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 C2XA10CL122Recovery Unit · out of adjustCLE FLT 2578 THE CREW REPORTED THE AIRCRAFT REQUIRED A SIGNIFICANT AMOUNT OF LEFT TRIM TO COUNTER A DISTINCT RIGHT ROLL. MAINTENANCE INSPECTED AND ADJUSTED THE LEFT AND RIGHT AILERON NEUTRAL RECOVERY UNIT. OPERATIONAL CHECKS WERE GOOD.SDR RYNA2010007020023Indication Sys · malfunctionedWHILE PERFORMING CONTROL WHEEL SURFACE CHECKS, LEFT O/B AILERON SHOWED NO MOVEMENT ON LOWER EICAS SCREEN. SWAPPED RT & LT STAB TRIM/AILERON LOCKOUT MODULES FOR TROUBLESHOOTING. CHECKS GOOD PER FIM 27-09-00, NO HELP. SWAPPED BACK, BOTH CHECK GOOD. TRANSFERRSDR HALA2010071600301Control Cable · brokenLEFT AILERON CONTROL CABLE (7F) HAS BROKEN STRANDS. REPLACED LEFT AILERON TAB CONTROL CABLE (7F) IAW M/M 20-00-02 & 27-10-00. OPERATION & RIG CHECK GOOD.SDR SWIA201024539Control Panel · defectiveRUDDER RUN AWAY TO RIGHT INFLIGHT, UNCOMMANDED. (FLT 591) REPLACED AILERON/RUDDER TRIM CONTROL PANEL.SDR UALA2010070102350Actuator · failedAILERON LOCKOUT EICAS. CONFIRMED BOTH CB C17 LT AILERON LOCKOUT AND C18 R AILERON LOCKOUT POPS WITH OR WITHOUT PERFORMING AILERON LOCKOUT TEST. IT POPS WITHIN 30 TO 60 SECS AFTER RESET. REF SSM 27-10-02, WDM 27-11-12, 27-11-22 SHOWS SYSTEMS ARE INDEPENDENT ANSDR ASAA1058015Bearing · lack of lubeDURING MANEUVERING FOR LANDING ON SHORT FINAL WHILE APPLYING AILERON TO ROLL LEFT YOKE MOMENTARY LOCKED AND REQUIRED EXCESSIVE FORCE TO OBTAIN DESIRED ROLL INPUT F/O HAND FLYING DURING FAULT. ISOLATION/TROUBLESHOOTING FOUND SIGNIFICANT NOISE CLICKING COMING FSDR SWAA103782Shaft · corrodedDURING SCHEDULED 16Y CHECK, FOUND CORROSION ON SHAFT OF AILERON BODY QUADRANT. REMOVED AND REPLACED SHAFT PER MM.SDR UALA2010062302210Shutoff Valve · faultyON TAXI COULD ONLY GET 2040 PSI FROM LT ELEC HYD PUMP ALONG WITH EICAS MESSAGE AND AUDIO. LT ELEC HYD PMP PSI AT 2200. LT ELEC PUMP, ELCU REPLACED, NO HELP. SUSPECT INTERNAL COMPONENT BYPASSING. WILL NEED TO ACP CHECKS. WITH REF TO LOW PRESSURE ON LT ACMP, FSDR CA100617007Pulley · seized(CAN) AILERON CONTROL REPORTED AS STIFF. RECTIFICATION, WITH ROLL CONTROL DISCONNECTED FOUND THE PILOTS SIDE TO BE STIFF. FOUND CAPT CONTROL COLUMN HAND WHEEL BEARING TO BE ROUGH. HAND WHEEL REMOVED AS PER 27-32-17 AND BEARINGS (P/N- MS27641-10) REPLACED. SDR SWIA201024716Rod End · corrodedLEFT AILERON TRIM TAB ROD ENDS CORRODED. (C-CHECK) REPLACED LEFT AILERON TRIM TAB ROD ENDS.SDR NSVA201093Control Cable · chafedDURING A SCHEDULED 4A CHECK WHILE PERFORMING WC 27-900-705 DETAILED VISUAL INSPECTION OF THE EXPOSED AILERON WING CABLES, THE LEFT FORWARD INBOARD CABLE WAS FOUND SEVERELY CHAFED, APPROX 40-50 PERCENT THROUGH, AT WING STATION Y-194.219 AND APPROX STATION Y-200SDR UALA2010060701971Control Cable · misroutedFLIGHT CONTROLS STIFF IN PITCH AND ROLL ON GROUND AND IN AIR. HEAVY CONTROLS FELT ON BOTH CONTROL COLUMNS, AP'S DISENGAGED, HYD'S PRESS AND QTY'S NORMAL. CHECKED LT AND RIGHT AILERON PCU. COMPLETED SYSTEM TEST. SYSTEM WILL INCREASE WHEEL FORCE. HAD TO FLY APPSDR DXTA2010061104120Bearing · wornRUBBING HEARD/FELT IN YOKE & FLOOR DURING FORE & AFT MOVEMENT OF YOKE ONLY WHEN AIRBORNE & AT ALL AIRSPEEDS & CONFIGURATIONS. NO RUBBING INDICATED WITH LT/RT MOVEMENT OF YOKE. RUBBING HEARD/FELT ON BOTH SIDES YOKE & FLOOR OF COCKPIT WITH EACH PILOT CALLING RSDR SWIA201024351Flap · defectiveAIRCRAFT ROLLS WHEN FLAPS SELECTED TO 45 DEGREES. (FLT 1005) REMOVED EXCESSIVE PAINT BUILDUP ON FLAPS LEADING EDGE.SDR CA100608008Control Cable · obstructedWHEN ELEVATOR CONTROL PULLED ALL THE WAY BACK THE AILERONS WERE LOCKED UP. HOSE CLAMP WAS HOLDING STRUCTURE CLOSER TO CONTROL COLUMN SHAFT. WHEN CONTROL COLUMN WAS PULLED OUT, A ROLLER ADJUSTMENT SCREW CONTACTED THE STRUCTURE, BINDING. THE AILERONS, AS HOSE CSDR UALA2010060101893Actuator · faultyRT AILERON LOCK OUT ACTUATOR. NEED TO REPLACE RT AILERON LOCK OUT ACTUATOR. IT DID HIT AGAIN. REPLACED RT AILERON LOCKOUT ACTUATOR. OPS CHECKED GOOD.SDR 2010FA0000507Control Cable · frayedDURING INSPECTION THE AILERON CABLES ARE INSPECTED WITH MAGNIFICATION WHERE KNOWN
WEAR/FRAYING IS COMMON. THIS CABLE, P/N-0510105-360 WAS FOUND WORN AT F.S.: 65.53.
THERE WERE BROKEN STRANDS AND THE AREA IS EXTREMELY SHINY. THIS IS A COMMON DISCREPANCY
FOR SDR UALA2010052501799Actuator · faultyLT & RT AILERON LOCKOUT MSGS. DUE TO REPEAT WRITE UP OF AILERON LOCKOUT NEED TO REPLACE THE RT & LT AILERON LOCKOUT ACTUATORS. REPLACED THE RT & LT AILERON LOCKOUT ACTUATORS. FUNCTION TESTS OK.SDR DXTA2010052404097Control Unit · bindingON APPROACH AFTER DISENGAGING THE AUTO PILOT/YAW DAMP AT 180KTS THE ACFT WOULD ONLY ROLL (5) DEGREES TO THE RT. BOTH THE CAPTAIN AND COPILOTS CONTROLS SEEMED JAMMED. ONCE ON THE GROUND WE ARE ABLE UNJAM THE CONTROLS WITH FULL MOVEMENT. REPLACED AILERON AFU.SDR 2010FA0000498Control Cable · wornDURING A PREFLIGHT INSPECTION WITH THE AILERON UP, EXCESSIVE WEAR OF THE FORWARD OUTBOARD AILERON CABLE WAS NOTED AT THE RBS 189 FAIRLEAD. THE PHENOLIC PROTECTOR WAS IN GOOD CONDITION EVEN THOUGH THE CABLE HAD BEEN RUBBING ON IT. MANY STRANDS WERE WORN THROUGHSDR A6WA201040365Actuator · bindingDURING APPR F/O FELT BINDING IN AILERONS (BOTH LT AND RT) UPON LANDING, PERFORMED AILERON CHECK AND FELT BINDIING IN BOTH DIRECTIONS ON BOTH SIDES. R & R AILERON TRIM ACTUATOR IAW AMM 27-12-01. OPS TEST GOOD.SDR 2010FA0000492Control Cable · frayedDURING INSPECTION THE AILERON CABLES ARE INSPECTED WITH MAGNIFICATION WHERE KNOWN WEAR/FRAYING IS COMMON. THIS CABLE, CESSNA P/N-0510105-364 WAS FOUND WORN AT W.S.: 71.125. THERE WERE BROKEN STRANDS AND THE AREA IS EXTREMELY SHINY. THIS IS A COMMON DISCREPANCYSDR 2010FA0000491Control Cable · frayedDURING INSPECTION THE AILERON CABLES ARE INSPECTED WITH MAGNIFICATION WHERE KNOWN WEAR/FRAYING IS COMMON. THIS CABLE, CESSNA P/N-0510105-364 WAS FOUND WORN AT FS 65.33. THERE WERE BROKEN STRANDS AND THE AREA IS EXTREMELY SHINY. THIS IS A COMMON DISCREPANCY FORSDR 2010FA0000490Control Cable · frayedDURING INSPECTION THE AILERON CABLES ARE INSPECTED WITH MAGNIFICATION WHERE KNOWN WEAR/FRAYING IS COMMON. THIS CABLE, P/N-0510105-360 WAS FOUND WORN AT F.S.: 65.53. THERE WERE BROKEN STRANDS AND THE AREA IS EXTREEMLY SHINY. THIS IS A COMMON DISCREPANCY FOR THISDR MASA2010050900475Warning System · activatedCONFIG TRIM MASTER WARNING ON T/O ROLL. RTG; PERFORMED AILERON EXCESSIVE BACKLASH CHECK PER AMM.SDR UALA2010050301477Servo · out of toleranceAIRFRAME VIBES. GOES AWAY WITH ROLL INPUTS. VIBRATION REPORT CHECKLIST COMPLETE. FLIGHT CRE W REPORT STATES, SLOWING TO 300 KIAS AT FL280 IN CLIMB, ALL VIBES WENT AWAY. DEFINITELY SPEED RELATED, MEDIUM FREQUENCY FELT LIKE ELEVATOR OR AILERON FLUTTER, BUT INTESDR 2010FA0000411Control Cable · frayedDURING A ROUTINE INSP, THIS CABLE WAS FOUND WORN WITH BROKEN STRANDS. IT IS VERY DIFFICULT TO SEE WITHOUT MAGNIFICATION AND APPEARS ONLY AS A SHINY SPOT ON THE CABLE. THIS CABLE AND (2) OTHERS PASS ACROSS THE CEILING THROUGH 3 PULLEYS JUST ABOVE THE REAR SEAT SDR N6WA20100406Aileron · bindingAILERONS JAMMED IN FLIGHT. INSPECTED AILERON CONTROL CABLES IN PRESSURIZED AND UNPRESSURIZED ZONES, AVIONICS BAY, WHEEL WELL, UNDER SPOILER PANELS FOR DAMAGE OR FOD, NO DAMAGE NOTED IAW AMM 27-11-00. NO DAMAGE ON AILERONS FOUND AT THIS TIME.SDR UALA2010041901292Bearing · bindingAILERONS BIND DURING FLIGHT CONTROL CHECK. FOUND ROD END BEARINGS WORN ON CONTROL ROD BETWEEN THE RT LCCA TORQUE TUBE AND THE AILERON CONTROL OVERRIDE MECHANISM. VERIFIED ROD ENDS REPLACED ON BENCH COMPARITOR. ROD LENGTH AT ORIGINAL CONFIG. REPLACED ROD ENDSDR MYWA100068Actuator · leakingETOPS SIGNIFICANT ITEM - UPPER AILERON POWER CONTROL UNIT IS LEAKING FROM ACTUATOR PISTON.SDR A6WA201040277Feel Sensor · out of adjustHIGHER THAN NORMAL CONTROL FORCE REQUIRED WHEN APPLYING AND NEUTRALIZING RT ROLL INPUTS FROM CTR OS ON BOTH YOKES IN FLIGHT. INSPECTED RIGGING OF AILERON FEEL AND SENSORY MECHANISM ON BOTH SIDES. ADJUSTED IAW AMM 27-11-00. OPS CHECK GOOD.SDR HALA2010032900140Bearing · bindingETOPS SIGNIFICANT SYS - "IAW FLIGHT CREW" BINDING IN AILERONS WHEN DOING FULL TRAVEL CHECKS, LT TURNS ONLY, RT TURNS OK. REPLACED AILERON CONTROL FEEL BEARING. - OPS CHECK OK, REF CMM 27-11-23-701-3D (9).SDR 22AA201000067AControl Cable · brokenACFT ROLLS WHEN SPEED BRAKE IS EXTENDED. DIFFERENCE SHOWS ON SPI. DURING INSP FOUND RT/LT INBD AILERONS OUT OF RIGGING. ALSO ON PRE/FLT FOUND LT WING GROUND SPOILERS NOT DEPLOYING FULLY & SPOILER HANDLE NOT RETRACTING AUTOMATICALLY. ALSO SPOILER PANEL 1 & 2 NOSDR UALA2010032200943Servo Control · faultyLT AILERON ISSUE, FLIGHT DIVERTED. AILERON JERK HAPPENED WITH A-P ON, AP WASN'T DISENGAGED AND DID NOT KICK OFF. SPOILERS DIDN’T DEPLOY OR MOVE TO CAUSE ANY ROLL. AILERON FLOATED UNTIL AN INPUT WAS MADE THEN AILERON JERKED INTO COMMANDED POSITION. UNCOMMANSDR HALA2010031900131Seal · out of positionETOPS SIGNIFICANT SYSTEM - LEFT AILERON BINDS. FOUND RIGHT INBOARD AILERON OUTBOARD LOWER SEAL AT LEADING EDGE STICKING OUT FOUR INCHES. RE-SECURED SEAL, SECURITY AND OPS CHECK OK REF FIM 27-11-00 FIG 107.SDR 2010FA0000230Cable · brokenRT AILERON BUS CABLE PN 3763151-501 BROKEN JUST OTBD OF THE RT INBD AILERON. FOUND LT AILERON WAS INOPERATIVE; THEREFORE PLACING HIGH TENSION ON THE BUS CABLE. WE ARE QUARANTINING THE ACTUATOR AND CABLE ASSY UNTIL FURTHER INVESTIGATION.SDR SIMA201006704Fitting · wornDURING THE MAINTENANCE BASE VISIT THE LEFT AILERON ACTUATOR FITTINGS WERE FOUND TO BE LOOSE IN BORES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT AILERON FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 2010F00054Cable · brokenRT AILERON BUS CABLE PN 3763151-501 BROKEN JUST OTBD OF THE RT INBD AILERON. FOUND LT AILERON ACTUATOR WAS INOPERATIVE THEREFORE PLACING HIGH TENSION ON THE BUS CABLE. QUARANTINED THE ACTUATOR AND CABLE ASSY UNTIL FURTHER INVESTIGATION.SDR UALA2010030100734Control Rod · bindingCAPT FELT BINDING ON AILERON ON APPROACH AFTER LANDING ON GROUND. FLT CONTROL BINDING AILERON DISCONNECTED AND CONNECTED CONTROL RODS. OPS CHECKS NORMAL. NO BINDING FOUND IN SYS. RII INSPECTION METHOD NR 1 OF REMOVED AILERON CONTROL RODS AS CALLED OUT IN FIM.SDR 2010FA0000215Control Cable · frayedDURING A PRE-PURCHASE INSPECTION, FOUND CONTROL YOKE BINDING WHEN TURNED TO THE LT AT APPROX 45 DEGREES. INSPECTED AILERON CNTRL SYS AND FOUND SCREW LODGED IN PULLEY GROOVE AND DAMAGED CABLE. ACFT HAD FLOWN 2.0 HRS SINCE LAST ANNUAL INSPECTION. THE SCREW APSDR SWIA201023689Pcu · out of rigUNCOMMANDED RIGHT ROLL WHEN FLAPS EXTENDED TO 45 DEGREES. (FLT 6016) RIGGED LEFT AILERON PCU AND RIGHT FLAP BPSU.SDR SWIA201023697Aileron · out of rigAIRCRAFT ROLLS TO THE RIGHT WHEN FLAPS ARE SELECTED PAST 30°. (FLT 4556) ADJUSTED LEFT AILERON RIG AND CLEANED WINGS.SDR UALA2010021100521Bearing · wornCREW REPORTS ON FLT CONTROL CHECK FOR AILERON, THE CONTROL WHEELS (CAPTS AND FO'S) FEEL AN UNUSUAL HARD SPOT AT ABOUT THREE-QUARTERS TRAVEL LT WING DOWN. LT AIL LCCA UPR & LWR TORQUE TUBE SUPPORT BEARINGS (3EA) FOUND WORN & CORRODED AT LWR LINK ARM FOR FEEL, SDR SWIA201023646Pcu · out of adjustUNCOMMANDED LEFT ROLL WITH FLAPS SELECTED FOR LANDING. (FLT 4731) RIGGED RIGHT AND LEFT AILERON PCU'S.SDR CLCA02092010.1Warning System · activatedAFTER TAKEOFF (SBKP) LEVEL 2 DEFLECT AILERON DISAGREEMENT WARNING APPEARED ON EAD. PERFORMED CHECKLIST, WARNING REMAINED, RETURNED TO AIRPORT (SBKP). ENTERED ON DEFERRED MAINTENANCE ITEM (DMI) PER MEL 27-13-2, CAT "C", PLACARD INSTALLED, AIRCRAFT RELEASE BACSDR SIMA201003502Fitting · damagedDURING MAINTENANCE BASE INSPECTION FOUND RIGHT AILERON ACTUATOR FITTING TO BE DAMAGED BEYOND LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED AILERON ACTUATOR FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CLCA01282010.1Warning System · activatedAFTER TAKEOFF (SBKP) EAD INDICATES LEVEL 2 AILERON DEFLECT DISAGREE. PERFORMED QRH CHECKLIST AND INDICATION STILL PRESENT. RETURNED TO AIRPORT. ENTERED ON DEFERRED MAINTENANCE ITEM (DMI) PER MEL 27-13-2, CAT "C", PLACARD INSTALLED, AIRCRAFT RELEASE BACK TO SDR CA100121001Control Cable · worn(CAN) THE AILERON CABLES ON LAKE ACFT, MODELS, LA-4, -200, -250 HAVE BEEN FOUND WEARING AT FUS STA 117 0N LA-4, 200`S AND FUS STA 176 ON LA-250 WRE THE CABLE CONTACTS THE PHENOLIC FAIRLEAD. THE WEAR OF THESE CABLES IS DEPICTED IN AC43.13-1B, CHAP. 7, PG7-36, FSDR UALA2010011500187Aileron Sys · malfunctionedAILERON CONTROL ISSUE, FLIGHT DIVERTED. INSPECTED CABLES AND PULLEYS FROM WHEEL WELL TO AILERON PCU'S BOTH LT AND RT WING. ALSO CHECKED AILERON QUADRANTS AND COLD SOAKED QUADRANT BRGS IN WHEEL WELLS AND DAMPER UNDER COCKPIT PIT FLOOR FOR TROUBLESHOOTING. NOSDR ANCF09123000056AController · malfunctionedAIR TURN BACK. LT AND RT AILERON FAULT WAS PRESENTED AFTER TAKE OFF. IAW TSM 27-95-00-810-802 FAILURE OF THE FCDC 2 WAS PERFORMED AND TEST OK AND AMM 27-96-00-740-0021 THE BITE TEST OF THE EFCS GROUND SCANING WAS PERFORMED AND SATISFACTORY.
Back to JASC 2710