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.

SDR UPS01834906Aileron · bindingINSPECTION TYPE:IN AILERONS BINDING CYCLED AILERONS, POWER AND FLIGHT SPOILER HYDRAULIC PUMP AND CYCLED FLAPS, AILERONS, AND SPEEDBRAKES. OPS CK OK. NO BINDING FOUND. A/C OK FOR SERVICE. IAW MM 27-10-00Feb 7, 2001 · N874UP · Doug DC873FSDR UPS01234824Control Cable · lack of lubeINSPECTION TYPE: IN, AILERON BINDING (REPEAT W/U). TROUBLESHOT PER MM 27-10-00 PAGE 111 INSP CABLE AA & AB NO DEFECT NOTED LUB CABLE, OPS CHECK GOOD.Feb 1, 2001 · N937UP · Boeing 72725CSDR UPS01834773Control Cable · contaminatedINSPECTION TYPE: IN, AILERON POWER S/O LEVER FROZEN. CLEANED AND LUBED AILERON HYD S/O CABLES GOING THRU BULKHEAD IN LT W/W CABLES HAD BUILD UP OF ANTI CORROSION COMPOUND. SYS OPS CKS GOOD PER MM 27-10-00.Jan 25, 2001 · N868UP · Doug DC873FSDR 20010504AP007Actuator · failedLOW SPEED AILERON FAILED TO DISCONNECT IN AUTO AND MANUAL. DMI NR 1452 CLEARED BY REMOVING AND REPLACING OF AILERON PICKOFF PER 27-11-63 ALTERNATE PROCEDURE. OPS CHECK GOOD. (M)Jan 19, 2001 · N823SC · Airbus A300B4203SDR 2002FA0000160Wire Rope · wornLEFT AILERON BALANCE CABLE, DURING A ROUTINE INSPECTION, THE LEFT AILERON BALANCE CABLE WAS FOUND WORN WHERE THE CABLE PASSES OVER THE CENTER PULLEY IN THE MIDDLE OF THE FUSELAGE.Jan 16, 2001 · N4145R · Piper PA32300SDR 20010504AP009Actuator · inoperativeLOW SPEED AILERON FAILED TO DISCONNECT IN AUTO AND IN DISCONNECT POSITION AFTER SLAT RETRACTION. FUEL DUMPED, 40,000 LBS. AIRCRAFT RETURNED TO LOCKBORNE. LANDING NORMAL. ASSIGNED DMI NR 1452 IAW MEL 27-11-01, CAT ''B'' EXPIRES 1-18-01. LOCKOUT PROCEDURES Jan 15, 2001 · N823SC · Airbus A300B4203SDR 20010504AP008Actuator · failedLOW SPEED AILERON WOULD NOT DISCONNECT IN AUTO OR MANUAL. LEFT LOW SPEED AILERON ACTUATOR REMOVED AND SENT TO REPAIR FACILITY. ACTUATOR REINSTALLED AND OPS CHECKED GOOD IAW 27-11-47. AIRCRAFT RETURNED TO SERVICE. DMI NR 1442 CLEARED. (M)Jan 13, 2001 · N823SC · Airbus A300B4203SDR 20010129CW016Torque Tube · corrodedAFT AILERON SECTOR TORQUE TUBE CORRODED THE LENGTH OF THE TUBE BETWEEN THE UPPER AND LOWER BELLCRANKS.Jan 8, 2001 · N690QS · Cessna 560XLSDR CA010126003Control Cable · worn(CAN) DURING SCHEDULED INSPECTION, THE RT LOWER AILERON CABLE WAS FOUND TO BE WORN AND SPIKED IN AN AREA IMMEDIATELY OUTBOARD OF THE RT NACELLE. THE CABLE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. TTAF 22,210 HRS.TCAF 32,196 CYC.Jan 4, 2001 · Dhav DHC8311SDR UPS01834583Control Valve · bindingINSPECTION TYPE:N/A AILERON BINDING, DURING CONTROL CHECKS AILERON WOULD NOT RETURN TO NEUTRAL ON ITS OWN AFTER BEING DISPLACED TO THE RIGHT. RTB *S/D* REMOVED AND REPLACED RT AILERON POWER CYLINDER/CONTROL VALVE UP TO STEP B2 AGE 204 MM 27-11-06. OPS CK LJan 3, 2001 · N866UP · Doug DC873FSDR 0004595514Service difficultyON APPROACH, AILERON CONTROL DESCRIBED AS BINDING BADLY. ROLL CONTROL NOTED AS VERY UNRESPONSIVE WITH UNCOMMANDED ROLL OSCILLATIONS DURING LAST 200 FT OF LANDING. MAINTENANCE REPLACED BEARING IN THE AILERON FEEL AND TRIM MECHANISM. OPERATIONAL CHECK OK.Dec 29, 2000 · N514US · Boeing 757251SDR DHL2001724009Powerpack · stuckIN FLIGHT,FLIGHT CONTROL MOMENTARILY STICKS AT 15 DEGREES CONTROL WHEEL RIGHT REF LOG PAGE 199761. REPLACED AILERON POWER PACKAGE PER M/M 27-10-101 NO HELP PERFORMED ADJ TEST OPS CKS OK ENGINEERING FLIGHT PERFORMED OP CK OK NO DEFECTS NOTED.Dec 28, 2000 · N724DH · Boeing 727228SDR A6WA200000080Aileron · malfunctionedAILERON OUT OF TRIM LIGHT ON M/A TURNED OFF A/P MASTER SWITCH, ALL FLIGHT CONTROLS AND TRIM WORK OK. MAINTENANCE OPERATIONAL TEST OK, COULD NOT DUPLICATE.Dec 24, 2000 · N179US · Bag BAE146200ASDR 20010227CW003Control Cable · frayedAILERON BALANCE CABLE FRAYED ABOUT 8 INCHES FROM TURN BUCKLE, NEW CABLE INSTALLED.Dec 20, 2000 · N4142Q · Piper PA28181SDR SWIA972249Aileron · malfunctionedAILERON, RUDDER TRIM SHOW FULL SCALE DEFLECTIONS AND NO INDICATION OF FLAP EXTENSION SWAPPED BOTH FCC CARDS NO HELP PUT CARDS BACK IN ORIGINAL POSITION AC IS NOW DOWN GRADED TO CAT I DUE TO NON QUALIFIED MECHANIC WORKDec 20, 2000 · N423SW · Cndair CL6002B19SDR AU001204Control Cable · misinstalled(AUS) FORWARD LH FLAP RETRACTION CABLE AND RH AILERON CABLES CROSSEDOVER EACH OTHER UNDER THE FLOOR BEHIND THE LANDING GEAR BULKHEAD. FLAP AND AILERON CABLES INCORRECTLY FITTED TO BOTH LOWER OUTERAND LH AND RH PULLEYS BEHIND THE CABIN DOORS. AILERON CABLE STRADec 20, 2000 · Cessna 172ASDR AU001202Bracket · worn(AUS) UPPER AILERON BELLCRANK BRACKET WORN ON THE LOWER SIDE. THE WEAR WAS CAUSED BY THE BELLCRANK/CABLE ATTACHMENT CLEVIS PINS RUBBING.Dec 12, 2000 · Cessna 310RSDR CA010115004Actuator · failed(CAN) AILERON LOCKOUT IN CRUISE/LANDING/GATE.FOUND CIRCUIT BREAKER POPPED, RIGHT AND LEFT AILERON RESET, CARRIED OUT TEST. SPOILER AILERON MODULE FAULTED RIGHT HAND AILERON LOCKOUT. CIRCUIT BREAKER POPPED AGAIN. CHANGED RIGHT HAND AILERON LOCKOUT ACTUATOR.Dec 8, 2000 · Boeing 767233SDR AWXA0001019Servo · malfunctionedPHX - AIR TURNBACK - ON CLIMB OUT AND CRUISE AIRCRAFT HAD LEFT WING DOWN 5 TO 7 DEGREES AND RUDDER TRIM 2.8 DEGREES RT. MOST NOTICABLE AT 250 KTS. AND ABOVE; AT 210 KTS. CONDITION LESS NOTICABLE AND AT 170 KTS. FLAP 2 RUDDER TRIM WAS NORMAL AND AIRCRAFT WAS STDec 6, 2000 · N646AW · Airbus A320231SDR AALA20002020Bracket · misdrilledTUL - FOUND HOLES DRILLED IN RIGHT WING BRACKET D78803-403 ARE APPROX .25 INCH TOO HIGH PER ECO 50527FX PAGE 2 STP 9. AFTER INSTALLATION OF RIGHT AILERON DFDAU TRANSMITTER TURN BARREL ADJUSTED FOR CORRECT OCTAL READING THIS COMPENSATION FOR BRACKET MISLOCATIONov 29, 2000 · N1469D · Fokker F28MK0100SDR CA010102011Cable Guard · worn(CAN) DURING AN ANNUAL INSPECTION, WE HAVEFOUND A CABLE GUARD THAT WAS RUBBING ON THE AILERON MULTIPLIER REAR CABLE WHICH COMES FROM THE PILOTS SIDE CABLE. WE THEN CHECKED A/C 2017 AND FOUND THE SAME PROBLEM. WE WILL CARRY OUT AN INSPECTION OF ALL CL415.AT THINov 28, 2000 · Cndair CL2156B11415SDR 00FDEA00793Warning System · activatedDURING R/O CHECK GOT A DEFLECTED AILERON DISAGREE LEVEL 2 ALERT.Nov 28, 2000 · N604FE · Doug MD11FSDR F3LA200000260Spring · unserviceableDURING C-7 CHECK TEST FLIGHT, FLIGHT CREW REPORTED AILERONS STIFF IN MANUAL REVERSION. REPLACED AILERON CONTROL SPRING AND CHECKED OKAY.Nov 24, 2000 · N313FL · Boeing 7373L9SDR MASA00135Warning Light · illuminatedFLT 5793 - ROC-LGA - DIVERTED TO ISLIP NEW YORK WITH A AILERON ROLL DISCONNECT LIGHT ON. THE CREW DID NOT EXPERIENCE A DISCONNECT JUST A DISCONNECT LIGHT. AN UNEVENTFUL LANDING AT ISLIP. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. THE AIRCRAFT WAS RETOct 29, 2000 · N828MJ · Emb EMB145LRSDR SWIA972072Actuator · failedAILERON TRIM WHEEL FREEZES INFLIGHT IN NEGATIVE TEMPS. REPLACED AILERON TRIM ACTUATOR IAW MM 27-12-01. OPS CHECKS GOOD. P/N ON: 5301, S/N: 394, S/N OFF: 408.Oct 29, 2000 · N293SW · Emb EMB120ERSDR 2000UALA00624Aileron · jammedAT FL370 SAT-60C, AUTOPILOT EICAS MESSAGE AND LIGHT SHOWN. A/P DISCONNECTED, AILERONS APPEARED JAMMED. AILERONS REGAINED BY APPLICATION OF 50 - 75 POUND FORCE. FLIGHT CONTINUED AND LANDED UNEVENTFULLY.Oct 26, 2000 · N603UA · Boeing 767222SDR SWIA972046Connector · damagedCONT DISENGAGE LIGHT CAME ON, ON TAKEOFF ROLL. ABORTED TAKEOFF. FOUND BROKEN WIRE AT AILERON DISCONNECT CANNON PLUG BACKSHELL. REMOVED AND REPLACED PINS AT CANNON PLUG IAW MM 20-50-01. CONTROL DISENGAGE INDICATION OPS CHECKS GOOD.Oct 23, 2000 · N190SW · Emb EMB120ERSDR CA001101023Control Unit · faulty(CAN) AT 80 KTS DURING TAKEOFF ROLL, THE AILERON WARNING MSG APPEARED.THE FLIGHT CREW ABORTED TAKEOFF AT 85 TO 90 KTS. (UNEVENTFUL). AIRCRAFT WAS ROUTED TO THE HANGAR FACILITY FOR HIGH SPEED TAKEOFF INSPECTION AND AILERON INVESTIGATION. NO DEFECT NOTED, AIRCROct 20, 2000 · Cndair CL6002B19SDR CA001101021Aileron · failed(CAN) AP RWD MESSAGE. TRANSFERED TO MANUAL FLIGHT. ON FLIGHT CONTROL SYNOPTIC PAGE, ONLY THE LEFT AILERON WAS DEFLECTING. THERE WAS THE FEELING OF A BLOCKAGE. AFTER PILOT TOOK OVER, HEAVY JERK DURING A LEFT TURN AND NORMAL FLIGHT AFTER. AILERON MOVES AGAIN.Oct 20, 2000 · Cndair CL6002B19SDR COMA0060834Control Unit · malfunctionedCONFIG AILERON WARNING MESSAGE DURING T/O. RESET SECU, COULD NOT DUPLICATE. RESET SECU NR 1 AND 2.Oct 14, 2000 · N952CA · Cndair CL6002B19SDR RRXA001065Actuator · failedAS ACFT SPEED INCREASES ACFT WANTS TO ROLL TO THE RIGHT FLAPS/SLATS RETRACTED. REMOVED AND REPLACED RIGHT INBOARD AILERON ACTUATOR IAW DC-10 MM 27-13-01 PAGES 401 - 407. OPS AND LEAK CHECKS GOOD.Oct 11, 2000 · N68041 · Doug DC1010FSDR COMA0060808Warning System · false activationAILERON CONFIG WARNING DURING T/O. INSPECTED AILERONS AND TRIM SYSTEM, NO DEFECTS FOUND.Oct 7, 2000 · N781CA · Cndair CL6002B19SDR 20001025SH015Control Cable · frayedAILERON CONTROL CABLE FRAYED. (X)Oct 3, 2000 · N4128X · Piper PA34220TSDR HALA0000323Control Cable · brokenHNL - FLT 288 - AILERON INPUT CAUSES EXCESSIVE ROLL ON LANDING. FOUND FDR AILERON POSITION SENSOR CABLE BROKEN. REMOVED, REPLACED AND NULLED FDR AILERON SURFACE POS SENSOR. OPS CHECKED OK FOR SERVICE. (X)Oct 2, 2000 · N660HA · Doug DC951SDR 20001025SH011Control Cable · frayedRIGHT AILERON CABLE FRAYED. (X)Sep 29, 2000 · N4142N · Piper PA34220TSDR CA001019013Control Cable · broken(CAN) PILOT REPORTED ON WALKAROUND, ITEM STICKING OUT OF FLAP WELL, MAINTENANCE CALLED IN, DISCOVERED BROKEN CABLE STRANDS AT STATION YW 174 AT THE FAIR LEAD. ITEM WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.Sep 26, 2000 · Dhav DHC8*SDR 20000927SH003Pulley · burredWHILE PERFORMING SB 00-27-02, DATED AUGUST 14, 2000, TO INSPECT FOR PROPER RADIUS WHERE INTERCONNECT CABLE IS ATTACHED TO QUADRANT, AILERON CABLE 0510105-328 WAS FOUND SEVERELY WORN. CABLE WEAR WAS WHERE CABLE CONTACTED PULLEY GROOVE (OUTER SECTION OF 1260112Sep 26, 2000 · N543MC · Cessna 182SSDR 20001026SH007Cable Guard · inaccurateDURING THE INITIAL INSPECTION OF THE AILERON INTERCONNECT CABLE QUADRANT (RT AND LT) IAW CESSNA SB SB00-27-02, IT WAS DETERMINED THE REQUIRED RADIUS AROUND THE EDGE OF THE HOLE WHERE THE INTERCONNECT CABLE PASSES WAS NOT PRESENT. SUBSEQUENT INSPECTION OF THE Sep 25, 2000 · N7273Q · Cessna 206HSDR 20001026SH006Cable Guard · inadequateDURING INITIAL INSPECTION OF THE AILERON INTERCONNECT CABLE QUADRANTS (RT AND LT) IAW CESSNA SB SB00-27-02, IT WAS DETERMINED THE REQUIRED RADIUS AROUND THE EDGE OF THE HOLE WHERE THE INTERCONNECT CABLE PASSES WAS NOT PRESENT. SUBSEQUENT INSPECTION OF THE INTSep 25, 2000 · N7273Q · Cessna 206HSDR CA001122003Control Unit · failed(CAN) EN ROUTE CREW REPORTED AILERONS WERE STIFF, BEYOND 5 DEGREES INPUT WITH AUTOPILOT SELECTED OFF. AUTOPILOT ON AILERONS WERE BETTER. AIRCRAFT TAKEN OUT OF SERVICE FOR TOURBLESHOOTING. AILERON POWER CONTROL UNIT RIGGING CARRIED OUT AS PER WORK CARD 51143, ISep 20, 2000 · Boeing 737296SDR 20001026SH005Cable Guard · inadequateDURING INITIAL INSPECTION OF THE AILERON INTERCONNECT CABLE QUADRANTS (RT AND LT) IAW CESSNA SB SB00-27-02, IT WAS DETERMINED THE REQUIRED RADIUS AROUND THE EDGE OF THE HOLE WHERE THE INTERCONNECT CABLE PASSES WAS NOT PRESENT. SUBSEQUENT INSPECTION OF THE INTSep 20, 2000 · N7281M · Cessna 206HSDR 20001026SH004Cable Housing · inadequateDURING INITIAL INSPECTION OF THE AILERON INTERCONNECT CABLE QUADRANTS (RT AND LT) IAW CESSNA SB SB00-27-02, IT WAS DETERMINED THE REQUIRED RADIUS AROUND THE EDGE OF THE HOLE WHERE THE INTERCONNECT CABLE PASSES WAS NOT PRESENT. SUBSEQUENT INSPECTION OF THE INTSep 20, 2000 · N7281M · Cessna 206HSDR 20001019SH019Control Cable · frayedLEFT HAND AILERON BALANCE CABLE FRAYED, LOCATED UNDER THE REAR SEATS. (X)Sep 18, 2000 · N4175V · Piper PA28181SDR 20001019SH018Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED. (X)Sep 18, 2000 · N4177R · Piper PA34220TSDR 20001018SH007Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED AT WING ROOT PULLEY. (X)Sep 14, 2000 · N9299E · Piper PA34220TSDR 20001017SH002Control Cable · frayedDURING A ROUTINE INSPECTION, THE LEFT AILERON BALANCE CABLE WAS FOUND FRAYED BY THE LEFT WING ROOT RIB. (X)Sep 14, 2000 · N4145X · Piper PA28181SDR 20010116SG003Actuator · failedMEL 27-11-01 ON AIRCRAFT LOW SPEED AILERON. MEL CLEARED. REMOVED AND REPLACED SERVO CONTROL ACTUATOR. ALSO, FOUND DAMAGED WIRES AND REPAIRED SAME IAW MM 20-53-29. OPS CHECK GOOD IAW MM 27-11-00. AIRCRAFT RETURNED TO SERVICE. (M)Sep 13, 2000 · N820SC · Airbus A300B4203SDR SWIA971982Aileron · fodON APPROACH AILERONS WERE BINDING WHEN DEFLECTED RIGHT OR LEFT. FOUND SCREW TRAPPED BETWEEN INNER AILERON AND WING SURFACE, INNER ROOT OF LEFT AILERON. REMOVED SCREW, INSPECTED AFFECTED AREA, NO DAMAGE FOUND. FUNCTIONAL CHECK OF AILERON TRAVEL OK ON GROUNDSep 13, 2000 · N1105G · Emb EMB120RTSDR 20010117SG002Controller · malfunctionedAFTER TAKEOFF, L/N LOW SPEED AILERON WOULD NOT DISCONNECT AND POPPED CB 7A6. CREW ACCOMPLISHED PROCEDURE A 29 AND RETURNED TO LAX AT A SPEED OF LESS THAN 250 KNOTS. NO FUEL WAS DUMPED. AIRCRAFT LANDED NORMAL. AILERON WAS INOPERABLE IN AUTO MODE ONLY AND PLSep 8, 2000 · N820SC · Airbus A300B4203SDR CA001002007Pcu · failed(CAN) FLIGHT CREW REPORTED THE A/C WANT TO ROLL TO THE RIGHT, REQUIRED EXCESSIVE TRIM LWD TO MAINTAIN FLIGHT LEVEL. MAINTENANCE REPLACED THE R/H AILERON PCU CONNECTING HARDWARE.Sep 4, 2000 · Cndair CL6002B19
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