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 MALA040145Control Cable · looseDURING POST FLIGHT 3351, CONTROL COLUMN REQUIRES EXCESSIVE FORCE TO BANK AIRCRAFT TO THE LEFT. DOES NOT SPRINGLOAD BACK TO POSITION ON GROUND. MAINTENANCE FOUND LT AILERON CABLE TENSION LOW. ADJUSTED CABLE TENSION WITHIN LIMITS IAW AMM 27-11-00-2. LUBED LTJan 25, 2004 · N362PX · Saab 340BSDR AUS20040041Gearbox · faulty(AUS) RT INBOARD AILERON ANGLE GEARBOX FAULTY.Jan 24, 2004 · Boeing 767338SDR CA040225005Control Cable · frayed(CAN) CABLE FRAYED AT PULLEY AREA. WING ROOT PULLEY WAS NOT SEIZED.Jan 21, 2004 · Cessna 180CSDR CA040204005Control Cable · frayed(CAN) AILERON DIRECT CABLE LT AND RT FRAYED EACH IN 3 DIFFERENT PLACES AT PULLEYS, PULLEYS WERE NOT SEIZED, ROTATES FREELY, ALSO FRAYED AILERON CARRY THROUGH CABLE P/N 0510105-113 AT PULLEY AREA.Jan 21, 2004 · Cessna 180CSDR MYNR748KControl Tube · wornAILERON CONTROL SHAFT, WHERE IT MOUNTS TO FIREWALL BEARING WAS RUSTED AND GROVED BEYOND LIMITS, REPLACED LT AND RT SHAFTS AND BEARINGS. BEARING PN 0760633-1 END.Jan 14, 2004 · N3231T · Cessna 177SDR QXEA200400007Actuator · failedAFTER TAKEOFF FROM SEA, THE A/C HAD A SLIGHT ROLLING MOTION TO THE RT. THE CONTROLS FELT HARD TURNING TO THE LT. THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RT AILERON TRIM TAB SPRINGS AND THE AILERON TRIM ACTUATOR. Jan 10, 2004 · N358PH · Dhav DHC8202SDR CA040106011Control Cable · contaminated(CAN) WHILE TAXING DURING FLT CONTROL CHECK FOUND AILERONS NOT RETURNING TO NEUTRAL. AFTER INVESTIGATION FOUND WHEEL WELL CONTAMINATED WITH DIRT AND MOISTURE. AREA CLEANED AND LUBRICATED.Jan 4, 2004 · Cndair CL6002B19SDR 03353644Pulley · dirtyDURING OPERATIONAL OF AIRCRAFT CREW REPORTED DIFFICULTY UTILIZING THE AILERON CONTROLS. MAINTENANCE PERSONNEL FOUND HEAVY DEPOSITS OF DIRT ON THE CONTROL CABLES AND PULLEYS. THE CABLES AND PULLEYS WERE CLEANED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMDec 19, 2003 · N644BR · Cndair CL6002B19SDR DXTA200300201Control Cable · frayedPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED AGAINST WING ACCESS COVE ASSEMBLY, FOUND ALL FOUR CABLES FRAYED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XDec 16, 2003 · N621QS · Cessna 560XLSDR 2003FA0001246Link · mismanufacturedWHILE RIGGING AC, USING TORQUE SPEC FROM MFG MM. AILERON FINAL CONTROL LINK THREADS WERE DESTROYED WHILE ATTEMPTING TO REACH LOW END OF SPECIFIED TORQUE (REF MFG MM CHAP 27, SECT 27-10, B., STEP 9). THE MFG WAS NOTIFIED OF THIS SITUATION AND RESPONDED WITH: Dec 16, 2003 · Lancar LC40550FGSDR DXTA200300196Control Cable · brokenPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Dec 12, 2003 · N663QS · Cessna 560XLSDR DHL2003802578Mechanism · crackedRIGHT WING INBD AILERON MANUAL REVERSION MECHANISM CRACKED. REMOVED AND REPLACED MANUAL REVERSION MECHANISM AT RIGHT WING INBD AILERON IAW MM 27-11-8 PG 401-404. PERFORMED ADJUSTMENT TEST, GOOD IAW MM 27-10-0 PAGES 510 THRU 515. SEE NR 1456 FOR OPS CHECK.Dec 11, 2003 · N802DH · Doug DC873SDR CA031212004Control Cable · out of adjust(CAN) CONTROL WHEEL VERY STIFF WHEN DEFLECTED LT AND SLOW TO RETURN ON RT DEFLECTION. LOST MOTION CABLES ADJUSTED IAW MM 27-10-0 AILERON INPUT PUSHROD ADJUSTED IAW MM 27-10-0CENTERING PUSHROD ADJUSTED A PER MM 27-10-0 SPOILER MIXER CONTROL ROD ADJUSTED MM 27-6Dec 9, 2003 · Boeing 727243SDR GSB2004F00000Rod End · wornDURING 100 HR INSPECTION, THE FORWARD AILERON ROD ENDS REQUIRED REPLACEMENT. AFTER REMOVAL OF AILERON ROD ASSY. THE FORWARD ROD END. THEREADED SHANK WAS FOUND TO BE BROKEN IN HALF IN THE AREA WHERE A ROLL PIN IS INSTALLED INSTEAD OF A JAM NUT. WHICH THE AFDec 5, 2003 · N107TA · Piper PA32300SDR 2003FA0001238Pushrod Tube · corrodedFOUND BOTH AILERON OB PUSH ROD TUBES RUSTING INTERNALLY. IF RUST IS NOTICED ON EXTERIOR OF TUBE, IT IS ALREADY AT POINT OF FAILURE. TT 5140 HRS RECOMMEND REPLACING BOTH AILERON PUSH ROD TUBE ASSEMBLIES ON ANY AC WHICH HAVE NOT BEEN REPLACED IN PAST FIVE YEADec 1, 2003 · N231PF · Mooney M20KSDR DXTA200300192Control Cable · chafedPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 29, 2003 · N641 · Grumav G21ASDR CA031212002Control Cable · misrigged(CAN) AILERON CTRL CABLES FOUND TO BE INCORRECTLY ROUTED AT OB CNTL QUADRANTS ON BOTH WINGS, UNDER ACCESS PANELS 532AT AND 632AT. IT WAS ONLY DUE TO OTHER AILERON MAINT THAT PANELS 532AT, 632AT WERE LIFTED TO FACILITATE RIGGING CHECKS. INCORRECT ROUTING ISSUNov 27, 2003 · Dhav DHC8301SDR AUS20031241Control Cable · inoperative(AUS) LT AND RT WING AILERON CONTROL CABLES INCORRECTLY ROUTED AT OUTBOARD CONTROL QUADRANTS ON BOTH WINGS UNDER PANELS 532AT AND 632AT. CABLES HAD NOT BEEN LOCATED IN THE QUADRANT GROOVE AND WERE OPERATING ON TOP OF THE QUADRANT CAUSING RUBBING ON THE QUADRANNov 27, 2003 · Dhav DHC8315SDR DXTA200300188Control Cable · brokenPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 27, 2003 · N628QS · Cessna 560XLSDR DXTA200300189Control Cable · chafedPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 27, 2003 · N630QS · Cessna 560XLSDR 2003FA0001266Control Cable · damagedDURING A PHASE 5 AIRFRAME INSPECTION, THE RT SIDE AILERON CABLES WERE FOUND TO BE RUBBING THE RT SPOILER ACTUATOR HYDRAULIC LINE. THE DAMAGED AREAS ON THE CABLES WERE AT RT WING STA 266 ON THE AFT SIDE OF THE WING REAR SPAR. THE PROTECTIVE SLEEVES ON THE CABNov 26, 2003 · N559AM · Cessna 650SDR DXTA200300191Control Cable · brokenPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 26, 2003 · N637QS · Cessna 560XLSDR DXTA200300186Control Cable · chafedPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 26, 2003 · N695QS · Cessna 560XLSDR DXTA200300183Control Cable · chafedPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 26, 2003 · N684QS · Cessna 560XLSDR DXTA200300195Control Cable · brokenPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 25, 2003 · N652QS · Cessna 560XLSDR DXTA200300182Control Cable · brokenPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 25, 2003 · N671QS · Cessna 560XLSDR SWIA200312722Control Unit · malfunctionedRT AILERON CONTROL HAS (UNUSUAL FEELING), CLICKING NOISE. (DISCOVERED DURING C-CHECK INSPECTION) SERVICE LETTER NR RJ-SL-27-045 COMPLIED WITH IAW CRJ AMM 27-11-05-420-001 PARAGRAPH 11.Nov 24, 2003 · N423SW · Cndair CL6002B19SDR DXTA200300193Control Cable · brokenPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LT AND RT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 24, 2003 · N645QS · Cessna 560XLSDR DXTA200300190Control Cable · brokenPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 24, 2003 · N632QS · Cessna 560XLSDR DXTA200300185Control Cable · chafedPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 23, 2003 · N692QS · Cessna 560XLSDR DXTA200300181Control Cable · chafedPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LT AND RT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 23, 2003 · N668QS · Cessna 560XLSDR DXTA200300184Control Cable · chafedPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 22, 2003 · N690QS · Cessna 560XLSDR 206541Aileron · malfunctionedFLT NR 4568 FROM LYH TO PIT. ON TAKE-OFF, AFTER PASSING CONTROL OF AIRCRAFT FROM CAPTAIN TO FIRST OFFICER. AIRCREW EXPERIENCED GRINDING IN AILERONS. AIRCREW ABORTED TAKE-OFF AND RETURNED TO GATE.Nov 21, 2003 · N40SZ · Saab SF340ASDR CMR2003F00000Rod · brokenIMMEDIATELY AFTER TAKE OFF, THE PILOT NOTICED MINIMAL REACTION FROM AILERON CONTROL INPUTS. PILOT LANDED SAFELY. INVESTIGATION REVEALED LT AILERON DISCONNECTED FROM CONTROL ROD. FOUND THAT CONTROL ROD HAD BROKEN IN THREADED AREA JUST FORWARD OF AILERON CONTNov 17, 2003 · N35561 · Cessna 206HSDR IXXA0300077SBracket · crackedDURING A ROUTINE B-CHECK INSPECTION MAINTENANCE FOUND RT AILERON INBOARD CONTROL TAB CABLE BRACKET CRACKED. AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE REMOVED AND REPLACED INBOARD AILERON, RT AILERON MANUAL REVERSION CONTROL ROD, 5Nov 17, 2003 · N828BX · Doug DC871FSDR DXTA200300187Control Cable · chafedPERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.Nov 15, 2003 · N699QS · Cessna 560XLSDR CA031113008Control Cable · frayed(CAN) DURING A SCHEDULE INSPECTION ON RT WING OB FLIGHT SPOILER. THE OB RT SPOILER ACTUATING CABLE (FOR THE FLT SPOILER ACTUATOR) WAS FOUND FRAYED UNDER A PULLEY ASSY.Nov 13, 2003 · Cessna 650SDR CA031113014Control Cable · broken(CAN) PILOT REPORTED CONTROL FELT DIFFERENT DURING LANDING. MAINT FOUND RT WING AILERON CABLE ASSY WING UP, BROKEN. CABLE AND PULLEYS ARE ORIGINAL HAVE NOT BEEN REPLACED. CABLE BROKE AT AFT PULLEY AT WS53.07, BRAKE WAS NOT POLISHED. PRELIMINARY INSPECTION RNov 11, 2003 · Cessna 560XLSDR COMA0360488Pulley · defectiveFLIGHT 5369 DURING CRUISE FLIGHT THE AILERON CONTROLS SEEMED TO REQUIRE MORE THAN NORMAL FORCE TO OPERATE. CREW ELECTED TO PERFORM AN EMERGENCY DESCENT TO LOWER ALTITUDE WHERE THE AILERONS RETURNED BACK TO NORMAL OPERATION. REPLACED AILERON CONTROL PATH PULLNov 6, 2003 · N918CA · Cndair CL6002B19SDR COMA0360461Pulley · frozenFLIGHT 5530 AILERON CONTROLS BINDING, THEN BROKE FREE AT 6000 FT. REPLACED FROZEN CONTROL PULLEY IN LEFT WING.Oct 16, 2003 · N735CA · Cndair CL6002B19SDR SWAA032245Pcu · leakingDIVERSION, DECLARED EMERGENCY HYD 'A' SYS QTY IND DECREASED AND 'A' SYS ENG DRIVEN PUMP LOW PRESS LIGHT ILLUMINATED. FOUND HYD FLUID LEAK AT 'A' SYS AILERON PCU. REMOVED AND REPLACED SAME PER MM.Oct 13, 2003 · N357SW · Boeing 7373H4SDR 2003FA0001074Hinge · damagedINSP ON STOP-TO-STOP TRAVEL OF LT AILERON, NOTICED ODD DOUBLE BUMP SOUND, MVMT AT STOPS. LT WINGTIP, AILERON WERE REMOVED TO FACILITATE FURTHER INSP. IB AILERON HINGE MOVED UP AND DOWN WITH FORCE APPLIED TO IT. VERT MVMT (0.053”) WAS MEASURED APPROX AT BRG Oct 8, 2003 · N501NA · Cirrus SR22SDR CA031002003Cable · misrouted(CAN) DURING A DUAL FLIGHT CONTROL INSPECTION,( ON A SCHEDULED AILERON CONTROL CABLE REPLACEMENT). FOUND CABLE MIS-ROUTED INSIDE THE CONTROL COLUMN ASSY BOROSCOPE INSPECTION CONFIRMED THE CABLE WAS NOT ROUTED THROUGH THE CABLE GUIDE. CABLE WAS RE-ROUTED.Oct 1, 2003 · Lear 35LEARSDR CA031003002Bushing · loose(CAN) ROLLING AILERON BEYOND 3 UNITS ON CONTROL COLUMN BINDING FELT. WHEEL VERY SLOW TO RETURN TO NORMAL. NOT AS STIFF WITH INPUT TO THE LEFT. WHEEL WOULD NOT RETURN TO NEUTRAL ON ITS OWN. FOUND INBOARD DROOP QUADRANT SIEZED. (CROSS SHAFT) ON INSPECTION OFSep 29, 2003 · Boeing 767333SDR 2003FA0001036Lever · bindingDURING FLEET WIDE INSPECTION, FOUND BEARINGS IN AILERON LEVER 2 ASSY. PN 120A4242 TO BE DAMAGED AND BINDING. DAMAGE APPEARS TO BE CAUSED BY THE BUSHING PN 120A4435.02 IN THE FORK ENDS PN 120A4435.01. IT APPEARS THAT DESIGN LIMITATIONS OF THE FLIGHT CONTROL SSep 29, 2003 · N861AF · Grob G120ASDR 2003FA0001015Lever · bindingDURING FLEET WIDE INSPECTION, FOUND BEARING IN AILERON LEVER 2 ASSY. PN 120A-4242 TO BE DAMAGED AND BINDING. DAMAGE APPEARS TO BE CAUSED BY THE BUSHING PN 120A-4435.02 IN THE FORK ENDS PN 120A4435.01. IT APPEARS THAT DESIGN LIMITATIONS OF THE FLIGHT CONTROLSep 29, 2003 · N862AF · Grob G120ASDR 2003FA0001014Lever · bindingDURING FLEET WIDE INSPECTION, FOUND BEARINGS IN AILERON LEVER 2 ASSY. PN 120A-4242 TO BE DAMAGED AND BINDING. DAMAGE APPEARS TO BE CAUSED BY THE BUSHING PN 120A-4435..02 IN THE FORK ENDS PN 120A4435.01. IT APPEARS THAT DESIGN LIMITATIONS OF THE FLIGHT CONTRSep 29, 2003 · N863AF · Grob G120ASDR 2003FA0001013Lever · bindingDURING FLEET WIDE INSPECTION, FOUND BEARINGS IN AILERON LEVER 2 ASSY. PN 120A4242 TO BE DAMAGED AND BINDING. DAMAGE APPEARS TO BE CAUSED BY THE BUSHING PN 120A4435.02 IN THE FORK ENDS PN 120A4435.01. IT APPEARS THAT DESIGN LIMITATIONS OF THE BEARINGS ALLOWISep 29, 2003 · N867AF · Grob G120ASDR 2003FA0001012Lever · bindingDURING PRE-FLIGHT INSPECTION, FLIGHT CREW FELT BINDING ON THE AILERON SYSTEM UPON FURTHER INSPECTION FOUND BEARINGS IN AILERON LEVER 2 ASSY. TO BE DAMAGED AND BINDING. DAMAGE APPEARS TO BE CAUSED BY THE BUSHING PN 120A4435.02 IN THE FORK ENDS PN 120A4435.01.Sep 29, 2003 · N865AF · Grob G120ASDR JBXA03017Aileron · frozenFLIGHT 5119 FROM PWM TO DCA PILOT REPORTED LT AILERON WAS FROZEN. PERFORMED DISCONNECT. ON DESCENT PILOTS RECONNECTED AND NO FURTHER PROBLEMS WERE REPORTED. PROBABILITY OF ICE ON CONTROL SURFACE OR CABLES. AIRCRAFT LANDED UNEVENTFULLY. MX PREFORMED FUNCSep 23, 2003 · N652ML · Cndair CL6002B19
Back to JASC 2710