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 CA090211004Link · wornDURING THE REPLACEMENT OF THE BEARING IN THE ELEVATOR BELL CRANK ASSY, THE LINKS AND SPACERS WERE THE ELEVATOR CABLE ATTACHES WERE FOUND WORN, SPACERS WERE WORN RIGHT THROUGH (PN C2CF349ND). THE AN3 BOLT THAT ATTACHES LINK IN PLACE WAS WORN 1/3 THROUGH. SPACSDR HALA2009011500018Power Supply · malfunctionedETOPS SIGNIFICANT SYSTEM - "WARNING ELUX" EICAS MSG. PERFORMED FIM 31-51-00
AND RESET ELUX POWER SUPPLY B. MSG CLEARED. OPS CK GOODSDR CA090123004Torque Tube · cracked(CAN) WHILE ACFT WAS IN FOR MAJOR OVERHAUL AND PAINT, THE ELEVATOR BELLCRANK TORQUE TUBE WAS REMOVED FOR ROUTINE MX. THE BELLCRANK ARMS WERE FOUND LOOSE. AFTER THE ARMS WERE REMOVED THE STEEL TORQUE TUBE WAS NDT INSPECTED. CRACK INDICATIONS WERE FOUND ON TWO (SDR DXTA2008122403434Elevator System · stiffELEVATOR CONTROL FEELS STIFF.SDR DXTA2008122303434Control Cable · looseDURING CLIMB THROUGH 12,000 FT AT 200 KIAS, AUTO PILOT OFF, ELEVATOR CONTROL FELT STIFF FROM LT SEAT. AN ABNORMAL BUMP COULD BE FELT WHEN MOVING YOKE FORE AND AFT. ADDITIONALLY, A GRINDING SENSATION OR VIBRATION COULD BE FELT THROUGH THE FLOOR. ALL 3 SYMPTOSDR DXTA2008122003417Control Cable · frozenAT V/R ACFT WOULD NOT ROTATE WITH CONTROL INPUTS AND ELEVATOR /AIL TRIM LIGHT COME ON. DUE TO LOCAL ATMOSPHERIC CONDITIONS. (RAIN/ COLD WEATHER) SUSPECT MOISTURE FOUND IN LWR REAL EQUIPMENT BAY AREA MAY HAVE ACCUMULATED AND FROZE ON PRIMARY AND SECONDARY FLIGHSDR UALA2008122206926Actuator · faultyEICAS MESSAGE 'ELEV ASYM' IS DISPLAYED. REPLACED ASSY LIMITER ACTUATOR. CHECKS OKAY.SDR NOCA09208Arm · corrodedELEVATOR FEEL AND CENTERING UNIT INPUT ARM HAS LEVEL 1 CORROSION. REPAIRED INPUT ARM UNIT AS PER MM 27-31-17-055 AND PER ESO EAB757-27-005076.SDR DL76L081710Computer · malfunctionedAFTER PUSHBACK GOT STATUS MSG ELEV FEEL, IT CLEARED AFTER STARTING BOTH ENGINES READ NEEDED HYD PRESSURE IN MDM. AFTER A COUPLE OF MINUTES IT RETURNED AND WOULD NOT CLEAR. MSG FIRST APPEARED AFTER STARTING FIRST ENGINE. REMOVED AND INSTALLED ELEV FEEL COMPUSDR CA081222004Control Cable · corroded(CAN) DURING A PREFLIGHT, THE LEFT ELEVATOR DID NOT MOVE WITH THE CONTROL COLUMN INPUT. MAINTENANCE INVESTIGATED AND FOUND ONE OF THE CABLES SNAPPED UNDER THE LAVATORY. SUSPECT THAT A PREVIOUSLY REPAIRED LEAK FROM THE LAVATORY HAD LEAKED ON THE CABLES, AND TSDR UALA2008120106705Computer · faultyCREW COMMENTS: ELEVATOR FEEL STATUS MESSAGE. REPLACED ELEVATOR FEEL COMPUTER.SDR COEA2008120102775Torque Tube · corrodedTHE RT INBOARD CONTROL HORN ATTACHMENT RIVETS FOUND WORKING ON ELEVATOR TORQUE TUBE ASSY. RT ELEVATOR CONTROL HORN EXHIBITED ROTATIONAL AND LATERAL MOVEMENT ON TORQUE TUBE. RIVET HOLES, CONTROL HORN AND TORQUE TUBE EXHIBITED FRETTING CORROSION. REMOVED AND SDR COEA2008120101976Torque Tube · looseTHE LT INBOARD CONTROL HORN ATTACHMENT RIVETS FOUND WORKING ON ELEVATOR TORQUE TUBE ASSY. LT ELEVATOR CONTROL HORN EXHIBITED ROTATIONAL MOVEMENT ON TORQUE TUBE. UPON REMOVAL OF HORN FROM TORQUE TUBE, FOUND WEAR WAS LIMITED TO RIVETS. REMOVED AND REPLACED TORSDR DXTA200811233369Actuator · lack of lubeWHEN LEVEL AT 41 000 FT EXPERIENCED A (JAMMED ELEVATOR TRIM) (NO ELECTRIC OR MANUAL TRIM FORE/AFT) AFTER APPROX 20 MIN AND AT 10 000 FT TRIM MANUAL AND ELECTRIC STARTED WORKING AGAIN. LUBED ELEVATOR TRIM ACTUATORS WITH GREASE PN: 5565450-28 REF AMM 12-21-01. SDR DXTA2008112403369Elevator · jammedWHEN LEVEL AT 41,000 FT EXPERIENCED A, JAMMED ELEVATOR TRIM.SDR SWIA200820460Servo · bindingFLT 5749 - ELEVATOR BINDING. REPLACED NR 1 STICK PUSHER SERVO, PN 622-5734-002, SN ON 3079, SN OFF 3640.SDR UPS08854017Elevator · out of balanceINSPECTION TYPE:SV RIGHT ELEVATOR REQUIRES WEIGHT AND BALANCE. ACCOMPLISHED IAW 27-30-01-4.SDR DL764081504Computer · malfunctionedELEV FEEL EICAS MSG 1 HOUR INTO CRUISE. RETURNED TO ATL. FOUND FLUID IN DRAIN LINES. REPLACED THE ELEV FEEL COMPUTER PER AMM.SDR DXTA2008110303334Warning System · activatedPITCH FEEL FAIL" CAS MESSAGE ILLUMINATED IN FLIGHT. COMPLETED SUCCESSFUL OPS CHECK OF NK122 PITCH FEEL LOGIC MODIC IAW MM 45-24-10. OPERATED PITCH FEEL SYS AT VARIOUS AIRSPEEDS AND ALTITUDES AS DESCRIBED IN FUNCTIONAL TEST WITH NO FAULTS OR FAILURES IAW MM 27SDR CA081021006Jackscrew · frozen(CAN) CREW REPORT THE ELEVATOR TRIM WAS DIFFICULT TO MOVE IN FLIGHT. UPON INSPECTION BY MX IT WAS FOUND THE ACTUATOR WAS CORRODED INTERNALLY AND THE GREASE WAS CONTAMINATED AND HARDENED. HAWKER BEECHCRAFT ALREADY HAS SB 27-3840 R1 TO CHECK FOR THIS SAME ISSUE SDR CA081014002Control Tube · gouged(CAN) THE BOLT PN AN21-10 ATTACHING THE LT ELEVATOR CONTROL CABLE PN 0510105-90 TO THE LT BELLCRANK CONTROL ARM ASSEMBLY PN 0760686-1 IS RUBBING ON THE LT BELLCRANK CONTROL TUBE SUPPORT PN 0760693-1. THE DAMAGE IS 0.039 DEEP, 1.750 LONG AND 0.250 WIDE.SDR DL76G081336Indicator · malfunctionedON TAXI OUT ELEVATOR CONTROL POSITION INDICATOR SHOWS RIGHT ELEVATOR ONLY QUARTER MOVEMENT. LEFT INDICATOR NORMAL. INDICATION BACK NORMAL AFTER ENG SHUT DOWN AND APU PWR. RESTART ENG ALL IND NORMAL.SDR 2008FA0000703Bolt · out of adjustDURING A PHASE 1-4 INSPECTION ON AC. BOLT FOR ELEVATOR CONTROL SYS. WAS FOUND TO BE ADJUSTED ALL THE WAY DOWN AND WAS NOT PROVIDING A STOP FOR THE BALLAST. IN THIS CONDITION, THE POSSIBILITY EXISTS FOR THE INTERCONNECT LINK BETWEEN THE BALLAST WEIGHT BELLCRANSDR CA080930004Yoke · corroded(CAN) ASSEMBLY WAS FOUND CORRODED WHEN INSPECTED IAW SEB01-3.SDR DXTA200809193278Trim System · unknownAIRCRAFT RUNS OUT OF FWD TRIM NEAR VMO AT 25000 FT AND 310 KNOTS, THE TRIM WAS AT THE FWD STOP. UNABLE TO MOVE TRIM WHEEL FWD. T/S ELEVATOR TRIM BY COMPLYING WITH THE FOLLOWING TESTS, ELEVATOR CONTROL SYS FUNCTIONAL TEST, ELEVATOR TRIM CONTROL SYS FUNCTIONAL SDR DXTA200809123274Cable · looseACFT HAS AN AIRFRAME FLUTTER- INCREASE W/SPEED ABOVE 250KTS. SOME INDICATIONS W/ AP AND YD ON OR OFF, NOT NOTICED IN RUDDER OR AILERON FLUTTER APPEARS TO BE IN ELEVATOR. BALANCED LT AND RT ELEVATORS. FOUND ELEVATOR SERVO CABLE TENSIONS LOW. ADJUSTED TENSIOSDR 2008UALA05588Actuator · failedELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. LEFT ELEV GREEN ACT FAILING. REPLACED ELEV LG ACTUATOR 34CE1, OPS TESTED OK.SDR DL76G081140Elevator System · malfunctionedRT ELEVATOR IND NOT RESPONDING TO CONTROL INPUTS. VERIFIED ELEVATOR MOVEMENT PER MEL FWD TO MCO/PLAC PER MEL 27-08-01 YELLOW PLAC INSTALLED.SDR DL764081124Computer · malfunctionedELEVATOR FEEL EICAS MESSAGE DURING CLIMB-OUT. REPLACED ELEV FEEL COMPUTER PER AMM. LEAK CK OK. ADJ AND TEST CK OK PER 767-400 AMM. MFG NR 162900-100.SDR UALA2008111304268Control Unit · faultyFLIGHT CONTROL SYSTEM STATUS MESSAGE. REPLACED CENTER ACE AND B27143 COUPLER IN P312-E01 PANEL. FAULT CLEARED.SDR 26N2008F00002Control Cable · frozen7/24/2008, AC TT: 461.8, TC:302 CREW REPORTED AILERONS FROZEN AFTER FLYING THROUGH MOISTURE (FROM FORM 26NA-210A, ATTACHED) 7/25/2008, AC REPOSITIONED TO MFG SERVICE CENTER FOR FURTHER EVALUATION AND RESOLUTION. 8/1/2008, AC TT: 462.3 MFG MTR FOR RESOLUTION. SDR CA080723005Control Cable · frayed(CAN) CABLE WAS DISCOVERED FRAYED DURING REGULARY SCHEDULED MAINT.SDR 2008FA0000571Control Cable · brokenPILOT COMPLAINED OF POOR ELEVATOR TRIM OPS. UPON INSP, FOUND ELEVATOR TRIM CABLE 311AS-14-7245 BROKEN (RT CABLE). 311AS-14-7362 (LT CABLE), 010A-61179-81 (RT AFT) CABLES FRAYED. IDLER PULLEY SHAFT ON PITCH TRIM SERVO SHEARED. REPLACED CABLES & SERVO, OPS CSDR CA080806009Drive Assy · stripped(CAN) DURING CLIMB OUT AT 800 FEET ALTITUDE THE ACFT SUDDENLY STARTED TO SHAKE VIOLENTLY. THE PILOT ABORTED THE CLIMB, PROCEEDED STRAIGHT AHEAD FOR 4 MILES TO A LANDING STRIP AND LANDED SAFELY WITH NO INJURIES TO PERSONS ON BOARD. UPON INVESTIGATION AS TO THE SDR S9BA2008025Bellcrank · wornDURING AD 89-24-06 FOUND ELEVATOR BELL CRANK WORN. REMOVED AND REPLACED ELEVATOR BELL CRANK. NO OTHER DEFECTS NOTED. (S)SDR CA080818002Controller · frozen(CAN) APPROXIMATELY 50 MIN OUT, AUTOPILOT BEGAN TO CLIMB, THE A/P WAS DISCONNECTED AND ACFT MANUALLY BROUGHT BACK TO ALTITUDE. A/P WAS REENGAGED AND THEN BEGAN TO DESCEND FOLLOWED BY THE AP TRIM FAIL ANN. A/P DISCONNECTED, ELECTRIC TRIM CHECK AND APPEARED SERVSDR REX2008F00004Unknown · jammedON SHORT FINAL ELEVATOR CONTROL BECAME WHAT APPEARED TO BE "JAMMING" INTERMITTENTLY. ELEVATOR SYSTEM CHECKED GOOD ON GROUND. UPON FURTHER INSPECTION NOTICED VERTICAL STABILIZER VISOR PANELS DEFORMED. PANELS REMOVED, ELEVATOR ATTACHMENT POINTS, ATTACHMENT HASDR DXTA200803143Servo · inoperativeABORTED TAKEOFF AT APPROXIMATELY 130 KIAS DUE TO NO ELEVATOR AUTHORITY. REPLACED ELEVATOR SERVO MOTOR ASSY WITH OVH ASSY. PERFORMED SYSTEM CHECKS, TEST GOOD. ALL WORK IAW MM 22-10-30.SDR 2008FA0000520Jackscrew · damagedFOUND SCREW-DRIVE INTERNAL THREADS STRIPPED AND SAFETY SPLIT, PIN MISSING. PILOT HAD DIFFICULTY CONTROLLING ELEVATOR. PART HAD 196.2 IN SERVICE, SINCE REPAIR. RECOMMENDED TO INSPECT LT ELEVATOR TRIM TAB FOR EXCESSIVE PLAY IAW MM AS PART OF PREFLIGHT AND EVESDR 2008UALA03495Pcu · defectiveWHILE TROUBLESHOOTING DF053 WITH A RT ELEVATOR PCU MESSAGE, GOT LT PCU MESSAGE ON EICAS. TROUBLESHOT MESSAGE DOWN TO LT ELEVATOR RT PCU BAD. REPLACED PCU, OPS CHECKED GOOD.SDR 2008UALA03459Rod End · wornAIRFRAME VIBRATION ON CLIMBOUT. *S/D* LEFT OUTBOARD BLUE ELEVATOR ACT ROD END HAS PLAY. REPLACED LT OUTBOARD ELEV ROD.SDR SWAA083301Torque Tube · wornDURING SCHEDULED 20Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR UALA2008111303323Actuator · faultyCREW REPORTS EXCESSIVE CONTROL COLUMN FORCE REQUIRED FOR PITCH. REMOVED AND REPLACED ELEV FEEL ACTUATOR & ELEVATOR FEEL COMPUTER. ALSO REPLACED LT OUTBOARD AND INBOARD FLAP CARRIAGE ASSEMBLIES.SDR FIS2008F00000Fitting · crackedTHE COLLAR HAS A CRACK WHERE THE TAPER PIN GOES THROUGH. POSSIBLE SOMEONE OVER TORQUED THE TAPER PIN. (K)SDR 2008UALA03191Control Unit · faultyELAC 2 FAULT INDICATIONS. SERVO 34CE1 FAILING CAUSING ELAC 2 TO FAULT CHRONICALLY. REPLACED LT INBOARD ELEVATOR SERVO CONTROL UNIT 34CE1, ADJUSTED AND OPS TESTED OK.SDR 2008UALA03132Control Unit · faultyACTUATOR CONFIDENCE FAILED. MSG 27-10110, ELEVATOR POWER CONTROL UNIT (LEFT OUTBOARD) BLOCKING SOLENOID OPERATED VALVE IS NOT IN COMMANDED POSITION. AFTER EXTENSIVE TROUBLESHOOTING FOUND FAULTY L1 ACE. REPLACED L1 ACE, OP CHECK GOOD. AC OK FOR SERVICE.SDR DLM88080799Tab · wornDURING HMV3 WEAR WAS FOUND ON TRAILING EDGE OF LT ELEVATOR GEARED TAB. WEAR WAS REPAIRED IAW DRD 55-04D PARA 3D FIG 2.SDR QXEA200800516Dcu · malfunctionedPDX - FLIGHT 2521 - RETURNED TO THE FIELD FOR ELEVATOR SPLIT CAUTION MESSAGE. MAINTENANCE REPLACED THE NR 1 AND NR 2 DCU'S AS A PRECAUTION. AIRCRAFT RETURNED TO SERVICE.SDR 2008UALA02901Servo · failedELEV SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. - F -CTL ELEV SERVO FAILURE. REPLACED 3EC1 LT INBOARD SERVO CONTROL, ALL OPS CHECKS NORMAL.SDR 2008UALA02873Unknown · malfunctionedELAC 2 PITCH FAULT AFTER FIRST ENG START ON GROUND SWITCH CYCLE. RESET ECAM.
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