPORT ASSY ACTUATOR FRAME, O/B BARREL NUT BOLT HOLE IS CORRODED. REAMED BARREL NUT BOLT HOLE TO 0.925 DIA" TO REMOVE CORROSION. REQUESTED EA AILERON SUPPORT SUPPORT ASSY ACTUATOR "A" FRAME BOLT HOLE REPAIRED PER EA 8-5740-102045.SDR MASA200601971Sensor · faultyASH 7095 DEN. AILERON TRIM INDICATION FLUCTUATES. MAINTENANCE REMOVED AND REPLACED AILERON POSITION INDICATION SENSOR.SDR 2006FA0000828Control Cable · frayedDURING AN ANNUAL INSPECTION OF THE AIRFRAME IT WAS FOUND THAT THE RT AILERON CROSSOVER CABLE WAS FRAYED AT THE FAIRLEAD ASSY. THE PROBABLE CAUSE IS THE CABLE RUBBING AGAINST THE FAIRLEAD ASSY. A POSSIBLE SOLUTION IS TO MAKE THE FAIRLEAD ASSY OUT OF A SOFTER SDR 2006FA0000827Control Cable · unserviceableDURING AN ANNUAL INSPECTION OF THE AIRFRAME IT WAS FUND THAT THE RT AILERON DIRECT CABLE WAS FRAYED AT THE FAIRLEAD ASSEMBLY. THE PROBABLE CAUSE IS THE CABLE RUBBING AGAINST THE FAIRLEAD ASSY. A POSSIBLE SOLUTION IS TO MAKE THE FAIRLEAD ASSY OUT OF A SOFTER SDR 2006FA0000826Control Cable · frayedDURING AN ANNUAL INSPECTION OF THE AIRFRAME IT WAS FOUND THAT THE LT AILERON CROSSOVER CABLE WAS FRAYED AT THE ABBRASSION STRIP. THE PROBABLE CAUSE IS THE CABLE RUBBING AGAINST THE ABBRASION BLOCK. A POSSIBLE SOLUTION IS TO MAKE THE ABBRASION BLOCK OUT OF ASDR CA060726004Control Unit · worn(CAN) RT AILERON CABLES PN: 82742409-001 ( WS Y14.25-Y232.00) AND CABLE PN: 82742410-001 (WS Y14.25-Y258.00) WERE APPROACHING PERMISSIBLE WEAR LIMITS AT PULLEY CONTACT AREAS. CABLES REPLACED THIS PROBLEM IS ALREADY KNOWN BY MFG REF TO ALL OPERATOR MESSAGE NRSDR CHQA200600090Control Cable · brokenFLT 3036 - ON T/O OUT OF LGA AS PF, JUST AFTER LIFTOFF NOTED LT ROLLING TENDENCY REQ`D ABOUT HALF OF AVAILABLE RT AILERON AUTHORITY TO CORRECT, WHICH ATTRIBUTED TO A WIND GUST FROM RT CROSSWIND REPORTED BY ATIS, VERY NORMAL IN LGA. MX FOUND RT AILERON CONTROLSDR FDKA200607172Switch · dirtyASH 6146 GSO - CREW REPORTED THE AILERON SYS NR 2 WOULD NOT TURN OFF DURING PRE FLIGHT. MAINTENANCE CLEANED SWITCH, OPS CHECKED NORMAL.SDR CA060719003Potentiometer · separated(CAN) VISUAL INSPECTION CARRIED OUT ON ELEVATOR FDR SYSTEM DUE TO A FAILURE OF THE FDR CORRELATION FLIGHT TEST. FLIGHT TEST RECORDER SHOWED ELAVATOR SYSTEM NO RESPONSE TO SIGNAL. VISUAL INSPECTION REVEALED FAILED POTENTIOMETER SHAFT. REPLACED WITH NEW PART IAWSDR ASMF200607010Flap · out of positionAIRCRAFT RETURNED TO PLATFORM DURING TAXING AND FLAP CONFIGURATION CHECK, THE TAKEOFF WARNING ALARM ACTIVATED WITH TAKEOFF FLAP CONFIGURATION. AIRCRAFT WAS RECEIVED WITH FLAPS AT 40 DEGREES AND FLAP LEVER IN UP/RET POSITION. TAKEOFF ALARM TEST WAS PERFORMED SDR HALA0600485Actuator · malfunctionedBTB - ON PUSH BACK "AILERON TRIM FAIL" ILLUMINATED. REMOVED AND REPLACED AILERON TRIM TAB ACTUATOR PER AMM 27-12-03, OPS CK OKAY.SDR C2XA06TY042Bracket · damagedPCA BRACKET MISSING BUSHINGS & DISPLACED METAL IN BUSHING HOLES. REMOVED AND REPLACED PCA BRACKET IAW EC5750-01177 REV B AND EMB145 SRM 51-40-02.SDR 2006FA0000725Control Cable · frayedDURING AN ANNUAL INSPECTION OF THE RT WING, THE AILERON CROSSOVER CABLE WAS FOUND TO BE FRAYED AT THE WEAR BLOCK. PROBABLE CAUSE IS THAT THE WEAR BLOCK IS CAUSING FRICTION AND WEAR ON THE CABLE. A RECOMMENDED SOLUTION IS TO REMOVE THE WEAR BLOCK. (K)SDR MASA200601805Status Message · false activationASH 7476 ORD - CAPTAIN REPORTED A PITCH FEEL FAULT STATUS MESSAGE. MX RESET THE SYSTEM. OP'S CHECK GOOD.SDR FDKA200606139Module · malfunctionedFDM RDU, THE CREW REPORTED THAT THE AILERON 2 SYSTEM WILL NOT SHUT OFF. MAINTENANCE REPLACED THE MODULE PANEL AND OPS CHECKED.SDR ASMF200606013Plate · stuckDURING TRANSIT CHECK, DETECTED THAT THE AILERON COMPENSATOR MECHANISM GOES TO THE RT SIDE AND STUCK. AIRCRAFT WAS SENT TO THE HANGAR AND THE SPIRAL DRIVE PLATE OF THE AILERON CONTROL TRIM MECHANISM WAS REPLACED IAW AMM 27-10-07, TESTED CORRECT IAW AMM 27-10-0SDR TRAX200600412Control Cable · damagedRANRC 329 LT AILERON CONTROL SYSTEM CABLE CONNECTED TO I/B SIDE OF TENSION REGULATOR TO TBI IN LT MLG WHEEL WELL HAS SEVERAL BROKEN STRANDS.SDR TRAX200600411Control Cable · damagedRANRC 328 LT AILERON CONTROL SYSTEM CABLE CONNECTED TO I/B SIDE OF TENSION REGULATOR TO TBI IN LT MLG WHEEL WELL HAS SEVERAL BROKEN STRANDS.SDR FDKA200606126Manifold · defectiveTHE CREW REPORTED THE AILERON SYSTEM 2 DOES NOT SHUT OFF WITH HYDRAULICS ON DURING THE TEST. MAINTENANCE REPLACED NR 2 MANIFOLD ASSEMBLY AND OPS CHECKED.SDR 4514606152006Control Cable · frayedPREFLIGHT INSP, NOTICED BINDING & CLICKING IN AILERON SYS WHEN ROTATING CONTROLS THROUGH COMPLETE TRAVEL. FOUND LWR AFT AILERON CONTROL CABLE FRAYED 70%. WHILE ROUTING NEW CABLE FOUND PREVIOUS CABLE ROUTED OVER A GUIDE PIN DISRUPTING ANGLE OF TRAVEL THROUGH SDR FDKA200606122Panel · faultyCREW REPORTED THE AILERON ROLL TRIM STUCK IN RIGHT POSITION. MAINTENANCE REPLACED THE TRIM PANEL AND OPS CHECKED.SDR MASA200601585Warning System · malfunctionedASH 7339 CHS - AILERON CONFIG WARNING ON TAKEOFF ROLL. CONTRACT MX RAN THE ENGINES AND COULD NOT DUPLICATE. OP'S CHECK NORMAL.SDR DL76G060488Controller · bypassingREPEAT GRIPE - RIGHT INBOARD AILERON FROZEN 1/3 UP POSITION REQUIRING 6 UNITS LEFT RUDDER TRIM IN CRUISE. REPLACED BOTH PCAS RT INBOARD AILERON AND PERFORMED AILERON RIGGING ADJ TEST. SUBSEQUENT NON-REVENUE VERIFICATION FLIGHT OK.SDR MASA200601513Caution Message · noneASH 5094 STL - PITCH FEEL FAULT CAUTION MESSAGE. THE ACFT POWER WAS REMOVED AND REAPPLIED. THE FAULTS CLEARED ON POWER UP AND AN S-POST TEST PERFORMED WITH NO DEFECTS NOTED.SDR 2006UALA01089Warning System · activatedAILERON LOCKOUT EICAS DURING DESCENT FL110 250 KIAS. CLEANED AND SECURED CANON PLUG ON RIGHT ACTUATOR. OPS OK NOW.SDR MASA200601404Status Message · illuminatedASH 6294 TUS - RTL FAULT STATUS MESSAGE. MX RESET AND PERFORMED SPOST TEST.SDR MASA200601402Warning Message · illuminatedASH 5098 CLT - GLD NOT ARMED EICAS MSG IN FLT. MX PERFORMED SPOST AND SSCU TESTS.SDR FDKA200605102Panel · faultyTHE CREW NOTED THE BACKUP TRIM WOULD NOT GO IN THE DOWN POSITION. MAINTENANCE REPLACED THE PANEL. OP’S GOOD.SDR CA060519003Spring · broken1 OF 2 AILERON GUST LOCK SPRINGS FOUND BROKEN WHEN PANELS REMOVED TO PERFORM OTHER MAINTENANCE REF IPC 27-12-00 FIG 20, ITEM 210. AIRCRAFT TOTAL TIME 19575 HOURS, 12119 CYCLES.SDR MASA200601351Warning Message · illuminatedASH 5008 CHS - GLD UNSAFE MSG. RESET SYSTEM. NO FURTHER ACTION NEEDED.SDR 2006FA0000549Cable · frayedDURING A 100 HOURS INSPECTION THE RT AILERON CROSSOVER CABLE WAS FOUND TO BE FRAYED AT THE PHANALIC BLOCK. PROBABLE CAUSE IS FRICTION BETWEEN THE CABLE AND THE WARE BLOCK. TO PREVENT RECURRENCE REMOVE PHANALIC BLOCK AND INCREASE TENSION ON CABLES. (K)SDR MASA200601334Mcu · malfunctionedASH 5079 CLT. PITCH FEEL AND STAB FAULT STATUS MESSAGE. MX REMOVED AND REPLACED MCU.SDR MASA200601324Aileron · defectiveASH 7294 IAD - CAPTAIN REPORTED THE A/C ROLLS LT ON APPROACH AND CAN NOT BE TRIMMED NORMALLY TO CORRECT THE PROBLEM. MX REMOVED AND REPLACED THE AILERON. TEST FLIGHT WAS GOOD.SDR MASA200601325Status Message · illuminatedASH 6428 BUR - RTL FAULT STATUS MESSAGE. MX PERFORMED SPOST TEST. OP'S CHECK GOOD.SDR FDKA200605085Trim Switch · obstructedTHE CREW REPORTED THE AILERON ROLL TRIM SWITCH STUCK IN FULL RIGHT POSITION. MAINTENANCE REMOVED FOD AND OPS CHECKED GOOD.SDR FDKA200605081Manifold · defectiveTHE CREW REPORTED A NR 2 AILERON SYSTEM INOP MESSAGE NOT SHOWN AT SHUTDOWN. CONTRACT MX ISOLATED THE PROBLEM TO THE SYSTEM MANIFOLD PRESSURE SWITCH. AIRCRAFT FERRIED TO MCO WHERE MAINTENANCE REPLACED THE PRESSURE MANIFOLD AND OP CHECKS WERE GOOD.SDR ASMF200604014Fairing · damagedDURING TRANSIT CHECK, IT WAS DETECTED THAT THE RT AILERON FAIRING WAS DELAMINATED ON THE TRAILING EDGE. THE AILERON FAIRING WAS REPLACED AND THE SYSTEM WAS TESTED IAW M/M 27-10-01, BEING ALL CORRECT. DURING OVERNIGHT CHECK THE SYSTEM WAS TESTED IAW M/M 27-10SDR 05032006ABellcrank · unknownAILERONS FEEL STIFF. R&R LT AILERON BELLCRANK ASSY. O/B IAW 27-11-40-4 OPS CHECK GOOD.SDR CA060508007Control Cable · frayedDURING EVENT INSPECTION OF DETAILED WING (RT) BROKEN STRANDS WERE OBSERVED ON RT AILERON BALANCE CABLE AS IT PASSED OVER A PULLEY AT WING STATION 22.00. CABLE AND PULLEY WERE REMOVED. CABLE WAS REPLACED NEW, PULLEY WAS CLEANED INSPECTED, LUBRICATED AND RETURSDR 04172006AConnector · dirtyMAIN AILERON ROLL TRIM DOESN’T RETURN TO DOWN POSITION. CLEANED LT AILERON TRIM ACTUATOR CANNON PLUG.SDR MASA200600965Circuit Breaker · trippedASH 7283 IAD, AILERON TRIM INOP. AILERON TRIM C/B POPPED AND RESET C/B. AILERON SYSTEM OP CHECK GOOD AND NO FURTHER DEFECTS NOTED.SDR CA060423001Link Assy · brokenRT AILERON OUTBOARD PCU OUTPUT LINK ASSEMBLY BROKEN. WHILE PERFORMING 5000 HOURS INSPECTION FOR THE FLUTTER DAMPENER MAINTENANCE FOUND RT AILERON OUTBOARD PCU OUTPUT LINK ASSEMBLY BROKEN.SDR CA060407002Control Cable · frozenRIGHT AILERON JAMMED IN DOWN POSITION AFTER FLIGHT. DURING LANDING GROUND ROLL AFTER CROSSWIND LANDING, STUCK CONTROL WHEEL TO RIGHT AFTER RT AILERON INPUT. RIGHT AILERON IN DOWN-POSITION. LT AND RT AILERON CABLE CIRCUIT AND PULLEYS CONTAMINATED WITH DEICINSDR VNAA0603013Link · brokenDURING THE 5000 FLIGHT HOUR DETAILED INSPECTION OF THE RIGHT AILERON FLUTTER DAMPER, MAINTENANCE FOUND THE RIGHT AILERON OUTBOARD POWER CONTROL UNIT OUTPUT LINK ASSEMBLY BROKEN. MAINTENANCE REPLACED THE LINK ASSEMBLY WITH A SERVICEABLE UNIT. RIGGING AND OPERSDR 06FDEA1273Regulator · obstructedAFTER TAKEOFF COULD NOT TURN AIRCRAFT TO LEFT MANUALLY WITH YOKE. TURN RIGHT NORMALLY, ENGAGED AUTOPILOT WITH 15 DEGREE BANK AND AIRCRAFT TURNED WHAT SEEMED TO BE NORMAL TO LEFT WITH AUTOPILOT ON. AFTER LANDING CONTROL STILL JAMMED TO LEFT. NOTE NORMAL FLIGSDR MASA200600951Warning Message · illuminatedASH 6259 PHX - AIRCRAFT HAD AN RTL FAULT STATUS MESSAGE. MAINTENANCE RESET THE SYSTEM.
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