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 CA991027012Control Cable · damaged(CAN) WHILE C/W SB 8-27-78, THE INBOARD UPPER LEFT AILERON CABLE WAS FOUND BLENDED BETWEEN PULLEYS AT STATION Y178. CABLE REPLACED. SUBMITTER STATED NOT KNOWN IF ORIGINAL EQUIPMENT.Oct 8, 1999 · Dhav DHC8311SDR AU991096Control Cable · worn(AUS) RIGHT AILERON CABLE WORN DUE TO CONTACT WITH THE PHENOLIC RUBBING BLOCK LOCATED OUTBOARD OF THE RIGHT FLAP ACTUATOR.Oct 4, 1999 · Cessna 172RSDR AU991079Control Cable · worn(AUS) RIGHT AILERON CABLE WORN ON PHENOLIC BLOCK.Oct 4, 1999 · Cessna 172RSDR 99ZZZX3925Control Cable · frayedONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND WITH FRAYED AILERON CABLES. LOCATION OF THE DAMAGE IS AT PULLEYS PN 62713-02 AND PN 62713-04. CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPED WITH A CLOTH, SMALL STRANDOct 4, 1999 · N925ER · Piper PA44180SDR 99ZZZX3924Control Cable · frayedONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND WITH FRAYED AILERON CABLES. LOCATION OF THE DAMAGE IS AT PULLEYS PN 62713-02 AND PN 62713-04. CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPED WITH A CLOTH, SMALL STRANDOct 4, 1999 · N925ER · Piper PA44180SDR 99ZZZX3923Control Cable · frayedONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND WITH FRAYED AILERON CABLES. LOCATION OF THE DAMAGE IS AT PULLEYS PN 62713-02 AND PN 62713-04. CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPED WITH A CLOTH, SMALL STRANDOct 4, 1999 · N925ER · Piper PA44180SDR 99ZZZX3922Control Cable · frayedONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND WITH FRAYED AILERON CABLE. THE LOCATION OF THE DAMAGE IS AT PULLEYS, PN 62713-02 AND PN 62713-04. THE CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPED WITH A CLOTH, SMALOct 4, 1999 · N926ER · Piper PA44180SDR 99ZZZX3921Control Cable · frayedONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND WITH FRAYED AILERON CABLE. THE LOCATION OF THE DAMAGE IS AT PULLEYS, PN 62713-02 AND PN 62713-04. THE CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPED WITH A CLOTH, SMALOct 4, 1999 · N926ER · Piper PA44180SDR 99ZZZX3920Control Cable · frayedONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND WITH FRAYED AILERON CABLE. THE LOCATION OF THE DAMAGE IS AT PULLEYS, PN 62713-02 AND PN 62713-04. THE CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPED WITH A CLOTH, SMALOct 4, 1999 · N926ER · Piper PA44180SDR 99ZZZX3919Control Cable · frayedONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND TO HAVE FRAYED AILERON CABLES. THE LOCATION OF THE DAMAGE IS AT PULLEYS, PN 62713-02 AND PN 62713-04. CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPED WITH A CLOTH, SMALOct 4, 1999 · N920ER · Piper PA44180SDR 99ZZZX3918Control Cable · frayedONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND TO HAVE FRAYED AILERON CABLES. THE LOCATION OF THE DAMAGE IS AT PULLEYS, PN 62713-02 AND PN 62713-04. CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPED WITH A CLOTH, SMALOct 4, 1999 · N920ER · Piper PA44180SDR 99ZZZX3917Control Cable · frayedONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND TO HAVE FRAYED AILERON CABLES. THE LOCATION OF THE DAMAGE IS AT PULLEYS, PN 62713-02 AND PN 62713-04. CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPED WITH A CLOTH, SMALOct 4, 1999 · N920ER · Piper PA44180SDR 99ZZZX4063Manifold · crackedMANIFOLD ASSY IS CRACKED APPROXIMATELY 80 PERCENT OF THE FILTER PORT CIRCUMFERENCE AND EXTENDS THROUGH TO THE THREADED AREA. FATIGUE, MISHANDLED, OVERPRESSURED AND/OR OVERTORQUED.Oct 1, 1999 · Boeing 737*SDR 99ZZZX3852Control Cable · wornDURING A ROUTINE INSPECTION, THE MECHANIC FOUND A SUSPICIOUS AREA ON THE AILERON BALANCE CABLE AT THE OUTBOARD PULLEY, PN 62713-02. THERE ARE FOUR SIMILAR PULLIES WHERE THE CABLES EXIT THE FUSELAGE AND ENTER THE WING. THESE PULLIES WEAR ON THE CABLES AND CAUSep 28, 1999 · N923ER · Piper PA44180SDR 99ZZZX3851Control Cable · wornDURING A ROUTINE INSPECTION, THE MECHANIC FOUND A SUSPICIOUS AREA ON THE AILERON BALANCE CABLE AT THE OUTBOARD PULLEY, PN 62713-02. THERE ARE FOUR SIMILAR PULLIES WHERE THE CABLES EXIT THE FUSELAGE AND ENTER THE WING. THESE PULLIES WEAR ON THE CABLES AND CAUSep 28, 1999 · N923ER · Piper PA44180SDR 99ZZZX3850Control Cable · wornDURING A ROUTINE INSPECTION, THE MECHANIC FOUND A SUSPICIOUS AREA ON THE AILERON BALANCE CABLE AT THE OUTBOARD PULLEY, PN 62713-02. THERE ARE FOUR SIMILAR PULLIES WHERE THE CABLES EXIT THE FUSELAGE AND ENTER THE WING. THESE PULLIES WEAR ON THE CABLES AND CAUSep 28, 1999 · N923ER · Piper PA44180SDR 99ZZZX3849Control Cable · wornDURING A ROUTINE INSPECTION, THE MECHANIC FOUND A SUSPICIOUS AREA ON THE AILERON BALANCE CABLE AT THE OUTBOARD PULLEY, PN 62713-02. THERE ARE FOUR SIMILAR PULLIES WHERE THE CABLES EXIT THE FUSELAGE AND ENTER THE WING. THESE PULLIES WEAR ON THE CABLES AND CAUSep 28, 1999 · N923ER · Piper PA44180SDR CA991007003Control Cable · loose(CAN) PILOT REPORTED CONSIDERABLE FREE PLAY IN CONTROL YOKE ROLL CONTROL. CABLE LOOP IN BOTH COLUMNS UNDERTENSIONED AND ADJUSTED.Sep 23, 1999 · Dhav DHC8102SDR COMA9960530Control Panel · inopAILERON TRIM IS INOPERABLE. REPLACED TRIM PANEL.Sep 16, 1999 · N983CA · Cndair CL6002B19SDR MWEA99607Control Cable · frozenAILERONS VERY DIFFICULT TO MOVE DURING DESCENT, FEELS FROZEN. MTC FOUND ICE BUILD-UP IN LEFT WHEEL WELL FORWARD TOP OUTBOARD AILERON CABLE/PULLEY STACK. MTC REMOVED OBSTRUCTION AND CLEANED DRAIN.Sep 13, 1999 · N206ME · Doug DC932SDR CA991004052Rod · broken(CAN) DURING FLIGHT, A STUDENT PILOT EXPERIENCED LOSS OF CONTROL OF THE AIRCRAFT. TAKING CONTROL, THE INSTRUCTOR NOTICED THAT THE LEFT AILERON FAILED TO RESPOND TO CONTROL WHEEL INPUT. THE INSTRUCTOR LANDED THE AIRCRAFT SAFELY. MAINTENANCE DETERMINED THAT TSep 13, 1999 · Cessna 172KSDR AU990893Control Cable · misinstalled(AUS) AILERON CABLES INCORRECTLY INSTALLED AT LEFT AND RIGHT BELLCRANKS IN WINGS. CABLES CROSSED BETWEEN WING STATIONS 47.83 AND 73.50 AND ALSO BETWEEN WING STATIONS 122.50 AND 133.50.Sep 8, 1999 · Cessna 310RSDR MZZA99183Control Cable · brokenTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A BROKEN AILERON BUS CABLE WAS FOUND AROUND PULLEY, JUST FORWARD OF LEFT MLG WALKING BEAM. THE DAMAGED CABLE WAS REMOVED AND REPLACED PER B727 MM CHAPTER 27-10-71, 27-10-00 AND OPERATIONAL CHECK FOUND SSep 5, 1999 · N79745 · Boeing 727224SDR MZZA99181Control Cable · rustedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A RUSTED AILERON CABLE WAS FOUND ON LEFT WING TE CAVITY, FORWARD OF APU OF FIRE EXTINGUISHER BOTTLE. THE DAMAGED CABLE WAS REMOVED AND REPLACED PER B727 MM CHAPTER 27-10-71, 27-10-00 AND OPERATIONALLY CSep 5, 1999 · N79745 · Boeing 727224SDR 99ZZZX3847Tube · chafedRIGHT AILERON PUSH/PULL TUB FROM BELL CRANK TO RT AILERON RUBBING AFT SPAR TO THE POINT THAT WALL OF TUBE IS WORN ALMOST COMPLETELY THROUGH.Sep 2, 1999 · N1127J · Beech A36SDR CA991104009Transmitter · failed(CAN) AILERON POSITION TRANSMITTER ARM INCORRECTLY INSTALLED WHICH CAUSED THE ARM TO RUB ON AILERON CABLE.Sep 1, 1999 · Cndair CL6002B16SDR 99ZZZX3540Control Cable · failedJFK - FLT 301 - RIGHT INBOARD AILERON CABLE BROKEN, FOUND ON TRANSIT CHECK. REMOVED AND REPLACED CABLE ASSY IAW 27-10-0.Aug 29, 1999 · N908PG · Boeing 727276SDR UPS99830527Cylinder · failedINSPECTION TYPE:N/A, LOSS OF MAIN RESERVOIR HYDRAULIC FLUID. AILERON AND RUDDER MAN LIGHT ON, PRESSURE FLUCTUATED. RAN LOSS OF HYDRAULICS CHECKLIST, RECOVERED NORMAL GEAR, FLAPS, BRAKES, NW STEERING. FLT CONT NOTIFIED, DECLARED INFLIGHT EMERGENCY W/ATC. NORAug 28, 1999 · N703UP · Doug DC871FSDR CA990927012Control Cable · worn(CAN) DURING SCHEDULED INSPECTION, THE RIGHT UPPER FORWARD ROLL CONTROL CABLE WAS FOUND WORN BEYOND SERVICE LIMITS.Aug 28, 1999 · Dhav DHC8301SDR CA990915088Control Cable · frayed(CAN) DURING INSPECTION, AILERON CABLES WERE FOUND TO HAVE SEVERAL BROKEN STRANDS. CABLE REPLACED.Aug 20, 1999 · Dhav DHC3SDR 2000ZZZX668Arm · crackedPERFORMED POST-REMOVAL INSPECTION OF AILERON REVERSION MECHANISM AND SUPPORT LT SIDE DAMAGE DURING REMOVAL. REMOVED AND REPLACED AILERON REVERSION CONTROL SUPPORTS (LT FOUND CRACKED) IAW DC-8 SRM 51-3-4 AND EO NR 99-136 WITH APPROVED 8110-3 DATED 11-1-99. Aug 20, 1999 · N812TC · Doug DC8F55SDR MZZA99173Cables · rustedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO INBOARD AILERON TAB CONTROL CABLES WERE FOUND RUSTED IN LEFT MLG WW. THE DAMAGED CABLES WERE REMOVED AND REPALCED WITH NWE ONES PER B727 MM CHAPTER 27-10-00 AND OPERATIONAL CHECK NORMALLY. (M)Aug 18, 1999 · N79743 · Boeing 727224SDR 99ZZZM758Cables · rustedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO INBOARD AILERON TAB CONTROL CABLES WERE FOUND RUSTED IN LEFT MLG WW. THE DAMAGED CABLES WERE REMOVED AND REPALCED WITH NWE ONES PER B727 MM CHAPTER 27-10-00 AND OPERATIONAL CHECK NORMALLY. (M)Aug 18, 1999 · N79743 · Boeing 727224SDR EIA990191Spring · brokenDURING FLIGHT, THE FIRST OFFICERS CONTROL COLUMNS LATERAL MOVEMENT BECAME HEAVY WITH A CONSIDERABLE AMOUTN OF SLACK. A LOUD POPPING NOISE WAS HEARD FROM F/O'S FLOOR AREA. MAINTENANCE PERSONNEL FOUND THE AILERON SYSTEM LOAD LIMIT SPRING BROKEN. SPRING WAS REPAug 17, 1999 · N485EV · Boeing 747212BSDR AALA991167Cseu · defectiveMIA - FLT 973 - EN ROUTE MIA-GIG, AT CRUISE, APPROXIMATELY 2 HOURS INTO FLIGHT, THE EICAS MESSAGE 'SPOILERS' AND 'R YAW DAMPER' ILLUMINATED. AT THE SAME TIME THE EICAS MESSAGE 'AILERON LOCKOUT' WAS FLICKERING AND THEN BECAME A STEADY MESSAGE, MOMENTS LATER THAug 14, 1999 · N320AA · Boeing 767223SDR 99ZZZX3476Control Cable · brokenYOKE WAS ABOUT 10 DEGREES TO THE LEFT DURING LEVEL FLIGHT. PILOT REQUESTED AN ADJUSTMENT. AN ATTEMPT WAS MADE TO ADJUST CABLES, WHEN PLASTIC COVER WAS REMOVED BEHIND INSTRUMENT PANEL, THE ROD END THAT SCREWED INTO TURNBUCKLE WAS BROKEN AND THE AILERONS WERE Aug 1, 1999 · N3788F · Cessna 172HSDR 99ZZZX3312Manifold · crackedMANIFOLD IS CRACKED DOWN INSIDE BORE WHERE INNER BEAERING FOR INPUT SHAFT RIDES.Jul 26, 1999 · Boeing 737*SDR 99ZZZX3311Manifold · crackedMANIFOLD IS CRACKED DOWN INSIDE BORE WHERE INNER BEARING FOR INPUT SHAFT RIDES.Jul 26, 1999 · Boeing 737*SDR AT9900558Bracket · corrodedDURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND RT WING AILERON OUTBOARD PULLEY BRACKET CORRODED. REMOVED AND REPLACED RT WING AILERON OUTBOARD PULLEY BRACKET. RIGGED AILERON BUS CABLES AND OPERATIONAL CHECK GOOD IAW DC9 MM 20-16-0, 20-17-0, 27-10-0 PG 3Jul 14, 1999 · N832AT · Doug DC932SDR 99ZZZX2801Rivet · misinstalledAIRCRAFT EXPERIENCED OBSTRUCTION IN AILERON OPERATION. MAINTENANCE FOUND RIVETS FROM SB (PIPER) 702 STRIKING UPPPER WING SKIN. MAINTENANCE CORRECTED AND RETURNED AIRCRAFT TO SERVICE. PROBLEM RESTRICTED TO LEFT AILERON. KIT SUBJECT TO AD 81-10-04.Jul 11, 1999 · N3063K · Piper PA44180SDR QXEA9901443Mechanism · out of adjustPDX - WHILE PERFORMING CHECKS OF THE AILERON CONTROL SYSTEM, FREE PLAY WAS NOTED IN FIRST OFFICERS CONTROL WHEEL WHEN ROLLING FROM LEFT TO RIGHT. REPAIRED IAW HORIZON AIR EA 2-27-18.Jul 1, 1999 · N347PH · Dhav DHC8202SDR UPS99230015Support · corrodedINSPECTION TYPE:C CORROSION UNDER AFT AILERON LOCKOUT GEARBOX ATTACH BOLT (NUTSIDE) ON L/W O/B AILERON LOCKOUT FITTING. REPLACED AILERON LOCKOUT FITTING (SUPPORT) PER ER NR 99-5678.Jun 28, 1999 · N929UP · Boeing 72722CSDR CA990719034Bracket · cracked(CAN) FIRST OFFICER'S RUDDER PEDAL ATTACH BRACKET CRACKED. REPLACED. REFER TO FAA AD 89-14-02.Jun 23, 1999 · Doug DC932SDR F3LA99083Pcu · failedDEN - ON FINAL APPROACH, AT ABOUT 8,000 FT AND 10 MILES OUT, FIRST OFFICER INITIATED A RIGHT TURN TO FINAL COURSE. AILERON CONTROL BECAME EXTREMELY STIFF AND FIRST OFFICER COULD NOT ROLL AIRCRAFT OUT OF THE TURN, EVEN USING APPROX 80 LBS OF FORCE. CAPTAIN ASJun 21, 1999 · N270FL · Boeing 7372L9SDR 99ZZZM781Pcu · failedDEN - ON FINAL APPROACH, AT ABOUT 8,000 FT AND 10 MILES OUT, FIRST OFFICER INITIATED A RIGHT TURN TO FINAL COURSE. AILERON CONTROL BECAME EXTREMELY STIFF AND FIRST OFFICER COULD NOT ROLL AIRCRAFT OUT OF THE TURN, EVEN USING APPROX 80 LBS OF FORCE. CAPTAIN ASJun 21, 1999 · N270FL · Boeing 7372L9SDR DL733991393Bearing · failedAILERONS BINDING WITH FLAPS AT 5 DEG DURING CONTROL CHECK. FOUND AILERON CENTERING CAM BEARING FROZEN. REPLACED BEARING AND SYS OPS NORMAL.Jun 18, 1999 · N948WP · Boeing 737301SDR 9902135527Control Mixer · malfunctionedEN ROUTE DTW-SFO CLIMBING THROUGH FL180, CREW REPORTED UNCOMMANDED RIGHT AILERON MOVEMENT. AN EMERGENCY WAS DECLARED. THE FLIGHT DIVERTED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LATERAL CONTROL MIXER AND RIGGED THE AILERON CONTROL SYSTEMJun 18, 1999 · N527US · Boeing 757251SDR 99ZZZX2554Retainer · crackedUNIT RECEIVED WITH A BLOWN OUT FILTER CAP THAT APPARENTLY HAPPENED DURING FLIGHT. P/N 69-36588-1 IS MADE OF ALUMINUM ALLOY. REPLACED FILTER CAP WITH P/N 69-35688-2 WHICH IS MADE OF FERROUS MATERIAL.Jun 16, 1999 · Boeing 737*SDR CA990614081Actuator · failed(CAN) AILERON LOCK-OUT ON EICAS STATUS REPORT. LEFT AILERON ACTUATOR REPLACED.Jun 15, 1999 · Boeing 747433SDR DL76L991328Aileron Controls · fodON TAXI OUT DURING FLT CONTROL CK, COULD NOT GET FULL LEFT AILERON CONTROL WHEEL TRAVEL AND THE EICAS DISPLAY INDICATION WOULD NOT MOVE FULL SCALE. RETURNED TO GATE. PERFORMED BITE OF STCMS, CHECKED OK AND NO FAULT FOUND. DURING T/S FOUND A SMALL ROCK PEBBLJun 11, 1999 · N180DN · Boeing 767332
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