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 SWAA2024040356797Actuator · crackedCRACK LEADING EDGE SLAT NOSE SKIN ACTUATOR RIB SLAT 6 RT WING 2024-164617<[01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN:200048001;DUE DATE:01-MAY-24.;[02] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 200053402; DUE DATE: 24-AUG-24;[03]SDR CALA2024022800594Actuator · faultedSLAT SYS FAULT. WARNINGS & CORRELATED FAULTS F/CTL SLATS FAULT 27-00 06 19:39:00 SLT 1 SYSTEM JAMCHECK SLT MECH DRIVE 27-80-00 SFCC 1 06 19:39:00 SLT 2 SYSTEM JAMCHECK SLT MECH DRIVE 27-80-00 SFCC 2 06 19:40:00. IN REF TO TSM 27-81-00-810-810-A. INSECTED TOSDR DALA2024022602671Actuator · inoperativeSHIP 3941 -ATB/UFC- DUE TO LEADING EDGE FLAP TRANSIT LIGHT WOULD NOT EXTINGUISH. #1 AND #2 SLATS SHOW AMBER. CORRECTIVE ACTION: MAINTENANCE RESET BOTH EXT/RET FUSES AND REPLACED NUMBER 3 LEADING EDGE SLAT ACTUATOR PER B737 AMM 27-81.SDR DALA2024022702754Actuator · trippedSHIP 6812 -FCNT/DE- LE SLAT DISAGREE ON APPROACH. CORRECTIVE ACTION: T/S REPLACED ROTARY ACTUATORS, PERFORMED LUBE, OPS / ADJ SATISFACTORY.SDR AALA202402262137Actuator · trippedAIRCRAFT WAS GROUNDED: WHILE DESCENDING ON THE ARRIVAL AND SELECTING FLAPS 1, RECEIVED ECAM MESSAGE FOR FLIGHT CONTROL SLATS FAULT AND FLIGHT CONTROL ALTERNATE LAW. FLIGHT CREW ACCOMPLISHED THE ECAM PROCEDURES AND FOLLOW UP ECAM ACTIONS. THE FLAPS/SLATS INDICSDR AALA202402199165Actuator · seizedAIRCRAFT WAS GROUNDED: FLIGHT CONTROL SLAT FAULT WHEN FLAP LEVER MOVE TO POSITION 1. REMOVED AND REPLACED (6037CM) B-SLAT ACTUATOR (AALA202402199165) AND (6015 CM) A-SLAT ACTUATOR (AALA202402197965).SDR AALA202402197965Actuator · seizedAIRCRAFT WAS GROUNDED: FLIGHT CONTROL SLAT FAULT WHEN FLAP LEVER MOVE TO POSITION 1. REMOVED AND REPLACED (6037CM) B-SLAT ACTUATOR (AALA202402199165) AND (6015 CM) A-SLAT ACTUATOR (AALA202402197965).SDR AALA202402136239Actuator · trippedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INBOUND INTO SEA DUE TO A FLIGHT CONTROL SLATS FAULT ECAM MESSAGE WITH ASSOCIATED MESSAGE SLAT 1 AND 2 SYSTEM JAM CHECK SLAT MECHANICAL DRIVE WHEN THE FLAPS WERE SELECTED TO 1 ON ARRIVAL. THE AIRCRAFT LANDED SAFSDR YENA2024020600245Actuator · failedFLT#2216, LAX-JFK. (AIRCRAFT DECLARED AN EMERGENCY INTO JFK) 'WHILE SELECTING FLAPS 1 FOR THE APPRACH INTO JFK WE GOT A "F/CTL SLATS FAULT" ECAM. SLATS STORED AT ZERO.LANDING WAS SMOOTH AND NORMAL; TSH PER MAINT MSAS PER TSM 27-81-00-810-810-A.FOUND A TRIPPED SDR AALA202401295585Actuator · trippedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED ON ARRIVAL INTO CLT DUE TO THE SLATS LOCKED AT 0 ON DESCENT AND A SLATS FAULT MESSAGE. THE AIRCRAFT LANDED SAFELY AT CLT WITH FLAPS 3 AND NO SLATS. MAINTENANCE FOUND THE RIGHT WING #7 SLAT TRACK ACTUATOR TRIPPEDSDR IPXA2024012647104Actuator · unserviceableAIR TURN BACK.AFTER TAKEOFF WHEN FLAPS AND SLATS RETRACTED, LEVEL 2 €ŒAIL DEFLECT DISAGREE€? ALERT DISPLAYED.RAN QRH PROCEDURE TO RESET, NO HELP.AIRCRAFT HAD ROLL TO THE RIGHT THROUGHOUT THE RETURN FLIG VERIFIED INSTALL AND SAFETIES, WITNESSED RIG, OPS CHECKSDR AALA202401113672Actuator · bindingAIRCRAFT WAS GROUNDED: SLATS JAMMED WOULD NOT LOWER. FLAPS OPERATED NORMALLY, "F/CTL SLATS FAULT". REPLACED #9 SLAT ACTUATOR PER AMM 27-84-49.SDR DALA2024010900361Unknown · unknownSHIP 3035 SLAT PCU REQUIRES REPLACEMENT DUE TO HIGH OIL CONSUMPTION. CORRECTIVE ACTION: REMOVED AND REPLACED SLAT PCU PER A321 AMM 27-84-51. OPS CHECK GOOD. (0146550)SDR DALA2023113009852Unknown · unknownSHIP 1023 - MISC/DE - DUE TO SLATS FAILING TO EXTEND. SLATS LOCKED ECAM. CORRECTIVE ACTION: FOUND LEFT #9 SLAT DRIVE ACTUATOR TORQUED LIMITER TRIPPED. REPLACED ACTUATOR. AIRCRAFT RTS. OK FOR SERVICE. (4260992)SDR ABXA20231025206Module · leakingAFTER TAKEOFF EICAS MSG 1) CHYD QTY 2)C HYD 2 OVHT CENTER HYD SYSTEM REAAD 0.16 AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT GROUNDED BY MAINTENANCE. TROUBLE SHOT AND FOUND OUTBOARD SLAT PDU CONTROL VALVE MODULE LEAKING .REMOVED AND REPLACED LEFT OUTBSDR YENA2023100401194Actuator · failedFLT#34, SFO-BOS. (AIRCRAFT DECLARED AN EMERGENCY INTO BOS) 'F/CTL SLATS FAULT WHEN FLAP HANDLE MOVED TO 1 DURING APPROACH. ECAM/QRH RECYCLE UNSUCCESFUL. SLATS STUCK AT 0. WHEN FLAP HANDLE MOVED TO 2 DURING QRH PROCEDURE, FCTL ALTN LAW ECAM OCCURRED. LANDING PESDR DALA2023091807654Unknown · unknownON TAKE-OFF FROM ORD, NOTICE MUSTY SOCK SMELL FOR SEVERAL MINUTES. C/W WORKCARD 0550-2001 ISOLATE SMOKE + FUMES IN COCKPIT/CABIN UP TO STEP#4. FOUND HYDRALIC LEAK ON RT SIDE OF THE WING TO THE BODY FAIRING. REMOVED PANEL 192BB AND FOUND SLAT ANGLE GEARBOX LEAKSDR DALA2023072105893Unknown · unknownSHIP 3506 SLAT POWER CONTROL UNIT HEALTH CHECK EXCEEDED MAX ALLOWABLE TORQUE. CORRECTIVE ACTION: R/R SLAT POWER CONTROL UNIT. (4723280)SDR R61A2023060600345Unknown · unknownFLAP FAIL AFTER TAKE OFF. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED FIM TASK 27-52-00-820-802-A. FOUND LH TORQUE TUBE F3 DISCONNECTED FROM FLAP ACTUATOR 1L. RECONNECTED TORQUE TUBE.SDR YENA2023042800454Actuator · failedFLT # 8352, PHX-BOS. ON APPROACH UPON SELECTING FLAPS 1, SLAT FAIL CAUTION ILLUMINATED. RAN ECL, SLATS INOPERABLE, BUT FLAPS OPERATED NORMALLY; REMOVED ACESS PANEL 522DB FOUND OVER TORQUE INDICATOR TRIPPED REMOVED PANEL IAW AMP J57-41-32.PER T/S REPLACED #3 LESDR SWIA2023012367161Actuator · failedSLAT FAIL IN FLIGHT, ARRIVED AT AIRCRAFT AND ATTEMPTED TO OPS CHECK SLAT SYSTEM. SLATS WOULD NOT MOVE. INTERROGATED MDC AND FOUND MULTIPLE INSTANCES OF FSACE 2 WRG FAULTS. REMOVED AND REPLACED FSACE 2 PER E175 AMM 27-53-02-000-801-A AND 27-53-02-400-801-A. SDR F3LA2023130100010Actuator · faultedFCLT SLATS FAULT. REMOVED AND REPLACED ACTUATOR 6045CM IAW AMM 27-84-48-400-001-A & AMM 27-84-49-000-001-A. RAN OPS TEST OF SLAT SYSTEM OPS CHECK GOOD T/W F9192.SDR AALA202301063211Actuator · bindingAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED ON ARRIVAL INTO CLT DUE TO A SLAT JAMMED MESSAGE. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND LEFT WING SLAT ACTUATOR (6037CM) TORQUE LIMITER TRIPPED AND REPLACED SLAT ACTUATOR SDR F3LA2023040100003Actuator · faultedFOUND SLAT ACTUATOR 6041CN (FIN) POP OUT, ACTUATOR NEEDS TO BE REPLACED IAW TSM 27-81-00-810-810-A. REMOVED AND REPLACED LEFT AND ACTUATOR FIN 6041CM IAW AMM 27-84-49-000-002-A & 27-84-49-400-002-A. T/W 81 ASSET N00038516 DD07/31/2023.//END//SDR YENA2022120501206Actuator · failedFLT#2536, STI-JFK. (AIRCRAFT DECLARED AN EMERGENCY) ' REF L/P 3347609 ITEM #1 CONTINUES WITH INSPECTION OF RH WING SLAT SYSTEM JAM PER TSM 27-81-00-810-810-A; CONTINUED INSPECTION OF RH SLAT JAMMED ACTUATORS, ALL OTHER ACTUATORS FOUND GOOD, WITH THE EXCEPTION SDR YENA2022120501205Actuator · faultedFLT#2536, STI-JFK. DECLARED AN EMERGENCY, ON THE FINAL APPROACH. SLATS INOPERATIVE. LANDED SLATS ZERO UAPP = 166K. SLAT ACTUATOR 6091CM WAS REPLACED AND OPS TEST WAS PERFORMED, REVIEWED CFOS/PFR, F/CTL HISTORY NOTED A/C ECAM FAULT "SLT 1 SYSTEM JAM"/SLT 2SDR F3LA2022091900111Actuator · bindingDISCREPANCY: REFERENCE LOG PAGE LP295662 ITEM 1, F/CTL SLATS FAULT ON APPROACH.
CORRECTIVE ACTION: REMOVED L/H WING SLAT ACTUATOR 6037CM REF. AMM 27-84-49-000-002-A. INSTALLED SERVICEABLE ACTUATOR REF. AMM 27-84-49-400-002-A. OPS CHECK GOOD. T/W F9TAB4788C DUSDR MASA2022082900220None · noneFLAP FAIL CAUTION (EMERGENCY DECLARED). RESET SFECU AND CLEARED INHIBITS, OPS CHECK GOOD.SDR DALA2022070604697None · noneREMOVE #2 LH SLAT ACTUATOR TO FOM. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0275:2021-2065-LH/012 00232 REMOVED AND REINSTALLED LH WING #2 SLAT ACTUATOR IAW A220 AMP 27-81-30. (LP# 2303406)SDR AALA202205177503None · noneAIRCRAFT WAS GROUNDED: FLIGHT CONTROL SLAT FAULT WHILE EXTENDING FLAPS 1 ON APPROACH TO PDX. DECLARED AN EMERGENCY AND LANDED SAFELY. REPLACED RIGHT WING TRACK 11 SLAT TYPE B ACTUATOR PER AMM 27-84-49. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. (SUPPLEMENTALSDR AALA202205107503Actuator · faultyAIRCRAFT WAS GROUNDED: FLIGHT CONTROL SLAT FAULT WHILE EXTENDING FLAPS 1 ON APPROACH TO PDX. DECLARED AN EMERGENCY AND LANDED SAFELY. REPLACED RIGHT WING TRACK 11 SLAT TYPE B ACTUATOR PER AMM 27-84-49. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.SDR YENA2022050900457Actuator · failedFLT#233, BTV- JFK (AIRCRAFT DECLARED A EMERGENCY). ' SLAT FAIL IN FLIGHT - SLATS WOULD NOT MOVE OUT OF 0 POSITION; PER TSM 27-83-00-810-814A. REMOVED AND REPLACED SLAT/FLAP ACTUATOR CONTROL ELECTRONIC UNIT IAW AMM 27-53-02. OPS CHECK GOOD, NO FAULTS NOTED.'SDR AALA202203282014Actuator · unserviceableAIRCRAFT WAS GROUNDED: ON APPROACH AT FLAPS 1, ECAM FLIGHT CONTROL SLATS FAULT. SLAT APPEARS STUCK UP. FLIGHT DECLARED AN EMERGENCY AND LANDED SAFELY. **SUPPLEMENTAL REPORT FOR AALA202203245267: REPLACED LEFT WING SLAT #1 ACTUATOR 6013CM (AALA202203245267) ANDSDR AALA202203285267Actuator · unserviceableAIRCRAFT WAS GROUNDED: ON APPROACH AT FLAPS 1, ECAM FLIGHT CONTROL SLATS FAULT. SLAT APPEARS STUCK UP. FLIGHT DECLARED AN EMERGENCY AND LANDED SAFELY. **SUPPLEMENTAL REPORT FOR AALA202203245267: REPLACED LEFT WING SLAT #1 ACTUATOR 6013CM (AALA202203245267) ANDSDR AALA202203245267None · noneAIRCRAFT WAS GROUNDED: ON APPROACH AT FLAPS 1, ECAM FLIGHT CONTROL SLATS FAULT. SLAT APPEARS STUCK UP. FLIGHT DECLARED AN EMERGENCY AND LANDED SAFELY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)SDR DALA2024031203261Pcu · unknownREMOVE THE SLAT PCU PER ER/A #597244 SECTION 01. THEN INSTALL THE NEW PCU WITH STK# 35-2784-9-0007. SPECIAL TOOLING WILL BE REQUIRED. MULTIPURPOSE ADAPTOR 98L20003001000 WILL BE USED TO LIFT AND SECURE THE PCU. REMOVE THE SLAT PCU PER ER/A #597244 SECTION 01. SDR FDEA202202120282Actuator · failedHYD GREEN RSVR LO LEVEL ECAM W/ ASSOCIATED GREEN HYD QUANTITY IN YELLOW ABOVE THE RED DOT THEN BELOW THE RED DOT. CROSS CHECKED ECAM HYD PAGE AND INDICATION CORRELATED W/GAUGE. FOLLOWED QRH PROCEDURE W/NEGRES. REMOVED R/H KRUEGER FLAP ACTUATOR PER A30SDR AALA202111036111Actuator · malfunctionedAIRCRAFT WAS GROUNDED: WHEN FLAPS POSITIONED TO "1"DURING APPROACH FLIGHT CONTROL SLATS FAULT ECAM RECEIVED. RECYCLED ABOUT 7 TIMES BEFORE SLATS EXTENDED. REMAINDER OF FLAP EXTENSION WAS NORMAL. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED AT DFW WITHOUT SDR T8VA2021111700001Shaft · wornCREW REPORTED FLAPS INOPERATIVE, STUCK AT 7 DEGREES. FAILED FL23 CURRENT LIMITER, REPLACED FL23 CURRENT LIMITER P/N ANL4. INVESTIGATED REASON FOR FAILED CURRENT LIMITER AND FOUND SEVERAL FLAP ACTUATORS SCREW SHAFTS TO BE ROUGH AND POSSIBLY BINDING UNDER A LOASDR HALA2021090700128Actuator · not reportedSHIP 361 REPLACE L WING SLAT OTBD ROTARY ACTUATOR PER AA 2781-01050-04A THIS IS AN RII PROCEDURE REFER TO TOPP 40-30-05. REPLACEMENT OF GEARED ROTARY ACTUATOR IS REQUIRED PRIOR TO FURTHER FLIGHT. AD 2019-19-06. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SSDR FDEA202108182031Actuator · faultedON CLIMB OUT GOT EICAS MESSAGE LE SLAT DISAGREE AND LEADING EDGE DISCRETE LIGHT RETRACTING THE FLAPS AT 200 KNOTS AND 3000 FEET QRH COMPLIED WITH. TROUBLESHOT PER B757 FIM 27-81 FAULT TREE 803 AND FOUND OVERLOAD INDICATOR TRIPPED ON THE INBD SLAT PDU TORQUE LSDR FDEA202107211830Actuator · failedDURING FLIGHT WE RECEIVED A LEVEL ONE HYD 1 OFF. FOLLOWED BY HYD 1 QTY LO. 2.3 GALLONS. SERVICES HYD QUANTITY AND REMOVED /REPLACED INBOARD SLAT ACTUATOR AS PER AMM 27- 82-01-4 , OPS AND LEAK CHECK GOOD NO LEAK NOTED.SDR FDEA202107141780Actuator · failedAS WE WERE BRINGING SLATS UP WHILE IN A RIGHT TURN. AIRCRAFT CONTINUED TO ROLL UPWARDS OF 40 DEGREES. COMMANDED TO EXTEND SLATS. DISCONNECTED AUTOPILOT. THEN RECEIVED SLATS DIAG WARNING. AS SLATS EXTENDED, WAS ABLE TO STOP ROLL AND REGAIN HEADING CONTROLSDR XMXR202104230006Actuator · failedFLAP FAIL MESSAGE YELLOW BOX ON FLAP INDICATOR ON POWER UP.SDR XMXR202104230008Actuator · failedAFTER ENGINE START, FLAP FAIL CAS MESSAGE WITH FLAP HANDLE IN POSITION ). FLAP HANDLE IN POSITION 1 CONTINUED WITH YELLOW FLAP INDICATIONS AND CAS MESSAGE. RETURN HANDLE TO POSITION 0 MADE CAS MESSAGE DISAPPEAR AND GREEN FLAP 0 INDICATIONS APPEARED.
SDR YENA2021012200076Actuator · failedFLT 1054, PBI-JFK. EMERGENCY DECLARED. F/CTL SLATS FAULT IN FLIGHT PRIOR TO LANDING. SLATS FAILED AT ZERO. ECAM/ QRH PROCEDURE DID NOT RESET SLATS. LANDED FLAPS 3, SLATS 0. LANDING WAS NORMAL, NO OVERSPEEDS. BRAKE TEMPS REMAINED WITHIN LIMITS, REF TSM 2SDR CALA2020122301406Actuator · faultedEMERGENCY ON APPROACH. SLATS FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL FLAPS WENT TO 3 SLATS O. ACCOMPLISHED OPERATIONAL TEST OF SLAT SYSTEM, PER AMM 27-84-00-710-001-A. AFTER REPLACEMENT OF NR 1 LT OUTBOARD SLAT ACTUATOR. LT OUTBOARD SLAT ACTUATOR TYSDR AALA202010309016Powerpack · inoperativeAIRCRAFT WAS GROUNDED. ON APPROACH ELECTRONIC CENTRALIZED AIRCRAFT MONITOR "FLAPS/SLAT DISAGREE" ILLUMINATED. COMPLIED WITH ELECTRONIC CENTRALIZED AIRCRAFT MONITOR ACTION NO HELP. ABANDONED APPROACH, TRIED ELECTRONIC CENTRALIZED AIRCRAFT MONITOR ACTION AGAISDR Q2SA20201021439Actuator · inoperativeAIRCRAFT GROUNDED. LEADING EDGE FLAP 1 EXTENDED INDICATION WHILE CRUISING AT FL 390. LEADING EDGE TRANSIT LIGHT ALSO ILLUMINATED. REMOVED AND REPLACED LEADING EDGE NR 1 FLAP ACTUATOR, IAW AMM 27-81-31-400-801. REMOVED LEADING EDGE LOCK OUT TOOL. OPERATIONSDR DALA2020091763104Rod End · brokenSHIP 9550, THE AIRCRAFT ROLLED AGGRESSIVELY TO THE RIGHT UPON SLAT DEPLOYMENT DURING APPROACH FOR LANDING. THE ROLL REACHED 10-20 DEGREES OF BANK AND THEN WAS CORRECT BACK TO WINGS LEVEL BY THE AUTOPILOT. NO OTHER FAULT MESSAGES OR INDICATIONS WERE OBSERVED.
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