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 2008UALA02730Warning System · activatedELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. FCDC FAILED---NO SHOP FINDINGS. REPLACED FCDC-2. SYSTEM CKS NORMAL, NO MSG'S DISPLAYED. ACCOMPLISHED AFS & LAND TESTS. CHECKS OK.
SDR SWAA082524Feel Unit · faultyDURING ROTATION A 2 INCH DEAD BAND INDICATION IN ELEVATOR. REMOVED AND REPLACED ELEVATOR FEEL & CENTERING UNIT PER MM.SDR SWAA082383Torque Tube · failedDURING SCHEDULED 16Y CHECK, RIGHT ELEVATOR FAILS FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM.SDR SWAA082382Torque Tube · failedDURING SCHEDULED 16Y CHECK, LEFT ELEVATOR FAILS FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM.SDR 2008UALA02514Control Unit · failedELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS, MULTIPLE ELAC 2 FAULTS ON DESC INTO DEN. AP2 WAS ENGAGED AT THE TIME. SWITCH TO AP1 NO ELAC2. INTERNAL CARD Q4 FAILING CH 2 INITIALIZING TEST. ELAC FAULTING. REPLACED ELAC 2, OPS TESTING GSDR RAIA00804032Elevator · stiffFLT 7972 - EWR - DURING CRUISE, PITCH BECAME STIFF WHEN PULLING ON YOKE. A FEW DEGREES OF TRAVEL IT WOULD SEEM FINE, AFTER THAT IT WAS STIFF. MAINTENANCE PERFORMED A DETAILED VISUAL INSPECTION OF THE ELEVATOR CONTROL SYSTEM, ELEVATOR SURFACES, TRIM TABS, ANDSDR CA080707007Bearing · worn(CAN) WHILE INSP IT WAS NOTICE THAT THE LT CONTROL TUBE WAS ROUGH AS IT WAS PULLED OUT AND PUSHED IN. AFTER TAKING IT OFF, IT WAS NOTICED THAT THE BEARINGS HAD WORN THE TUBE TO ITS LIMITS. THE CONTROL TUBE AND THE BEARINGS WERE CHANGED.SDR SWIA200819491Actuator · failedFLT 6126 - ELEVATOR IS VERY STIFF. REPLACED NR 2 LINEAR ACTUATOR IAW CRJ AMM 27-31-23. OPS CHECKS GOOD AT THIS TIME.SDR NWAA081659886Actuator · malfunctionedFLIGHT CREW REMARKED THAT THE AIRCRAFT WANTED TO ROTATE ON ITS OWN PRIOR TO V1 AND THAT A NOTICEABLE VIBRATION IN THE YOKE WAS FELT AFTER TAKEOFF. AIRCRAFT LEVELED AT 16000 FEET AND CREW ESTABLISHED COMMUNICATION WITH MAINTENANCE CONTROL. FLIGHT WAS DIRECTEDSDR 2008UALA02121Servo Valve · faultyDURING A CHECK, RIGHT ELEVATOR WILL NOT PASS FLIGHT TEST. 34CE1 SERVO FAULTY. REPLACED ELEV SERVO CONTROL, INBD GREEN (34CE1), OPS CHECKED OK.SDR BJNA080402Actuator · malfunctionedSTABILIZER TRIM WOULD NOT KEEP UP WITH THE COMMANDED POSITION, ASSOCIATED WITH A STAB OUT OF TRIM ANNUNCIATION. STABILIZER TRIMMED "UP" OK. REMOVED AND REPLACED STABILIZER JACK SCREW ASSEMBLY. OVERHAUL FOUND - P/N 54032-006 SCREW ASSEMBLY WORN; P/N 65C34615SDR 2008UALA01851Jackscrew · gougedHORIZONTAL STAB JACKSCREW MIDDLE SECTION HAS .001 GOUGE. HORIZONTAL STAB BALLSCREW SHOWS SIGNS OF GALLING AND WEAR ALONG MIDDLE 2 FOOT LENGTH OF BALLSCREW, JACKSCREW REMOVED AND REPLACED,
SDR HALA0800442Control Cable · brokenDUAL ELEVATOR SERVO FOLLOW UP CABLE BROKEN. FABRICATED ELEVATOR SERVO CABLE 207B PER AMM 91-10-02. INSTALLED ELEVATOR SERVO CABLE AND RIG PER AMM 27-30-00, OPERATIONAL CHECK OK.SDR UALA2008111301695Elevator System · malfunctionedPER CREW WHEN ONLY ELEVATOR MOVEMENT, HAD TOO MUCH RESISTANCE. WHEN ONLY AILERON MOVEMENT, RIGHT SIDE TOO MUCH RESISTANCE. WITH SPOILERS DEPLOYED AILERONS OK. ELEVATORS ALWAYS HAD TOO MUCH RESISTANCE. NO UNUSUAL AILERON FORCES NOTED. HEAVY ELEV FORCES ARESDR 2008UALA01630Control Unit · faultyELEVATOR SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. CAUSE, ELAC1 FAULTY, ISSUES WITH CPS BOARD (INTERNAL). REPLACED ELAC1, ALL TEST PASS NORMAL.SDR WGEA200800046Selector Switch · defectiveELEVATOR TRIM SPLIT - LEFT TAB FROZEN AT 7 PERCENT. REMOVED AND REPLACED CENTER SWITCH PANEL WITH NEW UNIT. PERFORMED TEST IAW EA500 AMM 31-10-00. CSP TEST GOOD.
SDR DLM90080299Shutoff Valve · failedON CLIMB-OUT FROM SLC THRU 23000, AIRCRAFT BEGAN VERTICLE OSCILLATIONS MORE THAN USUAL. AUTOPILOT WAS DISCONNECTED AND ELEV FEEL WAS STIFF. NO COCKPIT INDICATIONS TO IND ELEV IN MANUAL CONTROL. AIRCRAFT FLOWN MANUALLY TO LAS. T/S PER TSM ACS FAULT MOSV1 PRSDR 2008UALA01056Elevator · out of adjustAIRCRAFT REQUIRES 4 UNITS OF RUDDER TRIM IN LEVEL FLT. CHECKED RUDDER AND RUDDER TRIM SYSTEM OK. FOUND RT ELEVATOR NOT WITHIN LIMITS ON INDEX PLATE AND E-ST9 RIG PIN HOLE NOT LINING UP. ADJUSTED, ALL CHECKS NORMAL.
SDR 2008UALA01032Computer · faultyCREW REPORTS ELAC 2 FAULT. ELAC FAULT/FAILURE-NFF. REPLACED ELAC2.SDR 2008UALA01026Control Unit · defectiveF-CTL ELEV SERVO FAULT ECAM AFTER T/O. EXCESSIVE PLAY IN ROD END CONNECTOR(S). REPLACED LT BLUE ELEVATOR SERVO CONTROL UNIT (34CE3), TESTS GOOD.SDR RAIA00802024Elevator · malfunctionedFLT 8025 - IAD - DURING TAKEOFF THE ELEVATORS SEEMED TO BE NON-RESPONSIVE WHEN THE YOKE WAS PULLED BACK. MAINTENANCE INSPECTED THE AIRCRAFT'S ELEVATOR FOR STRUCTURAL DAMAGE, PERFORMED A DEFLECTION CHECK OF THE ELEVATOR CONTROL SURFACE, PERFORMED AN OPERATIONASDR CA080225009Control Cable · frayed(CAN) LWR ELEVATOR CABLE FRAYED AT BULKHEAD STA 140, WHERE CABLE RIDES ON THE PHENOLIC BLOCK.SDR SWAA080965Rod End · corrodedDURING SCHEDULED 20Y CHECK, FOUND LT ELEVATOR TAB CONTROL ROD ENDS CORRODED. REMOVED AND REPLACED ROD ENDS PER MM.SDR QXEA200800208Dcu · unknownSEA - FLIGHT 2548 - ON CLIMB RECEIVED A ELEVATOR SPLIT CAUTION AND CAS MISCOMPARE MESSAGE. NO ABNORMAL INDICATIONS ON FLIGHT CONTROL PAGE. NO ABNORMAL FLIGHT CONDITIONS NOTED. MAINTENANCE PERFORMED A GVI OF THE ELEVATOR AND LINKAGE AND TENSION CHECK OF THE SDR QXEA200800207Transmitter · malfunctionedSEA - FLIGHT 2634, RECEIVED A ELEVATOR SPLIT CAUTION AND A "CAS MISCOMPARE" STATUS MESSAGE DURING CLIMB THROUGH 22,000. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE ELEVATOR POSITION TRANSMITTER. OPERATIONAL CHECKS GSDR 2008UALA00897Pulley · crackedCABIN CEILING AREA ELEVATOR CONTROL CABLE PULLEY CRACKED OB SIDE BETWEEN BS 333 AND BS 350 L4L. STRESS FRACTURE. REPLACED ELEVATOR CONTROL CABLE PULLEY.SDR CA080225011Control Cable · frayed(CAN) LWR ELEVATOR CABLE FRAYED AT BULKHEAD STA 140 AT THE PHENOLIC BLOCK.SDR CA080225010Control Cable · frayed(CAN) LWR ELEVATOR CABLE FRAYED AT BULKHEAD STA140 AT PHENOLIC BLOCK.SDR USAASA08004Rod End · wornCLT FLT 1845 EN ROUTE PHL TO FPO - AIRFRAME VIBRATION WAS FELT AT FL 320 AND HIGHER SPEEDS. A DECISION WAS MADE TO DIVERT TO CLT. VIBRATION STOPPED BELOW 18,000 FEET AND SLOWER SPEEDS. FLIGHT LANDED IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED 3SDR RAIA00802002Unknown · unknownFLT 7961 - RUDDER PEDALS WILL NOT MOVE. HYDRAULIC PRESSURE INDICATED GOOD. FOLLOWED BY A YAW DAMPER FAIL MESSAGE ON THE EICAS. MAINTENANCE DISENGAGED THE AUTOPILOT/YAW DAMPER AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK OF THE RUDDER. MAINTENANCE PLACED TSDR SWAA080527Control Valve · failedDURING SCHEDULED HC2 CHECK, ELEVATOR TAB CONTROL SYSTEM FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED ELEVATOR TAB CONTROL VALVE PER MM.SDR YENA2008006Pcu · out of limitsFLT 562, FLL-SWF, AIR RETURN TO FLL, AIRFRAME VIBRATION AT 300-320 KIAS CLIMBING THROUGH FL230. VIBRATION FADED AS AIRCRAFT SLOWED BELOW 230 KTS. ENG AND FLIGHT CONTROLS INDICATED NORMAL. PERFORMED TSM TASK 05-50-00-810-801. PER CREW INPUT VIBRATION REPORTSDR SWIA200819039Pcu · inoperativeFLT 6500 - RIGHT ELEVATOR DOES NOT MOVE WITH HYDRAULIC SYSTEM 3 PRESSURIZED. REPLACED RIGHT NR 3 HYD ELEVATOR PCU IAW 27-33-01. OPS CHECK GOOD.
PN 27600-3, SN OFF 8783.SDR DL764080033Actuator · leakingCENTER HYD RSVR LIGHT JUST AFTER LEVEL-OFF FOLLOWED CHECKLIST RETURNED FOR LANDING LND WT 398.0LBS. FOUND RIGHT ELEVATOR CENTER HYD PCA LEAKING. REPLACED PER AM LEAK CHECK OK. RII INSPECTION COMPLETED PER TOPP 40-30-05.SDR DL764080026Actuator · leakingSHORTLY AFTER TAKEOFF FROM HNL FLIGHT 1282 NOTIFIED MCC THAT CTR SYS HYD WAS LOSING FLUID. HAD THE CREW SECURE CTR PUMPS AND QTY STABILIZED. CREW RETURNED TO HNL. TROUBLESHOOTING IN PROGRESS. FOUND RT ELV PCA LEAKING. REPLACE CK OK.SDR SWAA080192Torque Tube · wornDURING SCHEDULED BRDG CHECK, RT HORIZONTAL STABILIZER FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE PER MM.SDR SWAA080028Torque Tube · wornDURING SCHEDULED 22Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE PER MM.SDR 2008UALA00025Elevator · faultyFIRST OFFICER'S ELEVATOR CONTROLS FEEL HEAVY. CREW COMMENTS: ELEVATOR VERY HEAVY ON TAKEOFF. RECURRED ON FLT 0053-12JAN. THIS A/C WAS A CHRONIC PROBLEM FOR SEVERAL WEEKS. AFTER MANY TESTS AND RIG CHECKS, SEVERAL TEST FLIGHTS BY DIFFERENT CREWS IT WAS SUSPSDR 2008UALA0025Unknown · unknownFIRST OFFICER'S ELEVATOR CONTROLS FEEL HEAVY. CREW COMMENTS: ELEVATOR VERY HEAVY ON T/O.SDR MASA200700919Pulley · lack of lubeASH FLT 2677 CLT - ON LANDING ROLL OUT, THE ELEVATOR LOCKED UP ON THE CREW. CHECKED AND LUBED PULLEYS TO FO ELEVATOR CONTROL, OPS CHECK GOOD.SDR HNAA0700290Elevator · icedDURING TAKEOFF ROLL, THE AIRCRAFT REACHED 104 KNOTS AND THE CREW ATTEMPTED TO ROTATE THE AIRCRAFT TO LIFT OFF, BUT WERE UNABLE TO DO SO. THE CAPTAIN IMMEDIATELY ABORTED THE TAKEOFF AND USED THE REMAINDER OF THE RUNWAY FOR STOPPING. CONDITIONS WERE WET AND SNSDR 2007FA0001075Adapter · wornLT ELEVATOR TORQUE TUBE ARM ADAPTER RIVET HOLES WERE WORN POSSIBLY DUE TO UNSECURED CONTROLS IN GUSTY WINDS.SDR SIMA200733704Control Unit · malfunctionedPITCH TRIM INOP. REMOVED AND REPLACED HSCU IAW AMM 27-10-01-000-801-A AND 27-40-01-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200733705Actuator · failedMAIN PITCH TRIM FAILED. CAPT ELECTED TO RETURN TO THE FIELD IAW AMM 27-40-02 REF NRWC 2004864. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR IAW AMM 27-40-03-000-801. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVICE.SDR SWAA075908Pushrod · wornDURING SCHEDULED BRDG CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED PUSH ROD PER MM.SDR CA071118001Rod End · broken(CAN) REPORT FROM AIR ONE: REF /A/ - AIPC 27-33-01, FIG 1 WHILE PERFORMING TASK CARD 000-27-220-010 - OPERATIONAL TEST OF THE ELEVATOR PCUS, AIR ONE FOUND THAT WITH HYD 1 ONLY, THE ELEVATOR WOULD NOT MOVE. AFTER INSPECTION, THEY FOUND THAT PCU 1 ROD END (ONSDR 754002Control System · unstableDURING CLIMB-OUT, THE VERTICAL SPEED WHEEL MOVED TO FULL NOSE UP POSITION WITH "B" AUTOPILOT SELECTED. IN CRUISE AUTO STAB "B" LIGHT ILLUMINATED SEVERAL TIMES. AT FL 340 WITH ALTITUDE HOLD SELECTED, VERTICAL SPEED VARIED +/- 2000 FPM. WITH AUTOPILOT OFF, THESDR 2007FA0001068Bonding Jumper · frayedTROUBLESHOT REPORT OF HORIZONTAL STABILIZER ANTI-ICE SYSTEM FAIL INDICATION. NOTED ELEVATOR HORN HEAT SYSTEM RESISTANCE READINGS ERRATIC WHEN ELEVATORS MOVED. FOUND ELEVATOR BONDING JUMPERS FRAYED AND CORRODED. REPLACED ELEVATOR BONDING JUMPERS, ELEVATOR HOSDR QXEA200701641Elevator · noneSEA - ELEVATOR CONTROL HAS A FLAT FEEL. THE CONTROLS MOVE BACK AND FORTH A COUPLE OF INCHES WITH NO ELEVATOR MOVEMENT. AIRCRAFT FERRIED TO PORTLAND FOR REPAIRS. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE ELEVATOR CONTROL SYSTEM IAW AMM TASK 27-31-00-71SDR SWAA075481Torque Tube · wornDURING SCHEDULED BRDG CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED TORQUE TUBE PER MM.
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