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 USAA2014013000006Computer · faultyAFTER TAKEOFF FROM PHX CREW RECEIVED AN ECAM FOR FLIGHT CONTROL ELAC2 PITCH FAULT. FLIGHT RETURNED TO FIELD AT PHX & LANDED WITHOUT INCIDENT. R & R THE NR 2 ELAC IAW 27-93-34-401 & 27-93-00-710-001.SDR CA140120008Rod End · broken(CAN) FOUND DURING A-CHECK WORKS ON RT ELEVATOR PCU NR 1 AND PCU NR 2 WITH BROKEN ROD ENDS.SDR ANCF201401100175Elevator System · out of toleranceDURING CLIMB, LEAVING FL 230 WITH 340 KNOTS, EXTREME VIBRATION IN STRUCTURE, VIBRATION STOPPED, SPEED
REDUCED TO 250 KNOTS & RETURNED TO FL 230 IAW TSM FIGURE 05-50-00-991-00400-C SHEET 1, DECISION TABLE WAS ACCOMPLISHED TYPE 13, 12, 11 & 10. THE PAX DOORSDR CA140121004Servo · failed(CAN) ELEVATOR HARD TO MOVE.SDR USAA2014010800010Computer · faultyELAC 2 PITCH FAULT IN FLIGHT CAUSING ACFT TO PITCH DOWN. REPLACED ELAC NR 2 IAW A320 AMM 27-93-34-000-001-A & 27-93-34-100-001-A, & ELECTRONIC MODULE IN POS NR 1 IAW LP 8448757, IAW A320 AMM 27-44-57-000-002-A.SDR USAA2014010600033Control Servo · inoperativeVIBRATION FELT IN FLIGHT AT 260 - 300. THE LAST HOUR OF FLIGHT VIBRATION FELT THE WORST IN THE TAIL. REPLACED LT INBD SERVO ACTUATOR IAW A320 AMM 27-34-51-400. ADJUSTED ELEVATOR ACTUATION SYS IAW A320 AMM 27-34-00-820-002-A & ELEVATOR FREE PLAY CHECKED IAW SDR USAA2013123100005Control Servo · out of adjustDURING CLIMB THRU APPROXIMATELY FL 1800 AT 320KTS AND IN LIGHT CHOP ENCOUNTERED AIRFRAME VIBRATION. VIBRATION STOPPED BY INCREASING PITCH AND CLIMB RATE AND DECREASING SPEED. VIBRATION AGAIN ENCOUNTERED AT FLT260 AT .79 MACH STOPPED BY DECREASING SPEED SEE VSDR CALA2013123194066Servo Control · unknownIAW CH8798 REQ LT ELEV SERVO CTRL 34-CE-1 REPLACEMENT. R & R LT ELEV SERVO CTRL 34-CE-1 IAW AMM 27-34-51-400-001-A UP TO INCLUDING STEP 4F2.SDR SIMA20131227009Transmitter · faultySHORTLY AFTER TAKEOFF, ELEVATOR SPLIT CAUTION CAS MISCOMP STATUS. R & R ELEVATOR POSITION TRANSMITTER, LT SIDE, IAW AMM 27-34-01. OPERATIONS CHECKED IAW AMM 27-34-10. OPERATIONS CHECKED GOOD.SDR SIMA20131226010Dcu · faultyELEVATOR SPLIT AT FL280 DIVERTED RDU. R & R DCU NR 1 IAW CRJ700 AMM 31-41-04, OPERATIONS CHECKED GOOD. PERFORMED OPERATION CHECK OF ELEVATOR CONTROL SYS AMM 27-31-00 OPERATION CHECKED GOOD, NO SPLIT OR DEFECTS NOTED.SDR 1MBD2013121300001Control Cable · misroutedDURING A 24 MO, 600 FLT HOUR INSPECTION, RT ELEVATOR UPPER SECTOR CONTROL CABLE HAD BEEN MISROUTED, OVER RATHER THAN BEHIND A GUIDE PIN. THE CONDITION OF THE CABLE HAD ALREADY BEEN COMPROMISED WITH A FEW STRANDS OF THE .1562 CABLE BEING FRAYED. IF LEFT UNDESDR CALA2013121693756Servo Valve · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED LT GREEN ELEV SERVO CONTROL SERVO VLV 34CE1 REF 27-34-51, OPERATIONS CHECKED NORMAL.SDR 29GA2013121593627Elevator · out of rigON TAKEOFF, WITH FLIGHT TRIM SET, 1.5 HAD TO FIGHT ELEVATOR TO KEEP FROM PITCHING UP IN LEVEL CRUISE, FORWARD TRIM AT 2. COMPLIED WITH ELEVATOR CONTROL SYSTEM RIGGING AND ELEVATOR TRIM TAB CONTROL RIGGING.SDR CALA2013121693713Computer · faultyELAC 2 PITCH FAULT DISPLAYED ON ECAM WITH ENGS RUNNING & FLIGHT CONTROLS OPERATED. REPLACED ELAC 2 & COMPLETED ASSOCIATED GND TESTS, INDICATIONS NORMAL. LAND TEST ACCOMPLISHED ON CF324. REPLACED RT YELLOW ELEVATOR SERVO UNIT & RIGGED IAW 27-34-00-82 0-003-BSDR 2014FA0000027Sprocket · shearedDURING FLIGHT, ELEVATOR TRIM BECAME STIFF AND ELECTRIC TRIM WOULD NOT OPERATE. FOLLOWED BY COMPLETE LOSS OF ELEVATOR TRIM ABILITY. DURING INSPECTION FOUND CHAIN SPROCKET ON ELEVATOR TRIM HAD SHEARED FROM TRIM ACTUATOR ASSY.SDR CALA2013121293624Computer · faultyDURING APPR ELEVATOR SLOW TO TRIM. ACFT NOT TRIMMING SO NOSE HAS LOAD DEMAND TO PITCH. IAW CREW REPORT PILOT PUSHED SIDE STICK FWD & THIS TRIMMED TO POSITION. HOWEVER WHEN SIDE STICK RELEASED AIRCRAFT PITCHES UP. REPLACED ELAC 2, ACCLRM 3 & ACCLRM 4 IAW TSSDR ASAA2013121096714Sensor · failedWHEN ENGAGING A AND B AUTOPILOT BOTH YOKES WOULD BUMP AND KICK 1 UNIT LT ON CONTROL WHEEL. ACFT GROUNDED. DFCS LAND VERIFIY GRP 49 FAILS TEST 49.35. DUAL TEST ALL POS FAIL, AIL POS SENSOR 1, MS622.11145. R & R AILERON POSITION SENSOR IAW MM 22-11-29 PERFORMSDR DXTA2013120505591Actuator · faultyPITCH FEEL FAIL CAS MESSAGE ILLUMINATED AFTER TAKEOFF. MESSAGE CYCLED OVER 6 TIMES & THEN STAYED ON THROUGHOUT APPROACH & LANDING. TROUBLESHOT TO LT LINEAR ACTUATOR. R & R LT LINEAR ACTUATOR, SYS OPERATIONAL CHECK IS GOOD. WORK DONE IAW CE-750 MM 27-33-00.SDR CALA2013120393394Status Message · activatedRT ELEVATOR PCU STATUS MESSAGE.SDR GLBA2013112900352Switch · failedPILOT DETECTED A BURNING ELECTRICAL ODOR COMING FROM THE CAPTAIN`S SIDE ELECTRICAL TRIM. REPLACED THE CAPTAIN'S TRIM SWITCH, OPS CHECKED GOOD, NO ABNORMAL ODORS NOTED.SDR CA131126004Pressure Switch · failed(CAN) ON DEPARTURE, AUTOPILOT B WOULD NOT STAY ENGAGED. TRIED AUTOPILOT A AND IT WAS TOTALLY LOCKED OUT, B WOULD ENGAGE FOR ONLY A SECOND OR TWO. ACFT DID AN AIR TURNBACK FOR MAINTENANCE. FAULT WAS ISOLATED TO THE A SYSTEM ELEVATOR PRESSURE SWITCH. UNIT WASDR SIMA20131119008Dcu · faultyIN CRUISE ELEVATOR SPLIT ON EICAS. PERFORMED OPERATIONS CHECK OF ELEVATOR SPLIT IAW CTJ 700 FIM 27-31-00, OPERATIONS CHECKED NORMAL. R & R DCU NR 1 IAW CRJ 700 MM 31-41-05, GND OPERATIONS CHECKED NORMAL.SDR CALA2013111993057Nut · looseRF ON CTR HYD 65 QUANTITY. FLANGE NUT ON RT INBD ELEVATOR PCU LEAKING. TIGHTENED FLANGE NUT LEAK, CHECKED GOOD.SDR DXTA2013111805570Servo · damagedIMMEDIATELY AFTER TAKEOFF, A GRINDING COULD BE FELT IN THE YOKE WHILE APPLYING FORWARD OR AFT MOVEMENT. VIBRATION WAS FELT IN FLOOR AT THE SAME TIME. NO GRINDING DURING FLIGHT CONTROL CHECK ON GROUND. GRINDING IS EXCESSIVE. REMOVED AND REPLACED THE ELEVATSDR CALA2013111993038Actuator · faultyELEVATOR ASYMMETRY STATUS MESSAGE. R & R NEW ASYMMETRY LIMITER ACTUATOR IAW MM.SDR PAI5201108111348Control Cable · frayedDURING ANNUAL INSPECTION, NOTED ELEVATOR UP CABLE SEVERELY FRAYED WHERE IT PASSES THROUGH THE FAIRLEAD IN THE MAIN SPAR, UNDER THE CABIN FLOOR IAW THE ACFT RECORDS, THIS CABLE IS THE ORIGINAL STAINLESS STEEL CABLE INSTALLED AT MANUFACTURE. THE ACFT HAS FLOWN SDR CALA2013102992481Module · faultySTABILIZER TRIM FAULTS DUE TO AN UNSCHEDULED STAB TRIM MOVEMENT & NO DEFINITIVE FINDINGS DURING TESTING IAW AM1568 & PTT 8132005. ACCOMPLISHED A MACH TRIM & SPEED STABILITY TEST IAW MM22-24-00 P501. REPLACED THE STAB TRIM ELEVATOR ASYM MODULES LT & RT & RECOSDR CA131115007Spring · failed(CAN) THE AFFECTED SPRING 71056-03 WAS IN COMPLIANCE WITH AD 98-08-18 AND WAS NOT DUE FOR MANDATORY REPLACEMENT, YET IT FAILED. 1 FACT THAT MAY HAVE CONTRIBUTED TO ITS PREMATURE FAILURE, THE ACFT DOES NOT HAVE A CONTROL LOCK AND IT HAD BEEN SOP TO LOCK THE COSDR CA131120009Control Cable · frayed(CAN) DURING A DETAILED CABIN INSPECTION, THE FORWARD UP ELEVATOR CABLE WAS FOUND TO HAVE ALL STRANDS SEPARATED FROM THE CORE OF THE CABLE. CABLE DEFORMITY WAS LOCATED WHERE THE CABLE GOES OVER THE BELLCRANK. CABLE REPLACED.SDR DXTA2013102905550Actuator · frozenAFTER BEING AT ALTITUDE FOR APPROXIMATELY 45 MINS THE ELECTRIC AND MANUAL PITCH TRIM FROZE UP, IT BROKE FREE WHILE DESCENDING THROUGH THE LOW 20'S. SUP: R &R LT AND RT ELEVATOR TRIM TAB ACTUATORS WITH O/H UNITS IAW THE MM CH 27-32-04 RIG, TRAVEL AND OPS CHECKSSDR HSYA2013101800013Trim System · malfunctionedFLIGHT 8573. DURING CLIMB OUT, ATTEMPTING TO TRIM ACFT VIA ELECTRIC TRIM BUT WHEEL WOULD NOT TURN. ATTEMPTED TO TURN TRIM WHEEL MANUALLY BUT WHEEL WOULD SNAP BACK TO STARTING POSITION. ELECTED TO RETURN TO DEPARTURE.SDR IPXA2013100900517Spring · brokenDUE TO ABNORMAL PITCH RESPONSE VS CONTROL INPUT. ROUND SPRINGS 690, IAW CMM 27-31-09, BROKEN ON EICU FEEL UNIT. R &R SPRING IAW CMM. SYS TEST CHECKED GOOD IAW AMM 27-31-00-825-060, PAR 3, STEP B.SDR CALA2013100791774Rivet · looseFIRST OFFICER`S ELEVATOR CONTROL AFT QUADRANT ASSEMBLY 251N2061-26 HAS PLAY AT THREE EACH RIVETS, SEE CMM 27-31-70 PG1010. REMOVED FWD & RT HAND RIVET & REAMED HOLES TO .260 INCHES IAW ECRA 2731-01384 & CMM 27- 31-70. REPLACED FASTENER OPERATIONS CHECKED OK SDR CALA2013100391697Warning System · activatedLT ELEV PCU STATUS. UNABLE TO CLEAR MESSAGE. CYCLED BREAKERS, CYCLED ALT HYD SWITCHES & RAN ELEVATORS. MESSAGE DID NOT CLEAR, APPLIED MEL 2721D. PARTS 643-9091 MR27314 C1283/SFO/03OCT.SDR CA131003003Control Cable · frayed(CAN) 2 STRANDS BROKEN ON AFT ELEVATOR CABLE AT AFT PULLEY LOCATION.SDR CALA2013100291652Servo Valve · faultyELEV SERVO FAULT DISPLAYED, REPEAT. CFDS FAULTING LT G ELEV SERVO VALVE 34CE1. REPLACED LT ELEV SERVO CONTROL VALVE IAW AMMS 27-34-51-000-008-A & 27-34-51-400-003-A. OPERATIONS CHECKED NORMAL ALL MODES NO MESSAGES.SDR CALA2013100191614Servo · faultyELEVATOR SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN, - F -CTL. GOT ECAM DURING FLT CONT CHECK. FLT ATTENDANT REPORTED LOUD CLUNK FROM TAIL COINCIDENTAL W-ECAM PROG TEXT: - ITEM ROLLED FORWARD. REPLACED LT OTBD BLUE ELEVATOR SERVO IAW MM, OPERATIONS CHECKEDSDR QXEA2013092801406Switch · failedPITCH TRIM CAUTION ON TAKEOFF, ABORTED TAKEOFF AT ABOUT 60 KNOTS. REPLACED PILOTS PITCH TRIM SWITCH. RETURNED TO SERVICE.SDR CALA2013092791534Servo · faultedELEVATOR SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. ITEM ROLLED FORWARD. REPLACED ENTIRE ELEVATOR SERVO, PCN 644-9014. REPLACED LT BLUE SYS ELEVATOR SERVO IAW MM & RIGGED IAW MM 27-34-00. OPERATIONS CHECKED GOOD.SDR CALA2013092791531Servo · faultyAIRFRAME VIBRATION FELT DURING CLIMB CRUISE DESCENT. COMPLETED VIBRATION REPORTING CHECKLIST. CREW REPORTS VIBRATION WAS MORE NOTICEABLE DURING CLIMB WHEN A-P WAS OFF & DECREASED WHEN A-P WAS ON. CREW REPORT ALMOST NOT DETECTABLE DURING DESCENT. HAVE VERIFISDR CALA2013092491395Pca · faultyIAW EQ7069 LT ELEV CENTER SYSTEM PCA WOULD NOT GIVE LT ELEV PCU FAULT IN EICAS. R & R LT ELEV PCA FOR CENTER SYSTEM IAW MM.SDR CA130923005Cable · corroded(CAN) DURING A SCHEDULED INSPECTION, BOTH ACFT ELEVATOR CONTROL CABLES WERE FOUND BADLY CORRODED. BOTH ELEVATOR CONTROL CABLES WERE REPLACED WITH NEW CABLES, PN 100-618-4412-D01, AND PN 100-618-4413-D01. CABLES WERE INSTALLED IAW QUEST MM. THE CORRODED CABLESDR SIMA20130913004Actuator · inoperativeTHE CREW REPORTED THAT AT FL 320 WITH AUTOPILOT ENGAGED, WE RECEIVED EICAS "AP ELEV MISTRIM". THE CREW DISCONNECTED THE AUTOPILOT AND SHORTLY AFTER RECEIVED EICAS "PTRIM MAIN INOP". THE CREW DECLARED AN EMERGENCY AND UTILIZED BACKUP PITCH TRIM FOR LANDING. TSDR CALA2013091091162Elevator · out of rigACFT VIBRATION CLIMBING-THRU FL 290 AT.80 MACH, SLOWED .78 M. WENT AWAY. SAMC TEXT: THIS AIRCRAFT HAS HISTORY OF REPORTED VIBRATION & CREW REQUESTED TO COMPLETE VIBRATION CHECK LIST & LEAVE WITH LOG BOOK TOMC ALLHOFF -ACCOMPLISHED ADJUSTMENT OF ELEVATOR PCU SDR CA130911011Actuator · failed(CAN) AFTER TAKEOFF, UPON FLAP 2, RETRACTION NOTICEABLE VIBRATION OCCURRED ON BOTH FLIGHT CONTROLS. VIBRATION PERSISTED AFTER FLAP 1 RETRACTION, AS SPEED INCREASED SO DID VIBRATION. RETURNED TO DEPARTURE AND AUTOPILOT WAS SELECTED OFF WITH VIBRATION PRESENT SDR CALA2013090691069Servo Control · faultyAIRFRAME VIBRATION ON CLIMBOUT PASSING FL280 & AT 310KIAS. REDUCED A-S & VIBRATION ENDED. ACCOMPLISHED STEP 1&2 IAW 27-24-00-200 & MM27-34-00-200. STEP 3 COMPLETE MOVING TO STEP 4 & NEXT STEP IS TO REPLACE LT SIDE INBD ELEV SERVO CONTROL IAW MM.SDR N6WA20130904003Drain · contaminatedDURING START OF TAKEOFF ROLL, STALL FAIL CAUTION MESSAGE ILLUMINATED CLEARED WITH IN 3 SECONDS, ABORTED TAKEOFF. FOUND WATER IN THE P3 DRAIN. DRAINED WATER AND PERFORMED OP'S CHECK OF STALL PROTECTION SYS IAW AMM 27-35=01. OPS CHECKED GOOD.SDR USAA2013082100011Computer · unknownENROUTE, CREW REPORTED A FLT CTL ELAC 1 & 2 PITCH FAULT. FLIGHT RETURNED TO FIELD LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX PERFORMED TROUBLESHOOTING IAW REF TSM 27-93-00-810-837-A AND 27-93-00-810-843-A. NO FAULTS. AS PRECAUTION, R &SDR QXEA2013080701207Indicator · malfunctionedAS THE POWER LEVERS WERE ADVANCED FOR TAKE OFF, WARNING HORN SOUNDED. ABORTED THE TAKE OFF AND RAN CHECKLISTS. DURING THE TAKE OFF WARNING TEST ON THE GROUND THE WARNING HORN DID NOT SOUND. R & R ELEVATOR TRIM INDICATOR IAW AMM 27-32-16-000-801 AND 27-32-16SDR CALA2013080590137Bellcrank · looseELEVATOR BUMP, FOUND AFT QUADRANT CAPTAIN BELLCRANK ATTACH RIVETS HAVE PLAY. REPLACED BLIND LOCK BOLTS.
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