JASC 2782
Service difficulty reports · 1,225
Reports filed under 2782 · Leading Edge Slat Actuator, 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 = '2782' 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 = '2782' 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 C8GA20090179Actuator · leakingDURING CLIMB OPERATION A TOTAL "A" HYD SYS FAILURE OCCURRED. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. THE NR 3 SLAT ACTUATOR INBD FITTING WAS CRACKED. REMOVED AND REPLACED THE NR 3 SLAT ACTUATOR, REMOVEDSDR CA090904002Actuator · failedON APPROACH, THE CREW EXPERIENCED A FLAP/SLAT FAILURE WITH FLAPS AT POSITION 2, AND SLATS AT POSITION 0. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS CARRIED OUT. LT NR 5 SLAT ACT CHANGED DUE TO TORQUE LIMITER IND TRIPPED.SDR UALA2009081702503Plate · damagedRT WING KRUEGER FLAP ROTARY ACTUATOR OUTBOARD SUPPORT PLATE BENT AND CRACKED. INSTALLED NEW SUPPORT PLATE P/N 114T6124-2.SDR CA090813003Actuator · malfunctioned(CAN) SLAT FAIL CAUTION ON APPROACH. QRH CARRIED OUT, AND MSG PERSISTS. FIM ACCOMPLISHED, FOUND SLAT ACTUATORS NR 5 AND 8 TRIPPED TORQUE LIMITER INDICATORS. RE-SET PER AMM. NR 8: P/N 1703911, S/N 0320, MFR: HAMILTON SUNDSTRAND (TC# 20090813003)SDR C8GA20090133Actuator · leakingFLT 721 FROM TOL TO ROC. AFTER DEPARTING THE RUNWAY THE GEAR WOULD NOT RETRACT, A LOSS OF SYSTEM "A" HYDRAULICS WAS NOTED. THE AIRCRAFT RETURNED TO TOL WHERE AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT SDR AALA20090801DFW01Actuator · faultedDFW - AUTO SLAT FAIL LIGHT ILLUMINATED ON TAKEOFF OUT OF AUS THEN HAD FLAP DISAGREE LIGHT ON DESCENT. LANDED DFW WITHOUT INCIDENT. FOUND FORWARD AUTO SLAT ACTUATOR FAULTED. REPLACED ACTUATOR AND ADJUSTED CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERATIOSDR FDEA200907272792Actuator · failedFLIGHT TEST-THE NR 2 LED FAILED TO RETRACT AFTER TAKEOFF. NR 2 SLAT ASSY FOUND TO BE RETRACTED WITH ACFT INBOUND AND NR 2 SLAT INTRANSIT AMBER LIGHT ILLUM IN COCKPIT ON FWD PNL AND S/O IND PNL. T/S NR 2 SLAT INDICATION IAW MM 27-82-000-1 AND FOUND TO BE FASDR CA090727004Actuator · binding(CAN) PILOTS REPORTED ALL SYS NORMAL. ON PRE-FLIGHT THE PILOTS COULD NOT GET THE SLATS TO MOVE WHEN SELECTED FLAPS DOWN. MX WAS CALLED AND COULD NOT DETECT WHAT WAS FAILED ON THE SYS. ACFT PROCEEDED TO COMPLETE A FERRY FLIGHT WITH SLATS RETRACTED USING BYPASDR YENA20090704070Indicator · trippedEICAS AMBER SLAT FAIL MESSAGE, REFERENCED QRH. TROUBLESHOOTING REVEALED THAT SLAT BRAKES WERE SET AND ACTUATOR TRIP INDICATOR TRIPPED (SLAT ACTUATOR 6 ON TRACK 7). CLEANED INSPECTED AND RESET SLAT ACTUATOR AND PERFORMED FUNCTIONAL CHECKS IAW AMM 27-81-01. NSDR AALA2009042700002Rotary Actuator · malfunctionedSFO - UPON RETRACTING FLAPS FROM 1 DEGREE TO 0 DEGREES LEADING EDGE LIGHT AND LEADING EDGE SLAT DISAGREE MESSAGE ILLUMINATED. EMERGENCY DECLARED RETURNED SFO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 AND 20 ROTARY DRIVE ACTUATORS. SDR AALA2009033100005Actuator · leakingCREW REPORTED THAT ON APPROACH THERE WAS A NR 4 SLAT IN TRANSIT PROBLEM. EMERGENCY DECLARED LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND THE NR 4 LEADING EDGE SLAT ACTUATOR LEAKING. REPLACED THE NR 4 LEADING EDGE SLAT ACTUATOR. SYSTEMSDR AALA2009032100001Pdu · leakingMIA - CREW REPORTED ELECTRIC BURNING SMELL AND HAZE IN COCKPIT. LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND THE LEFT WING POWER DRIVE UNIT DRIVE MOTOR PUMP LEAKING HYDRAULIC FLUID. REPLACED BOTH HEAT EXCHANGERS, RECIRCULATION FANS, ANSDR R61A20090011Actuator · faultyCREW REPORTED SLAT FAIL INDICATION ON EICAS DURING APPROACH. CREW DECLARED EMERGENCY INTO PHL, AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE A/C. TROUBLESHOT AND FOUND SFACE NR 2 TO BE AT FAULT. REPLACED PER EMB AMM, OPS CHECKED AND FOUND SDR I5PA0308091Actuator · defectiveAIRCRAFT, AIR RETURN DUE TO NR 3 L/E SLAT REMAINED EXTENDED AND NR 3 SLAT REMAINED IN TRANSIT DURING FLAP RETRACTION. REMOVED AND REPLACED NR 3 L/E SLAT ACTUATOR THEN CLEANED AND RESEATED NR 2 L/E SLAT SWITCH. OPERATIONAL CHECK OK.SDR NWAA09439948Actuator · damagedON APPROACH, AFTER FLIGHT CREW CONFIGURED THE ACFT FOR LANDING, THE AMBER "SLAT DISAGREEMENT" LIGHT ILLUMINATED, THE BLUE "SLAT EXTEND" LIGHT DID NOT COME ON, AND AN UNCOMMANDED ROLL OF THE ACFT TO THE RT OCCURRED. THE SLATS WERE RETRACTED WITHOUT DIFFICULTY,SDR CALA2009012600055Rotary Actuator · inoperativeLEADING EDGE SLAT DISAGREE LIGHT ILLUMINATED DURING CLIMBOUT, PERFORMED ABNORMAL CHECKLIST. SLAT WOULD NOT RETRACT, RETURNED TO AIRPORT (EWR). REMOVED AND REPLACED NUMBER 11 AND 13 ROTARY ACTUATORS PER AMM 27-81-18. OPERATIONAL CHECKS NORMAL.SDR R61A20090002Sensor · failedON CLIMBOUT CREW REPORTED, THEY RECEIVED SLAT/FLAP FAIL MESSAGE ON EICAS. CREW DECLARED EMERGENCY FOLLOWED QRH PROCEDURES AND RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO A/C TROUBLESHOT SYSTEM FOUND SLAT 2/3 SKEW SENSOR TO BE BAD. REPLASDR FDEA200901090107Actuator · failedAFTER TAKEOFF WHILE RAISING FLAPS NR 1 LEADING EDGE DEVICE REMAINED EXTENDED AT 2 DEG AND 0 DEG FLAP SETTING. RAN QRH PROBLEM REMAINED. RETURNED TO BASE FOR NORMAL LANDING. LEADING EDGE DEVICE RETRACTED ON SCHEDULE AFTER LANDING CLEAN UP. VISUAL INSPECTION SDR FDEA200901080103Actuator · failedAFTER TAKEOFF WHILE RAISING FLAPS NR 1 LEADING EDGE DEVICE REMAINED EXTENDED AT 2 DEG AND 0 DEG FLAP SETTING. RAN QRH PROBLEM REMAINED. RETURNED TO BASE FOR NORMAL LANDING. LED RETRACTED ON SCHEDULE AFTER LANDING CLEAN UP. VISUAL INSPECTION OF NR 1 LEADINGSDR R61A20080048AActuator · failedON APPROACH CREW REPORTED, RECEIVED A SLAT FAIL MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE CLEARED SF-ACE INHIBITS PERFORMED OPERATIONAL CHECK OF SYSTEM, SYSTEMS OPERATIOSDR YENA200812020123Actuator · malfunctionedFLT 1150, MCO-PWM, DIVERTED TO BOS, SLAT FAIL IN FLIGHT. T/S PER FIM 27-81-00-810-802A, FOUND SLAT ACT NR 6 TORQUE LIMITER TRIPPED. REMOVED AND REPLACED PER AMM 27-81-01, OPS CHECK NORMAL.SDR YENA200811240119Pdu · failedORD-JFK, SLAT FAIL ON APPROACH TO LANDING, QRH ITEMS COMPLETED. AFTER EMBRAER ANALYZED THE FHDB FOR SLAT FAIL EVENT (REPEAT ITEM) IT WAS DETERMINED THAT THE SLAT SURFACES JAMMED IN FLIGHT DURING APPROACH. FIM TASK 27-81-00-810-802-A. PERFORMED FIM TASK 27-8SDR FDEA200811194925Actuator · failedNR 7 LEADING EDGE DEVICE FAILED TO RETRACT AFTER TAKEOFF. WHEN GOING FROM 2 DEG TO 0 DEG. RAN QRH LED DID NOT RETRACT FLIGHT CONTROL INPUTS INDICATE THE LEADING EDGE DEVICE WAS ACTUALLY EXTENDED. R & R NR 7 SLAT ACTUATOR IAW MM 27-81-032-4. OPS CK AND LSDR 08FDEA04925Actuator · failedNR 7 LED FAILED TO RETRACT AFTER TAKEOFF. WHEN GOING FROM 2 DEG TO 0 DEG, RAN QRH LED DID NOT RETRACT FLIGHT CONTROLS INPUTS INDICATE THE LED WAS ACTUALLY EXTENDED. REMOVED AND REPLACED NR 7 SLAT ACTUATOR PER M/M 27-81-032-4. OPS CKS AND LEAK CKS NML.SDR YENA200811200115Actuator · failedFLT 1219, BOS-BUF, AOA FAIL EICAS MESSAGE, SLAT FAIL EICAS MESSAGE QRH COMPLIED WITH EMERGENCY LANDING ACCOMPLISHED. T/S PER FIM TASK 27-81-00-810-802-A. FOUND NR 6 RT SLAT ACTUATOR TRIPPED DUE TO PREVIOUS HISTORY, REMOVED & REPLACED NR 6 RT SLAT ACTUATOR PSDR R61A20080043Actuator · malfunctionedON APPROACH CREW REPORTED A SLAT/FLAP FAIL MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TROUBLESHOT. REMOVED AND REPLACED THE NR 5 SLAT ACTUATOR COMPLETED OPERATIONAL CHECK OF THE SYSTEM, OPERATIONAL SDR R61A20080042Actuator · malfunctionedCREW REPORTED FLAP/SLAT FAIL ON APPROACH. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 2 AND NR 3 ACTUATOR TRIPPED. MAINTENANCE RESET ACTUATORS AND SYSTEM OPERATIONAL CHECK COMPLETED, SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT WAS RSDR AALA200802456AActuator · faultedBOS INFLIGHT - LEADING EDGE SLAT DISAGREE INDICATION WHEN FLAPS SELECTED TO ONE AT 21 KNOTS. LANDED BOS WITHOUT INCIDENT. FOUND NUMBER ONE SLAT AND NR 2 ROTARY ACTUATOR TRIPPED. REPLACED NR 2 SLAT ROTARY ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA200802341AActuator · trippedBOS INFLIGHT, DURING APPROACH CREW REPORTED SLAT DISAGREE INDICATION. LANDED BOS WITHOUT INCIDENT. FOUND LEFT INBOARD ROTARY ACTUATOR TRIPPED. REPLACED LEFT LEADING EDGE SLAT DRIVE INBOARD ROTARY ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR CA081016006Actuator · malfunctioned(CAN) SLAT FAIL ON APPROACH CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. T/S IAW FIM, SLAT INHIBIT CLEARED, OPS CHECK PASSED. CONSIDERED TRANSITORY CONDITION OF THE SLAT CONTROL SYS. 2 SLAT ACTUATORS REPLACED: LT SLAT ACT POS 04L REPLACED, P/N S/N ASDR PCSA2008093001Actuator · leakingLOST A HYDR SYS AFTER FLAP RETRACTION DEPARTING. ON APPROACH TO POS NR 7 L/E SLAT FAILED TO EXTEND. LANDING GEARS WERE EXTENDED MANUALLY, THE AC LANDED SAFELY AND WAS TOWED FROM THE RUNWAY. MAINT DISCOVERED THE NR 7 L/E ACTUATOR BODY HAD FAILED CAUSING A LOSSDR CA080911003Actuator · failed(CAN) DURING CLIMB THROUGH APPROX 2,000 FT NR1 ENGINE LOW HYDR PRESSURE LIGHT ILLUMINATED, SYS `A` HYDRAULIC OIL AND PRESSURE LOSS. ACFT RETURNED TO DEPARTURE. NR5 KRUGER FLAP ACTUATOR FOUND FAILED AND ATTACH BRACKET DAMAGED. REPLACED ACTUATOR AND TESTED IAW ASDR YENA2008083Actuator · failedFLT NR 293, SEA-LGB, SLAT FAIL ON APPROACH TO LGB, FOUND LT NR 5 SLAT ACTUATOR TRIPPED. R/R LT SLAT ACTUATOR IAW AMM 27-81-01. PERFORMED SLAT CTL MECH RIGGING PER 27-80-00-820-801 & SLAT CTL ELEC RIGGING PER 27-80-00-820-802A/200. NO FAULTS NOTED. OPS TESTSDR 08FDEA03633Actuator · failedNR 8 SLAT FAILED TO RETRACT NORMALLY. LED AMBER ON FRONT PANEL AND S/O PANEL. REMOVED PANELS ON EACH SIDE OF ACTUATOR. FOUND WIRING CLAMPS LOOSE TIGHTENED. WILL CHANGE ACTUATOR OR SWITCH FOR MOCC. REPLACED NR 8 SLAT ACTUATOR REF MM 27-81-032-4. OPS AND LSDR USAASB08060Actuator · failedCLT FLT 1631, ON CLIMBOUT FROM CLT, EN ROUTE TO TPA, THE NR 3 LEADING EDGE SLAT FAILED TO RETRACT CAUSING THE ACFT TO ROLL APPROXIMATELY 10 TO 15 DEGREES. PILOT WAS ABLE TO CORRECT THE ROLL WITH REDUCED SPEED AND AILERON INPUT. FLIGHT RETURNED TO FIELD AT CLSDR USAASB08039Actuator · leakingCLT FLT 1457 - ON CLIMBOUT FROM CTL, EN ROUTE TO FLL, CREW RECEIVED A LEADING EDGE SLAT INDICATION LIGHT. UNSURE OF WHICH SLAT GAVE THE INDICATION, CAPTAIN DECIDED TO RETURN TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED.SDR DHLA200800050Actuator · leakingFLIGHT 1612 ON TAKEOFF ROLL, A/C SUSTAINED HYD A-SYSTEM FAILURE PRIOR TO 60 KIAS. FOUND NR 5 KRUEGER FLAP LEAKING. REMOVED AND REPLACED NR 5 KRUEGER FLAP ACTUATOR. SERVICED A-SYS. INSP NR 1 & 2 CASE DRAIN FILTERS. OPS CHECK GOOD. NO FURTHER LEAKS NOTED. SDR DHL2008764522Mount Bracket · crackedNR 1 K-FLAP ACTUATOR TRUNNION MOUNTING BRACKETS CRACK INDICATION WS 305. REMOVED NR 1 K-FLAP MOUNTING BRACKETS WS 305 IAW B727 SRM 51-30-2. FAB NEW BRACKETS WITH 2024-T3 .063", DIM 7.5" X 4" AND PO 9006027 IAW BOEING ENGINEERING DWG 65-16275.SDR DHL2008764520Bracket · crackedNR 2 K-FLAP ACTUATOR, TRUNNION MOUNTING BRACKETS CRACK INDICATION (WS 235 APPROX). REMOVED NR 2 K-FLAP TRUNNION MOUNTING BRACKETS FROM ACTUATOR WS 235 IAW B727 SRM 51-30-2. FAB NEW BRACKETS WITH 2024-T3 .063" DIM 9" X 6.5 AND PO 9006773 IAW BOEING ENGINEERINSDR P5CA0801561Pdu · malfunctionedLEADING EDGE DRIVE, LEADING EDGE MULTI DRIVE STATUS MESSAGES RECEIVED. REPLACED NR 2 RT LEADING EDGE PDU PER MM 27-81-03. OPERATIONAL CHECK NORMAL.SDR BB08088Rotary Actuator · overtorquedPHX FLT 146 - PHX TO LIH. ON DEPARTURE FROM PHX, THE CREW RECEIVED A 'LE SLAT DISAGREE' EICAS MESSAGE WITH A LEADING EDGE LIGHT ILLUMINATED. THE FLAPS INDICATOR REMAINED BETWEEN FLAPS UP AND FLAPS ONE POSITIONS. THE FLIGHT RETURNED TO FIELD AND LANDED WITHSDR BB08087Rotary Actuator · overtorquedPHX FLT 146 PHX TO LIH. ON DEPARTURE FROM PHX, THE CREW RECEIVED A 'LE SLAT DISAGREE' EICAS MESSAGE WITH A LEADING EDGE LIGHT ILLUMINATED. THE FLAPS INDICATOR REMAINED BETWEEN FLAPS UP AND FLAPS ONE POSITIONS. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOSDR BB08085Rotary Actuator · overtorquedPHX FLT 146 - PHX TO LIH. ON DEPARTURE FROM PHX, THE CREW RECEIVED A 'LE SLAT DISAGREE' EICAS MESSAGE WITH A LEADING EDGE LIGHT ILLUMINATED. THE FLAPS INDICATOR REMAINED BETWEEN FLAPS UP AND FLAPS ONE POSITIONS. THE FLIGHT RETURNED TO FIELD AND LANDED WITHSDR SWAA082579Actuator · malfunctionedON APPROACH FLAPS EXTENDED TO 5 DEGREES HAD AMBER L/E FLAP TRANSIT LIGHT ILLUMINATED, AND HAD IMMEDIATE ROLL. REMOVED AND REPLACED NR 3 L/E ACTUATOR PER MM.SDR AALA200801193Transmitter · inoperativeLAX INFLIGHT T1913/04MAY - CREW REPORTED LEADING EDGE SLAT DISAGREE INDICATION ON APPROACH. REPLACED LEADING EDGE DRIVE TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR DHL2008784001Support Bracket · crackedNR 5 K-FLAP ACTUATOR BOX HAS SMALL CRACK ON THE O/B SUPPORT BRACKET L/E STA 243.977 CRACK LOCATED AT LOWER FWD CORNER OF BRACKET.SDR DXTA200803006Actuator · out of adjustSLATS FAILED TO RETRACT SLAT UNBALANCED AND FLAP/SLAT MAINT CAS MESSAGES PRESENT. ADJUSTED RT NR 2 SLAT BALLSCREW ACTUATOR OK TO CONTINUE SERVICE. NO DEFECTS NOTED.SDR DHL2008763528Support Fitting · crackedNR 6 K-FLAP ACTUATOR MOUNT SPT FITTING CRACKED AT WS 307.5. REMOVED ACTUATOR SUPPORT MOUNT ASSY. FABRICATED SUPPORT WEBS FROM 2024-T3, .063" BY 8" BY 3.5" (2 EA), PO NR 9006027, AND MOUNT DOUBLERS FROM 7075-T6, .125" BY 5" BY 2", (2 EA), PO NR 9005685, ASSEMSDR DHL2008763527Support Fitting · crackedNR 1 K-FLAP ACTUATOR MOUNT SPT FITTING CRACKED AT WS 307.5 AND 315.3. REMOVED ACTUATOR SUPPORT MOUNT ASSY, FABRICATED SUPPORT WEBS FROM 2024-T3, .063" BY 8" BY 3.5" (2 EA), PO NR 9006027, AND MOUNT DOUBLERS FROM 7075-T6, .125" BY 5" BY 2", (2 EA), PO NR 90056SDR USAA920080597Actuator · malfunctionedFLT 1643 - CLT-PHX - EMERGENCY LANDING - DURING APPROACH, SLATS FAILED TO DEPLOY. CREW MADE A CONFIG 3 LANDING AND LANDED AT APPROXIMATELY 158 KTS. NO BRAKING ISSUES. EMERGENCY EQUIPMENT HAD RESPONDED BUT AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT. MAINT
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