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 SIMA200209427Link · corrodedMBV - DURING FOUND LEFT AILERON DUAL LOAD PATH LINK CORRODED. REPLACED LEFT AILERON DUAL LOAD PATH LINK IAW JIC 27-11-72-RAI-10000-002. (M)SDR SIMA200209426Link · corrodedSAW - DURING INSPECTION, FOUND RIGHT AILERON DUAL LOAD PATH LINK FITTINGS ON WING IS CORRODED. REPLACED WING FITTINGS FOR RIGHT AILERON DUAL LOAD PATH LINK IAW ATR-42 SRM 51-25-02. (M)SDR SIMA200209424Link · corrodedSAW - DURING INSPECTION, FOUND RIGHT AILERON DUAL LOAD PATH LINK CORRODED. REPLACED RIGHT AILERON DUAL LOAD PATH LINK IAW ATR-42 JIC 27-11-72 RAI 10000-002. (M)SDR 2002FA0000420Turnbuckle · separatedWHILE IN LEVEL FLIGHT AT 5500FT MSL, ATTEMPTING TO TURN THE AIRCRAFT LEFT WITH THE AILERON A SMALL BUMP/BANG WAS FELT. THE CONTROL WHEEL WENT FULL LEFT,AND THE AIRCRAFT COMMENCED ROLLING TO THE RIGHT. APPLICATION OF HARD RIGHT RUDDER STOPPED THE ROLL AT ABOUT SDR EVAS91009Control Quadrant · failedDURING CRUISE, CAPTAIN FOUND AILERON AND RUDDER TRIM FUNCTION, MANUAL CONTROL FAIL TOO, AIRCRAFT AIR TURN BACK. ON GROUND FOUND DRIVE LINKAGE DETACHED, AFTER SECURE AND PERFORM RIGGING CHECK, NORMAL.SDR QXEA0200512Rod End · brokenPDX - RT AILERON POSITION SYNCHRO PUSH PULL ROD END BROKEN OFF. REPLACED SYNCHRO PUSH PULL ROD.SDR DBC2002F00001Indicator · failedSHORTLEY AFTER TAKEOFF, PILOT NOTED THAT THE AILERON TRIM INDICATOR FAILED. PILOT RETURNED TO AIRPORT WITHOUT INCIDENT. T/S TO FAILED INDICATOR. REPLACED INDICATOR (PN 6608217-11) (SN 879) OFF, (SN 372) ON. OPS CHECKED OK. DBCA-122DSDR 02FDEA00200Aileron · illuminated02-67 AILERON DEFLECT DISAGREE ALERT CAME ON IN FLT. DIVERT TO RCTP DUE TO INCREASE FUEL BURN. ** S/D ** COMINGSDR CA020326007Control Cable · failed(CAN) DURING ROUTINE INSPECTION FOUND RT WING OUTBOARD AILERON CONTROL CABLE RUBBING AGAINST TOP AILERON FUEL SYNC TRANSMITTER LINK. FURTHER DETAIL INSPECTION DISCOVERED AILERON DUAL SYNC TRANSMITTER LEVER INSTECTED APPROX 180 DEG. OUT OF NORMAL POS. PERFORMESDR 2002FA0000371Cable · wornDURING A ROUTINE INSPECTION THE RIGHT AND LEFT FORWARD STABILATOR CABLE WERE FOUND WORN AND FRAYED. THE AILERON RIGHT AND LEFT BALANCE CABLES WERE ALSO FOUND IN A SIMILAR CONDITION. THE WORN AND FRAYED PARTS OF THE CABLES WERE FOUND AT PULLEYS FAIRLEADS OR ASDR 2002FA0000370Control Cable · wornDURING A ROUTINE INSPECTION THE RIGHT AND LEFT FORWARD STABILATOR CABLE WERE FOUND WORN AND FRAYED. THE AILERON RIGHT AND LEFT BALANCE CABLES WERE ALSO FOUND A SIMILAR CONDITION. THE WORN AND FRAYED PARTS OF THE CABLES WERE FOUND AT PULLEYS FAIRLEADS OR ANY SDR 02FDEA00198Aileron · malfunctionedAFTER T/O RIB HAD DEFLECTED AILERON DISAGREE ALERT C/W RED TABS. MX DEF DEFLECTED AILERON SYS PER IAW MEL 27-2, PER METHOD A AILERON RETRACTED UP.SDR AUS20020273Link · cracked(AUS) AILERON CONTROL LINK CRACKED AT WELDED JOIN.SDR AUS20020272Link · cracked(AUS) AILERON CONTROL LINK CRACKED IN WELD JOIN.SDR DL764020247Actuator · crackedON LAYOVER, FOUND LT OUTBOARD AILERON ACTUATOR CRACKED. REPLACED SAME.SDR F3LA200200106Cartridge · defectiveUPON ARRIVAL, FLIGHT CREW REPORTED AILERONS BECAME EXTREMELY TIGHT AND FELT AS IF IN MANUAL REVERSION. HYDRAULIC SYSTEM PRESSURES WERE BOTH NORMAL. RUDDER AND ELEVATOR FELT NORMAL. ACCOMPLISHED NORMAL LANDING. REPLACED AILERON SPRING CARTRIDGE PER MM 27-11SDR AUS20020382Control Rod · cracked(AUS) LT AND RT AILERON CONTROL LINKS CRACKED. FOUND IAW AD/M20/52 & MOONEY SB M20-264.SDR 2002FA0000374Cable · wornDURING A ROUTINE INSPECTION THE RIGHT AND LEFT FORWARD STABILATOR CABLES WERE FOUND WORN. THE LEFT AILERON BALANCE CABLE WAS ALSO FOUND IN A SIMILAR CONDITION. THE WORN PARTS OF THE CABLE WERE FOUND AT PULLEYS, FAIRLEADS.SDR CA020225001Bearing · corroded(CAN) R/H AILERON FOUND WITH EXSCESSIVE UP AND DOWN PLAY.PLAY WAS CAUSED DUE TO R/H AILERON TERMINAL BELLCRANK BEARING WORN.BALL INSIDE BEARING WAS FOUND HEAVILY CORRODED AND OUT OF SHAPE.SDR DLM88020230Link · looseON APPROACH AILERONS JAMMED -REPLACED THE LEFT AILERON I/B CRANK ASSY FOR EXCESSIVE PLAYSDR XNOA01038Connector · looseAFTER TAKEOFF LT LO SPEED AILERON INDICATION SHOWS NOT DISCONNECTED. CONNECTED LOOSE CONNECTOR AT LT LO SPEED AILERON DISCONNECT ACTUATOR. OPS CHECKS GOOD ON GROUND AND FLT MODE, IAW A300 MM 27-11-00.SDR CA020221010Aileron · frozen(CAN) "AT 24,000 FEET DURING CLIMB LEFT AILERON CONTROL FROZE - LIGHT PRESS UNSTUCK CONTROL". VERBAL REPORT FROM PILOT STATES: "PUDDLES OF WATER ON TAXI/RWY WHEN LEAVING MEMPHIS. DID NOT HAVE CONTROL OF AILERON AT 24,000 FEET & MINUS 20 DEG C. DISCONNECTED AILSDR HALA0200045Actuator · failedFLT 932 - HNL - DURING TAXI, FOUND LEFT AILERON NOT SHOWING FULL DEFLECTION ON SPI. REMOVED LEFT OUTBOARD ACTUATOR PER MM 27-13-02. INSTALLED LEFT OUTBOARD ACTUATOR PER MM 27-13-02 STEP 3B. FINISHED STEP 15-20. LVDT NULLED AND A/P ROLL FOR LVDT CHECK OK PESDR CA020211011Actuator · failed(CAN) AP TRIM RWD CAUTION POSTED ON EICAS. DISCONNECTED AP AND FOUND AILERON SYSTEM JAMMED. OVERPOWERED SYSTEM ACC. CHECKLIST AFTER SEVERAL ATTEMPTS. SUDDENLY SYSTEM GOT FREE AGAIN. VISUALLY INSPECTED AILERON SYSTEM CABLES AND PULLEYS FOR SIGN OF JAMMING NO FISDR G1X2002F00001Bracket · bentFDR POTENTIOMETER BRACKET INTERFERING WITH AILERON ACTUATOR AT FULL TRAVEL, BRACKET IS MOUNTED TOO FAR FORWARD DUE TO .1250 SHIM USED BETWEEN AFT SPAR AND THE BRACKET. SHIM SHOULD BE REMOVED AND POTENTIOMETER ADJUSTED FOR NEW POSITION. SHIELD SHOULD ALSO BE SDR AUS20020039Pcu · faulty(AUS) RT INBOARD AILERON POWER CONTROL UNIT (PCU) FAULTY.SDR CA020130001Control Cable · worn(CAN) AILERON CABLE WORN BEYOND LIMITS.SDR CA020116002Bushing · worn(CAN) BUSHING WAS FOUND TO BE ROTATING IN BELLCRANK ASSEMBLY.SDR COMA0260026Circuit BreakerFLIGHT 5763 AILERON CONFIG WARNING DURING T/O.RESET TRIPPED AILERON CIRCUIT BREAKER.SDR UPS02237545Crankshaft · corrodedINSPECTION TYPE:C AILERON PCU INPUT CRANK IN LT WHEEL WELL IS BADLY CORRODED AROUND PIVOT BOLT. PCU INPUT CRANK REPLACED IAW OHM 27-40-00 & OHM 29-00-00.SDR COMA0160968Servo · draggingFLIGHT #5965 - AP RWD AND LWD MESSAGE ON EICAS. AILERON CONTROL BINDING.COULD NOT DUPLICATE. REPLACED THE AILERON SERVO FOR TROUBLE SHOOTING.SDR CA020130002Control Cable · worn(CAN) AILERON CABLE WORN BEYOND LIMITS.SDR COMA0160969Control Panel · stuckFLIGHT 5281 AILERON TRIM STICKING INTERMITTENTLY.REPLACED THE AILERON/RUDDER TRIM CONTROL PANEL.SDR COMA0110162Control Panel · stuckFLIGHT 5281 AILERON TRIM STICKING INTERMITTENTLY.REPLACED THE AILERON/RUDDER TRIM CONTROL PANEL.SDR QXEA0102079Pulley Bracket · corrodedPDX - AILERON CABLE PULLEY BRACKET IS CORRODED AROUND LOWER BOLT HOLE IN LEFT HAND WHEEL WELL. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8, PARAGRAPH 3C4.SDR WRLA200121Aileron · malfunctionedAILERON DEFLECT DISAGREE LEVEL 2 ALERT, AIRCRAFT RETURNED TO ATL. RAN FLAPS THROUGH 28 DEGREES. NO AILERON DEFLECTION NOTED. (M)SDR WRLA200120Actuator · failedAIRCRAFT HAS AILERON CONTROL PROBLEM. AIRCRAFT RETURNED TO SNN WERE THE AILERON SYSTEM WAS CHECKED. REMOVED AND REPLACED AILERON DEFLECTION ACTUATOR OUTBOARD. FOLLOW PROCEDURE IAW MM 27-43-00 RTS TEST FCC 1/FCC 2 ALL PASSED. OPS CHECK MM. NO FAULTS. (M)SDR 2001FA0000588Control Cable · wornDURING A ROUTINE INSPECTION, SUBSTANTIAL WEAR WAS FOUND WHERE THE AILERON BALANCE CABLE RUNS THROUGH THE RIGHT SIDE OF THE FUSELAGE. CABLE WEAR WAS PROBABLY CAUSED BY IMPROPER CABLE ALIGNMENT DURING ASSEMBLY BY MFG. THIS IS THE SECOND OCCURRENCE OF THIS TYPESDR P5CA0100614Aileron · delaminatedR/H OUTBD AILERON TOP CENTER HONEYCOMB PANEL TOP SKIN DELAMINATED 5' FROM I/B END, APPROX. 15" DIA. REMOVED & REPLACED R/H OUTBD AILERON PER MM 27-11-02SDR COMA0160874Trim Switch · inoperativeFLIGHT #5464. AILERON TRIM WOULD NOT WORK.REPLACED THE TRIM CONTROL PANEL.SDR AUS20011170Control Rod · bent(AUS) LT AILERON CONTROL ROD BENT. SUSPECT CAUSED BY WIND GUST.SDR IU62001F00013Manifold · crackedMANIFOLD IS CRACKED AROUND THE FILTER BOWL AREA.SDR 01FDEA00940Actuator · failed01-356 ON T/O UPON FLAP RETRACTION RECEIVED LEVEL 2 DEFLECTED AILERON DISAGREE ALERT. ** S/D ** COMINGSDR 2001FA0000521Control Cable · corrodedCONTROL CABLES FOUND TO HAVE CORRODED END FITTINGS AS DESCRIBED IN NTSB LETTER OF APRIL 16, 2001 TO FAA. AILERON, RUDDER,AND STABILATOR CABLES ALL REPLACED WITH NEW. MECHANIC NEEDS TO USE A LOW POWER(5X OR 10X) MAGNIFING GLASS TO SEE PITTING CLEARLY.SDR AUS20011159Gearbox · faulty(AUS) RT AILERON GEARBOX OUTPUT CRANK FAILED TO RESPOND TO FLAP POSITION.SDR CA011121015Bearing · failed(CAN) CREW REPORTED AILERON JAMMED IN FLIGHT, QRH CARRIED OUT SYSTEM CHECK SERVICEABLE ON THE GROUND BUT THE AIRCRAFT WAS FERRIED BACK TO MONTREAL FOR FURTHER INVESTIGATION. AN FMR TO REMOVE THE LEFT END AFT AILERON QUADRANT WAS ORDERED DUE TO THE FACT THAT A SDR SWIA200110336Control Cable · wornLEFT AILERON UPPER AND LOWER CABLES WORN ON WING. REPLACED LEFT UPPER AND LOWER AILERON CABLES IAW EMB120 MM 27-00-01.SDR SWIA200110334Control Cable · wornUPPER AND LOWER AILERON CABLES WORN AT INBOARD NACELLE FAIRLEADS, RIGHT SIDE. REPLACED RIGHT UPPER AND LOWER AILERON CABLES IAW EMB120 MM 27-00-01.SDR UPS01237237Tab Hinge · corrodedINSPECTION TYPE:C L/H INBD AILERON TAB O/B HINGE CORRODED. HINGE REPLACED IAW OHM 57-50-11SDR UPS01237211Lever · corrodedINSPECTION TYPE:C LT W/W AILERON PCU, LINKAGE/CRANK TO TAB DRUM IS BADLY PITTED. LEVER ASSY REMOVED IAW OHM 27-17-01, NEW LEVER ASSY INSTALLED IAW OH M 27-17-01 FASTENERS INSTALLED IAW SRM 51-30-02
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