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.

SDR MASA2020021300064Stall Strip · inoperativeSTALL FAIL IN FLT - DIVERTED. PLACED ON MELFeb 13, 2020 · N942LR · Cndair CL6002D24SDR EPUA20200210001Elevator System · bindingDURING FLIGHT PILOT REPORTS THAT "ELEVATOR IS GETTING HUNG UP. VERY STIFF ON CONTROL OF ELEVATOR". MAINTENANCE IS CURRENTLY INSPECTING AIRCRAFT FOR THE NOTED DEFECT.Feb 7, 2020 · N15503 · Beech 1900CSDR SWIA2020031049225Damper · corroded*RH ELEV CENTER HINGE INBD FLUTTER DAMPER CORRODED HARDWARE AT ELEV ATTACH POINT (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED RH ELEVATOR INBD AND OTBD FLUTTER DAMPER CORRODED HARDWARE REF. CRJ-200 AMM. PERFORMED OPERATIONAL TEST OF THE ELEVATOR COJan 22, 2020 · N905EV · Cndair CL6002B19SDR IPXA2020021091961Cam · gougedINSPECTION TYPE:2CELEVATOR LOAD FEEL ASSEMBLY CAM HAS GOUGE DAMAGE.REPAIRED DAMAGED ELEVATOR LOAD FEEL ASSEMBLY CAM IAW VT-SAA EA 011-2730-01-A8010 REV. I/R AND UPS EO MD11-2730-75438-A. (MINOR)Jan 14, 2020 · N288UP · Doug MD11FSDR ASAA2020011331832Pcu · bindingREF LP 11995043, BINDING IN FLIGHT CONTROLS CONTINUE IN THE FWD AND AFT POSITION. MUCH MORE NOTICABLE WHEN RELEASED AFTER BEING PUSHED TO THE FULL FWD POSITION. DID NOT CHECK LEFT AND RIGHT MOVEMENT. GROUNDED - YES. TROUBLSHOT TO A FAULTY A SYSTEM ELEVATOR PCUJan 10, 2020 · N492AS · Boeing 737990ERSDR AALA202001069018Spring · brokenAIRCRAFT IN BASE VISIT: DURING L/H ELEVATOR TAB INSPECTION, FOUND LOWER R/H SPRING BROKEN. REPLACED LOWER R/H TAB CONTROL MECHANISM SPRING (LT ELEV) IAW AMM 27-31-34.Jan 1, 2020 · N992AN · Boeing 737823SDR HNAA2019121100383Sensor · failedSPS 1 INOP MSG ON T/O ROLL...FIX:R&RD #1 AOA SENSOR IAW EMB AMM 27-36-01-04 OPS CHECK GOOD. OK FOR SERVICEDec 10, 2019 · N652RS · Emb EMB145LRSDR QXEA2019112700432Elevator · bindingAFTER ENGINE START, DURING CONTROL CHECK WHEN PERFORMING AFT ELEVATOR CHECK THERE IS A BINDING VIBRATION UNTIL BACK TO NEUTRAL. CHECKED MULTIPLE TIMES. THE VIBRATION WAS CONSISTENT. BOTH CA AND FO SIDES HAD SAME ISSUE. AIRCRAFT REMOVED FROM SERVICE. INTERROGATNov 27, 2019 · N651QX · Emb ERJ170200LRSDR VNAA2019111521103Warning Message · false activationFLIGHT 5513 RECEIVED MULTIPLE PITCH FEEL FAULT CAUTION MESSAGES IN FLIGHT. THE CREW RAN THE QRH AND CONTINUED TO DCA WHERE THEY LANDED WITHOUT INCIDENT BUT DID DECLARED AN EMERGENCY AS A PRECAUTION, EMERGENCY VEHICLES DID RESPOND BUT WERE CALLED OFF AFTER THE Nov 12, 2019 · N505AE · Cndair CL6002C10SDR IPXA2019111148877Elevator · malfunctionedINSPECTION TYPE:N/A**SUPPLEMENTAL SDR**EMERGENCY DECLARED -** A/C TAKEN OOS**. ON DESCENT AUTOPILOT WAS MANUALLY SELECTED OFF ELEVATORS WERE EXCESSIVELY HEAVY TO LEVEL OFF THE AIRPLANE. AUTOPILOT REENGAGED WITH AN UNEVENTFUL APPROACH AND LANDING. REMOVED R/H ONov 8, 2019 · N258UP · Doug MD11FSDR SWIA2019110546710Control Cable · out of adjustELEVATOR AUTOPILOT CONTROL CABLE OUT OF TENSION LIMITS. (C-CHECK) RO: 11/04/2019 ADJUSTE AUTOPILOT CONTROL CABLES IAW AMM.Nov 5, 2019 · N679SA · Cndair CL6002B19SDR HNAA2019110400341Actuator · faultyPDIS 608 27-31 2128242 03NOV19 CLT CLOSE CONTROL COLUMN FEELS LIKE IT CATCHING ON SOMETHING WITH INCREASED FRICTION WHEN PULLED BACK ACCOMPANIED BY FAINT CLICKING NOISES FACT 03NOV19 06:54 ROA FOUND STICK PUSHER ACTUATORNov 3, 2019 · N608LM · Emb EMB145LRSDR AALA201911019009Control Servo · malfunctionedAIRCRAFT IN BASE VISIT: ELEVATOR VIBRATION (BUZZ) WHEN SLIGHT PRESSURE APPLIED EITHER UPOR DOWN, FELT AT ALL ALTITUDES AND SPEEDS IN ALL CONFIGURATIONS.ALSO FELT ON GROUND IN COCKPIT. REMOVED AND REPLACE I/B ELEVEVATOR SERVO CONTROL LT IAW AMM 27-34-51-400-001Oct 31, 2019 · N768US · Airbus A319112SDR AALA201910289017Hinge Fitting · wornAIRCRAFT NOT GROUNDED: VERTICAL VIBRATION DURING CLIMB THROUGH FL190 AT SPEEDS ABOVE 315 KTS, SLOWING DOWN IMPROVED IT. NOT PRESENT DURING DESCENT. OAT6C DURING CLIMB. REMOVED AND INSTALLED NEW HINGE FITTING (#5) AND HARDWARE ON #2 FITTING. SEE AALA20191028902Oct 23, 2019 · N715UW · Airbus A319112SDR AALA201910289025Servo Control · wornAIRCRAFT IN BASE VISIT: DURING ELEVATOR FREE-PLAY CHECK, FOUND R/H ELEVATOR FAILS FREEPLAY CHECK WITH YELLOW, INBOARD SERVOCONTROL ISOLATED. (7.3MM) REMOVED WORN I/B SERVO CONTROL AND INSTALLED SERVICEABLE SERVOCONTROL (34CE2) IAW A320 AMM 27-34-51-400-001A. AOct 23, 2019 · N715UW · Airbus A319112SDR DJSR201910243001Trim System · out of limitsDURING TAKEOFF PHASE, YOKE HIT MECHANICAL STOP BEFORE AIRPLANE PITCH DOWN OCCURRED. CREW TRIMMED TAIL PLANE ACTUATOR NOSE DOWN, WHICH CORRECTED THE PROBLEM. CREW RETURNED TO DEPARTURE AIRPORT.Oct 23, 2019 · N581FL · Amd FALCON20F5SDR DJSR201910248001Feel Unit · erraticAFTER TAKEOFF PITCH CONTROL ARTIFICIAL FEEL BECAME ERRATIC/SLUGGISH. ABORTED FLIGHT AND RETURNED TO DEPARTURE AIRPORT.Oct 18, 2019 · N581FL · Amd FALCON20F5SDR DALA2019101605932Sensor · failedELEVATOR SPLIT INDICATION IN FLIGHT 12000 MSL 320 KTS. T/S PER NO-GO ODI PROCEDURES. CONFIRMED CONTORL COLUMNS NOT DISCONNECTED. VISUALLY CONFIRMED ELEVATOR SURFACES MOVE TOGETHER . DFGC FAULT REVIEW SHOWED ELEVATOR POS 1 SENSOR SIGNAL FAILURE FOR LAST 4 FLIGHOct 15, 2019 · N936DN · Doug MD9030SDR QXEA2019101400383Actuator · leakingIN FLIGHT EICAS MESSAGE "HYD 2 LO QTY" LIGHT ILLUMINATED. ON FINAL APP AFTER LANDING GEAR WAS LOWERED "HYD 2 PUMP FAIL". RAN QRH CHECKLIST. MISSED APPROACH PERFORMED, AND LANDED SAFELY. DURING FLIGHT SYSTEM 2 HYD LEVEL WENT FROM 20% TO 0 % WAS NOTED AFTER LANDOct 12, 2019 · N646QX · Emb ERJ170200LRSDR UATA2019101424209Control Cable · frayedFOUND CO-PILOT'S ELEVATOR FORWARD DOWN CABLE FRAYED WITH BROKEN STRANDS. REPLACED CABLE WITH A NEW ASSEMBLY.Sep 18, 2019 · Casa C212CCSDR UATA2019101424208Control Cable · frayedCOPILOT'S FORWARD ELEVATOR UP CABLE IS FRAYED WITH BROKEN STRANDS. REPLACED CABLE ASSEMBLY WITH NEW.Sep 18, 2019 · Casa C212CCSDR UATA2019101414207Control Cable · frayedPILOTS FORWARD ELEVATOR DOWN CABLE WAS FOUND FRAYED WITH BROKEN STRANDS. A NEW CABLE ASSEMBLY WAS INSTALLED.Sep 18, 2019 · Casa C212CCSDR UATA201910144206Control Cable · frayedPILOTS FWD ELEVATOR UP CABLE IS FRAYED WITH BROKEN STRANDS. REPLACED CABLE ASSEMBLY WITH NEW.Sep 18, 2019 · N424CA · Casa C212CCSDR SWIA2019101846526Control Cable · damagedWHILE PERFORMING TENSION CHECK OF THE ELEVATOR CONTROL CABLES FOUND THE RH ELEVATOR CONTROL CABLE CIRCUIT TO BE OUT OF LIMITS. AT 70 DEGREES THE MEASUREMENT IS 120, THE ALLOWABLE MEASUREMENT AT 70 DEGREES IS 125-135 (C-CHECK) RO: 10/16/2019 PERFORMED RIGGING TSep 17, 2019 · N979SW · Cndair CL6002B19SDR VNAA2019090911102Transmitter · out of rigIN LEVEL FLIGHT CREW RECEIVED ELEVATOR SPLIT CAUTION MESSAGE. CREW RAN THRU THE QRH, DECLARED AN EMERGENCY AND LANDED GSP WITHOUT INCIDENT. RE-RIGGED/INDEXED LEFT ELEVATOR POSITION TRANSMITTER. SYSTEM OPS CHECKED GOOD.Sep 9, 2019 · N607NN · Cndair CL6002D24SDR DALA2019081534767Bearing · damagedLEFT HORIZONTAL MIDDLE PCA INPUT ROD - ROD END BEARING RUSTED AND FROZEN. REPLACED POGOPER B757 AMM 27-31-06.Aug 12, 2019 · N692DL · Boeing 757232SDR FDEA201908071817Relay · malfunctionedELEVATOR EXTREMLY STIFF ON LANDING RUNWAY 36L KMEM. GW 238.4 LBS. STAB TRIM 3.8 NOSE UP. NR 2 FLC FAULT LIGHT ON PITCH FEEL POWER LOOP. REPLACED RELAY 308CY2 IAW TSM 27-33-01 FIGURE 103. PERFORMED OPS TEST IAW AMM. OPERATIONAL TEST GOOD. OK FOR SERVICE.Aug 7, 2019 · N683FE · Airbus A300F4605RSDR CA190812013Control Servo · failed(CAN) ON TAKEOFF OF NO MORE THAN 45 KNOTS, MESSAGE OF ELAC 1 PITCH FAULT. CREW FOLLOWED THE QRH AND RESET THE ISSUE AND DEPARTED AGAIN WITHOUT INCIDENT. RESOLUTION ELEVATOR SERVO 34CE4 REPLACED IAW AMM 27-34-51/401. RIGGED IAW AMM 27-34-00-820-002-A AND CHK`DAug 4, 2019 · Airbus A319114SDR CA190807006Nut · missing(CAN) WHILE CONDUCTING A PHASE 4 INSPECTION ON THE EMPENNAGE SECTION OF C-XXXX, ONE OF THE ENGINEERS OPENED A BUTTON SIZE COVER (APPROXIMATELY 1 AND A HALF INCH DIAMETER) TO HAVE A LOOK AT THE ELEVATOR BELLCRANK. AFTER REMOVING THE COVER, HE FOUND THAT THERE WAug 2, 2019 · Beech B200GTSDR CA191004003Control Unit · malfunctioned(CAN) AFTER A FAIRLY ABRUPT LEVEL OFF AT ALTITUDE RECEIVED AN ELEVATOR SPLIT CAUTION MSG. RAN QRH AND RETURNED TO FIELD. CORRECTIVE ACTION: FOUND THE RH ELEVATOR DID NOT REACH FULL `UP` TRAVEL ON EICAS AND THE ELEVATOR SURFACE DID NOT PHYSICALLY MOVE FULL `UPJul 22, 2019 · Cndair CL6002C10SDR UATA2019072211119Control Cable · frayedFOUND RT FWD UP ELEVATOR CABLE (OUTBOARD) HAS MULTIPLE BROKEN STRANDS. REPLACED CABLE WITH NEW.Jul 11, 2019 · N352CA · Casa C212CCSDR UATA2019072201119Control Cable · frayedFOUND LT FWD UP ELEVATOR CABLE (OUTBOARD) TO HAVE MULTIPLE BROKEN STRANDS. REPLACED CABLE WITH NEW.Jul 11, 2019 · N352CA · Casa C212CCSDR R61A201906090700Disconnect Unit · faultedPITCH CONTROL DISCONNECT/AP FAIL IN FLIGHT. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. R&R ELEVATOR/PITCH CONTROL COLUMN DISCONNECT DEVICE IAW AMM 27-31-06. OPS CHECK GOOD.Jul 9, 2019 · N637RW · Emb ERJ170100SESDR FDEA201907051488O-Ring · rupturedGOT A "L HYD QTY" EICAS MESSAGE APROXIMATELY 2.5 HOURS INTO FLIGHT. L HYD QTY WAS .46 ON STATUS PAGE WITH RF MAGENTA. ALSO HAD "QTY" LIGHT ON OVERHEAD. HYD QTY .07 ON SHUTDOWN. FLIGHT CREW VERBALLY RELAYED TO ACMX THAT THE LEFT HYDRAULICS NEVER LOST PRESSUREJul 5, 2019 · N157FE · Boeing 7673S2FSDR DALA2019070203983Position Sensor · faultyELEVATOR SPLIT MESSAGE DISPLAYED ON OAP IN FLIGHT. FOUND RT ELEVATOR POSITION SENSOR SHOWING 78.53 DEGREES TEU WHEN FAIRED. R/R RT ELEVATOR POSITION SENSOR PER AMM 27-34 AND WDM 22-11. PERFORMED ACS RTS AND CLEARED LOCKED FAULT. MESSAGE CLEARED OPS NORMAL. (LPJul 1, 2019 · N927DN · Doug MD9030SDR SIMA20190613001Switch · dirtyAFTER TAKEOFF, CAPTAIN'S PITCH TRIM WOULD NOT WORK. PTRIM MAIN INOP THEN DISPLAYED ON EICAS-C/A-CLEANED CAPT'S AND 1ST OFFICERS PITCH TRIM SWITCHES. PERFORMED OPS CHECK, OPS CHECK GOOD IAW EMB 140 AMM 27-40-04Jun 13, 2019 · N836AE · Emb EMB135KLSDR CA190612006Guard · worn(CAN) DURING SCHEDULED MAINTENANCE A CABLE GUARD PIN BRACKET FOR THE RIGHT HAND ELEVATOR CABLE CIRCUIT WAS OBSERVED TO BE WORN AT THE GUARD PIN HOLE ALLOWING THE GUARD PIN TO SLIDE FROM THE HOLE AND THUS INEFFECTIVE. BRACKET TO BE REPLACED IAW THE SRM. AIRCRAFJun 12, 2019 · Bombdr DHC8400SDR CA190607011Warning Message · false activation(CAN) R ELEVATOR FAIL CAUTION IN CRUISE. TROUBLESHOOTING CARRIED OUT, FAULT CLEARED, BIT TEST SATIS AIRCRAFT BACK IN SERVICE. (TC# 20190607011)Jun 6, 2019 · Airbus BD5001A11SDR CA190604017Turnbuckle · cracked(CAN) DURING A PHASE 3 INSPECTION, INSPECTION OF THE DOWN ELEVATOR CABLE TURNBUCKLE REVEALED A CRACK EMANATING FROM ONE END AND PROGRESSING TO VERY CLOSE TO THE CENTER OF THE TURNBUCKLE HOLE. USING A 10 POWER MAGNIFIER IT APPEARS THAT THE CRACK ENDS IN CLOSE PJun 3, 2019 · Beech 200BEECHSDR AALA201906049041Computer · faultyAIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT STAB TRIM ISSUES WITH AUTO-PILOT FAIL. STAB TRIM WOULD JUMP 8 UNITS A/C PITCH UP A/P WOULD KICK OFF RECOVERED TRIED A/P 2 SAME AFTER MULTIPLE FAILS A/P OFF STILL GOT FAULT UNTIL ELAC 1 AND ELAC 2 PITCHJun 2, 2019 · N737US · Airbus A319112SDR AALA2019060439039Computer · faultyAIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT STAB TRIM ISSUES WITH AUTO-PILOT FAIL. STAB TRIM WOULD JUMP 8 UNITS A/C PITCH UP A/P WOULD KICK OFF RECOVERED TRIED A/P 2 SAME AFTER MULTIPLE FAILS A/P OFF STILL GOT FAULT UNTIL ELAC 1 AND ELAC 2 PITCHJun 2, 2019 · N737US · Airbus A319112SDR CA190605008Elevator System · malfunctioned(CAN) WHEN THE CREW ROTATED THE AIRCRAFT, THERE WERE NO RESPONSE TO PITCH CONTROL INPUT AND THE CREW ELECTED TO EXECUTE A REJECTED TAKEOFF. THE AIRCRAFT IS CONFIGURED IN A Y29 COMBI VERSION (HUNTING CARGO/COMBI 8/2822) WITH 28 ADULT AND ON CHILD + 412 KGS BAGSMay 30, 2019 · Dhav DHC8202SDR AALA201905269010Computer · inaccurateAIRCRAFT WAS GROUNDED: PILOT REPORTS AIRFRAME VIBRATION ABOVE APPROX FL 180 AND ABOVE 300 KTS. VIBRATION WAS APPROX 7-10 CYCLES/SECOND. MAINTENANCE REMOVED AND REPLACED THE #1 ELEVATOR AND AILERON COMPUTER IAW AMM 27-93-34 & REMOVED AND REPLACED THE RT ELEVATOMay 23, 2019 · N834AW · Airbus A319132SDR AALA201905279011Servo Control · out of toleranceAIRCRAFT WAS GROUNDED: PILOT REPORTS AIRFRAME VIBRATION ABOVE APPROX FL 180 AND ABOVE 300 KTS. VIBRATION WAS APPROX 7-10 CYCLES/SECOND. MAINTENANCE REMOVED AND REPLACED THE #1 ELEVATOR AND AILERON COMPUTER IAW AMM 27-93-34 & REMOVED AND REPLACED THE RH ELEVATOMay 23, 2019 · N834AW · Airbus A319132SDR CA190430001Bolt · loose(CAN) CONTROL COLUMN STICKS/CATCHES WHEN PULLING AFT DURING FLIGHT CONTROL CHECK. COULD NOT DUPLICATE AT FIRST, EXCEPT PLAY IN DISCONNECT MODULE. PUT FINGERS ON THE BOLTS THAT HOLD THE DISCONNECT TO THE PILOTS TORQUE TUBE AND THE BOTTOM TWO WERE TIGHT BUT SHAApr 29, 2019 · Bombdr BD1001A10SDR FDEA2019042650929Unknown · vibrationON APPROACH AT 150 FT A STRANGE /MODERATE ELEVATOR RYTHMIC VIBRATION, ALMOST NOT CONTROTABLE ACCURED, LASTED ALL THE WAY TO LANDING FLAP 25 137 KTS WIND 190 AT 12 GUST 18. PERFORMED BITE ON BOTH SAM COMPUTERS, NO FAULTS FOUND, PERFORMED A BITE CHECKS ALLApr 25, 2019 · N781FD · Boeing 757222SDR 3SVA20190425001Push-Pull Rod · corrodedDUE TO AGING AIRCRAFT CONCERNS THIS OPERATOR HAS EMBARKED ON A FLEET CAMPAIGN TO REMOVE THE ELEVATOR PUSH PULL TUBES FROM THE C441 AIRCRAFT AND SEND THEM OUT FOR AN XRAY INSPECTION. WE HAVE PERFORMED INSPECTIONS ON FOUR TUBES P/N 5815144-204 (ORIGINAL P/N 581Apr 25, 2019 · Cessna 441SDR CA190424012Rod End · worn(CAN) ROD END ATTACHMENT RIVETS LOOSE/SMOKING. ROD REPLACED WITH NEW. (TC# 20190424012)Apr 24, 2019 · Dhav DHC2MK3SDR CA190424016Rod End · worn(CAN) ROD END ATTACHMENT RIVETS LOOSE/SMOKING. ROD REPLACED WITH NEW. (TC# 20190424016)Apr 24, 2019 · Dhav DHC2MK3SDR CA190424015Rod End · worn(CAN) ROD END ATTACHMENT RIVETS LOSE/SMOKING. OF REPLACED WITH NEW (TC# 20190424015)Apr 24, 2019 · Dhav DHC2MK3
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