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 AU971408Control Cable · frayed(AUS) RH AILERON BALANCE CABLE STRANDS BROKEN. FOUND DURING INSPECTIONIAW AD/P68/44 (PARTENAVIA SB 75 REV3).SDR AU971407Control Cable · frayed(AUS) LH AILERON BALANCE CABLE STRANDS BROKEN. FOUND DURING INSPECTIONIAW AD/P68/44 (PARTENAVIA SB 75 REV3).SDR AU971406Control Cable · frayed(AUS) RH AILERON OUTBOARD CONTROL CABLE STRANDS BROKEN. FOUND DURINGINSPECTION IAW AD/P68/44 (PARTENAVIA SB 75 REV3).SDR AU971403Control Cable · frayed(AUS) LH OUTBOARD AILERON CABLE STRANDS BROKEN. FOUND DURING INSPECTION IAW AD/P68/44 (PARTENAVIA SB 75 REV3).SDR CA971110019Push Pull Tube · cracked(CAN) DURING INSPECTION OF RIGHT HAND NR 2 AILERON, PUSH/PULL TUBE WAS FOUND CORRODED AND CRACKED AT THE END WHERE THE BEARING ATTACHES.SDR 97ZZZX4890Control Cable · frayedCABLES (ALL 3) WERE FRAYED ON FUSELAGE 90 DEGREE PULLEYS. THE AIRCRAFT HAD BEEN TREATED INTERNALLY WITH 'THERMAL GARD'. THE TREATMENT WAS FOR ANTI-CORROSION. THE TREATMENT FORMED A SMOOTH BARRIER THAT MADE VISUAL INSPECTION LOOK OK. CLEANING CABLES WITH SOLSDR 97ZZZX4889Control Cable · frayedCABLES (ALL 3) WERE FRAYED ON FUSELAGE 90 DEGREE PULLEYS. THE AIRCRAFT HAD BEEN TREATED INTERNALLY WITH 'THERMAL GARD'. THE TREATMENT WAS FOR ANTI-CORROSION. THE TREATMENT FORMED A SMOOTH BARRIER THAT MADE VISUAL INSPECTION LOOK OK. CLEANING CABLES WITH SOLSDR COMA9710462Cables · wornWHILE PERFORMING TASK 5720-681-01I ON RIGHT WING, 2C INSPECTION, FOUND BOTH AILERON CABLES WORN BADLY AT NACELLE FAIR LEADS. REPLACED CABLES IAW EMB 120 MM.SDR COMA9710461Control Cable · wornWHILE PERFORMING TASK 5720-581-01I ON LEFT WING, 2C INSPECTION, FOUND BOTH AILERON CABLES WORN BADLY AT NACELLE FAIRLEADS. REPLACED CABLES IAW EMB 120 MM.SDR 9719509926Control Sector · looseAILERON CONTROL WHEEL HAD TO BE ROTATED 10 DEGREES BEFORE AILERON MOVEMENT. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH AILERON LATERAL CONTROL SECTORS LOOSE ON SHAFT. REPLACED LEFT AND RIGHT MIXER INPUT DRUMS, SHAFTS AND CONTSDR RRXA97284Aileron Control · malfunctionedON TAKEOFF WITH STAB SET AT 1.7 AIRCRAFT WOULD NOT ROTATE. HELD NOSE UP TRIM AND AIRCRAFT FLEW OFF WITH STAB TRIM AT 3, 2 UNITS. AFTER TAKEOFF AIRPLANE ROLLED LEFT. AIRPLANE REQUIRED 3 TO 4 UNITS OF RIGHT AILERON TRIM AND 1/2 UNIT RIGHT RUDDER TO STOP ROLL.SDR AU971345Control · jammed(AUS) AILERON CONTROL SYSTEM JAMMED. EVIDENCE OF FOD LODGED BETWEEN CHAIN AND SPROCKET.SDR 97ZZZX4601Indicator · gear strippedUPON CHECKING AILERON TRIM FOR PROPER RIGGING, THE INDICATOR WAS NOT MOVING AS AILERON TRIM WHEEL WAS TURNED. FURTHER INVESTIGATION FOUND THE GEAR ASSY FOR THE INDICATOR HAD MOST OF THE TEETH STRIPPED OFF. THE AILERON TRIM TABS WERE MOVING OK. THE GEAR WAS SDR CA971024005Roll Control · disconnected(CAN) ON LANDING THE CREW REPORTED THAT THE ROLL CONTROL DISCONNECTED, THEN WITH OPPOSITE DIRECTION INPUT, RECONNECTED WITH NO FURTHER INCIDENT. SB 8-27-79 PT. 3 COMPLETED AGAIN, NO FAULTS FOUND WITH THE EXCEPTION OF A SMALL AMOUNT OF GREASE ON THE CLUTCH PLATSDR ABXA9701660Bracket · corrodedDURING C-CHECK, FOUND LEFT AILERON PULLEY BRACKET PITTED AND CORRODED. REPLACED PULLEY BRACKET IAW DC9 MM 20-16-0.SDR QXEA9700664Actuator · malfunctionPDX- AILERON TRIM HARD TO TURN AT CRUISE ALTITUDE IN FREEZING CONDITIONS. REPLACED BOTH LEFT AND RIGHT AILERON TRIM ACTUATORS. COMPLIED WITH CABLE TENSION AND TRAVEL CHECK. NO DEFECTS NOTED.SDR CA971015028Lockout · torn boot(CAN) DUST BOOT ON RIGHT HAND AILERON LOCKOUT MECHANISM TORN, REPLACED.SDR MASA97170Control Cable · wornDURING NIGHT MAINTENANCE, THE LEFT AILERON CONTROL CABLE WAS FOUND WITH BROKEN STRANDS. THE AREA OF DEFECT WAS WHERE THE CABLE RUNS THROUGH THE LEFT ENGINE NACELLE FAIR LEAD. MAINTENANCE REMOVED AND REPLACED THE LEFT UPPER AILERON CABLE, OPS CHECK GOOD. AIRSDR MASA97169Control Cable · wornDURING NIGHT MAINTENANCE, THE LEFT AILERON CONTROL CABLE WAS FOUND WITH BROKEN STRANDS. THE AREA OF DEFECT WAS WHERE THE CABLE RUNS THROUGH THE LEFT ENGINE NACELLE FAIR LEAD. MAINTENANCE REMOVED AND REPLACED THE LEFT UPPER AILERON CABLE, OPS CHECK GOOD. AIRSDR 97ZZZX4507Control Cable · wornDURING REPLACEMENT OF PAN UNDER WING WALK IN THE GEAR WELL, RIB WAS FOUND CRACKED. THE WING WAS REMOVED AND FOUND SEVERAL WING ATTACHMENT BOLTS CORRODED. BOLTS AND SPECIAL WASHERS NOT IN PROPER LOCATIONS PER PA28 MM. (WING ATTACH). NO SHIMS AT EITHER WING SSDR 97ZZZX4494Feel Bungee · freeze upPILOT REPORTED RECEIVING 'TRIM LEFT AILERON WARNING' AT FL 41,000, 20,000, AND A FINAL WARNING AFTER LEVELING OFF JUST BELOW 11,000. AFTER EACH OF THE 2 WARNINGS, PILOT DISCONNECTED AUTOPILOT AND FOUND NO DISCREPANCIES. WHEN PILOT DISCONNECTED AUTOPILOT AFTESDR 97ZZZM1086Knob · looseAILERON CONTROL KNOW FALLS OFF POTENTIALLY CAUSING A CONTROL PROBLEM IF PILOT EXPERIENCES ENGINE FAILURE ON TAKEOFF. A POTENTIAL LOSS OF CONTROL AND OR AIRCRAFT MAY OCCUR.SDR 97ZZZX4672Push/Pull Tube · brokenDURING CONTROL CHECK JUST PRIOR TO TAKEOFF, NOTED THE RIGHT AILERON DID NOT MOVE. INVESTIGATION REVEALED THE PUSH ROD LOCATED IN THE BELLY OF THE AIRCRAFT WAS BROKEN AT A WELD WHERE PART HAS A 90 DEGREE BEND. THE BREAK WAS JUST AT THE EDGE OF THE WELD. IT ASDR MASA97155Cable · wornDURING NIGHT MAINTENANCE, THE RIGHT AILERON CONTROL CABLE WAS FOUND WITH TWO BROKEN STRANDS. THE AREA OF DEFECT WAS WHERE THE CABLE RUNS THROUGH THE RIGHT ENGINE NACELLE FAIR LEAD. MAINTENANCE REMOVED AND REPLACED THE RT UPPER AILERON CABLE, OPS CHECK GOOD. SDR MASA97152Control Cable · wornDURING NIGHT MAINTENANCE, THE LEFT UPPER AILERON CABLE WAS FOUND WITH APPROXIMATELY ONE INCH AREA THAT WAS WORN. THE AREA OF DEFECT WAS LOCATED WHERE THE CABLE RUNS THROUGH THE LT ENGINE NACELLE FAIR LEAD. MAINTENANCE REMOVED AND REPLACED THE LT AILERON UPPESDR 98ZZZX4554Balance Cable · brokenDURING AN ANNUAL INSPECTION, DISCOVERED A FLAT SHINEY AREA ON THE BOTTOM SIDE OF THE LT AILERON BALANCE CABLE. THE LOCATION OF THE CABLE IN QUESTION IS IN THE LT WING ROOT AREA JUST INBD OF THE WHEELWELL. AN IDLER PULLEY IS LOCATED IN THIS AREA. UPON FURTHESDR 98ZZZM99Control Cable · corrodedRIGHT AILERON CONTROL CABLE 35B-C IS CORRODED AT LOWER PULLEY UNDER FWD WING ROOT FAIRING. REMOVED AND REPLACED BOTH RT WING ROOT MAIN AILERON CABLES, TENSIONED AND SAFETIED. GEN W/C FOR FUNCTIONAL TEST REF 5067. (M)SDR 98ZZZM104Control Cable · wornLEFT AILERON INTERCONNECT OB CABLE IS WORN THROUGH ALUMINUM CLAD. REMOVED AND REPLACED LEFT OUTBOARD INTERCONNECT CABLE, TENSIONED AND SAFETIED. GEN W/C FOR FUNCTIONAL TEST 5067.SDR 98ZZZM103Control Cable · corrodedAILERON INTERCONNECT CENTER FORWARD CABLE IS CORRODED AT LEFT WING ROOT PULLEY. REMOVED AND REPLACED BOTH FORWARD AND AFT CENTER LOOP INTERCONNECT CABLES, TENSIONED AND SAFETIED. GEN W/C FOR FUNCTION TEST, REF 5067.SDR 98ZZZM102Control Cable · wornRIGHT AILERON INTERCONNECT CABLE, OUTBOARD CABLE WORN ALMOST THROUGH ALUMINUM CLAD. REMOVED AND REPLACED RT OUTBOARD CONNECT CABLE, TENSIONED AND SAFETIED. GEN W/C FUNCTIONAL TEST 5067.SDR 97ZZZX4290Control Cable · mismanufacturedDURING SCHEDULED CABLE INSPECTION, THE AILERON CABALE WHICH RUNS THROUGH THE FUSELAGE WAS FOUND TO HAVE BROKEN STRANDS. UPON RECEIPT OF THE NEW CABLE, FOUND THE TERMINAL END WAS INCORRECT (CLEVIS TYPE INSTEAD OF 'EYE' TYPE). THE MANUFACTURER WAS CONTACTED ANSDR 97ZZZX4010Control Cable · frayedWHILE PERFORMING SB 226, THE LEFT AILERON CABLE WAS FOUND SEVERELY FRAYED AT WS 142.0. THE CABLE WAS PROPERLY ROUTED AND RUBBING ON THE FAIRLEAD AS IT WAS INTENDED TO DO. SUBMITTER SUGGESTS INSPECTING ALL OF AILERON CABLES BEHIND WING TO FLAP FAIRINGS WHILE SDR 97ZZZX4270Control Cable · frayedLEFT PRIMARY AILERON CABLE WAS FOUND FRAYED DURING ROUTINE INSPECTION. SEVERAL HARD TO SEE AREAS OF CABLE WERE FRAYED (TOTAL TIME ON CABLE 4,101.1 HOURS. SUBMITTER RECOMMENDED CABLES BE REPLACED ON A TIME CHANGE BASIS, CABLE PN 0510105-224.SDR GLBA97131Pulley · failedORD - BANGING NOISE HEARD UNDER FLOOR BOARDS IN-FLIGHT. FOUND AILERON CABLE LOOSE. REPLACED AILERON CABLE PULLEY. (X)SDR GLBA97130Control Cable · wornRIGHT LOWER AILERON CABLE WORN TO LIMITS. REMOVED AND REPLACED RT LOWER AILERON CABLE IAW EMB-120-MM. (X)SDR GLBA97129Control Cable · wornLEFT UPPER AILERON CABLE WORN TO LIMITS. REMOVED AND REPLACED UPPER LT AILERON CABLE IAW EMB-120 MM. (X)SDR GLBA97128Control Cable · wornLEFT LOWER AILERON CABLE WORN TO LIMITS. REMOVED AND REPLACED LOWER LEFT AILERON CABLE IAW EMB-120 MM. (X)SDR GLBA97127Control Cable · wornRIGHT UPPER AILERON CABLE WORN TO LIMITS. REMOVED AND REPLACED UPPER RIGHT AILERON CABLE IAW EMB-120 MM. (X)SDR 98ZZZM60Control Cable · corrodedRIGHT AILERON CABLES CORRODED AT BELLCRANK AT RIB NR 10. REMOVED AND REPLACED BOTH RIGHT MAIN AILERON OUTER CONTROL CABLES, TENSIONED AND SAFETIED IAW BAE MM.SDR 98ZZZM59Control Cable · corrodedLEFT OUTER AILERON CONTROL CABLE HAS RUST ON OUTER CABLE QUANDRANT. REMOVED AND REPLACED BOTH LEFT MAIN AILERON OUTER CONTROL CABLES, TENSIONED AND SAFETIED IAW BAE MM .SDR SRAA970805Actuator · failedAFTER TAKEOFF OUT OF BRU, FLIGHT 131 - AIRCRAFT LOST ALL HYDRAULIC FLUID, FOUND NR 3 ENGINE HYDRAULIC LOW PRESSURE LIGHT ON, FOLLOWED BY NR 2 ENGINE SYSTEM. FLUID CAME DOWN TO EMERGENCY LEVEL, ACCOMPLISHED AIR TURN BACK TO BRU AFTER DUMPING 19,000 LBS OF FUELSDR MALA975571Pushrod · wornDURING E-5 CHECK, FOUND LEFT AILERON ROD END BEARING WORN. MAINTENANCE REPLACED LEFT AILERON BEARING. ALL CHECKS GOOD. (M)SDR DHL97801004O Ring · failedHYDRAULIC PRESSURE DROPPED TO ZERO, PERFORMED ABNORMAL PROCEDURE, AUX PUMP ON, HYD SYSTEM INDICATED FULL. AUX PRESSURE 2500 PSI. FOUND O-RING ON RT AILERON POWER PACK DETERIORATED AND LEAKING. REPLACED O-RING SERVICED HYDRAULIC SYSTEM. SYS OPS NORMAL.SDR DHL97724004Contl Mech · out of adjustWITH FLAPS UP, NEED 20 TO 25 DEGREE CONTROL WHEEL DEFLECTION TO TURN AIRCRAFT LEFT. DEAD SPOT BETWEEN 0-25 DEGREES. CHECKED AND RERIGGED AILERONS AND SPOILERS PER M/M 27-61-0.SDR 97ZZZX3539Piston Assy · bentINSPECTION OF AILERON ACTUATOR FOUND PISTON ATTACHMENT POINTS WHERE THE PISTON ATTACHES TO THE PISTON CONNECTOR, 15 ARE BENT OUTWARDS. AREA OF PISTON BENT UNDER NORMAL OPERATION.SDR MALA975518Control Mech · out of adjustMSP - FLT 3103 - ON APPROACH, AILERON ROLL COMMAND JAMMED. CREW DE-CLUTCHED AND NO FURTHER PROBLEMS NOTED. MAINTENANCE ADJUSTED TENSION ON PILOT'S CONTROL WHEEL. OPS CHECK OF AILERON CONTROL SYSTEM GOOD. (X)SDR 97ZZZM871Control Cable · corrodedLEFT AILERON INTERCONNECT CABLE CORRODED AT OUTBOARD END. REMOVED AND REPLACED LEFT AILERON INTERCONNECT SHEATHED CABLE TENSIONED, SAFETIED AND COMPLIED WITH AILERON SYSTEM FUNCTIONAL AND TRAVEL CHECKS IAW BAE MM. (M)SDR 97ZZZM867Cables · corrodedBOTH RIGHT AILERON MAIN CIRCUIT CONTROL CABLES ARE CORRODED AT WING ROOT PULLEYS. REMOVED AND REPLACED BOTH RIGHT MAIN AILERON CENTER CABLES, TENSIONED, SAFETIED AND COMPLIED WITH AILERON SYSTEM FUNCTIONAL AND TRAVEL CHECK IAW BAE MM.SDR 97ZZZM866Control Cable · corrodedLEFT MAIN AILERON CABLES ARE CORRODED AT THE FRA NR 24-25 PULLEY JUST PRIOR TO CABLE ENTERING THE FUSELAGE. REMOVED AND REPLACED BOTH LEFT MAIN AILERON CENTER CABLES, TENSIONED, SAFETIED, AND COMPLIED WITH AILERON SYSTEM FUNCTIONAL AND TRAVEL CHECKS IAW BAE MSDR 97ZZZM865Cables · corrodedBOTH AILERON INTERCONNECT CABLES ARE CORRDED AT WING ROOT PULLEYS. REMOVED AND REPAIRED BOTH CENTER AILERON INTERCONNECT CABLES, TENSIONED, SAFETIED, AND COMPLIED WITH AILERON SYSTEM FUNCTIONAL AND TRAVEL CHECKS IAW BAE MM. (M)
Back to JASC 2710