JASC 2710
Service difficulty reports · 2,967
Reports filed under 2710 · Aileron Control System, newest first.
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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 022708Attach Fitting · rotatedPILOT REPORTED BINDING AND NOISE IN THE OVERHEAD IN AILERON CONTROL SYSTEM. FLIGHT CONTINUED NORMAL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE ATTACH BLOCK OF THE AILERON CONTROL CABLE LOOP SYSTEM ROTATED AND WAS STRIKING THE LOWER BELLSDR ABXA080092Bearing · wornTHE LEFT INBOARD AILERON OUTBOARD PCA SUMMING LINKAGE HAD A WORN BEARING. REPLACED LEFT INBOARD AILERON OUTBOARD PCA IAW B767 AMM 27-11-48-2.SDR SWIA200819602Bushing · wornFOUND AT C-CHECK, HORIZONTAL STABILIZER HINGE BUSHINGS AND INNER PIN SHOWS SIGNS OF WEAR. REPLACED STABILIZER HINGE PIN AND BUSHINGS IAW CRJ200 AMM SUBTASK 12-20-27-640-008.
SDR SWIA200819226Pulley · dirtyFLT NR 5848. CONTROL YOKE HAS A NOTCHY SPOT WHEN MOVING AILERONS, REMOVED A PEBBLE FROM THE RT AILERON CONTROL PULLEY AT WING ROOT AT INBOARD FLAP. NO DAMAGE NOTED.
SDR CA080211015Control Cable · broken(CAN) DURING CONTROL CABLES INSPECTION ON LT AND RT WINGS, FOUND AILERON CABLES (LT PN 170-05825-401, P/N 170-05826-401, RT PN 170-05827-401, PN 170-05828-401) WORN AND WITH WIRES BROKEN AT SEVERAL FAIRLEADS, LOCATED AT LT AND RT WINGS IB OF THE 17 FLEET ENGISDR CA080211009Control Cable · broken(CAN) C02 CHECK: DURING AILERON CONTROL CABLES INSP ,ON LT AND RT WINGS, FOUND AILERON CABLES (LT P/N 190-04212-401 AND P/N 190-04209-401, RT P/N 190 -05550-401 AND P/N 190-04209-401) WORN AND HAS SEVERAL WIRES BROKEN AT FAIRLEAD LOCATED AT LT AND RT WINGS RIBSDR DXTA200802837Pcu · malfunctionedROLL CONTROL FEELS ABNORMAL. CONTROLS ARE BINDING, THEN RELEASING. ESPECIALLY NOTICEABLE DURING SLOW FLIGHT. REMOVED AND REPLACED LT AND RT AILERON PCU'S IAW MM 27-11-05. OPS AND RIGGING CHECK GOOD.SDR CA080211014Control Cable · broken(CAN) DURING CONTROL CABLES INSP ON LT AND RT WINGS, FOUND AILERON CABLES (LT P/N 170-05825-401, P/N 170-05826-401, RT P/N 170-05827-401, P/N 170-05828-401) WORN AND WITH WIRES BROKEN AT SEVERAL FAIRLEADS, LOCATED AT LT AND RT WINGS IB OF THE RIB 12, 15, 17 ANSDR FAA012408001Cable · wornDURING A PHASE 5 IT WAS FOUND THAT THE AILERON CABLES WERE LOCATED IN THE WRONG GROVES OF THE FUSELAGE SECTOR, CAUSING GROOVES TO BE WORN INTO THE SECTOR BY THE CABLES. THERE IS A SPECIAL "NOTE" IN THE MAINTENANCE MANUAL 27-11-08 SECTION 7 FOR THE AILERON LEFTSDR CA080211012Control Cable · broken(CAN) DURING AILERON CONTROL CABLES INSP ,ON LT AND RT WINGS, FOUND AILERON CABLES (LT PN 190-04212-401 AND PN 190-04209-401, RT PN 190 -05550-401 AND PN 190-04209-401) WORN AND HAS SEVERAL WIRES BROKEN AT FAIRLEAD LOCATED AT LT AND RT WINGS RIB 4A WS -3025.80SDR 2008UALA00388Unknown · unknownAILERON LOCKOUT SLOWING THRU 250 KNOTS.SDR CA080128001Control Cable · broken(CAN) DURING AILERON CONTROL CABLES INSP, ON LT AND RT WINGS, FOUND AILERON CABLES (LT PN 190-04212-401 AND PN 190-04209-401, RT PN 190 -05550-401 AND PN 190-04209-401) WORN AND HAS SEVERAL WIRES BROKEN AT FAIRLEAD LOCATED AT LT AND RT WINGS RIB 4A WS -3025.80SDR COMA0870004Warning System · malfunctionedFLIGHT 5448 - ABORTED TAKEOFF DUE TO CONFIG AILERON WARNING MESSAGE. COMPLIED WITH FAULT ISOLATION TASK FOR CONFIG AILERON WARNING. NO DEFECTS NOTED.SDR UPS08M51440Actuator · faultyINSPECTION TYPE:N/A ATB - ON DEPARTURE, LEVEL 2 AILERON DEFLECT DISAGREE. RAN CHECKLIST, LEVEL 2 ALERT RETURNED. T/S PERFORMED AS PER FIM 27-10-00-1 & A/C DATA OBTAINED FROM AMC. FOUND LOB AILERON DEFLECTION ACTUATOR AT FAULT. SAME REPLACED AS PER MM 27-16SDR CA080115007Pcu · frozen(CAN) THE AC ARRIVED AT DESTINATION AND WAS ON A TURN-AROUND WHEN THE CREW NOTICED ON TAXI OUT, THAT THE AILERONS HAD FROZEN UP. THE AC RETURNED TO THE RAMP WHERE MAINT INSPECTED THE SYS. IT WAS DETERMINED THAT THE AILERON POWER CONTROL UNIT HAD FROZEN UP. HESDR CA080115008Control Rod · bent(CAN) AFTER RECEIVING A REPORT OF AN ANOMALY WITH THE CONTROL ROD FROM ANOTHER OPERATOR, WE INSPECTED THE ROD ENDS ON OUR AC. ALSO FOUND THE ROD ENDS ON BOTH LT AND RT AILERONS BENT. THE ROD ENDS APPEAR TO HAVE BEEN BENT TO ACCOMODATE THE MOVEMENT OF THE AILESDR CA080115006Pushrod · bent(CAN) AFTER RECEIVING A REPORT OF AN ANOMALY WITH THE CONTROL ROD FROM ANOTHER OPERATOR, WE INSPECTED THE ROD ENDS ON OUR AC. WE ALSO FOUND THE ROD ENDS ON BOTH LT AND RT AILERONS BENT. THE ROD ENDS APPEAR TO HAVE BEEN BENT TO ACCOMODATE THE MOVEMENT OF THE AISDR CA080115005Pushrod · bent(CAN) AFTER RECEIVING A REPORT OF AN ANOMALY WITH THE CONTROL ROD FROM ANOTHER OPERATOR, INSPECTED THE ROD ENDS ON OUR AC. ALSO FOUND THE ROD ENDS ON BOTH LT AND RT AILERONS BENT. THE ROD ENDS APPEAR TO HAVE BEEN BENT TO ACCOMODATE THE MOVEMENT OF THE AILERONSDR FDKA200801020Control Unit · malfunctionedFDM 6181 CLT (0406 PHX LCL) - CONTROL RESISTANT/GRINDING WITH AILERON AND ELEVATOR CONTROL INPUT. MX IS CURRENTLY TROUBLESHOOTING.SDR CA080211011Control Cable · broken(CAN) C02 CHECK: DURING AILERON CONTROL CABLES INSPECTION ,ON LT AND RT WINGS, FOUND AILERON CABLES (LT P/N 190-04212-401 AND P/N 190-04209-401, RT PN 190 -05550-401 AND PN 190-04209-401) WORN AND HAS SEVERAL WIRES BROKEN AT FAIRLEAD LOCATED AT LT AND RT WINGSSDR CA080115003Rod End · bent(CAN) WHILE RIGGING THE AILERON SYS FOLLOWING MAINT, NOTICED BOTH THE LT AND RT AILERON CONTROL ROD END FITTINGS WERE BENT WHERE THE CONTROL ROD IS ATTACHED TO THE BELLCRANK AT THE MOST OB POINT. NEW STRAIGHT FITTINGS WERE INSTALLED BUT THIS CAUSED THE AILERONSDR SWIA200819060Bracket · bindingON APPROACH, AILERONS WERE VERY RESTRICTED IN THEIR MOVEMENT, FLIGHT NR 5446. REPLACED LEFT AILERON RVDT CONTROL ARM BRACKET IAW SRM 51-10-02. OPS CHECK GOOD.
SDR 2008UALA00027Pcu · faultyTHE "FLIGHT CONTROLS" EICAS APPEARED AFTER ENGINE START. SUSPECT AILERON POWER CONTROL UNIT. REPLACED LT INBOARD AILERON PCU PER MM 27-11-11. ACP'D MAT CKS AND ADJUSTMENTS. RAN ENGINES, NO MSG'S DISPLAYED OR ACTIVE. AC OK FOR SERVICE.SDR HALA0800001Module · malfunctionedETOPS SIGNIFICANT SYSTEM, EICAS MESSAGE AILERON LOCKOUT ILLUMINATED ON DESCENT THRU 7000 FT 230 KTS FLAP 5 AUTOPILOT ON. REPLACED RT SAM PER AMM 27-09-00. PERFORMED TEST AMM 27-11-00 CK OK. PERFORMED MCDP TEST 60 CK OK GRND CK 1 AT 2 ADC OK, OK FOR SERVICE.SDR HALA0700563Aileron · malfunctionedETOPS SIGNIFICANT SYSTEM, AILERON LOCKOUT AT 260 KTS. T/S PER FIM 27-11-00 FIG 104 TO BLOCK 15. NO FAULTS ON LT OR RT SAMS. NO MSGS. SYS TESTS GOOD.SDR HALA0700561Control Unit · malfunctionedETOPS SIGNIFICANT SYSTEM, EICAS MSG "AILERON LOCKOUT" ILLUMINATED AT 9000 FT ON DESCENT, DECREASING AIRSPEED THRU 240 KTS DISAPPEARED AT 220 KTS AS A/S DECREASED THRU 6000 ALT DID NOT REAPPEAR THRU LANDING. REPLACED SAM PER AMM 27-09-00. PERFORMED TEST AMM 2SDR NWAA074339872Drain Line · obstructedWHILE AT CRUISE ALTITUDE FL 250 WITH AUTOPILOT ENGAGED, AIRCRAFT WOULD NOT RESPOND TO AUTOPILOT ROLL COMMAND IN EITHER HEADING, SELECT MODE OR TURN KNOB. DISENGAGED AUTOPILOT AND CONTINUED ROLL CONTROL WAS SEVERELY RESTRICTED WITH MANUAL INPUT TO CAPTAIN AND SDR HALA0700564Aileron · malfunctionedETOPS SIGNIFICANT SYSTEM, AILERON LOCKOUT 11000 FT 270 ORH NO ACTION. FOLLOWED FIM 27-11-00 FAULT CLEARED ON LSAM. OPS CK OF AILERON GOOD. NO DEFECTS NOTED.SDR FDKA200712412Solenoid Valve · malfunctionedFDM 6109 JFK (1105 PHX LCL) - NO AILERON SYSTEM 2 INOP INDICATION WITH SYSTEM OFF. MX REMOVED AND REPLACED SOLENOID VALVESDR CA071224002Aileron · iced(CAN) PILOT’S REPORTED ON APPROACH INTO AIRPORT, COULD NOT GET ANY ROLL ON AC CONTROLS. IT APPEARED THAT AILERONS WERE FROZEN. SHORTLY BEFORE TOUCHDOWN THEY WERE ABLE TO GAIN CONTROL OF THE AILERON MOVEMENT. THE AC LANDED WITHOUT INCIDENT. MAINT WAS CALLED ANDSDR UPS07M51286Actuator · warning lightATB - AILERON DEFLECT DISAGREE ALERT ON FLAP RETRACTION. A/C ROLLED RT WITH FLAPS UP. NO EMERGENCY DECLARED. R&R RH I/B AILERON DEFLECT ACTUATOR PER AMM 27-16-01-4 AND FUNCTION TEST C/W PER AMM 27-16-00-5. RESULT NORMAL.SDR SWAA075960Control Rod · wornDURING SCHEDULED BRDG CHECK, LT AILERON FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD PER MM.SDR A6WA200740648Pcu · unknownEXCESSIVE LEFT DOWN AILERON TRIM REQUIRED FOR LEVEL FLIGHT, REQUEST INSPECTION. REMOVED AND REPLACED NR 1 AILERON PCU PER AMM 27-14-01, OPS AND LEAK CHECK GOOD. RIG CHECK PER AMM 27-11-00, RIG CHECK GOOD. (M)SDR CA071206006Control Cable · worn(CAN) PILOTS REPORTED THAT THE AILERON CONTROLS WERE STIFF (OAT -20C). INSPECTION OF THE AIRCRAFT WAS CARRIED OUT AND THE AILERON CABLE WAS FOUND TO BE WORN WHERE IT CROSSED A ROLLER FAIRLEAD AT APPROX STN YW189.00. THE ROLLER FAIRLEAD WAS NEARLY SEIZED. THE OSDR FDKA200711342Control Panel · malfunctionedFDM 6049 JFK (0612 PHX LCL) - NR 2 AILERON SYSTEM WILL NOT TURN OFF. MX REMOVED AND REPLACED MANIFOLD AND CONTROL PANEL.SDR FDKA200711335Manifold · malfunctionedFDM RON MCO (1903 PHX LCL) - AILERON SYSTEM 2 WON'T DEACTIVATE. MX REMOVED AND REPLACED AILERON MANIFOLD ASSY.SDR FDKA200711325Control Lever · malfunctionedFDM 6127 FLL (0449 PHX LCL) - ELECTRIC GUSTLOCK WILL NOT DIS-ENGAGE. MX MOVED THE CONTROL LEVER AND THE GUSTLOCK UNLOCKED.SDR SIMA200731203Switch · failedROLL TRIM SWITCH FAILED IN FLIGHT. CLEANED TRIM SWITCHES IAW EMB AMM 27-14-0. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVICE.SDR CA071029011Control Cable · chafed(CAN) GRINDING NOISE UNDER PILOT FLOOR WHEN AILERONS ARE MOVED. CONTROL CABLE FOUND CHAFING ON STEEL BRAIDED NITROGEN LINE. APPROX 3 INCH DEFLECTION OF CONTROL CABLE CAUSED, DUE TO INCORRECT ROUTING OF NITROGEN LINE. NITROGEN PRESSURE LINE REROUTED. AILERON CSDR FDKA200710269Switch · dirtyFDM 6121 ORF (0341 PHX LCL). AILERON SYSTEM 2 WILL NOT DISCONNECT. MX CLEANED AILERON SHUT OFF SYSTEM 2 SWITCH. OPS CHECK GOOD.SDR 2007UALA04134Computer · faultyRECEIVED AN "ELAC1 AILERON ORDER DISAGREE" MESSAGE. NR 1 ELAC COMPUTER FAULTY. REPLACED NR 1 ELAC COMPUTER, NO REPEATS.SDR FDKA200710521Actuator · malfunctionedFDM 6021 JFK (0920 PHX LCL) AILERON ABNORMAL CONTROL FORCE AND FEEL DURING CHECK. MX REMOVED AND REPLACED ARTIFICIAL FEEL ACTUATOR AND PCA, OPS CK GOOD.SDR SWIA200719095Bearing · wornLEFT AILERON HINGE BEARINGS ARE WORN, FOUND AT C-CHECK. REPLACED AILERON HINGE BEARINGS PER CRJ200 AMM TASK 20-26-00-910-810.
SDR SWIA200719094Bearing · wornRIGHT AILERON INBOARD AND OUTBOARD PCU LINK BEARINGS FAIL BACKLASH CHECK, FOUND AT C-CHECK. REPLACED AILERON PCU LINKS PER CRJ200 AMM 27-14-15-00-801/400-801.
SDR SWIA200719093Bearing · failedLT AILERON INBD AND OTBD PCU LINK BEARINGS FAIL BACKLASH CHECK, FOUND AT C-CHECK. REPLACED LEFT AILERON INBOARD AND OUTBOARD PCU LINKS IAW CRJ200 AMM 27-14-15-000-801 AND 27-14-15-400-801.SDR ZZDA2007271Bearing · wornDURING TAXI OUT ON THE FLIGHT CONTROL CHECKOUT AILERON CONTROL WHEEL IS BINDING AND WILL NOT RETURN TO NEUTRAL. FOUND WORN BEARING IN ARM ASSY OF AILERON FEEL CENTERING UNIT. REMOVED AND REPLACED ARM ASSY REF B 737 AMM 27-11, PERFORMED AILERON FEEL AND CTR USDR CA070924007Fitting · damaged(CAN) NEW AILERON CABLE P/N JNL-C6CF1153-3 FROM JNL (W/O 022. THE CSP FITTING MEASURES .4405. THE CSP FITTING WILL NOT ENGAUGE INTO THE AILERON QUARDRANT. ORIGINAL CABLE CSP FITTING MEASURES .4320 (TC NR 20070924007)SDR CA070924005Fitting · mismanufactured(CAN) NEW AILERON CABLE P/N JNL-C6CF1125-3 FROM JNL (W.O. 091) THE CSP FITTING ON IT MEASURES .4405. THE CSP FITTING WILL NOT ENGAUGE INTO THE RECEPTICAL ON THE QUADRANT. THE CABLE REMOVED MEASURES .4310. (TC NR 20070924005)SDR 2007UALA03859Aileron · sticksAILERON STICKS WHILE INFLIGHT AND HESITATES WHEN CHECKED ON GROUND AFTER LAG. 10-19-07 REPLACED LEFT LATERAL CONTROL ACTUATOR TORQUE TUBE REF MM 27-11-16. AILERON OPS CHECKS GOOD.SDR FDKA200709477Gust Lock · inoperativeFDM 6179 JFK (0500 PHX LCL) - GUST LOCK WILL NOT DISENGAGE. MX RESET SYSTEM, OPS CK GOOD.
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