JASC 2730
Service difficulty reports · 2,649
Reports filed under 2730 · Elevator 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 = '2730' 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 = '2730' 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 QXEA2019042500189Elevator System · faultedELEVATOR FAULT. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACED P-ACE 1 REF E175 AMM TASKS 27-03-03-000-801A & 27-03-03-400-801-A AS A PRECAUTIONARY MEASURE. AIRCRAFT RETURNED TO SERVICE.SDR CA190417011Turnbuckle · corroded(CAN) BOTH ELEVATOR CABLES FORK END ARE IN A VERY CORROSIVE LOCATION FOR MARINE FLOAT PLANES. ONE FORK END SNAPPED JUST BY UNSCREWING IT FROM THE TURNBUCKLE BY HAND DURING AN INSPECTION. I WOULD SUGGEST TO REPLACE BY THE EQUIVALENT IN STAINLESS STEEL P/N: MS21SDR CA190503009Cable · failed(CAN) DURING HEAVY CHECK, A R/H ELEVATOR CABLE WAS FOUND TO BE DAMAGED AT A FWD QUADRANT. AFTER THE CABLE WAS ORDERED, USING THE RELEVANT IPC, THE CABLE CAME IN AND WAS FOUND TO BE WAY TOO LONG. FURTHER INVESTIGATION IN THE REST OF THE AIRPLANE REVEALED SEVERASDR CA190411016Bolt · loose(CAN) DURING PILOT PRE TAKE OFF FLIGHT CONTROL CHECK, WITH CONTROL LOCK DISENGAGED, ELEVATOR MOVEMENT RESTRICTED, UNABLE TO MOVE AFT OF NEUTRAL POSITION. AIRCRAFT RETURNED TO BAY FOR MAINTENANCE ACTION. MAINTENANCE TROUBLESHOOTING CARRIED OUT. FARING ON RH ELSDR AALA201904019029Hinge Arm · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR #4 HINGE ARM CRACKED. REPLACED HINGE ARM PER SRM 51-72-11.SDR AALA201904019028Hinge Arm · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR #2 HINGE ARM CRACKED. REPLACED HINGE ARM PER SRM 51-72-11.SDR AALA201904019027Hinge Arm · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR #4 HINGE ARM CRACKED. REPLACED HINGE ARM PER SRM 51-72-11.SDR CA190327021Switch · faulted(CAN) EN ROUTE ECAM YELLOW SERVO JAM. ECAM ACTIONS HAD ALREADY BEEN PERFORMED. YELLOW SERVO CTL SWITCHED OFF. SUSPECT AN INDICATION PROBLEM. CREW IS CHECKING THEIR ETOPS AND FUEL REQUIREMENTS. DUE TO FAULT AND RELATED INOP HYD SYSTEM FLIGHT UNABLE TO CONTINUE SDR SWIA2019032645659Warning System · false activationELEVATOR SPLIT CAUTION MESSAGE ON DESCENT. EMERGENCY DECLARED. (FLT#4196) CLOSED PERFORMED RESET OF ELEVATOR SPLIT CAUTION IAW FIM. MESSAGE CLEARED. CYCLED ELEVATORS COMPLETE CYCLE. NO DEFECTS NOTED.SDR CA200114034Actuator · failed(CAN) EXCESSIVE CONTROL COLUMN FORCE REQUIRED DURING ROTATION & CLIMB. RESOLUTION STEP 1: ELEV. FEEL FUNCTION TEST PRIOR TO COMPONENT CHANGE-BOTH CAPT AND F/O TEST TO THE SAME VALUES AND WITHIN LIMITS (PASSED) STEP 2: ELEV. SHAFT DETAILED INSPECTION- NFF STEPSDR HALA2019032500142Transducer · defectiveATB - "F/CTL ELEV SERVO FAULT" ILLUMINATED ON CLIMB OUT. PERFORMED OPS TEST OF SIDE STICK ASSY PER AMM 27-96-00-710-020-A. PERFORMED WIRING CHK OF POS RVDT MON SIGNAL FROM ELAC 1 MON PART TO FIRST TERMINAL BLOCK REF 27-93-07. SWAP ELAC 1 AND ELAC 2 NO HELP SWASDR AALA201904019013Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR HINGE FITTING HAS EXCESSIVE PLAY AND IS WORN. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.SDR CA190313006Shaft · worn(CAN) THE ELEVATOR TORQUE SHAFT ASSEMBLY WAS FOUND TO HAVE PLAY IN ONE OF THE ARMS. THE ASSEMBLY WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. UPON FURTHER INSPECTION IT WAS FOUND THAT THE TAPER PIN INSTALLED IN THE ARM WAS NOT SEATED PROPERLY CAUSING WEAR OFSDR CA190319010Servo · faulted(CAN) DURING APPROACH, AUTOPILOT KICKED OFF 10 TIMES. DIVERTED TO DIFFERENT AIRPORT. CORRECTIVE ACTION: REMOVED AND REPLACED ELEVATOR SERVO.SDR SWAA2019032230913Pushrod · corrodedLT HORIZONTAL BOTH ELEVATOR TAB CONTROL RODS CORRODED ON FORWARD ROD ENDS. R&R ELEVATOR TAB PUSHROD ASSEMBLY PER AMM.SDR CA190305012Bushing · missing(CAN) DURING HEAVY CHECK IT IS ROUTINE PROCEDURE TO DO A DVI [ REGARDLESS OF WHETHER OR NOT THERE IS A TASK CARD] ON THE RUDDER, ELEVATOR AND AILERON BEARING FOR DAMAGE, INDICATIONS OF RUST, RETAINING SLEEVE SECURITY AND THE BEARINGS ARE CHECKED FOR LOOSENESS.SDR ASAA2019021128533Mechanism · brokenLEFT ELEVATOR MECHANISM HAS 2 EACH SPRING BROKEN; REQUIRES AN ODR. REF: CARD G1127029 FOR INBOUND ELEVATOR FAILED POWER OFF 18 TURNS NOSE DOWN. GROUNDED - YES. REMOVED AND REPLACED L/H ELEVATOR TAB CONTROL MECHANISM IAW AMM 27-31-34. OPS CHECKS GOOD.SDR SWIA2019021245508Control Rod · out of rigON CLIMB WE RECEIVED ELEVATOR SPLIT CAUTION FOLLOWED SOON AFTER BY AP TRIM AND CAS MISCOMP. WE RAN THE QRH AND RETURNED TO THE FIELD. REMOVED HARDWARE FROM ALL LH AND RH MECHANICAL CONTROL PATH LOCATIONS FOR THE ELEVATOR. RE-RIGGED THE LH AND RH UPPER CONTROSDR IPXA2019020138505Actuator · unserviceablePITCH CONTROL DURING CLIMBOUT WAS DIFFICULT TO PREDICT. HEAVY DOWNWARD FORCE WOULD COME AND GO. CONTROLL COLUMN WOULD OSCILLATE.REPLACED RH ELEVATOR INBOARD ACTUATOR PER MM 27-30-00-710-801/802.SDR CVGA20190125002Torque Tube · corrodedFOUND RT ELEVATOR TORQUE TUBE HAS CORROSION. REFERENCE AMM 27-31-01 AND SRM 55-20-01.SDR CVGA20190125001Torque Tube · corrodedFOUND LT ELEVATOR TORQUE TUBE HAS CORROSION. REFERENCE AMM 27-31-01 AND SRM 55-20-01.SDR CVGA20190119002Torque Tube · corrodedFOUND LT ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED LT ELEVATOR TORQUE TUBE IAW SRM 51-40-03, 51-40-06 AND 55-20-01.SDR CVGA20190119001Torque Tube · corrodedFOUND RT ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED RT ELEVATOR TORQUE TUBE IAW SRM 51-40-03, 51-40-06 AND 55-20-01.SDR 2019FA0000078Pushrod · brokenDURING THE TAKEOFF ROLL AT MYNN, THE FLIGHT CREW EXPERIENCED A LOSS OF ELEVATOR AUTHORITY. THE FLYING PILOT FIRST OFFICER ELECTED TO REDUCE POWER, DECELERATE, EXIT THE RUNWAY AND TAXIED BACK TO THE RAMP.SDR HNAA2019010200001Warning System · false activationPDIS 652 27-38 1735201 01JAN19 MKE CLOSE PTRIM MAIN INOP EICAS MESSAGE ON TAKEOFF. HISTORY: YES FACT 01JAN19 17:08 MKE REST MAIN CHANNEL IN REFERENCE TO FIM 27-43-00-810-801-A OPS CK GOOD IAW AMM 27-40-00-700-802-A NO FAULTS NOTED OK FOR SERVICE.SDR JJBA201812107005Actuator · inoperativeMAIN PITCH TRIM INOPERATIVE. R&R HORIZONTAL STAB ACTUATOR. OPS CHECK SAT. INSTALLED AND SEALED PANELS 324EL, 321EL, 325LR, 321DR, 321CL, 333DC, 321AL. NO DEFECTS NOTED AT THIS TIME.SDR SIMA20181111001Not Reported · malfunctionedSPS 2 INOP DURING LEVEL CRUISE FLIGHT. NO CMC MSG. TROUBLESHOT SAPS IAW FIM 27-36-00-810-802-A BLOCKS 1 & 10. OPS CHECK GOOD. CONDITION CONSIDERED TRANSITORY.SDR DALA2018110506468Pushrod · out of limitsAPPROX 45 MIN AFTER T/O AT STABLE CRUISE .795M, NOTED UNUSUAL AIRFRAME VIBRATION WITH YOKE VISIBLY VIBRATING, BOTH ENGINE INDICATIONS STABLE. C/W FREEPLAY CK ON RT ELEV PUSHROD PER WORKCARD 2730-7550. RT PUSHROD OUT OF LIMITS AT 0.300". REMOVED RT ELEV PUSH ROSDR FDEA201810313070Plug · looseAT CRUISE FL 340 REC'D L HYD QTY EICAS W/ QTY = .41 IN 5 1/2 MINUTES L HYD QTY WENT TO ZERO. IN ANOTHER 4 MIN L HYD PRESS BEGAN TO DROP. COMPLIED W/ QRH (TURNED "ON" L ELEC HYD PUMP) & PRESSURE RECOVERED. NEXT CAME EICAS L HYD PRIM PUMP. SECURED SAME PER QSDR FDEA201810263022Switch · inoperativeDURING PUSHBACK, AND DURING SECOND ENGINE START, RECEIVED A YELLOW SERVO CONTROL JAMB. REMOVE AND REPLACED RIGHT ELEVATOR YELLOW SYSTEM SERVO CONTROL CONTROL JAMB DETECTION SWITCH IAW MM 27-34-12-04, OPS TESTED GOOD IAW MM 27-34-12-04, OK FOR SERVICE.SDR CVGA20190125004Torque Tube · corrodedFOUND RT ELEVATOR TORQUE TUBE HAS CORROSION. REFERENCE AMM 27-31-01.SDR CVGA20190125003Torque Tube · corrodedFOUND LT ELEVATOR TORQUE TUBE HAS CORROSION. REFERENCE AMM 27-31-01.SDR DJFA2018111200001Controller · faultedDIVERTED DUE TO SWPS FAULT, PTRIM BKP FAIL, FLAP FAIL, SPOILTER FAULT CAS MESSAGES DURING FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. R&R #1 FCE. PERFORMED RIGGING. OPS CHECK GOOD.SDR 3FPY201810078002Control Cable · corrodedELEVATOR CONTROL CABLE CORRODED AT REAR FUSELAGE - FOUND DURING C1-C12 INSPECTION.SDR MASA2018091811378Dcu · malfunctionedELEVATOR SPLIT CAUTION. RERACKED DCU 1.SDR YENA2018091840347Computer · malfunctionedFLT 252, MCO-BOS. ELAC 1 FAULT. NO RESET. SMALL SMELL OF ELECTRICAL WAS PRESENT. (ELEVATOR AILERON COMPUTERS (ELAC)ELAC 1 FAULT) R&R NR 1 ELAC & NR 2 ELAC PER AMM 27-93-34. OPS CHECK OF BOTH ELAC'S SYST GOOD AT THIS TIME PER AMM 27-93-00-710-001-A. PERFORMED ISDR HNAA2018090400213Servo · faultyDURING CLIMB/CRUISE PHASES OF FLT A LOUD BANG/THUD SOUND WAS NOTED. IT APPEARED TO COME FROM FLOOR BELOW BOTH PILOTS SEATS SIMULTANEOUSLY AND BOTH CONTROL YOKES JERKED. EVENT OCCURED THREE TIMES DURING FLT. R&R ELEVATOR SERVO IAW AMM 22-11-04. A/P FUNC CHECK GSDR CVGA20180920002Torque Tube · corrodedFOUND RT ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED ELEVATOR TORQUE TUBE IAW AMM 27-31-01 AND SRM 55-20-01.SDR CVGA20180920001Torque Tube · corrodedFOUND LT ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED ELEVATOR TORQUE TUBE IAW AMM 27-31-01 AND SRM 55-20-01.SDR RAIA2018091370003Control Rod · corrodedRT ELEVATOR CONTROL ROD ENDS SHOW SIGNS OF CORROSION. REMOVED AND REPLACED RT ELEVATOR CONTROL ROD.SDR RAIA2018091370002Control Rod · corrodedLT ELEVATOR CONTROL ROD ENDS SHOW SIGNS OF CORROSION. REMOVED AND REPLACED LT ELEVATOR CONTROL ROD.SDR RAIA2018081530001Control Unit · faultedMAIN PITCH TRIM INOPERATIVE. REMOVED AND REPLACED HSCU. OPS CHECKED GOOD.SDR RAIA2018081510001Pitch Control · malfunctionedMAIN PITCH TRIM FAILED, R2 PRIMARY PITCH TRIM CUTOUT SWITCH PUSHBUTTON POPS, CHECKED GOOD.SDR DXTA2018080821212Pushrod · not reportedAT 11000 FEET, AIRCRAFT ACCELERATING THROUGH 270 KNOTS, AIRCRAFT STARTED VIBRATING. AT 300 KNOTS YOKE STARTED BOUNCING FORWARD AND AFT 3-6 INCHES. NOTICED WINGS VIBRATING AT A HIGH FREQUENCY AS WELL. SLOWED AIRCRAFT DOWN TO 200 KNOTS AND VIBRATION WAS ONLY SLSDR CVGA20181005002Torque Tube · corrodedFOUND RT ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED RT ELEVATOR TORQUE TUBE IAW SRM 51-40-03.SDR CVGA20181005001Torque Tube · corrodedFOUND LT ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED LT ELEVATOR TORQUE TUBE IAW SRM 51-40-03.SDR DXTA2018071701195Unknown · malfunctionedFO ON SHORT FINAL WAS UNABLE TO MAINTAIN DECENT. UPON TRANSFERRING THE CONTROLS WITH YOKE FULL FORWARD PITCH CONTINUED TO INCREASE. PERFORMED RDO, NO PROBLEMS FOUND.SDR DALA2018070504388Computer · faultyEXPERIENCED AN ELAC 1 FAULT WITH AN UNCOMMANDED AIRCRAFT ROLL, DISCONNECTED ELAC 1 PER QRH AND CONTINUED THE FLIGHT. REPLACED ELAC 1.SDR 2018FA0000199Push-Pull Rod · corrodedINTERNAL CORROSION FOUND ON ELEVATOR PUSH/PULL ROD. THE CORROSION PRESENTED ITSELF AS A SMALL BIT OF TOPICAL EXTERNAL CORROSION BUT WHEN UNIT WAS CLEANED FOR FURTHER INSPECTION AND ANALYSIS IT APPEARS CORROSION WAS INTERNAL TO EXTERNAL AND PENETRATED THE TUBINSDR ASMF20180821002Computer · failedDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE HYDRAULIC SYSTEM B ON THE FEEL ELEVATOR COMPUTER. MAINTENANCE PERFORMED A REVISION, DETECTING A HYDRAULIC LEAK AT HYDRAULIC SYSTEM B FEEL ELEVATOR COMPUTER REDUCER. THE FEEL ELEVATOR COMPUTER WAS REP
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