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 2010FA0000033Control Cable · damagedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSP FLAT SPOTS WERE NOTICED ON 3 AILERON CONTROL CABLES. ROLLED CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS AND WAS ABLE TO CATCH FRAYED WIRES WITH A RAG AND COUSDR CA100107005Guard · missing(CAN) COCKPIT COMPONENTS REMOVED FOR ACCESS. ROLL DISCONNECT HANDLE REMOVED. UPPER MOST CABLE PULLEY FOR ROLL DISCONNECT WAS FOUND MISSING QUANTITY X2 PULLEY GUARD PINS. INSPECTION OF TWO OTHER DASH-8`S, S/N`S 668 AND 669 DID NOT FIND SAME CONDITION. REFERSDR SIMA201001103Fitting · nickedDURING MAINTENANCE BASE VISIT FOUND THE LEFT AILERON ACTUATOR FITTING TO HAVE SEVERAL NICKS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR NOCA07109Warning System · activatedAFTER ENGINES START, AILERON LOCKOUT EICAS MSG WITH ASSOCIATED OVERHEAD LIGHT DISPLAYED. GATE TURNBACK IN RMS. TROUBLESHOT PER FIM 27-11-00 FIG 104. SYSTEM IS OK.SDR DL76G091968Actuator · unserviceableRTB DUE TO AILERONS BINDING DURING FLT CONTROL CHECK, M.I.P FOUND LT LCCA BINFING. REMOVED LT LCCA IAW AMM 27-11-14. MECH 195867/ OK TO INSTALL LT LCCA IAW AMM. INSTALLED LT LCCA IAW AMM 27-11-14-424-016. PERFORM ALL REQUIRED INSP ETOPS CATEGORY 'E': PROBSDR DL76G091967Actuator · malfunctionedDURING FLIGHT CONTROL CHECK FOUND YOKE WOULD PITCH AND BIND, AND NEEDED MORE FORCE THAN NORMAL TO RELEASE. FOUND LT LCCA BINFING. REMOVED LT LCCA AMM 27-11-14 /MECH 195867/ OK TO INSTALL LT LCCA IAW AMM. INSTALLED LT LCCA IAW AMM 27-11-14-424-016. PERFORMEDSDR SIMA200934907Bracket · gougedDURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT AILERON PCA BRACKET GOUGED ON THE INSIDE OF THE OUTBOARD BUSHING HOUSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW AILERON PCA FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR DL76L091940Computer · malfunctionedRUDDER RATIO AND AILERON LOCKOUT EICAS MESSAGE AND LIGHT ON OVERHEAD. ALSO L.C. AND R AUTOPILOTS WOULD NOT ENGAGE. T/S FOUND FAULT BALL SHOWS ON BOTH SAM. RESET AND PERFORMED MCDP TEST 1/30/40/65. FAILED FCCR SAM. ALSO FAULT BALL SHOWS ON RT SAM. R & R RT SASDR HALA2009112800554Aileron Sys · malfunctionedETOPS SIGNIFICANT SYS - AIL LOCK LIGHT ILLUMINATED AT LOW SPEED. EICAS MESSAGE AILERON LOCKOUT DISPLAYED. OTBD AILERONS DID NOT INDICATE MOVEMENT. AT FLAPS 20 MESSAGE CLEARED. TROUBLESHOT IAW FIM 27-11-00 FIG 104 SHEET 3 BLOCK 67. THE SYS IS OK OPS CHECK NORSDR HALA2009112700551Actuator · faultedETOPS SIGNIFICANT SYS - AILERON LOCKOUT EICAS MSG. PERFORMED FIM 27-11-00 FIG 104 FOUND RT OB ACTUATOR LOCK FAULTING REPLACED RT OB LOCKOUT ACTUATOR IAW AMM 27-11-44-422-016 OB CHECK GOOD.SDR 2009FA0000956Control Cable · chafedDURING A ROUTINE INSP, THE AILERON CABLE PN-0510105-364 WAS FOUND SHINY WHERE IT PASSES THROUGH THE CEILING PULLEY CLUSTER. WHEN VIEWED THROUGH A STRONG MAGNIFYING GLASS, MANY BROKEN STRANDS CAN BE SEEN.SDR 2009FA0000955Control Cable · chafedDURING A ROUTINE INSPECTION THE AILERON CABLE P/N-0510105-365 WAS FOUND CHAFING AND WORN IN THE CENTER CEILING AREA WHERE IS PASSES THROUGH THE 3 PULLEY CLUSTER. THE STRANDS APPEAR SHINY TO THE NAKED EYE, BUT WITH A SUITABLE MAGNIFYING GLASS CAN BE SEEN TO HAVSDR SIMA200931701Fitting · wornDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE RIGHT AILERON POWER CONTROL ACTUATOR FITTING LUG HAS WORN HAT BUSHING BORES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AILERON POWER CONTROL ACTUATOR FITTING WITH A NEW FITTING IAW EO ESDR CA091106006Bearing · seized(CAN) TO MAINTAIN STRAIGHT FLIGHT IN CLIMB (HAND FLYING), REQUIRED AILERON TRIM 3 1/2 UNITS, CONTROL COLUMN AT 18 DEG. MX FOUND CABLE ROD END BROKEN AT SPOILER MIXER MECHANISM. BRG IN ROD END SEIZED. ROD END REPLACED.SDR CA091105002Control Cable · frayed(CAN) DURING AN INSP WHICH INCLUDED REMOVING THE FLOOR, THE AME NOTICED A SHINY SPOT ON THE RT AILERON CABLE WHERE IT PASSES A PULLY AND MEETS THE FUSELAGE. UPON FURTHER INVESTIGATION IT WAS EVIDENT THAT THE CABLE WAS FRAYED. THERE WERE SEVERAL BROKEN STRANDS SDR UALA2009110403406Actuator · malfunctionedAILERON LOCKOUT EICAS MSG AND OVERHEAD ANNUNCIATOR LIGHT. REPLACED AILERON LOCKOUT ACTUATOR, CHECKS OKAY.SDR CA091029002Control Cable · twisted(CAN) WHILE ACCOMPLISHING TASK CARD TC 27-226-00-03 CONTROL CABLES - LT WING AFT SPAR DURING A PHASE 4 SCHEDULED MX CHECK, THE LT AILERON CABLES ABSA-L1 AND ABSB-L1 WERE FOUND TWISTED BETWEEN WING STA 278 AND 326, AFT OF THE NR 1 ENG. WEAR ON THE CABLES WAS FSDR SWIA200923171Bellcrank · corrodedRIGHT AILERON BELLCRANK CORRODED. (C-CHECK) REPLACED RIGHT AILERON BELLCRANK PER AMM.SDR CALA2009102200643Pcu · faultyAILERON CONTROL WHEEL SLOW TO RESPOND WHEN TURNED TO THE RIGHT. REMOVED AND INSTALLED B SYS PCU PER AMM 27-11-71-400-801, ROTABLE PARTS CHANGE WAS INDICATED - TT 1371744, S/N OFF 00346 UNIT, POWER CON OFF 29-2711-9-0004 0346 ON 29-2711-9-0004 1188.SDR CALA2009102200642Control System · lack of lubeBOTH CAPT AND F/O AILERON ROLL CONTROL APPEARS TO BE STIFF AND BINDING AT TIMES, ALMOST AS IF THE HYDRAULIC PRESSURE IS LOW. NO INDICATION OF LOW PRESSURE IN HYDRAULIC SYSTEM. PERFORMED FIM TASK 27-11-00-810-804 AND 27-11-00-700-805 AILERON CONTROL WHEEL FORSDR C2XA09SH371Support Bracket · corrodedSHV - DURING C-CHECK FWD AILERON QUADRANT TORQUE TUBE SUPPORT BRACKET HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 12A-13 AND BETWEEN STRINGERS 21R-20R. MAINTENANCE REMOVED AND REPLACED FWD AILERON QUADRANT TORQUE TUBE SUPPORT BRACKET AT FRAME 12A-13 BETWEEN STRINGSDR C2XA09SH356Support Bracket · corrodedSHV - DURING C-CHECK FWD AILERON QUADRANT TORQUE TUBE SUPPORT BRACKET HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 12A-13 AND BETWEEN STRINGER 21L-20L. MAINTENANCE REMOVED AND REPLACED FWD AILERON QUADRANT TORQUE TUBE SUPPORT BRACKET AT FRAME 12A-13 BETWEEN STRINGESDR CA091021001Pulley · damaged(CAN) DURING B02N01 CHECK IT WAS DISCOVERED THAT THE LT AND RT AILERON PULLEYS BETWEEN RIB 2 AND RIB 4 IS OUT OF ALIGNMENT WITH THE CABLE RUN. AILERON PULLEY SUPPORT BRACKETS P/N 170-32541-001 AND 170-32541-002 MIS-ALIGNED WITH CABLE RUN CAUSING PREMATURE WEASDR SWIA200922903Pulley · wornCONTROL FOR AILERON INPUT IS VERY STIFF AND DIFFICULT TO CONTROL. (FLT 6262) REPLACED LEFT AND RIGHT OUTBOARD PULLEYS PER AMM.SDR CALA2009101400623Mechanism · faultyTHE AILERONS ARE VERY STIFF TO MOVE THROUGHOUT FULL TRAVEL. REMOVED AND REPLACED AILERON TRANSFER MECHANISM IAW 737 AMM 27-11-61. ROTABLE PARTS CHANGE WAS INDICATED - TT 1054666, S/N OFF 01332.SDR C2XA09SH345Fitting · wornSHV - DURING C-CHECK LT AILERON DAMPENER FITTING ON AILERON OTBD HAT BUSHING NOT INSTALLED (CAME OUT WITH BOLT). MAINTENANCE REMOVED AND REPLACED LT AILERON DAMPENER FITTING ON AILERON IAW EMB-145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVISDR 2009FA0000815Control Cable · wornTHE LT AND RT WING AILERON CABLES, 2 EA P/N 145-71009-405 AND 2 EA -401 CABLES WERE WORN BEYOND AMM IN-SERVICE LIMITS. NO STRANDS WERE BROKEN. THE WEAR OCCURED WHERE THE CABLES PASS THROUGH THE NYLON FAIR LEADS ALONG THE WING LEADING EDGE WHEN THE AILERONS ARESDR C2XA09SH311Bushing · wornSHV - DURING C-CHECK LT AILERON PCA ATTACHMENT BRACKET HAS MIGRATING HAT BUSHING. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA ATTACHMENT BRACKET HAT BUSHINGS IAW EC5740-01152 REV B AND REMOVED AND REINSTALLED LT AILERON IAW AMM 27-10-00. THE AIRCRAFT WASDR USAA2009092892650Support Fitting · crackedCLT - RON - MAJOR REPAIR - CRACK IN LT AILERON QUADRANT IN LT W/W LOWER SUPPORT FITTING FRAME 42. REPAIRED LT AILERON QUADRANT IN LT W/W LOWER SUPPORT FITTING FRAME 42 IAW EA 101428 & EO 538P198.SDR DL76S091543Control Rod · lack of lubeRTB DUE TO ON TAXI OUT AILERONS BINDING. DURING FLT CONTROL CHECK BINDING OCCURRED 1/2 WAY THRU LEFT ACTUATION. MULTIPLE OCCURRENCES BOTH SIDES LT AND RT BIND INTERMITTENTLY. T/S PER FIM 27-11-00-101. REMOVED, CLEANED, LUBRICATED AND REINSTALLED CONTROL ROSDR SIMA200926104Fitting · wornDURING THE MAIN BASE VISIT INSPECTION FOUND RIGHT AILERON TO POWER ACTUATOR CONTROL ATTACHED FITTING WORN AT OUTBOARD HAT BUSHING LUG. AIRCRAFT REMOVED FROM SERVICE. MAINTENANCE REMOVED POWER ACTUATOR CONTROL FITTING AND INSTALLED NEW RIGHT AILERON POWER ACTSDR DL77L091523Pcu · leakingEICAS RT HYD QTY LOW. SECURED RT HYD UNTIL 20 MIN FROM LDG. ON APPROACH TURNED ON RT HYD WENT TOWARDS .01, HOWEVER PRESS REMAINED AT 3000 PSI EXCEPT SLIGHT DROPS DURING DEMANDS, THROUGHOUT LANDING AND ROLLOUT. FOUND RT INBOARD FLAPERON PCU LEAKING. REMOVEDSDR UALA2009091802958Pcu · leakingRIGHT INBOARD AILERON PCA LEAKING. RIGHT INBOARD AILERON ACT LEAKING 8 DROPS PER MIN. NEEDS AILERON PCU REPLACED. REPLACED INBOARD RIGHT AILERON PCU. OPS CHECK GOOD. NO LEAKS FOUND.SDR UALA2009090402795Actuator · failedRIGHT AILERON LOCKOUT ACTUATOR FAILS LOCKOUT ACTUATOR AND MECHANISM TEST. RIGHT AILERON LOCKOUT ACTUATOR REPLACED. TESTED AILERON LOCKOUT SYSTEM, OPS NORMAL.SDR CA090904009Torque Tube · unknownFLIGHT DECK CREW REPORTED THAT WHILE HAND FLYING ACFT, THERE WAS SOME AILERON RESISTANCE (BINDING) FELT DURING RT ROLL INPUT GOING THROUGH CENTER.SDR CA090902003Fairlead · wornAILERON CABLES IN THE RT WING ARE DEFLECTED OVER A FAIRLEAD STRIP TO CLEAR AUTOPILOT ROLL SERVO CAPSTAN. SYNTHETIC MATERIAL USED FOR THE RUB STRIP IS VERY HARD AND HAD WORN THE STAINLESS STEEL AILERON CABLES IN AN UNUSUALLY SHORT PERIOD OF TIME. SUGGEST THATSDR CA091023001Control Cable · broken(CAN) DURING THE COMPLETION OF ENGINEERING SERVICE ALERT 120105-01A INSPECTION OF AILERON POSTITION SENSORS, THE CABLE BETWEEN THE SENSOR AND THE AILERON WAS FOUND BROKEN. SENSOR REPLACED AND SYSTEM FUNCTION CHECKED SERVICEABLE. THIS SERVICE ALERT APPLIES TO ASDR CA090828001Control Cable · frayedDURING PHASE INSP, LT AFT OTBD AILERON CABLE WAS FOUND TO HAVE 3 BROKEN STRANDS IN MIDDLE OF CABLE BETWEEN PULLEYS AND FAIRLEADS. NO OBVIOUS REASON FOR DEFECT, OTHER CABLE OK. CABLE REPLACED WITH NEW PART.SDR DXTA2009082103763Pushrod · out of adjustAFTER TAKEOFF ACFT ROLLED LEFT. EXCESSIVE PRESSURE NEEDED TO FLY STRAIGHT. A/P WAS OFF AND TRIMS WERE NEUTRAL. YOKE TURNED APPROX 45 DEG TO THE RT TO MAINTAIN HEADING. ADJUSTED AILERON TRIM TAB PUSH RODS AND SAFETIED REF MM 27-10-00. TRAVEL CHECKS ARE GOOD.SDR UALA2009081902539Pcu · faultedAILERONS HEAVY ON CONTROLS. REPLACED RIGHT & LEFT INBD AILERON PCA(S), LEAK AND OP CHECKED OKAY. ACCOMPLISHED RII INSPECTION OF RIGHT & LEFT INBD AILERON INSTALLATIONS. AIL FORCES STILL HIGHER THAN NORMAL. NO BINDING. MOST APPARENT BETWEEN 0 +-- 4 UNITS L OR SDR UALA2009081902546Actuator · leakingRT WING OTBD AILERON LEAKING HYDRAULIC FLUID FROM ACTUATOR. REPLACED OTBD PCA ASSY - RT AILERON. ACCOMPLISHED INSPECTION.SDR UALA2009081702509Actuator · leakingRIGHT WING UNDER AND NEAR RIGHT AILERON IS WET WITH HYDRAULIC FLUID. REPLACED RT WING INBOARD AILERON ACTUATOR. VERIFICATION FLIGHT CONFIRMS NORMAL OPERATION.SDR SWAA095243Bearing · wornROLL CONTROL VERY STIFF WITH AUTOPILOT OFF, RUDDER TRIM ALSO SEEMS TO STICK BEFORE YOKE ADJUSTS TO INDEX. REMOVED AND REPLACED BEARINGS IN AILERON CONTROL WHEEL DRUM PER MM.SDR 2009FA0000684Control Cable · frayedDURING A ROUTINE INSP, THIS CABLE LOCATED IN CTR CEILING, AT STA 65.33, WAS FOUND BADLY WORN WHERE IT CONTACTS ONE OF 3 PULLEYS. PULLEY FREELY ROTATES HOWEVER THERE IS NOT ENOUGH "TRACTION" FROM CABLE TO ROTATE THE PULLEY DURING NORMAL OPERATION. THIS CAUSES SDR 2009FA0000681Control Cable · frayedDURING A ROUTINE INSP, THIS CABLE LOCATED IN RT WING, AT STA 100.50, WAS FOUND BADLY WORN WHERE IT CONTACTS A FAIRLEAD. THE CABLE APPEARS SHINY, BUT IF VIEWED WITH A STRONG MAGNIFIER MANY INDIVIDUAL STRANDS CAN BE SEEN BROKEN.SDR 2009FA0000680Control Cable · frayedDURING A ROUTINE INSP, THIS CABLE LOCATED IN CTR CEILING, AT STA 65.33, WAS FOUND BADLY WORN WHERE IT CONTACTS ONE OF THE 3 PULLEYS. THE PULLEY FREELY ROTATES HOWEVER THERE IS NOT ENOUGH "TRACTION" FROM THE CABLE TO ROTATE THE PULLEY DURING NORMAL OPERATION. TSDR 2009FA0000679Control Cable · frayedDURING A ROUTINE INSP, THIS CABLE LOCATED IN THE CTR CEILING, AT STA 65.33, WAS FOUND BADLY WORN WHERE IT CONTACTS ONE OF THE 3 PULLEYS. THE PULLEY FREELY ROTATES HOWEVER THERE IS NOT ENOUGH "TRACTION" FROM THE CABLE TO ROTATE THE PULLEY DURING NORMAL OPERATIOSDR 2009FA0000678Control Cable · frayedDURING INSPECTION THIS CABLE WAS FOUND BADLY WORN AT WS 100.25 NEAR THE SUPPORT ARM. THE CABLE APPEARS SHINY AND SMOOTH, BUT WHEN MAGNIFIED MANY BROKEN STRANDS CAN BE SEEN.SDR UALA2009081002407Pca · faultyFLIGHT CONTROL SYSTEM STATUS MESSAGE. UNABLE TO RESET. REPLACED AILERON PCA & PRIMARY FLIGHT CONTROL, CHECKED OKAY. OPS SOFTWARE LOADED, ALL MAT TESTS PASSED.SDR SWIA200922265Pulley · bindingFLIGHT CONTROLS STIFF IN RIGHT TURNS. (FLT 100) REPLACED THREE PULLEYS IN RIGHT AILERON CONTROL CIRCUIT.
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