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 SWIA2021091361066Pcu · leaking* RH ELEVATOR PCU #1 LEAK (C-CHECK RO 9/8/2021) REMOVED AND REPLACED RH ELEVATOR PCU #1 WITH SERVICEABLE UNIT. REF CRJ900 AMM 27-33-01-000-801-A01 AND 27-33-01-400-801-A01. OPS TESTS AND LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 27-320-1003-SKYSDR SWIA2021091361064Pcu · leaking* RH ELEVATOR PCU #2 LEAK (C-CHECK RO 9/8/2021) REMOVED AND REPLACED RH ELEVATOR PCU #2 WITH SERVICEABLE UNIT. REF CRJ900 AMM 27-33-01-000-801-A01 AND 27-33-01-400-801-A01. OPS TESTS AND LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 27-320-1003-SKY.SDR YENA2021070200421Servo · failedFLT 400, MSY-BOS. F/CTL ELAC 2 PITCH FAULT. SHORT SHARP BRIEF PITCH JOLT FOLLOWED BY ABOVE ECAM. RESET SUCCESSFUL ; R+R LH INBD ELEVATOR SERVO IAW AMM 27-34-51. OP CHECKED GOOD BUT FAILS ELEVATOR DAMPING TEST. REFER TO DEFECT 3181961 ITEM 2 FOR REPLACEMENT. R+SDR YENA2021070200420Servo · failedFLT 400, MSY-BOS. F/CTL ELAC 2 PITCH FAULT. SHORT SHARP BRIEF PITCH JOLT FOLLOWED BY ABOVE ECAM. RESET SUCCESSFUL ; R+R LH INBD ELEVATOR SERVO IAW AMM 27-34-51. OP CHECKED GOOD BUT FAILS ELEVATOR DAMPING TEST. REFER TO DEFECT 3181961 ITEM 2 FOR REPLACEMENT. R+SDR YENA2021070200419Servo · failedFLT 400, MSY-BOS. F/CTL ELAC 2 PITCH FAULT. SHORT SHARP BRIEF PITCH JOLT FOLLOWED BY ABOVE ECAM. RESET SUCCESSFUL ; R+R LH INBD ELEVATOR SERVO IAW AMM 27-34-51. OP CHECKED GOOD BUT FAILS ELEVATOR DAMPING TEST. REFER TO DEFECT 3181961 ITEM 2 FOR REPLACEMENT. R+SDR ASAA2021062535181Warning Message · false activationREF L/P 60181794 & 60181796, DFCS LAND VERIFY TEST FAILS "ELEVATOR POSITION SENSOR -1, MSG# 22-11125.". GROUNDED - YES. ACCOMPLISHED LAND VERIFY TEST PER B737-800 AMM 22-11-00/201. NO FAULTS NOTED. ELEV SENSOR VALUES A & B ARE WELL WITHIN LIMITS. AUTOTHROTTLE SDR YENA2021061400367Actuator · out of rigFLT 1952, MCO-BOS. RETURNED TO FIELD. VIBRATION AT FL 240 . NO NOTICABLE ENG VIBRATION. FILLED OUT VIBRATION REPORT; APPLIED TSM 05-50-000-991-00400-00-C. VIBRATION SURVEY & DECISION TABLE POINTED TO RUDDER AND ELEVATORS AS PROBABLE CAUSE. INSPECTED INTEGRITYSDR HNAA2021060200232Warning Message · false activationPDIS 632 27-36 2379001 01JUN21 EVV CLOSE
SPS 1-2 INOP, SPS ADANCE, NO TAKEOFF CONFIG DURING TAKEOFF MESSAGES CLEARED WHEN A/C STOPPING.
FACT 01JUN21 10:52 EVV
PERFORMED SPS OPS CHECK IAW AMM 27-36-00-700-801-A. OPS CHECK GOOD.SDR 9JLA2021060324827Control Servo · failedTHE FLIGHT CREW REPORTED RECEIVING AN AUTO-PILOT AND YAW DAMPENER FAIL MESSAGE; NEITHER WOULD ENGAGE. THE MAINTENANCE VENDOR TROUBLESHOT DETERMINED THE ELEVATOR ACTUATOR SERVO WAS DEFECTIVE. THE DEFECTIVE SERVO ACTUATOR AND INSTALLED AN OVERHAULED UNIT. FUNCTISDR CALA2021052600738Servo · faultedELEVATOR SERVO FAULT ON ECAM. - TOMC KROWN PERFORMED TSM 27-93-00-810-861-A. FOUND CONNECTOR AT SERVO 34CE4 DISCONNECTED. INSPECTED CONNECTOR FOR DEFECTS. NONE NOTED. CLEANED INSTALLED AND SECURED CONNECTOR. CHECKED ALL CONNECTIONS FOR SECURITY. CHECKS GOOD. RSDR 9JLA2021052527923Actuator · defectiveTHE FLIGHT CREW REPORTED THAT A PITCH FEEL FAIL AMBER CAS MESSAGE WAS DISPLAYED DURING FLIGHT. THEY REPORTED THAT THE MESSAGE WAS ILLUMINATED THROUGH AIRCRAFT SHUTDOWN. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE LEFT PITCH FEEL ACTUATOR WAS DEFECTIVSDR VNAA2021051699955Control Cable · damagedRH ELEVATOR CABLE CIRCUIT HAS NO TENSION VERIFIED SLIPPAGE AT ABLE BLOCK TORQUE STRAP BROKEN. REQUIRES DUAL RUN INSPECTION.SDR AALA202105089008Computer · faultyAIRCRAFT WAS GROUNDED: DURING CLIMB OUT, UN-COMANDED NOSE DOWN PITCH WITH THE AUTO PILOT OFF; IN LEVEL FLIGHT, UN-COMMANDED PITCH UP WITH AUTOPILOT ON. REPLACED #2 ELEVATOR AILERON COMPUTER SYSTEM IAW AMM 27-93-34, OPS CHECK GOOD.SDR ASAA2021041734610Spring · brokenFLIGHT CONTROLS BEHAVING HYPER SENSITIVE AND DO NOT PROVIDE THE NORMAL FEEDBACK PRESSURE. ON TAKEOFF MY NORMAL FLIGHT CONTROL PRESSURE CAUSED A HIGH RATE OF ROTATION THAT WAS EVEN NOTICED BY THE NON-FLYING PILOT. DURING ALL PHASES OF FLIGHT THE CONTROLS FELT MSDR HNAA2021030700088Warning Message · false activationSPS 1 INOP ON TAKEOFF ROLL. CMC MSG OF SPC FAIL. CMC MSG SPC FAIL FOLLOWED FIM 27-36-00-810-807-A BLOCK 1 OPS CHECK AMM 27-36-00-700-801-A SPS OPS CHECK GOOD FOUND TO BE TRANSITORY CONDITION. OK FOR SERVICE.SDR SIMA20210302002Elevator System · malfunctionedLH ELEVATOR FAILED IN CRUISE. PERFORMED E175 FIM TASK 27-03-00-810-90Y-A AND RTS CHECK IAW AMM 27-00-00. OPS CHECK GOOD. TRANSITORY CONDITION OF FLIGHT CONTROL SYSTEMSDR MASA2021022800056Control System · malfunctionedABORTED TAKEOFF- ELEVATOR CONTROL MALFUNCTIONSDR SWIA202156357Control Rod · corrodedLEFT ELEVATOR CONTROL ROD 600-92602-81 AFT ROD END BEARING IS CORRODED AND HAS ROUGH MOVEMENT. (C-CHECK) RO 2/17/2021. REMOVED AND REPLACED LT ELEVATOR CONTROL ROD IAW CRJ200 AMM 27-31-35-400-801, RIG CHECK GOOD IAW CRJ 200 AMM 27-31-00-830-805, AND OPS CHECSDR HNAA2021010400003Warning Message · false activationDURING T/O ROLL, SPS2 INOPERABLE EICAS WARNING MESSAGE. T/S IAW FIM 27-36-00-810-807A TO STEP 3. R & R SPC IAW 27-36-02/400. OPERATIONS CHECK GOOD. OK FOR SERVICE AT THIS TIME.SDR AWKA2020121601Actuator · malfunctionedDURING CLIMB OUT FROM PBI, FLIGHT CREW RECEIVED AN AMBER "PITCH FEEL FAIL" CAS MESSAGE. CHECKLIST STATES TO LAND AS SOON AS POSSIBLE, SO THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO PBI, WHERE THEY LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTSDR SWIA202055311Bolt · corrodedLT ELEVATOR POSITION TRANSMITTER HAS CORRODED HARDWARE. C-CHECK RO 1/5/2021. REPLACED ELEVATOR POSITION TRANSMITTER HARDWARE LT, PER CRJ 700 AMM 27-34-10-400-801-A01. INSTALLED NEW 2 EA BOLTS, 3 EA WASHERS, 2 EA NUTS. OPERATIONAL TEST GOOD.SDR AALA202011309016Computer · defectiveAIRCRAFT WAS GROUNDED. DURING ROTATION JUST AFTER LIFTOFF AT AN IAS OF 166KIAS FELT A SLIGHT BUT NOTICEABLE INCREASE IN ELEVATOR FEEL FORCE WITH A MOMENTARY SLIGHT PULSATION IN THE ELEVATOR FOLLOWED WITHIN 1 SEC. BY ILLUMINATION OF THE FEEL DIFF PRESS LIGHT.SDR SWIA202055518Control Lever · corrodedLT AND RT ELEVATOR CONTROL LEVER ASSEMBLIES HAS EVIDENCE OF CORROSION AT UPPER AND LOWER LEVERS. C-CHECK RO 1/16/2021. REMOVE AND REPLACED LT AND RT ELEVATOR CONTROL LEVER UPPER AND LOWER LEVERS, IAW CRJ-200 AMM 27-31-35-000-801 AND 27-31-35-400-801. OPERATSDR DXTA2020110104330Control Unit · defectiveAT APPROXIMATELY 150' AGL THE PRIMARY TRIM FAIL LIGHT CAME ON AND THE TRIM STARTED TO RUN AWAY NOSE UP. I PRESSED THE AP/TRIM/NWS DISC BUTTON WHICH STOPPED THE NOSE TRIM UP CONDITION. DURING THE PROCESS HEAVY PRESSURE WAS REQUIRED TO STOP THE NOSE FROM RISINSDR FDEA202010302721Control Unit · wornEXCESSIVE ELEVATOR PLAY, FIRST FEW INCHES OF ELEVATOR YOLK INPUT, A DEAD SPOT WAS NOTED, WHERE THERE WAS VERY LITTLE RESISTANCE OR FEEL. VERY NOTEABLE DURING TO AND LANDING PHASE. PERF CAT I AUTOLAND AS FUNCTION CHECK AND OPERATIONS CHECKED GOOD. REMOVED ASDR 2020FA0000484Bearing · corrodedDISCREPANCY: WHILE DOING CONTROL CHECK NOTICED THE CONTROLS FELT COARSE AND HAD RESISTANCE. THEY DID NOT FEEL SMOOTH. THE CONTROLS STAY ON THE LAST POSITION AND DO NOT RETURN TO NEUTRAL POSITION. CORRECTIVE ACTION: ISOLATED LT AND RT ELEVATORS AT UPPER BELLSDR GTIA2020100835377Computer · faultedF/CTL ELAC 2 PITCH FAULT. ACCOMPLISHED TROUBLESHOOTING TASK 27-93-00-810-836-A SUBTASK 27-93-00-810-285-A/27-93-00-700-084-A/27-93-00-810-085B TASK 27-44-51-220-004-A/27-44-51-7810-802-A AND OPERATIONAL TEST OF THE THS ACTUATOR ELECT. CONTROL TSM 27-96-00-71SDR SWIA202053512Control Rod · corrodedRT ELEVATOR SYSTEM MECHANICAL CONTROL PATH INPUT ROD BEARING AND HARDWARE LOCATED AFT END OF VERTICAL STABILIZER CANTED RIB APPEARS TO HAVE CORROSION (RUST). C-CHECK RO 10/18/2020. REMOVED AND REPLACED LT ELEVATOR CONTROL PATH INPUT ROD AND FWD AND AFT HARDWSDR SWIA202053511Control Rod · corrodedLT ELEVATOR SYSTEM MECHANICAL CONTROL PATH INPUT ROD BEARING AND HARDWARE LOCATED AFT END OF VERTICAL STABILIZER CANTED RIB APPEARS TO HAVE CORROSION (RUST). C-CHECK RO 10/18/2020. REMOVED AND REPLACED LT ELEVATOR CONTROL PATH INPUT ROD AND FWD AND AFT HARDWSDR AALA202009249015Warning Message · false activationAIRCRAFT WAS NOT GROUNDED. ON TAKEOFF, FLIGHT CONTROL ELEVATOR SERVO FAULT APPEARED. ABORTED TAKEOFF. FAULT EXTINGUISHED BEFORE RETURNING TO GATE. CLASS II (F/CTL) FAULT MESSAGE ON ECAM. INTERROGATES SEC 1 COM FAULT. PERFORMED AMM TASK 27-94-00-710-002-ASDR 2020FA0000508Attach Bracket · brokenTHE TAIL TRIM ASSIST BRACKET BROKE ALONG THE MOUNTING FLANGE EDGE WHERE THE PUSH PULL ROD FOR ASSIST MECHANISM ATTACHES TO THE TAIL CONE.SDR SIMA202009098005Warning Message · illuminatedSPS 2 INOP WARNING AND SPS ADVANCED CAUTION ON EICAS DURING APPROACH TO LANDING. C/A PERFORMED FIM TASKS 27-36-00. SPS ADVANCED MESSAGE REMAINS, SEE AML 4558647 ITEM 2 FOR CONTINUED DISCREPANCY.SDR SWIA202052198Control Cable · frayedLEFT ELEVATOR DOES NOT MOVE UP DURING FLIGHT CONTROL CHECK. RIGHT ELEVATOR DOES NOT MOVE FULLY DOWN. RESISTANCE ON YOKE IS LIGHT WHEN PULLING AFT OF CENTER, BUT IT IS STRONG WHEN MOVING FORWARD OF CENTER. OUTSIDE OBSERVATION AFTER RETURNING TO GATE SHOWS LESDR YENA2020083100437Servo Control · failedFLT 119, ALB-MCO. ON DESCENT AT APPX. 16' K NOTICED VIBRATION. FA IN AFT CALLED AND ADVISE DRASTIC VIB IN REAR OF A/C. GALLEY AND FLOOR VIB; REF. T/S FOUND RH ELEV SERV CONTROL FIN 34CE2 OSCILLATING R & R RH ELEV SERVO CONTROL FIN 34CE2.SDR BO5F20200818003Control Unit · misinstalledDURING A 12M/800 HRS INSPECTION, THE PITCH AFU WAS FOUND INSTALLED UPSIDE DOWN. THE AMM TASK CARD 27-35-05-900-801 REMOVAL/INSTALLATION OF THE PITCH MAIN AFU INCLUDES A SPECIFIC WARNING TO PREVENT THIS INCORRECT INSTALLATION: THE PITCH MAIN AFU (524CW) IS INSSDR YENA2020073000406Servo Valve · failedFLT 1584, VERTICAL VIBRATION FOR 20-30S AIRSPEED 321 VIBRATION CAME AND WENT AT CONT SPD SLOWED IAS AND DID NOT RETURN. TROUBLESHOT IAW TSM 05-50-00-810-801A, IDENTIFIED ELEVATOR AT FAULT IAW DECISION TABLE. NO EXCESSIVE PLAY ON SERVOS OR HINGES NOTED; NOSDR YENA2020073000405Servo Control · failedFLT 1485, AIRFRAME VIBRATION IN FLIGHT, R & R THE RIGHT INBOARD SERVO CONTROL FOR THE ELEVATOR IAW AMM 27-34-51.SDR YENA2020073000404Servo Control · failedFLT 1485, AIRFRAME VIBRATION IN FLIGHT. R & R THE RIGHT INBOARD SERVO CONTROL FOR THE ELEVATOR IAW AMM 27-34-51.SDR IPXA2020071097582Fitting · wornINSPECTION TYPE:3CR/H I/B ELEVATOR O/B CAM FITTING IS WORNREMOVED,REPAIRED AND INSTALLED WORN RH I/B ELEV O/B CAM FITTING IAW VT SAA EA # 011-5520-01-A8384 I/R AND UPS EO MD11-5520-77027-A. (MINOR)SDR CVGA20200706001Control Cable · out of toleranceWHILE AT ALTITUDE (41,000FT) ELEVATOR (E) AMBER, THEN RED ILLUMINATED ON PFD, FOLLOWED BY AN OSCILLATING PITCH UP (APPX 3-5 DEGREES) AUTOPILOT WAS ENGAGED DURING THIS EVENT AND WAS DISCONNECTED. AN ELECTRIC SMOKE ODOR WAS THEN DETECTED BY BOTH CREW MEMBERS ASSDR AALA2020062549021Computer · defectiveAIRCRAFT GROUNDED, ABORTED TAKE-OFF. WHEN ADVANCING THRUST AT TAKE-OFF, FLIGHT CONTROL SPOILER 1 AND 2 FAULT. REMOVED AND REPLACED SEC (SPOILER ELEVATOR COMPUTER) 3 PER TSM 27-94-00 AND AMM 27-94-34, OPERATIONAL CHECK OKAY.SDR IPXA2020042954774Bearing · failedEMERGENCY DECLARED, AIRCRAFT PITCH BEGAN FEELING HEAVY IN CLIMB, GOT PROGRESSIVELY WORSE APPROACH FLIGHT CONTROLS BEGAN EXTREMELY HEAVY. UPON SAFE TAXI THE EMERGENCY WAS CANCELLED; NO EQUIP USED. REMOVED AND REPLACED UPPER BEARING ON LT NR 5 RIB BELLCRANK, SDR FDEA202004130739Unknown · malfunctionedUP ELEVATOR JAMMED DURING FLARE. ABLE TO FORCE CONTROLL COLUMN AFTER LANDING. VERIFIED ELEVATOR BUS SUPPORT IN GOOD CONDITION REF AMM 27-31-01-4-0. LOAD FEEL CHECK PASSED REF AMM 22-00-03-700-801. INSPECTED ALL ACCESABLE SECTORS, PULEYS, CONT. ROD AND CABLSDR FDEA202003270609Warning System · false activationPDIS 971 27-30 6467 ON CLIMB IN CLEAR CONFIGURATION RECIVED EICAS MSG RUDDER RATIO AND MACH / SDD TRIM (AND OVERHEAD LT) ALONG WITH ELEV ASYM ON STATUS PAGE, NO AUTO PILOT, RAN QRH, NO HELP, CONTACTED GOC & COORDINATED RETURN TO SERVICE PERFORMEDSDR HALA2020032500073Relay · failedAUTO TRIM FAIL ILLUMINATED DURING DESCENT APPROXIMATED 10000 FEET. WARNING WENT OUT AFTER LANDING.// REMOVED AND REPLACED ELV UP AND DOWN TRIM REPLAY PER 27-43-0. RTS PASSED PER 22-00-00. ALL TEST PASSED. OK FOR SERVICE.SDR MASA2020031600122Pitch Control · failedPTICH FEEL CAUTIONSDR A6WA2020032747247Control Cable · frayedL/H VERTICAL STABILIZER AUTO PILOT HAS RUST AND & FRAYED CABLE. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED FRAYED CABLES P/N 601R90020-131 & 601R90020-79, ELEVATOR SERVO MOTOR P/N 622-5027-101, AND CLUTCH ASSY 822-0260-001. OPS CHECKS OK AT THIS TSDR ASAA2020030332342Spring · brokenON THE GROUND AND DURING TAKE OFFS AND LANDINGS THE ELEVATOR FEEL ON PULLING AND PUSHING THE CONTROL WHEEL YOKE WAS UNUSUALLY LIGHT AND MUSHY. WE NEVER GOT A FEEL DIFF PRESS LIGHT. ALL HYDRAULIC PRESSURES AND QUANTITIES INDICATED NORMAL. GROUNDED - YES. FOUND SDR ASMF202006009Computer · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXIING. MAINTENANCE PERSONNEL PERFORMED THE FIM 27-31 TASK 812/813 PROCEDURE CONTINUING FAILURE. ELEVATOR FEEL COMPUTER WAS REPLACED IAW MM 27-31-37-000/400-801, TEST CORRECT.SDR O2GA2020021850601Actuator · lack of lubeAT FL400 THE PITCH TRIM ANNUNCIATOR ILLUMINATED WITH AUTOPILOT ON. THE PITCH TRIM WHEEL WAS FROZEN IN PLACE AND REMAINED THAT WAY UNTIL ABOUT 6,000 FT. EMERGENCY DECLARED, DIVERTED TO STL AND LANDING WAS UNEVENTFUL. MAINTENANCE LUBED LEFT AND RIGHT ELEVATOR PI
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