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 DALA2025112508578Servo Control · excess playEMPENNAGE RH ELEVATOR SERVO CONTROL BLUE HAS PLAY, IT HAS 7.45. REPLACED EMPENNAGE RH ELEVATOR SERVO CONTROL BLUE ACTUATOR EYE END IAW A319 AMM TASK 27-34-51-000-009-A AND AMM TASK 27-34-51- 400-006-A. (1319605).SDR DALA2025112508577Servo Control · excess playEMPENNAGE RT ELEVATOR SERVO CONTROL YELLOW HAS PLAY, IT HAS 7.02. REPLACED EMPENNAGE RT ELEVATOR SERVO CONTROL YELLOW ACTUATOR EYE END IAW AMM TASK 27-34-51-000-009-A AND AMM TASK 27-34-51- 400-006-A. (1319595).SDR DALA2025112508581Servo · excess playEMPENNAGE LH ELEVATOR SERVO CONTROL BLUE HAS PLAY, IT HAS 7.39. CORRECTIVE ACTION: REPLACED EMPENNAGE LH ELEVATOR SERVO CONTROL BLUE ACTUATOR EYE END IAW A319 AMM TASK 27-34-51-000-009-A AND AMM TASK 27-34-51- 400-006-A. (1319615).SDR JJBA20251125108Control Unit · inoperativePITCH TRIM INOPERATIVE MESSAGE AT V1. REMOVED AND REPLACED HORIZONTAL STAB CONTROL UNIT. OPS/INDICATION CHECK SAT.SDR N6WA2025111909Cable · frayedELEVATOR AUTO PILOT CABLE HAS FRAYED STRAND. REMOVE AND REPLACED ELEVATOR AUTO PILOT CONTROL CABLES IAW CRJ AMM 27-31-00 AND EO-C550-27SB-005SDR 2025FA0000768Torque Tube · debondedTHE ELEVATOR TORQUE TUBES HAD UNBONDED CREATING MOVEMENT BETWEEN ELEVATOR TORQUE TUBE & COLLAR. WE HAVE NOTED THIS CONDITION ON AT LEAST 10 DIFFERENT SERIAL NUMBERS OF ACFT. NOTE, THE RUDDER HAS SAME METHOD OF ATTACHMENT & FAILURES HAVE BEEN NOTED AT THAT LOSDR AALA202512027613Module · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING TAKEOFF AT APPROXIMATELY 100KTS DUE TO A VERY HARD YAW TO THE RIGHT THEN A REVERSAL TO THE LEFT. FELT LIKE WE POSSIBLY HAD A FLIGHT CONTROL ISSUE WITH THE RUDDER. FIRST OFFICER SAID THE FOOT PEDALSDR 2025FA0000741Control Cable · brokenELEVATOR CONTROL CABLE SEPARATED AT THE TURNBUCKLE DURING TAKEOFF ROLL; THE TAKEOFF WAS ABORTED WHEN A (NOISE) BANG WAS HEARD AND THE AIRCRAFT NOSE DROPPED. THE CABLE ATTACHMENT BROKE AS IT ENTERED THE TURNBUCKLE AND WAS ONLY HELD TOGETHER BY THE SAFETY WIRE. SDR SWI2025F01462Elevator System · splitELEVATOR SPLIT CAUTION MESSAGE AT CRUISE. (FLIGHT 4995 - FILED CLOSED)TROUBLESHOT ELEVATOR SPLIT CAUTION IN REFERENCE TO FIM 27-31-00. UPON ARRIVAL, NO MESSAGES WERE PRESENT. PERFORMED OPS CHECK OF THE ELEVATOR CONTROL SYSTEM IN REFERENCE TO AMM 27-31-00. FSDR 2025FA0000630Control Horn · brokenDURING CONDITIONAL INSPECTION AND OPENING UP AIRCRAFT FOR INSPECTION I WAS CHECKING FREEDOM OF MOVEMENT OF FLIGHT CONTROLS AND NOTICED THE LEFT ELEVATOR FELT BOUNCY AND THAT THEIR WAS TO MUCH PLAY IN THE CONTROL COMPARED TO THE RIGHT ELEVATOR. I CONTINUED TO ISDR IPXA2025091043242Elevator · inoperativeADD SDR FOR EO-85445-JIC1 STEP 137 PAPER FINAL CHECKED OK.ACCOMPLISHED ADD SDR FOR EO-85445-JIC1 STEP 137.SDR IPXA2025091043210Elevator · inoperativeADD SDR FOR EO-85445-JIC2 STEP 137 PAPER FINAL CHECKED OK.ACCOMPLISHED ADD SDR FOR EO-85445-JIC1 STEP 137.SDR DALA2025083106423Computer · faultedDIV- TO LHR DUE TO INTERMITTENT VIBRATIONS FELT BY CREW. REPLACED ELEVATOR FEEL COMPUTER DUE TO ONE CHANNEL INOP.(7600378)SDR DALA2025091806849Actuator · excess playFREE PLAY OUT OF LIMITS OUTBOARD ACTUATOR ELEVATOR LH. REPLACED OUTBOARD ACTUATOR ELEVATOR LH AS PER A320 FAM AMM 27-34 -51-000-001-A AND A320 FAM AMM 27-34-51-400-001-A. (1155012).SDR DALA2025091806848Actuator · excess playFREE PLAY OUT OF LIMITS INBOARD ACTUATOR ELEVATOR LH. REPLACED INBOARD ACTUATOR ELEVATOR LH AS A320 FAM AMM 27-34-51- 000-001-A AND A320 FAM AMM 27-34-51-400-001-A. (1154800).SDR YENA2025081200824Pressure Switch · faultedFLT#2260, MAD-BOS. (ETOPS) "CLASS II MX MSG F/CTL ON LOWER ECAM ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) FAULT(S) INDICATED BY F/CTL ); IN REF TO TSM 27-92-00-810-8222-B. R&R PRESS SW-B HYD FLT CTL (FIN:10CE1) IAWSDR YENA202508120823Warning Message · illuminatedFLT#2260, MAD-BOS. (ETOPS) "CLASS II MX MSG F/CTL ON LOWER ECAM ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) FAULT(S) INDICATED BY F/CTL ).SDR VNAA2025081311101Sensor · faultedELEVATOR SPLIT CAUTION MSG AND CAS MIS COMP STATUS MSG. REMOVED & REPLACED LH ELEVATOR POSITION SENSOR IAW CRJ 900 AMM 27-34-10-000/400-801-A02; OPS CHECK GOOD.SDR ABXA20250805172Elevator System · faultedDRUING TAXI OUT, LEFT SIDE ELEVATOR DID NOT MOVE ON STATUS PAGE. ACFT RETURNED TO THE GATE. MTX GROUNDED ACFT AND DEFERRED ELEVATOR INDICATION FOR DEPARTURE IAW MEL ABX-27-08-01. MTX RETURNED AC TO SERVICE.SDR N6WA2025080301Control Cable · brokenELEVATOR JAMS WHEN PULLED BACK. FOUND ELEVATOR AUTOPILOT SERVO CABLE BROKEN. REMOVED ELEVATOR AUTOPILOT CABLES IN ACCORDANCE WITH MHIRJ RIL (REFFERENCE INSTRUCTION LETTER) 12802 AND PERFORMED OPERATIONAL TEST OF ELEVATOR CONTROL SYSTEM IN ACCORDANCE WITH MHSDR VNAA2025073111103Elevator System · no discrepancyELEVATOR SPLIT CAUTION MSG IN CRUISE FLIGHT AT FL360. VERIFIED ELEVATOR CABLE TENSIONS THROUGHOUT FUSELAGE PER AMM 27-31-00-750-801 CABLE TENSIONS WITHIN LIMS. VISUALLY INSPECTED ELEVATOR CONTROL COMPONENTS PER FIM 27-31-00-810-803. PER AMM 27-31-00-70-80SDR ABXA20250723165Elevator · malfunctionedDURING CRITICAL CHECK, RT ELEVATOR INDICATION WAS 2/3 FROM TOP AND BOTTOM. LEFT ELEVATOR INDICATION WAS NORMAL. AIRCRAFT RETURNED TO BLOCKS. MAINTENANCE DEFERRED RT ELEVATOR INDICATION AS PER MEL 27-08-1 MBCB 08-02-2025. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20250716159Elevator System · malfunctionedDURING TAXI, L ELEVATOR SHOWING NO MOVEMENT DURING BEFORE TAKEOFF CHECKLIST. AIRCRAFT RETURNED TO BLOCKS. (BTB) DEFERRED IAW MEL C ABX-27-08-1. AIRCRAFT RETURNED TO SERVICE.SDR AALA202507179088Control Servo · vibrationAIRCRAFT WAS GROUNDED: MIA-CHS DIVERTED TO MCO ON ACCOUNT OF MAINTENANCE - ENGINE VIBRATION. EMERGENCY DECLARED AND NOT OVERWEIGHT FOR LANDING. MAINTENANCE FOUND R/H O/B ELEVATOR CONTROL SERVO ACTUATOR 34CE4 SHUDDERING AND SHAKING THE AIRCRAFT. REPLACED R/H SDR DXTA2025071404196Trim System · faultedIMMEDIATELY AFTER TAKEOFF WE HAD NO ABILITY TO TRIM THE AIRCRAFT USING PRIMARY TRIM AND RECEIVED PRI STAB TRIM FAIL.(ATC DECLARED EMERGENCY) SENT IN ARES DOWNLOAD TO TEXTRON IAW CE·680A AMM CH 31-33-00. TEXTRON STATED THAT THE REASON THE PRIMARY STAB TRIM FASDR DALA2025070905188Servo · faultedSHIP 3568 -ATB- DUE TO RIGHT ELEVATOR SERVO FAULT. CORRECTIVE ACTION: REPLACED RIGHT OUTBOARD YELLOW ELEVATOR SERVO (1CT2). (LP# 7307576)SDR SWIA2025070300002Sensor · faultedELEVATOR SPLIT CAUTION MESSAGE AND CAS MISCOMP STATUS MESSAGE ILLUMINATED DURING CLIMB OUT AT ABOUT 4000 FT. (FLIGHT 4290 - FILED CLOSED)TROUBLESHOT ELEVATOR SPLIT CAUTION AND CAS MISCOMP STATUS IN REFERENCE TO FIM 27-31-00 AND 31-41-00. NO VISIBLE ELEVATOR SSDR AALA202507042685Servo Control · inoperativeAIRCRAFT WAS GROUNDED: MODERATE AIRCRAFT VIBRATIONS DURING CLIMB ACCELERATING ABOVE 250KTS. YAWING MOTION.. FAST CYCLE. NOSE AND TAIL "WAGGING"ENG VIBES ALL BELOW 1.0. MAINTENANCE REPLACED L/H ELEVATOR SERVO CONTROL PER AMM 27-34-51.SDR AALA202507043899Servo Control · inoperativeAIRCRAFT WAS GROUNDED: MODERATE AIRCRAFT VIBRATIONS DURING CLIMB ACCELERATING ABOVE 250KTS. YAWING MOTION.. FAST CYCLE. NOSE AND TAIL "WAGGING"ENG VIBES ALL BELOW 1.0. MAINTENANCE REPLACED R/H ELEVATOR SERVO CONTROL PER AMM 27-34-51.SDR 2025FA0000390Cable · frayedFORWARD RIGHT STABILATOR CONTROL CABLE PART NUMBER 62701-37 HAS BROKEN STRANDS.SDR 2025FA0000389Cable · brokenWHILE TAXYING FOR DEPARTURE THE CREW NOTED THE MANUAL TRIM WAS NOT MOVING SMOOTHLY. ATTEMPTED TO MOVE THE MANUAL TRIM AND NOTED THE TRIM WHEEL WAS SPINNING FREELY. ALSO NOTED THE LEFT AND RIGHT CREW TRIM SWITCHES HAD NO EFFECT. THE CREW RETURN THE RAMP FOR FURSDR AALA202506045074Computer · leakingAIRCRAFT WAS GROUNDED: MODERATE MUSTY AND DIRTY SOCK ODOR JUST AFTER SETTING TAKEOFF THRUST, IT CONTINUED THROUGH CLIMB TO APPROXIMATELY 10,000 FT. SUSPECT OIL SEAL SEEPAGE. DURING FAULT ISOLATION FOR SOF EVENT, FOUND ELEVATOR FEEL COMPUTER LEAKING, WITH LEAKSDR DXTA2025052703622Actuator · failedOCF FAILED FOR ELEVATOR. SHORTLY AFTER TAKEOFF WITH FULL NOSE DOWN TRIM, AMBER CAS MSG APPEARED AND STAYED ON. I DISCONNECTED THE AUTOPILOT AND THE AIRCRAFT SHARPLY PITCHED UP. I HAD MINIMAL CONTROL TRYING TO KEEP THE NOSE DOWN. WE WERE ABLE TO MAINTAIN ASDR N6WA2025052102Control Cable · corrodedELEVATOR AUTO PILOT LOWER AFT CONTROL CABLE "C1" CORRODED. REMOVED AND REPLACED ELEVATOR AUTO PILOT CONTROL CABLE "C1" IAW CRJ AMM 27-31-00SDR 9WGA2025072354520Pushrod · corrodedDURING HEAVY CHECK RH INBD /OUTB ELEVATOR PUSH RODS HAVE CORROSION AS MARKED (REPLACE AS REQUIRED) (PUSH RODS OF ACTUATORS).SDR 9WGA2025061354510Rod · looseDURING HEAVY CHECK R/H INBOARD ELEVATOR ROD IS LOOSE. RESECURED HARDWARE R/H INBOARD ELEVATOR ROD IAW MD-11 AMM 20-50-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 3EJA950JS042925Control Cable · frayedDURING A SCHEDULED INSPECTION THE ELEVATOR CABLES FAILED INSPECTION WITH MORE THAN 6 STRANDS.SDR QXEA2025041600119Fault Code · activatedDURING CRUISE AT FL360 ELEVATOR FAULT MASTER CAUTION AND AP FAIL MASTER CAUTION. ACCOMPLISHED ELEVATOR FAULT CHECKLIST AND BOTH MESSAGES EXTINGUISHED. AMBER DASHED BOX ON ELEV RH LINE UNDER RIGHT ACTUATOR ON FLT CTC PAGE REMAINED. RECIEVED FLT CTRL NO DISPATCHSDR UIEA2025032700392Computer · leakingELEVATOR FEEL COMPUTER, WITH HYDRAULIC LEAK.(<P>ELEVATOR FEEL COMPUTER HYDRAULIC LINES WERE RE-TORQUED IAW AMM 27-31-19-424-015 REV. 144 22DEC24. TORQUE APPLIED 270 IN/LB AND 170 IN/LB, TORQUES WRENCH DATA S/N: 0422127314 D/D: 17SEP25 AND S/N: 1123126519 D/D: SDR N6WA2025032703Cable Assy · corrodedINNER CORROSION FOUND ON ELEVATOR AUTO PILOT CONTROL FORWARD CABLE (C3). REMOVED AND REPLACED ELEVATOR AUTO PILOT (C3) CABLE IAW CRJ AMM 27-31-00. OPS CHECK GOOD.SDR N6WA2025032702Cable Assy · corrodedINNER CORROSION FOUND ON THE ELEVATOR AUTO PILOT CONTROL UPPER AFT CABLE(C2). REMOVED AND REPLACED ELEVATOR CABLE (C2) IAW CRJ AMM 27-31-00. OPS CHECKS GOOD.SDR N6WA2025032701Cable · corrodedINNER CORROSION FOUND ON THE ELEVATOR AUTO PILOT CONTROL LOWER AFT CABLE (C1). REMOVED AND REPLACED ELEVATOR AUTO PILOT CABLE (C1) IAW CRJ AMM 27-31-00. OPS CHECKS GOOD. PERFORMED DOUBLE TENSION CHECK WITHIN SPEC OPS CHECK OF THE ELEVATOR CONTROL SYSTEM IAW ASDR UIEA2025030600214Actuator · out of limitsDURING ELEVATOR SURFACE FREE PLAY FUNTIONAL CHECK, ELEVATOR RH, OUTBOARD POWER CONTROL ACTUATOR OUT OF LIMITS.(<P>POWER CONTROL ACTUATOR WAS REPLACED, TEST FOR LEAKS AND ADJUSTMENTS WAS PERFORMED IAW AMM 27-31-05-424-027 REV 144. OPS CHECK GOOD.</P>)SDR UIEA2025030600217Actuator · out of limitsDURING ELEVATOR SURFACE FREE PLAY FUNTIONAL CHECK, ELEVATOR LH, OUTBOARD POWER CONTROL ACTUATOR OUT OF LIMITS.(<P>POWER CONTROL ACTUATOR WAS REPLACED, TEST FOR LEAKS AND ADJUSTMENT WAS PERFORMED IAW AMM 27-31-05-424-027 REV 144. OPS CHECK GOOD.</P>)SDR UIEA2025030800227Feel Unit · leakingLEAKAGE AT ELEVATOR FEEL UNIT IN HORIZONTAL STABILIZER TORSION BOX COMPARTMENT, LH SIDE.(<P>LEAKAGE AT ELEVATOR FEEL UNIT IN HORIZONTAL STABILIZER TORSION BOX COMPARTMENT, LH SIDE. ELEVATOR FEEL UNIT WAS REPLACED AND TEST WAS PERFORMED IAW AMM 27-31-19-424-015SDR YENA2025032600339Control Servo · faultedFLT#2466, FLL-BUF. 'DURING LEVEL FLIGHT AT FL350 A/C WOULD SHUTTER MOMENTARILY AND PITCH UP EVERY FEW MINUTES. IT DID IT WITH BOTH AUTOPILOTS 1 AND 2 AND WITH MANUAL FLYING. ALSO WAS NOTED DURING DESCENT THRU FL180; REMOVED AND REPLACED ELEVATOR SERVO CONTROL SDR YENA2025031800266Servo Valve · failedFLT#1349, MHT-RSW. (AIRCRAFT DIVERTED TO JFK) ' LEFT ELEVATOR INTERMITTENT DEFLECTION RODUCED UNWANTED FLIGHT PATH (CHOPPY SENSATION) AFTER LANDING F/CTRL ELEVATOR SERVO FAULT PRESENTED WITH AMBER BRACKETS AROUND BLUE SYSTEM MESSAGE DISAPPEARED AFTER SHUTDOWN;SDR N6WA2025031104Cable Assy · brokenELEVATOR AUTO/PILOT CABLE C1 HAS BROKEN STRANDS. REPLACED ELEVATOR AUTO/PILOT CABLE C1 AND C2 IAW CRJ AMM 27-31-00SDR KY7A2025021000038Damper · faultedREMOVED AND SERVICED ELEVATOR DAMPER AND REINSTALLED PER SA227 MM CH 27-30-10 PERFORMED CABLE TENSION INSPECTION PER SA22X TC 27.920SDR L16A2025041500001Cable · damagedAT CRUISE AUTOPILOT KICKED OFF DUE TO CAS MESSAGE: AP 1-2 FAIL-ELEV SRVO ALONG WITH STICK PUSHER FAIL. FLIGHT CREW OBSERVED ELEVATORS WERE VERY STIFF TO MOVE. CREW DECLARED AN EMERGENCY ONE HOUR OUT OF KPHX, AND LANDED UNEVENTFUL INTO KPHX. GULFSTREAM FAST TEC
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