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 ABXA060078Rod End · brokenUPON SLAT EXTENSION, AIRCRAFT ROLLED TO THE RIGHT AND SLAT DISAGREEMENT LIGHT ILLUMINATED AND THE SLAT EXTEND LIGHT DID NOT ILLUMINATE AFTER RECYCLING SLATS, NORMAL INDICATIONS WERE OBTAINED. FOUND BROKEN ROD END ON LEFT WING INBOARD SLAT ACTUATOR. REMOVED ASDR 06FDEA0309Actuator · weakNR 2 LE FLAP WOULD NOT RETRACT WITH FLAPS SELECTED UP. INSPECTED IND SWITCH AND LINKAGE NO DEFECTS NOTED. OPS CHECK SEVERAL TIMES AND ALL IND WERE NORMAL.CREW NOTED THAT SYSTEM WORKED CORRECTLY INITIALLY BUT THAN GOT YELLOW FLICKER. ALSO FLIGHT CREW INDSDR ABXA060077Actuator · brokenDURING MAINTENANCE INSPECTION AT RDU, ON RIGHT WING, FOUND SLAT ACTUATOR ASSEMBLY BROKEN. REMOVED AND REPLACED SLAT ACTUATOR CYLINDER ASSEMBLY IAW DC9 MM. OPS CHECKED GOOD. WORK ACCOMPLISHED ON WO 600240033.SDR EMB06001Actuator · unknownFLIGHT 1603 - PHL TO ORD, -SLAT LO RATE- EICAS MESSAGE INFLIGHT, SLAT ACE 1 AIRCRAFT POWER C/B TRIPPED. FUMES IN THE COCKPIT 80-100NM WEST OF PIT. THE CAPTAIN DECIDED TO DIVERT TO PIT. REMOVED AND REPLACED SLAT FLAP ACE. OPERATIONAL CHECK OF SLAT/FLAP ELECSDR GAIA06010Actuator · leakingDURING DESCENT/APPROACH, LOSS OF (A) SYSTEM HYDRAULIC FLUID. LANDING WAS MADE WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 KRUEGER FLAP ACTUATING CYLINDER IAW MM. RESERVICED HYDRAULIC SYSTEM TO FULL, RESAFETIED GUARDED HYDRAULICC SWITCHES, CHECKED CASE DRAINSDR 0600149881Rod End · failedWHEN THE LEADING EDGE SLATS WERE SELECTED FOR EXTENSION DURING APPROACH, THE AIRCRAFT ROLLED TO THE RIGHT. CREW NOTED THAT THE BLUE -SLAT EXTEND- LIGHT DID NOT ILLUMINATE AND THE AMBER -SLAT DISAGREEMENT- LIGHT WAS ILLUMINATED. AFTER APPROXIMATELY 90 SECONDSSDR DHL2006752508Actuator · crackedNR 2 SLAT ACTUATOR I/B SUPPORT MOUNT CRACKED. REMOVED CRACKED NR 2 SLAT ACTUATOR I/B SUPPORT MOUNT IAW B727 SRM 51-30-2. FABBED DOUBLER PLATE MIL 5-5059 301 1/2 HD .100 7.4" BY 3" PO 9001425 IAW S/B 727-57-0130 REV 3 DATED 4-24-03. FABBED SUPPORT MOUNT BAC SDR 200601041Actuator · trippedON TAKEOFF RECEIVED A FLAP FAIL EICAS MESSAGE. AFTER PILOT RAN QRH, PILOT DETERMINED THE FLAPS WERE STUCK IN THE FLAPS 1 POSITION. DECLARED AN EMERGENCY AND RETURNED TO FIELD. LANDED WITHOUT INCIDENT. FOUND FLAP ACTUATOR TORQUE LIMITER TRIPPED, REMOVED AND RSDR XN0A1292Position Switch · malfunctionedNR 3 LED FLAP NOT ON WITH FLAP HANDLE AT 15 DEGREES, AMBER L/E FLAP LIGHT ON. REMOVED AND REPLACED NR 3 KRUEGER FLAP POSITION SWITCH IAW MM 27-82-1. OPS CHECK GOOD IAW MM 27-82-0.SDR F3LA200500049Actuator · trippedUPON APPROACH, FLIGHT CREW REPORTED ECAM F/CTL SLATS FAULT. PERFORMED TSM TASK 27-81-00-810-810. FOUND TORQUE LIMITERS POPPED ON SLAT ROTARY ACTUATORS 6079 CM AND 6029 CM. REPLACED SLAT ROTARY ACTUATORS 6079 CM AND 6029 CM PER AMM 27-84-49-000-001 AND 27-84SDR AALA20050823Jackscrew · inoperativeJFK - SLATS DID NOT EXTEND UPON LANDING. REPLACED LEFT HAND 3 AND 6 AND RIGHT HAND 6 SLAT JACKSCREWS. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AU510001920Line · chafed(AUS) LT WING NR 2 LEADING EDGE SLAT ACTUATOR HYDRAULIC PIPE CHAFED AND LEAKING DUE TO INSUFFICIENT CLEARANCE BETWEEN THE PIPE AND THE ACTUATOR. LOSS OF HYDRAULIC FLUID. (CASA NR 510001920)SDR AU510001553Actuator · faultyLEADING EDGE SLAT DISAGEE MESSAGE. INVESTIGATION FOUND THAT THE INBOARD LEADING EDGE SLAT BYPASS VALVE ROTARY ACTUATOR WAS INTERMITTENT IN OPERATION.SDR FX7A200500011Actuator · inoperativeFLIGHT CREW REPORTED THAT DURING FLAP RETRACTION, THE NR 4 SLAT DID NOT RETRACT FROM 5 TO 2 FLAP SETTINGS, FUEL DUMPING WAS ACCOMPLISHED. LOG PAGE # 36436. REMOVED AND REPLACED THE NR 4 SLAT ACTUATOR ASSEMBLY AND THE SLAT SWITCH, IAW 727 MM REF 27-81-22 AND SDR ANCF200400061Actuator · failedBOTH FLAP POINTERS ARE ON HALF POSITION WITH THE FLAP LEVER UP. L/E SLAT DISAGREE LIGHT ILLUMINATED. L/E SLAT DISAGREE DISPLAY ON EICAS. VOICE RECORDER CB WAS PULL OUT AS SB REQUEST. IAW AMM 27-58-01 PAGE 501 ACCOMPLISHED RIGGING ON TRANSMITTER POSITION SLASDR DHL2005749017Rod · crackedNR 3 SLAT WS 515 AT ACT ROD END ATTACH HAS IB FRAMES CRACKED IN AFT RADIUS. REMOVED AND REPLACED DAMAGED IB RIB PN 65-17294-14 PO NR 540053 ON NR 3 SLAT IAW 727 SRM 51-30-2.SDR TSAA0527047Actuator · failedCOOPESA TO BROWNSVILLE TX FERRY FLIGHT 808. NR 5 SLAT DID NOT RETRACT. LEFT WING TO BODY OVERHEAT INDICATION. THE CREW RETURNED TO COOPESA WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 5 SLAT ACTUATOR AND PNEUMATIC DUCT AND CLAMP. OPS AND LEAK CHESDR XN0A1268Actuator · leakingLOSS OF HYDRAULIC SYSTEM "A" QUANTITY TO ZERO. REMOVED AND REPLACED LT NR 3 STAT ACTUATOR LEAK AND OPS CHECK GOOD IAW MM 27-81-32.SDR 05FDEA02728Actuator · malfunctionedLOST SYS A QTY DESCENDING OUT OF 12K FT. RAN APPROPRIATE CHECKLISTS INCLUDING MAN FLAP AND GEAR EXT. NR 7 SPOILER FAILED TO EXT DURING FLAP EXT. REMOVED AND REPLACED NR 7 SLAT ACT IAW M/M 27-81-032-4. REMOVED AND REPLACED CASE DRAIN FILTERS IAW M/M29-11-04SDR 2005UALA00909Actuator · failedLEADING EDGE SLAT DISAGREE MESSAGE. LEADING EDGE SLAT DISAGREE MSG PER CREW. FOUND NR 6 SLAT ACTUATORS NR 11 AND 12 OVERLOAD INDICATORS POPPED. REPLACED BOTH NR 11 AND 12 SLAT ACTUATORS.SDR 2005UALA00890Actuator · failedDIVERTED TO EWR WITH A SLAT DISAGREE PROBLEM. FOUND NR 6 SLAT ACTUATORS NR 11 AND 12 OVERLOAD INDICATORS POPPED. REPLACED BOTH NR 11 AND 12 SLAT ACTUATORS.SDR BMAC050011Actuator · leakingAFTER TAKEOFF, NR 1 SLAT WOULD NOT RETRACT. SYSTEM "A" HYDRAULIC QUANTITY DECREASED TO 0.3 GALLONS. MAINTENANCE REMOVED AND REPLACED NR 1 L/E SLAT ACTUATOR, LEAK AND OPS CHECK GOOD.SDR DHL2005748510Actuator · crackedNR 1 SLAT ACT TO SLAT ATTACH POINT CRACKED AT I/B RIB. OPENED ACCESS PANELS TO FACILITATE MAINT IAW B727 SRM 51-30-2. REMOVED DAMAGED RIB IAW B727 SRM 51-30-2. LOCATED & DRILLED NEW RIB P/N 65-17327-3 PO NR 531452 IAW B727 SRM 51-30-5 TREATED & PRIMED PARTSDR C1HA200592002Actuator · failedON DEPARTURE THE NR 6 L/E FAILED TO RETRACT, COMPLIED WITH COM PROCEDURE 2.27.12 SLAT WAS STILL EXTENDED. CONFERRED WITH DISPATCH/MDC, DECLARED AN EMERGENCY. COMPLIED WITH COM PROCEDURE 2.28.4 AND DUMPED APPROXIMATELY 23K LBS FUEL BEFORE RETURN TO STL. REMOSDR 2005FA0001040Piston · brokenPISTON BROKE AT THE KEY GROVE, FATIGUE. (196962/FXS) (K)SDR ASMF200506015Actuator · failedCAPTAIN REPORTED THAT DURING FLIGHT LIGHT AUTO SLAT FAIL CAME ON. DURING CHECK, APPLICABLE CIRCUIT BREAKERS WERE RESET AND FLAPS/SLATS WERE OPERATIONALLY TESTED TURNING ON THE OVERHEAD LIGHT IN THE SLATS PANEL LIGHTS. BITE TO BOTH STALL COMPUTERS WERE PERFORSDR 05FDEA01593Actuator · leakingLOSS SYSTEM-A HYDRALICS IN FLIGHT. COMPLETED QRH/RED TAB PROCEDURES. SYSTEM-A FLUID SHUTOFF SWITCHED CLOSED AT 1032, LANDED AT 1048. *S/D* REMOVED AND REPLACED A-HYD SYS PRESS FILTERS PER M/M 29-11-062-3, NO CONTAMINATION FOUND. REMOVED AND REPLACED A-HYD SDR CA050602008Actuator · inoperative(CAN) ON CLIMB OUT, CREW NOTICED THAT THE NR 1 KRUGER FLAP WOULD NOT RETRACT. THE CREW LEFT THE FLAPS IN THE DOWN POSITION AND RETURNED TO BASE. MAINTENANCE REPLACED THE NR 1 KRUGER FLAP ACTUATOR AND THE A/C WAS RETURNED TO SERVICE.SDR P5CA0501363Actuator · failedNR 22 LEADING EDGE PANEL BROKEN. REPLACED NR 22 LEADING EDGE PANEL, 2 ROTARY ACTUATORS AND TORQUE TUBE. RIGGED AND OPS CHECK IAW MM 27-81-00.SDR GTIA050160Actuator · malfunctionedDURING TAXI OUT, SELECTING FLAPS TO 11 FT THE AUTO-SLAT FAIL LIGHT ILLUMINATED AND THE DISAGREEMENT LIGHT REMAINED ON, RETURNED TO THE GATE AD AIRCRAFT TAIL SWAP WITH N811NK. ADJUSTED S1-467 NO HELP, REMOVED AND REPLACED S1-467 WITH SERVICEABLE UNIT FROM STOCSDR COMA0570055Actuator · malfunctionedFLIGHT 5472, SLATS FAIL CAUTION. REPLACED LT INBOARD SLAT ACTUATOR.SDR 2005FA0000910Housing · brokenAIRCRAFT RETURNED FROM A FLIGHT WITH HYDRAULIC FLUID LEAKING FROM ACTUATOR. FLIGHT ENGINEER WALK AROUND, FOUND BODY END BROKE OFF AT RETAINER END. UNKNOWN, THIS IS A NEW AND IMPROVED POST SB BODY. (K) (REF: 194950/LEB)SDR COMA0570042Actuator · malfunctionedFLT 5165 SLATS FAIL CAUTION. REPLACED THE LEFT NR 2 SLAT ACTUATOR.SDR CA050405010Actuator · failed(CAN) DURING CLIMB PHASE, SLATS RETRACTED, NR 1 SLAT, HOWEVER DID NOT SHOW RETRACTED. FLIGHT CREW CONFIRMED THAT AIRCRAFT DID NOT HAVE ANY UNCOMMANDED ROLL IN THE FLIGHT CHARACTERISTICS. THIS INDICATED AN INDICATION FAULT ONLY. CREW RETURNED TO POINT OF DEPSDR 05FDEA00331Actuator · malfunctionedFLAP DISAGREE ALERT AFTER TAKEOFF AT WSSS. CONFIG PAGE SHOWED SLATS EXT L22/25, R24/23. DID QRH PROCEDURE. DUMPED FUEL TO RETURN TO WSSS. REMOVED AND REPLACED FLAP DUPLEX ACTUATOR AND ALL 4 INBD FLAP CONTROL VALVE RESTRICTORS.SDR GAIA05005OPActuator · leakingFLT 544 - FWA-DTW - DURING TAKEOFF THE 'A' SYSTEM HYDRAULIC FLUID QUANTITY DECREASED AND BOTH A-PUMP LOW PRESSURE LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO FWA AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED NR 2 LEADING EDGE FLAP ACTUATOR AND NRSDR AWXA200500230Actuator · trippedON APPROACH, RECEIVED ECAM MESSAGE FOR F/CTL SLATS FAULT; DECLARED PRECAUTIONARY EMERGENCY LANDING AND LANDED WITHOUT FURTHER EVENT. MX TROUBLESHOT SLAT SYS PER TSM 27-81-00-810-810, SLAT SYSTEM OPERATED NORMALLY. INSP OF SLAT ACT FOUND RT OTBD NR 4 SLAT ACTSDR FX7A200500001Actuator · leakingDURING TAXI HYDRAULIC QUANTITY DROPS TO ZERO.SDR SWAA050020Actuator · failedAIR TURNBACK, NR 3 SPOILER STUCK IN UP POSITION, WITH HYDRAULIC PRESSURE. REMOVED AND REPLACED NR 3 SPOILER ACTUATOR PER MM.SDR C7WA200400071Actuator · leakingAIR RETURN; AFTER TAKEOFF AND FLAP RETRACTION SYSTEM (A) HYDRAULIC QUANTITY WAS DROPPING RAPIDLY. ACCOMPLISHED ABNORMAL PROCEDURE FOR LOSS OF SYSTEM (A) QUANTITY. FOUND NR 1 SLAT ACTUATOR LEAKING. REMOVED AND REPLACED SLAT ACTUATOR IAW MM. (K)SDR XNOA1215Actuator · malfunctionedON CLIMB-OUT, LEADING EDGE DEVICES WOULD NOT INDICATE UP AND LOCKED. X-FERRED TO DMI 4798, MEL 27-6 CAT "C". PLACARDS INSTALLED AS REQUIRED. R/R NR 2 SLAT ACTUATOR, OPS CK GOOD ON GROUND IAW B727 MM 27-81-32. THIS ACTION CLEARS DMI 4798. PLACARDS REMOVED. (SSDR DHL2004747009Actuator · inoperative"A" SYSTEM FAILED DURING LDG GEAR EXTENSION. PERFORMED ABNORMAL PROCEDURE AND LANDED. A/C TOWED IN. REMOVED AND REPLACED NR 1 SLAT ACTUATOR IAW M/M 27-81-31, NO LEAKS NOTED.SDR DL76S041009Rod · bentRIGHT WING INBD L/E SLAT OUTBD ACTUATOR ROD BENT DAMAGING L/E PANEL AND CAUSING A SLAT ASSYM. REPLACED ROD WITH NEW. ADJUSTMENT MADE ON OPN 7007. DRIVE ROD INSTALLATION OK /INSP.SDR 04FDEA03002Actuator · malfunctionedNR 1 SLAT LED FAILED TO RETRACT AND INDICATING AMBER ON FLAP RETRACTION TO FLAPS 2 IN FLIGHT. REMOVED AND REPLACED NR 1 SLAT ACTUATOR AS PER M/M 27-81-03-4, OP CKS NORM.SDR P5CA0401241Pdu · malfunctionedA/C RETURN TO BLOCK DUE TO EICAS MESSAGE FLAP PRIMARY, FLAP DRIVE FOLLOWED BY STATUS MESSAGE L/E MULTI DRIVE, FLAP SYSTEM MONITOR. REPLACED NR 2 RIGHT HAND LED PDU & TESTED ELECTRICALLY NORMAL.SDR COMA0470065Actuator · malfunctionedFLIGHT 5023 SLATS FAIL CAUTION MESSAGE. REPLACED THE NR 3 SLAT ACTUATOR.SDR COMA0470067Actuator · faultyFLIGHT 2225 DURING SRQ APPROACH RECEIVED A SLATS FAIL CAUTION, CREW DECLARED AN EMERGENCY AND LANDED SAFELY. REPLACED THE RIGHT OUTBOARD SLAT ACTUATOR.SDR CA040913007Bearing · separated(CAN) DURING DEPARTURE, THE CREW OBSERVED A CONTINUOUS SLAT PROBLEM INDICATION. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE FOUND THE NR 5 SLAT ROD END BEARING SEPARATED FROM THE PISTON, AND THE SLAT DAMAGED BY THE PISTON. THE ACTUATOR AND SLAT ASDR 0401399907Cylinder · damagedUPON CONFIGURING THE AIRCRAFT FOR LANDING, THE RIGHT SLAT DID NOT DEPLOY. THE AIRCRAFT DID ROLL UNCOMMANDED TO THE RIGHT. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AT DTW. MAINTENANCE AT DTW FOUND THAT ALL OF THE BOLTS FOSDR 2004FA0000678Fuse Pin · shearedRT WING OB SLAT CONTROL MECHANISM HAS ANTI-DROOP FUSE PIN SHEARED. REFERENCE NON-ROUTINE 39501.
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