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 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 LTSDR AUS20040041Gearbox · faulty(AUS) RT INBOARD AILERON ANGLE GEARBOX FAULTY.SDR CA040225005Control Cable · frayed(CAN) CABLE FRAYED AT PULLEY AREA. WING ROOT PULLEY WAS NOT SEIZED.SDR 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.SDR 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.SDR 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. SDR 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.SDR 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 PERFORMSDR 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 560XSDR 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: SDR 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.SDR 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.SDR 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 27-6SDR 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 AFSDR 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 YEASDR 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.SDR 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 ISSUSDR 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 QUADRANSDR 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.SDR 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.SDR 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 CABSDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 CONTSDR 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, 5SDR 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.SDR 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.SDR 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 RSDR 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 PULLSDR COMA0360461Pulley · frozenFLIGHT 5530 AILERON CONTROLS BINDING, THEN BROKE FREE AT 6000 FT. REPLACED FROZEN CONTROL PULLEY IN LEFT WING.SDR 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.SDR 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 SDR 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.SDR 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 OFSDR 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 SSDR 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 CONTROLSDR 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 CONTRSDR 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 ALLOWISDR 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.SDR 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 FUNC
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