JASC 2782

Service difficulty reports · 1,225

Reports filed under 2782 · Leading Edge Slat Actuator, newest first.

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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"

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SDR DHL2004762001Seal · failedLOSS OF ALL A-SYSTEM HYDRAULIC FLUID DURING FLAP EXTENSION 0 DEGREES TO 2 DEGREES. ACCOPLISHED CHECK LIST LANDED NORMALLY. RII OB SEAL BLOWN NR 2 LE FLAP ACTUATOR. REMOVED AND REPLACED NR 2 LE FLAP ACTUATOR IAW MM CH 27-81-22. OPS CHECK AND LEAK CHECK GOODJul 29, 2004 · N762AT · Boeing 7272B7SDR SWAA042113Rod End · out of adjustDURING TAKEOFF UNTIL APPROX 10 TO 15 SECONDS AFTER GEAR RETRACTION ABNORMAL RIGHT ROLLING TENDENCY, REQUIRING APPROX 30 DEGREES YOKE DEFLECTION. DURING FLAP EXTENSION ON GROUND TOOK SEVERAL CYCLES OF FLAPS TO EXTINGUISH, SLAT NR 3 AND 4 AMBER LIGHTS ON OVERHEJul 25, 2004 · Boeing 7372H4SDR DHL2004755014Actuator · malfunctionedNR 6 SLAT FAILED TO RETRACT AFTER TAKEOFF. ABNORMAL PROCEDURES COMPLIED WITH, WOULD NOT RETRACT. UPON CHECK AT ARRIVAL FOUND NR 7 SLAT AMBER LIGHT WOULD NOT EXTINGUISH. REMOVED AND REPLACED NR 7 SLAT ACTUATOR IAW MM 27-81-32. CHECKED OPERATION OF NR 6 CLEANJul 3, 2004 · N755DH · Boeing 727225SDR AWXA200400709Actuator · bindingON DESCENT, EN ROUTE RECEIVED A SLAT FLAP DISAGREE LIGHT WITH SLATS LOCKED OUT BETWEEN POSITIONS ZERO AND ONE, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LEADING EDGE STRUCTURE ATTACHMENT SCREW LOOSE AND PROTRUDING FROM SKIN AT NR 2 SLAT AREA AFFECTJun 30, 2004 · N620AW · Airbus A320231SDR CA040625004Actuator · inoperative(CAN) NR 6 LEADING EDGE SLAT WAS SLOW TO RETRACT ON DEPARTURE. AFTER IT DID RETRACT IT RE-EXTENDED FOR ABOUT 5 MINUTES THEN RETRACTED AGAIN. CREW WAS ALERTED BY SLAT INDICATION OF THE REDEPLOYMENT AND VISUALLY CONFIRMED THE EXTENSION AND RETRACTION. NO OTHER AJun 24, 2004 · Boeing 737217SDR SWAA041770Actuator · faultyAIR TURNBACK, LT WING NR 3 L/E FLAP ANNUNCIATOR ILLUMINATED AMBER AFTER FLAP RETRACTION ON TAKEOFF. CYCLED FLAPS, NO HELP. NORMAL INDICATIONS ON DESCENT. REMOVED AND REPLACED NR 3 L/E KRUEGER FLAP ACTUATOR PER MM.Jun 24, 2004 · N640SW · Boeing 7373H4SDR GAIA04080OPActuator · inoperativeFLT 716 - FWA-PHX - ON DEPARTURE AFTER RETRACTING FLAPS NOTED NR 2 LED DID NOT RETRACT, PROCEEDED TO CHECK LIST. RETURNED TO FWA WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND NR 2 L/E SLAT ACTUATOR INOPERATIVE. REMOVED AND REPLACED ACTUATOR. OPS CHECK GJun 16, 2004 · N281KH · Boeing 7272J0SDR 2004UALA00553Actuator · failedRETURNED TO FIELD DUE TO NR 3 LEADING EDGE FLAP PROBLEM. REPLACEMENT OF THE LEADING EDGE FLAP ACTUATOR CORRECTED THE DISCREPANCY. THE LEADING EDGE FLAP ACTUATOR WAS FOUND WITH A SEVERELY DETERIORATED PISTON HEAD SEAL. THE CONDITION OF THIS SEAL SUPPORTS THE REJun 7, 2004 · N386UA · Boeing 737322SDR TSAA0427044Actuator · failedFLIGHT 482, HNL-SNA: L/E FLAP TRANSIT LIGHT REMAINED ON AFTER TAKEOFF, QRH COMPLETED AND RETURN TO HNL. WEIGHT ON LANDING APPROXIMATELY 150,000 LBS, LOW SINK RATE AT TOUCHDOWN. FOUND THE NR 2 AND NR 5 SLAT ACTUATORS INTERNALLY BYPASSING, REPLACED NR 2 AND NJun 2, 2004 · N738AL · Boeing 73773ASDR SWAA041531Actuator · failedAIR TURNBACK, NR 2 L/E SLAT WOULD NOT RETRACT, VISUALLY CONFIRMED. REMOVED AND REPLACED NR 2 L/E SLAT ACTUATOR PER MM.Jun 1, 2004 · Boeing 7372H4SDR SWAA041528Actuator · failedAIR TURNBACK, ON TAKEOFF WITH FLAP RETRACTION L/E FLAPS TRANSIT LIGHT REMAINED ILLUMINATED WITH T/E FLAPS UP. CONFIRMED PARTIALLY EXTENDED. REMOVED AND REPLACED ALL EIGHT L/E SLAT ACTUATORS PER MM.May 30, 2004 · N785SW · Boeing 7377H4SDR CA040531001Actuator · damagedDURING A SCHEDULED ROUTINE MAINTENANCE CHECK IT WAS OBSERVED THAT THE LEFT HAND OUTBOARD SLAT ACTUATOR WAS DAMAGED. THE CORNER OF THE SLAT WAS GROUNDED OFF EXPOSING A SECONDARY STRUCTURAL EXTRUSION. THE AIRCRAFT WAS GROUNDED A SUSPECTED A WING TIP STRIKE ON LMay 28, 2004 · Boeing 727225SDR DL738040556Actuator · failedAFTER TAKEOFF UPON FLAP RETRACTION FROM FLAPS 1 TO UP L/E FLAPS TRANSIT LIGHT REMAINED ILLUMINATED WITH T/E FLAPS RETRACTED. PERFORMED LEADING EDGE FLAP TRANSIT CHECKLIST BUT NO CHANGE OCCURRED. T/E FLAPS OPERATED NORMALLY L/E DEVICES LOCKED OUT. REPLACED NMay 15, 2004 · N384DA · Boeing 737832SDR GAIA04074OPActuator · leakingNOTED ELEVATOR LOW PRESSURE LIGHT CAME ON, HYDRAULIC SYSTEM (A) QUANTITY INDICATED ZERO, SYSTEM (A) ENGINE PUMP LOW PRESSURE LIGHTS BLINKING. FLIGHT DIVERTED MAINTENANCE BASE WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND BROKEN INSERT IB TRUNNION FITTING May 14, 2004 · N69739 · Boeing 727224SDR TSAA0427038Actuator · failedL/E FLAP TRANSIT LIGHT ON AFTER FLAP RETRACTION. SOME LEADING EDGE DEVICES REMAIN EXTENDED. OVERWEIGHT LANDING 151,300 LBS AT 50 FEET PER MINUTE. PHASE 1A REF 05-51-35-2, LANDING SINK RATE WAS LOW TO MODERATE, INSPECTION COMPLETE, NO DEFECTS NOTED. REPLACED EXApr 24, 2004 · N738AL · Boeing 73773ASDR ANCF200400024Actuator · malfunctionedTAKE OFF WAS DISCONTINUED TWO TIMES BY SLAT DISAGREE LIGHT CAME ON AND FLAP7SLAT AURAL TAKE OFF WARNIN SOUNDED. IT WAS AT APROX 60 KNOTS. IT WAS REPLACED RT CYLINDER SLAT ACTUATOR ACC AMM27-80-05/202. TEST BY LEAKS WAS SATISFACTORY P/N ON OFF 5937021-5503. Apr 8, 2004 · N583AN · Doug MD83SDR C1HA200485002Actuator · malfunctionedNR 4 KRUGER FLAP WOULD NOT RETRACT AFTER T/O. R&R NR 4 KRUGER FLAP ACTUATOR PER M.M. 27-81-22. ACTUATOR OPS CHECKS GOOD.Apr 2, 2004 · N685CA · Boeing 7272S7SDR CA040325002Actuator · leaking(CAN) ON APPROACH INTO CYVR SELECTED FLAPS 2, AMBER IN-TRANSIT LIGHT STAYED ON. NR 7 SLAT DID NOT EXTEND. HYDRAULIC SYSTEM (A) LOW PRESSURE LIGHTS ILLUMINATED AND HYDRAULIC (A) SYSTEM QUANTITY INDICATED ZERO QUANTITY. AIRCRAFT WAS VECTORED AND CREW PERFORMED HMar 25, 2004 · Boeing 72722CSDR P5CA0401063Drive Unit · malfunctionedNR 1 L/E FLAP REQUIRES ALTERNATE PROCEDURE TO EXTINGUISH IN TRANSIT LIGHT. R&R NR 1 L/E DRIVE UNIT PER MM 27-81-03.Mar 23, 2004 · N921FT · Boeing 747283BSDR 04FDEA00605Actuator · failedNR 3 KRUEGER FAILED TO EXTEND ON APPROACH TO KRST, C/W RED TABS DIVERT TO KMSP. REMOVED AND REPLACED THE NR 3 KRUEGER FLAP ACTUATOR AND THE L/E FLAP-SLAT POSITION CONTROL MODULE IAW MM 27-81-22 AND MM 27-82-031-4.Mar 6, 2004 · N481FE · Boeing 727200SDR 0400349860Actuator · malfunctionedDURING APPROACH FOR LANDING, THE RIGHT LEADING EDGE SLAT DID NOT COME FULLY OUT ON EXTENSION. THE AIRCRAFT DID EXPERIENCE AN UNCOMMANDED ROLL TO THE RIGHT. THE SLAT DISAGREEMENT ANNUNCIATOR LIGHT DID ILLUMINATE AND THE BLUE SLAT EXTEND INDICATOR DID NOT. ASFeb 28, 2004 · N769NC · Doug DC951SDR 0400359860Actuator · malfunctionedON APPROACH WHEN SLATS WERE EXTENDED, THE AIRCRAFT ROLLED TO THE RIGHT. THE BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE BUT NO MENTION OF SLAT DISAGREEMENT ANNUNCIATOR STATUS. AS THE AIRCRAFT SLOWED TO 190 KTS, THE SLAT EXTEND LIGHT ILLUMINATED. IT WAS NOTED Feb 28, 2004 · N769NC · Doug DC951SDR Q752004F00000Actuator · leakingDURING CLIMB OUT, SLATS RETRACTED NORMALLY. THEN A MASSIVE HYDRAULIC LEAK APPEARED ON OB LEFT WING. NR 1 HYDRAULIC SYSTEM BEGAN TO EMPTY. LANDING GEAR WAS LOWERED AND LANDING WAS MADE NORMALLY. AFTER INVESTIGATING PROBLEMS WAS LT, OB SLAT ACTUATOR. THE REFeb 23, 2004 · N569DW · Amd FALCON10SDR 2004UALA00139Actuator · failedON FLAP RETRACTION THE L/E FLAP DISAGREE EICAS MESSAGE ILLUMINATED. EXCESSIVE TORQUE FORCES IN THE LE SLAT DRIVE SYSTEM INITIATED A LE SLAT DISAGREE FAULT WHICH WAS DETECTED BY THE FLAP/SLAT ELECTRONIC UNIT (FSEU) LE SLAT MOVEMENT IS AUTOMATICALLY INHIBITED Feb 16, 2004 · N576UA · Boeing 757222SDR 04FDEA00256Actuator · malfunctionedDURING FLAP RETRACTION FLAPS FROM 5 TO 2 DEGREE AMBER LIGHT. REMAINED ON AND NR 1 LED SHOWED INTRANSIT. COMPLIED WITH QRH AND RETURNED TO MEM. IN WORK, AFTER BLOCKING BACK INTO GATE, NR 1 LEADING EDGE FLAP WOULD RETRACT BUT WOULD CREEP BACK OPEN, WITH HYD SJan 31, 2004 · N223FE · Boeing 727200SDR 2004F00301Actuator · inoperativeDURING THE AFTER T/O CHECKLIST, NR 2 LEADING EDGE SLAT EXTENDED INDICATION REMAINED ON BOTH FORWARD AND AFT ANNUNCIATOR LIGHTS DUMPED FUEL AND RETURNED TO KCVG WITHOUT INCIDENT. REPLACED NR 2 LEADING EDGE SLAT ACTUATOR PER MM 27-81-32. AIRCRAFT RETURNED TO SJan 29, 2004 · N79750 · Boeing 727224SDR 2004UALA00001Actuator · jammedAFTER TAKEOFF WITH FLAP HANDLE SELECTED TO UP HAD A LE EDGE SLAT DISAGREE MESSAGE AND LIGHT. FOUND JAMMED NR 3 LEADING EDGE (LE) SLAT ROTARY ACTUATOR. JAMMING WAS ATTRIBUTED TO EXCESSIVE TORQUE LOADING IN THE LE SLAT DRIVE TORQUE TUBE SYSTEM. NR 3 ROTARY ACTJan 3, 2004 · N574UA · Boeing 757222SDR F3LA200300191Actuator · inoperativeDURING C-7 CHECK, INSPECTION REPORTED NR 3 SLAT ACTUATOR FAILED LOCK PIN TEST. REPLACED NR 3 SLAT ACTUATOR IAW MM 27-81-41 AND ACCOMPLISHED LE SLAT ACTUATOR LOCK PIN TEST AND LE SLAT ALTERNATE SYSTEM TESTS IAW TASK CARD 5-2710 AND MM 27-81-00.Dec 31, 2003 · N306FL · Boeing 73736NSDR 2003UALA00989Actuator · out of limitsSLATS FAILED TO DEPLOY, S-CTRL FAULT ILLUMINATED. THE TORQUE LIMITER OF THE LT NR 2 SLAT OUTBOARD ACTUATOR WAS FOUND TRIPPED. THE SLAT STOP TO FWD ROLLER DIMENSION WAS ALSO FOUND OUT OF LIMIT. REPLACEMENT OF THE FAULTY SLAT ACTUATOR AND SUBSEQUENT ADJUSTMENT Dec 29, 2003 · N421UA · Airbus A320232SDR 2004F00115Actuator · faultyAFTER TAKEOFF FROM ELP, DURING SLAT RETRACTION, NR 7 LEADING EDGE SLAT REMAINED EXTENDED WITH SLAT HANDLE AT 0 DEGREES. AMBER LEADING EDGE SLAT LIGHT WAS ILLUMINATED AND NR 7 INDICATED EXTENDED ON FLIGHT ENGINEERS LEADING EDGE PANEL. AIRCRAFT RETURNED TO ELPDec 24, 2003 · N302FV · Boeing 727230SDR AWXA200301514Actuator · malfunctionedON APPROACH INTO DTW EN ROUTE FROM LAS THE LEADING EDGE SLAT SYSTEM LOCKED OUT AT POSITION 1 WHEN SELECTED, TRAILING EDGE FLAPS OPERATED NORMALLY. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND LT WING SLAT WING TIP BRAKE INDICATOR PODec 6, 2003 · N633AW · Airbus A320231SDR AWX2004F00000Spring · wornEN ROUTE FROM PHX TO ABQ FLIGHT CREW REPORTED RT WING NR 5 SLAT HANGING DOWN APPROXIMATELY 5 INCHES, AIRCRAFT RETURNED TO PHX. MAINTENANCE REMOVED AND REPLACED NR 5 LEADING EDGE SLAT ACTUATOR PER AWA TASK CARD R3M27020, OPERATIONAL AND LEAK CHECK WAS GOOD. FUDec 2, 2003 · N189AW · Boeing 737277SDR AALA20031368Jackscrew · inoperativeJFK T610/01 EN ROUTE SJU-JFK DUAL SLAT FAULT. VISUALLY CHECKED SLATS NOT EXTENDED. LANDED JFK WITHOUT INCIDENT. REPLACED NR 3 RIGHT LEADING EDGE SLAT JACKSCREW IAW MM 27-84-22-4. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSEDDec 1, 2003 · N19059 · Airbus A300B4605RSDR 03FDEA01980Connector · contaminatedAFTER INITIAL TAKEOFF ON FLAP RETRACTION GOING FROM FLAPS 2 TO FLAPS 0. NR 4 LED SLAT WOULD NOT RETRACT. RETURNED TO PHL, HAD TO GO TO FLAPS 5 TO GET GREEN LIGHT AND NORMAL POSITION. FOUND MOISTURE IN NR 4 LEADING EDGE SLAT ACTUATOR CONNECTOR. CLEANED SAMENov 25, 2003 · N284FE · Boeing 727200SDR DHL200342539Mount Bracket · crackedDURING C-CHECK, N/R60109 NR 6 KRUEGER FLAP INBD ACT MOUNT CRACKED 2 EA PLACES. REMOVED SUPPORT BRACKETS IAW B727 SRM 51-30-02. FABRICATED AT 2 EA SUPPORT BRACKETS IAW B727 SRM 57-20-02. ALODINED AND PRIMED IAW B727 SRM 51-10-02. INSTALLED SUPPORTS IAW B727Nov 24, 2003 · N742DH · Boeing 727225SDR 03FDEA01959Actuator · failedON PUSHBACK MEM AFTER DISCONNECT WITH A PUMPS ON, L/E FLAPS REMAINED UNSAFE. CYCLED FLAPS 2-5 DEGREES WENT GREEN. CYCLED FLAPS BACK UP, UNSAFE WENT OUT. PASSING 10K UNSAFE L/E FLAPS RE-ILLUMINATED. CYCLED DOWN AND BACK LIGHT WENT OUT. PASSING 19K, UNSAFE Nov 19, 2003 · N216FE · Boeing 727200SDR 03FDEA01838Motor · failedALT FLAPS EXT SYSTEM DOES NOT EXTEND LED'S. FLAPS APPEAR TO WORK OK BUT DIDN'T GO BEYOND 2. TROUBLESHOT ALT FLAP SYS. REPLACED L/E MOTOR PUMP ASSY. REPLACED L/E FLAP AND SLAT SELECTOR VALVE. REPAIRED L/E STANDBY DRIVE SHUT OFF VALVE GROUND WIRES AT GD846.Oct 30, 2003 · N217FE · Boeing 727200SDR ASM2003F00004Actuator · failedAIRCRAFT RETURNED TO PLATFORM DURING TAXI, WHEN SLATS WERE EXTENDED AUTO SLAT FAIL LIGHT TURNED ON. SYSTEM WAS CHECKED WITH OTHER COMPUTERS, CONFIRMING THE FAIL IN BOTH AUTO SLAT ACTUATORS. ACTUATORS WERE REPLACED IAW MM 27-80-08 TESTS CORRECT. FURTHER, THEOct 28, 2003 · N945AS · Doug MD83SDR SWAA032099Actuator · leakingAIR TURNBACK, L/E DEVICES WOULD NOT FULLY RETRACT. FOUND INTERNAL LEAK AT L/E SLAT HYD ACTUATORS NR 1, NR 2, NR 3, NR 4, NR 6, AND NR 7. REMOVED AND REPLACED L/E SLAT HYD ACTUATORS PER MM.Sep 20, 2003 · N404WN · Boeing 7377H4SDR NACA20030096Switch · false indicationNR 2 SLAT INDICATES FORWARD AMBER LIGHT AND F.E. TRANSITE LIGHT WITH FLAPS UP. REPLACED NR 2 SLAT EXTEND SWITCH.Jul 22, 2003 · N930FT · Boeing 727100SDR NACA20030095Actuator · false indicationNR 2 SLAT LIGHT ON IN FLT WITH FLAPS IN UP POSITION. REPLACED SLAT ACTUATOR.Jul 21, 2003 · N930FT · Boeing 727100SDR RYN2004F00021Actuator · leakingAFTER TAKEOFF, DURING ASCENT TO FLIGHT LEVEL 24.0 NR 7 FLAP LED AND YELLOW LIGHTS STAYED ILLUMINATED DURING FLAP RETRACTION. IMPLEMENTED PROCEDURES IAW MM FOR TROUBLESHOOTING. MANUAL STATED TO PROCEED WITH FLIGHT IF LIGHT EXTINGUISHED. LIGHTS EXTINGUISHED.Jul 12, 2003 · N7639U · Boeing 727222SDR SWAA031432Actuator · failedAIR TURNBACK, DECLARED EMERGENCY, L/E DEVICES WOULD NOT RETRACT. REMOVED AND REPLACED NR 2 L/E FLAP ACTUATOR PER MM.Jun 29, 2003 · N756SA · Boeing 7377H4SDR CA030627018Actuator · failed(CAN) 'A' SYSTEM HYDRAULIC FAILURE T/O ABORTED AND A/C RETURNED TO BLOCKS. NR 6 SLAT ACTUATOR FOUND FAILED.REPLACED ACT AND A SYSTEM PUMP CASE DRAIN FILTERS INSPECTED/REPLACED. NO CONTAMINATION FOUND. AIRCRAFT RETURNED TO SERVICE.Jun 27, 2003 · Boeing 72722CSDR DHL2003726006Slat · malfunctionedDURING CLIMB, UPON FLAP RETRACTION NR 2 SLAT FAILED TO RETRACT. PERFORM ABNORMAL PROCEDURES. DID NOT FIX PROBLEM. AIRCRAFT TURNED BACK AND RETURNED TO BASE. INSPECTED NR 2 L/E SLAT ROLLERS TRACKS ACTUATOR ATTACH POINTS IAW B-727 MM. NO DEFECTS NOTED. INSP. LMay 28, 2003 · N726DH · Boeing 727228SDR MEX2003080Actuator · brokenDURING EXTERIOR INSPECTION, DETECTED A BREAK IN THE LEFT WING SLATS ACTUATORS ACCESS DOOR, THE FASTENER POINT OF THE UPPER SLAT ACTUATOR WAS BROKEN. BOTH CYLINDERS ACTUATORS WERE REPLACED IAW MM 27-80-5. (M)Mar 17, 2003 · N1003P · Doug DC932SDR 2003UALA00267Actuator · malfunctionedAIRCRAFT PREPARED FOR DIVERSION WHEN LEADING EDGE FLAP DID NOT DEPLOY. LEADING EDGE FLAP DEPLOYED ON FINAL APPROACH, AND AIRCRAFT LANDED AT PLANNED DESTINATION. THE NR 1 FLAP ACTUATOR WAS REPLACED. ACTUATOR WAS REMOVED AND SENT TO SHOP FOR REWORK.Mar 11, 2003 · N392UA · Boeing 737322SDR USAASB03022Actuator · malfunctionedPIT - FLT 865 - DURING APPROACH, CREW REPORTED THE NR 5 LEADING EDGE SLAT INTRANSIT LIGHT ILLUMINATED WHEN FLAPS/SLATS WERE SET TO 5 UNITS. CREW NOTED AIRCRAFT WANTED TO ROLL RT DURING FLAP/SLAT SET. NR 5 LEADING EDGE SLAT DID NOT RETRACT UNTIL APPROXIMATELY Feb 9, 2003 · N586US · Boeing 737301SDR 2003UALA00119Actuator · inoperativeAIRCRAFT RETURNED TO FIELD WHEN FLIGHT CREW WAS UNABLE TO RETRACT THE FLAPS. REPLACED NR 2 LE FLAP ACTUATOR.Jan 29, 2003 · N318UA · Boeing 737322SDR RYN2003F00000Actuator · defectiveDURING CLIMBOUT, NR 7 LEADING EDGE SLAT WOULD NOT RETRACT. EMERGENCY FLAP PROCEDURES FOLLOWED. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT.Jan 23, 2003 · N815EA · Boeing 727225
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