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 COOSDR010033Fitting · crackedLEFT WING AILERON, GEAR BOX ASSY P/N 65-24400-13 LUG CRACKED.SDR CA010629009Servo · failed(CAN) DURING FLIGHT, AILERON CONTROL LOST DUE TO AILERON SERVO SERVO PRIMARY JAMMED. AIRCRAFT RETURNED TO BASE. SERVO WAS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR USAA010704Bellcrank · brokenPIT - FOUND BELLCRANK HAD .75 INCH SECTION BROKEN OUT, RT INBOARD AILERON HINGE ASSY. NOTCHED OUT TOP OF FITTING, REMOVED LOWER FLANGE, INSTALLED TWO MACHINED DOUBLERS PER EA 71077. (M)SDR GTIA010940Bracket · corrodedFTW - AILERON AND TAB CONTROL MIXER BRACKET CORRODED IN NUMEROUS PLACES TO INCLUDE AROUND GUIDE PINS AND PULLEY MOUNTS. REMOVED RIGHT LATERAL CONTROL MIXER AS PER BOEING MD80 MM 27-61-04. INSTALLED REPLACEMENT LATERAL CONTROL MIXER BRACKET AS PER BOEING M80 SDR AUS20010903Control Unit · loose(AUS) AILERON CONTROL SYSTEM HAD EXCESSIVE PLAY. INVESTIGATION FOUNDUNIVERSAL PNO 46203-02 WORN COMPLETELY THROUGH BUSH PNO 453-824 AND INTO BRACKET PNO 29197-02 MOUNTED ON FORWARD BULKHEAD.SDR CA010629032Control Cable · defective(CAN) WHEN INSPECTING CONTROL CABLES AS PER 2000HR/5YR. INSPECTION REQUIREMENT, SOME ABNORMALITIES WERE NOTED ON THE 2 FORWARD AILERON CONTROL CABLES. ON ONE OF THE BUNDLES OF STRANDS IT APPEARED AS IF 2 OR 3 OF THE INDIVIDAL STRANDS WERE SEPARATED FROM EACHOTSDR 20010517CW006Toggle · wornBEARING SPINNING IN AILERON TOGGLE LINK.SDR ER00101Control Cable · crossedDURING SCHEDULED INSPECTION, THE RIGHT HAND AILERON INTERCONNECT CABLE WAS FOUND TO BE CROSSED OVER THE PRIMARY RUDDER CONTROL CABLE (PT NO 46845-0)AT THE UNDERFLOOR SECTION AFT OF THE CABIN DOOR. THERE IS NO WEAR APPARENT AT THIS TIME, THE AIRCRAFT LOG BOOKSSDR 20010523CW001Yoke · corrodedAIRCRAFT ON FINAL APPROACH, CONTROL YOKE FAILED AT APPROX 30 FT AGL. CONTROL YOKE FAILED JUST ABOVE PIVOT POINT BEHIND INSTRUMENT PANEL. CONTROL YOKE WAS EXTREMELY CORRODED AT FRACTURE POINT.SDR UPS01635750Aileron · bindingWHEN CHECKING FLIGHT CONTROLS BEFORE ENGINE START, THE RIGHT OUTBOARD AILERON STUCK IN THE FULL UP POSITION WITH CONTROL YOKE IN NEUTRAL. ORDERED RIGHT AILERON (OUTBOARD) INBD PCA. EMP 25110 ACCOMPLISHED FIM B-767 27-11-00 NO PROBLEMS FOUND PCU OPERATE NORMASDR SWIA972531Aileron · jammedAILERONS JAMMED, WILL NOT DEFLECT FOR A LEFT TURN ON TAXI. TIGHTENED SCREW THAT BACKED OUT ON RIGHT AILERON INSPECTION PANEL. CHECKED AILERONS FOR FREEDOM OF MOVEMENT IN BOTH DIRECTIONS. OPS CHECK GOOD.SDR UPS01235802Casting · corrodedINSPECTION TYPE:C, LT O/B AILERON LOCKOUT MECHANISM, MAIN SUPPORT CASTING HAS EVIDENCE OF CORROSION ON NUMEROUS BUSHING AREAS. CASTING REPLACED IAW SRM 51-30-02 & DRAWINGS 65-21776 & 65-21779SDR SWIA972527Aileron · jammedAT ABOUT 1000 FT ON FINAL JUST AFTER TURNING AUTOPILOT OFF AILERONS WERE LOCKED UP. AFTER ABOUT 15 TO 20 SECONDS THEY BECAME NORMAL. OPERATED AUTOPILOT WITH ALL 3 HYDRAULIC SYSTEMS, ALSO WITH INDIVIDUAL SYSTEMS ARMED, CONTROL AND INDICATION NORMAL. AP DISCOSDR UPS01235658Control Rod · lack of lubeINSPECTION TYPE:IN AILERON STIFF IN LEFT TURNS AILERON SPRING CARTRIDGE FOUND OUT OF RIG. RE-ADJUSTED I.A.W. B727 M .M.27-61-21. SPRING CARTRIDGE OPS CHECKS SERV. CONTROL WHEEL INPUTS (FORCE) THE SAME LEFT AND RIGHT NOTE: MIXER CONTROL ROD AND SPD BRK INPUSDR SWIA972529Bellcrank · obstructedON DOWNWIND THE AILERONS FROZE FOR 12 SECONDS, WE WERE UNABLE TO MOVE YOKE. ON BASE TURN THE AILERONS FROZE FOR 5 SECONDS AND ON FINAL THE AILERONS FROZE FROM APPROX 200 FT AGL UNTIL 20 SECONDS AFTER ROLLOUT. AUTOPILOT WAS CONFIRMED DISCONNECTED BY BOTH PILOSDR C2XA01TY082Bracket · gougedTYS DURING A SCHEDULED INSPECTION THE LEFT AILERON ACTUATOR ATTACH BRACKET WAS FOUND GOUGED ON THE SECOND FROM INBOARD FITTINGS. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB-GST-1299/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMSDR UPS01235809Casting · corrodedINSPECTION TYPE: C, EVIDENCE OF CORROSION ON LEFT OUTBOARD AILERON TURNAROUND GEARBOX CASTING. REPLACED GEARBOX CASTING IAW 27-10-131SDR UPS01635630Control Rod · lack of lubeAILERONS FEEL STIFF LIKE THERE IS NO HYD PWR CLEANED AND LUBED CENTERING MECHANISM SYSTEM CHECKS GOODSDR RRXA10992Aileron · bentDURING A MAINTENANCE VISIT FOUND BENT DAMAGE TO R/H OUTBOARD AILERON OUTBOARD TRAILING EDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1SDR RU3A0102Aileron · icedAFTER FLIGHT IN RAIN, SUBSEQUENT CLIMB ABOVE FREEZING LEVEL, AND DESCENT FOR LANDING: DURING VECTOR FOR ILS FINAL, AUTOPILOT WAS MANUALLY DISCONNECTED BY (PIC). AIRCRAFT IMMEDIATELY BANKED LEFT, NOTED FULL LEFT AILERON TRIM DEPICTED ON TRIM INDICATOR. AILEROSDR MALA010438Control Cable · chafedDURING 4K-INSPECTION IN CWA, MAINTENANCE FOUND RT O/B AILERON CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RT O/B AILERON CABLE P/N 7227151-522. SECURED AT AILERON O/B BELLCRANK, REQUIRES INSTALLATION ON IDLER END.SDR SCNA01030Control Unit · failedDURING CLIMBOUT FROM LAS THE A-SYSTEM HYDRAULICS FAILED. REMOVED AND REPLACED THE AILERON HYDRAULIC SYSTEM MODULAR UNIT.SDR RRXA10950Aileron · damagedDURING A MAINTENANCE VISIT FOUND BUCKLED SKIN L/H INBD AILERON UPPER LWR SKINS JUST FWD OF TAB O/B L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 57-2-0, FIG 1B.SDR MALA010417Control Cable · chafedFOUND DURING 4K INSPECTION LHIB FWD CABLE OF AILERON SYSTEM IS CHAFED. MX REPLACED LHIB FWD AILERON CABLE P/N 7227105-614 IAW SAAB AMM 27-11-01. SEE 409 NR 123627 FOR RIGGING.SDR MALA010415Control Cable · chafedFOUND DURING 4K INSPECTION IN CWA, FWD LHOB CABLE IS CHAFED. MX REPLACED FWD LHOB AILERON CABLE P/N 7227105-613 IAW SAAB AMM 27-11-01. SEE 409 123627 FOR RIGGING.SDR MALA010414Control Cable · chafedFOUND DURING 4K INSPECTION, FWD RT IB CABLE OF AILERON SYSTEM IS CHAFED. MX REPLACED FWD RT IB AILERON CABLE P/N 7227105-623 IAW SAAB AMM 27-11-01 SEE 409 NR 12627 FOR RIGGING.SDR UPS01835562Aileron · lack of lubeAILERONS STIFF. INSPECTED AILERON CONTROL SYSTEM AND FOUND AILERONS IN NEED OF LUBE. LUBRICATED AILERONS IAW 27-10-06 AND PERFORMED AILERON SYS ADJ/TEST IA W MM 27-10-00. AILERONS CHECKED NORMAL OK FOR SERVICESDR 01FDEA00268Actuator · failedAFT FLAP RETRACTION, AILERON DISAGREE ALERT DISPLACY. RED TAB PROC ACCOMP. DEFLECTED AILERON SYS INOP. RIGHT O/B ACT FAILED AND REPLACED WITH FIXED PUSHROD PER METHOD B.SDR AU010352Control Cable · broken(AUS) AILERON THREADED CABLE AND FITTING SEPARATED APPROXIMATELY MIDWAY BETWEEN THE THREADED END AND THE SWAGED NUT.SDR 01FDEA00251Aileron · malfunctionedAT 8000 FT ON DEPART RECEIVED A LEVEL 2 AIL DEFLECT DISAG ALERT ON CONFIG PAGE, LEFT AILERON WAS DROOPING, CREATING A RIGHT TURN. ADJUSTED LOB TO NEUTRAL POS PER MM 27-10-00. CYCLED FLAPS AND AILERONS 3X''S, NIL ALERTS AND SYNOPTIC DISPLAY SHOW NEUTRAL.SDR ABXA010108Mixer Box · bindingDURING PRE-DEPARTURE CHECKS, THE AILERON CONTROL YOKE WOULD BIND WHEN RETURNING FROM LEFT TO CENTER POSITIONS. MAINTENANCE INSPECTED, CLEANED, AND LUBRICATED THE LEFT AND RIGHT AILERON MIXER ASSEMBLIES. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WASSDR SWIA972498Aileron · stiffAIRCRAFT FEELS EXTREMELY STIFF IN ROLLING TO RIGHT. REQUIRES 3+ UNITS OF AILERON TRIM TO FLY STRAIGHT AND LEVEL. INSPECTED AILERON TRIM SYSTEM IAW EMB MM 27-12. ALSO INSPECTED AILERON CONTROL SYSTEM PER EMB MM 27-11. ALL CHECKS AND TESTS FOUND AILERON CONTSDR MALA010353Control Cable · chafedFOUND DURING 4K-INSPECTION, CWA. RT OB WING FWD AILERON CABLE IS CHAFED. MX REPLACED CABLE PN 7227151-522.SDR MALA010360Control Cable · chafedFOUND DURING 4K-INSPECTION, CWA. LT AILERON FWD OB WING CABLE IS CHAFED, MX REMOVED AND REPLACED CABLE.SDR 2001UALA00348Pulley · bindingDIVERTED DUE TO STIFF AILERONS. SUPPLEMENTAL DATA UPDATE FOUND RIGHT AILERON WING BODY LOWER PULLEY BINDING AT STA 664. REPLACED PULLEY AND SPACERS.SDR ABXA010107Torque Tube · brokenTHE RIGHT AILERON TORQUE TUBE WAS REPORTED TO BE BROKEN AT EWR. *S/D* THE AIRCRAFT ON DEPARTURE AND ARRIVAL HAD RIGHT ROLL TENDENCY THAT REQUIRED APPROX 30 DEGREES WINGS LEFT YOKE INPUT TO MAINTAIN LEVAL WINGS. MAINTENANCE INSPECTED AND FOUND THE RIGHT OUTBSDR 20010430CW001Control Cable · brokenDURING 100 HOUR INSPECTION, IT WAS DISCOVERED THAT THE LEFT AILERON CROSSOVER CABLE HAD A BROKEN STRAND AT A POINT 63.5 INCHES FROM THE TURNBUCKLE END. BROKEN STRAND WAS WHERE CABLE PARTED OVER A RUB BLOCK ATTACHED TO RIB AT WING STA. 56.875.SDR 0101109873Drain Valve · cloggedEN ROUTE FROM DFW TO DTW, THE AILERON FLIGHT CONTROLS FROZE. AIRCRAFT DESCENDED TO A LOWER ALTITUDE AND CONTROL RETURNED. FLIGHT DIVERTED TO MEM AND MADE A NORMAL SAFE LANDING. MAINTENANCE FOUND THE RIGHT SLANT PANEL DRAIN VALVE CLOGGED. CLEARED OBSTRUCTIOSDR 20010425CW007Tube · looseDURING ANNUAL INSPECTION THE TWO ALUMINUM RIVETS SECURING THE FORWARD END OF SHAFT WERE FOUND LOOSE AND THE BUCK TAILS MISSING . THE SQUARK TUBE PORTION OF ASSEMBLY APPEARS TO BE ALUMINUM. THE FORWARD THREADED END IS STEEL. THE FIT OF THE TWO PARTS IS NOT VSDR CA010404010Control Unit · leaking(CAN) DURING FLIGHT A SYSTEM HYDRAULIC SYSTEM QUANTITY BEGAN TO DROP, AT A RATE OF 1 GALLON PER HOUR. DUE TO POOR WEATHER ELECTED TO DIVERT. GEAR EXTENDED NORMALLY AND QUANTITY REMAINED STEADY. FLIGHT LANDED WITHOUT INCIDENT. FOUND A SYSTEM AILERON POWER CONTRSDR MALA010282Control Unit · malfunctionedDURING FLIGHT 2790 AFTER LT TURN, INFLIGHT, BANK ANGLE 30 DEGREES: AILERONS STUCK FOR ABOUT 1 SECOND AT 25 DEGREES: AS THE WINGS ROLLED LEVEL. MAINTENANCE PERFORMED AILERON RANGE OF MOVEMENT CHECK AND VISUAL CHECK OF AILERON SYSTEM. NO DEFECTS NOTED. CREW RESDR COMA0160301Computer · malfunctionedAILERON TRIM INOP, C/B TRIPPED. PREVIOUS HISTORY OF RUNAWAY AILERON TRIM REPORTED BY FLIGHT CREW. REPLACED THE NR 2 DCU PREVIOUS REPORTS OF RUNAWAY TRIM WERE ERRONEOUS INDICATIONS.SDR WRLA200103Transmitter · failedAFTER TAKEOFF, DEFLECTED AILERONS WOULD NOT RETRACT, AIR RETURNED TO KSEA BASE. MAINTENANCE PROCEDURES COMPLIED WITH, AIRCRAFT DEPARTED. FLAP HANDLE POSITION TRANSMITTER POSITION TRANSMITTER WAS CHANGED TO CORRECT PROBLEM. FLAP HANDLE POSITION TRANSMITTER. SDR AU010164Tube · corroded(AUS) OUTBOARD PUSH-PULL TUBE LOCATED IN RT WHEEL WELL CORRODED INTERNALLY.SDR SWIA972384Connecting Rod · brokenAFTER SHUTDOWN, AILERON CONTROL WHEEL WOULD NOT MOVE LEFT OR RIGHT WITHOUT EXCESSIVE FORCE. INSPECTED LEFT AND RIGHT AILERON CABLE ROUTING. NO DEFECTS NOTED. AILERONS HAVE FREE MOVEMENT. PSP MX REQUEST CHECK LEFT AND RIGHT RVIT (AILERON) FOR CONDITION. CHSDR CA010301025Control Unit · leaking(CAN) AT FL350 IN CRUISE, NR 2 B HYDRAULIC PUMP OVERHEAT LIGHT CAME ON. PUMP WAS SELECTED OFF. 30 SECONDS LATER THE NR 1 B HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON. PUMP WAS SELECTED OFF, B HYDRAULIC SYSTEM QUANTITY DROPPED TO 1.2 GALLONS. AIRCRAFT RETURNED WSDR 0100799956Drain Valve · cloggedWHILE AIRBORNE BETWEEN RDU AND MSP, THE AILERON TRIM CONTROL JAMMED. FLIGHT CONTINUED UNDER FULL CONTROL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CONTROL CABLE PULLEYS IN THE RIGHT WHEEL WELL LOCKED UP WITH ICE. FOUND TORN SEAL AT AFT BOTTOM OF FORWARSDR 20010403CW005Control Cable · chafedDURING INSPECTION FOUND THAT WHEN CONTROL COLUMN IS PULLED BACK AND AILERONS ARE OPERATED, THE BALLANCE CABLE ON CONTROL COLUMNS ARE RUBBING INTO LANDING GEAR UP HYDRAULIC LINE. LOCATION-UNDER COPILOTS FLOOR PANEL. PROLONGED USE LIKE THIS CAN CAUSE HYDRAULICSDR HNAA0100014Control Cable · out of toleranceUPON RELEASE OF AUTO PILOT, NOTED ROLL CONTROL VERY STIFF, SEEMS TO REDUCE WITH REDUCTION IN AIR SPEED. INSPECTED AILERONS AND ROLL SPOILERS, FOUND AILERON CONTROL CABLE TENSIONS OUT OF LIMITS. RE-TENSIONED CABLES. EVALUATION FLIGHT SATISFACTORY.SDR DHL2001362004Servo · failedUPON NR 2 ENGINE START, YELLOW SYSTEM JAM SERVO LIGHT ILLUMINATED. T/S TO LT LOW SPEED AILERON DISCONNECT SAME AND DEFERRED PEN.
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