JASC 2780

Service difficulty reports · 2,159

Reports filed under 2780 · Leading Edge Slat 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 = '2780'
  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.

SDR CA110418005Slat System · malfunctioned(CAN) CREW ADVISED FLIGHT DISPATCH OF A SLAT FAIL INBOUND. ON APPROACH TO RUNWAY 22, CREW SELECTED FLAPS CONFIG 2. SLAT FAIL MSG, CREW ADVISED ATC AND DID A GO-AROUND. ATC VECTORED THE FLIGHT AFTER THE GO-AROUND, THE QRH WAS COMPLETED, CREW LANDED RUNWAY 22 Apr 17, 2011 · Emb ERJ170200SUSDR CA110418001Slat System · failed(CAN) DURING THE APPROACH TO LAND THE ACFT HAD A SLAT FAILURE. THE CREW EXECUTED A GO AROUND AND REQUESTED EMERGENCY VEHICLE TO STAND BY FOR THE NEXT APPROACH AND LANDING. SLAT FAIL EICAS MESSAGE ILLUMINATED WHEN SELECTING FLAP 1. SLAT POSITION INDICATED ASApr 15, 2011 · Emb ERJ190100IGWSDR FDEA201104151501Slat System · malfunctionedNR 1 SLAT WOULD NOT RETRACT DURING FLAP RETRACTION COMPLIED WITH QRH LED STILL FAILED TO RETRACT, RETURNED TO MEM, ACFT DID NOT HAVE A NOTICEABLE ROLL, BOTH FRONT "L/E FLAPS" & NR 1 SLAT ON AUX PANEL "POSITION TEST" WERE AMBER INDICATION NR 1 LED STILL NOTApr 15, 2011 · N485FE · Boeing 727227SDR IPXA11166072Slat System · malfunctionedON FINAL, SLATS DIDN'T EXTEND. AIRSPEED WAS ABOUT 220 FOR INITIAL EXTENSION. EMERGENCY DECLARED. IAW TSM 27-80-02 FOUND RT L/E SCREW JACKS 1-2-4 TRIPPED. RESET SCREW JACKS & SERVICED IAW MM 12-13-27-00. OK FOR SERVICE. CLEARED FAULTS IN SFCC BOX. OPS CKD, NOApr 14, 2011 · N129UP · Airbus A300F4622RSDR C77A382147Wire Harness · failedSLAT FAIL EICAS MESSAGE, WHEN FLAPS 0 WHEN SELECTED FROM FLAP 1 PERFORMED QRH PROCEDURE 7.18 RESULTED IN SHAKER ANTICIPATED, AOA LIMIT FAIL AND SPOILER FAULT, ADDITIONAL EICAS MESSAGES. SLAT VISUALLY CONFIRMED PARTIALLY EXTENDED. ACCOMPLISHED FIM 27-33-00-810Mar 31, 2011 · N621C · Emb ERJ170200LRSDR CA110328006Slat System · malfunctioned(CAN) ON APPROACH THE L/E SLATS FAILED IN THE UP POSITION. AN EMERGENCY WAS DECLARED CHECKED/OPS CHECK CARRIED OUT, NO FAULTS OCCURED/CONS SERV, REF TASK 27-54-00-710-002. GENERAL WALKAROUND CARRIED OUT.Mar 28, 2011 · Airbus A320211SDR YENA20110324227Ace · failedFLT 1243 BOS-CLT, FLIGHT CREW DECLARED EMERGENCY DUE TO FLAP FAIL, FLIGHT CONTROL NO DISPATCH, WINDSHEAR FAULT, GRN PROX FAIL. AT FAIL, SHAKER ANTICIPATED, AP FAIL, SPOILER FAULT AUTO CONFIG TRIM FAIL. INFLIGHT AUTO PILOT TURNED OFF AND WE DID A O FLAP WITH Mar 24, 2011 · N318JB · Emb ERJ190100IGWSDR CA110323004Rvdt · misrigged(CAN) ON APPROACH THE CREW HAD A LE ASYMMETRY FAULT. PERFORMED A GO AROUND. QRH PROCEDURE WAS CARRIED OUT & THE FLIGHT THEN LANDED, FLAP & SLAT UNIT MSG M48. OTBD SLAT PDU RVDT MIS-RIG, SLAT & FLAPS ALTERNATE CYCLED. FLAP & SLATS OPERATED SEVERAL CYCLES ONMar 22, 2011 · Boeing 767375SDR FDEA201103191080Actuator · malfunctionedDURING CLIMBOUT NR 4 LT L/E SLAT DID NOT RETRACT. RAN QRH. RETURNED TO DEPARTURE. JUMPER INSTALLED ON NR 4 SLAT ACTUATOR. DO TO IND OF EXTEND POSITION. MM 27-82-000-1-0, INSTALLED NR 4 L/E SLAT EXTEND SWITCH JUMPER. SYS GROUND CHECKS NORMAL. JUMPER INMar 19, 2011 · N468FE · Boeing 727225SDR CA110314003Control Unit · failed(CAN) ON APPROACH TO RUNWAY, WHEN FLAP 1 WAS SELECTED, THE CREW EXPERIENCED LOCKED SLATS ASSOCIATED WITH OTHER FLIGHT CONTROL FAILURES. ON FLAP EXTENSION FLT CTR SLAT FAULT LOST AP`S, ATHR. FD`S WENT TO ALT LAW ON GEAR SELECTION DIRECT LAW. A MISSED APPROACH Mar 12, 2011 · Airbus A319114SDR CA110310005Sensor · failed(CAN) FLAP/SLAT FAIL ON APPROACH, UNABLE TO SELECT FLAPS FULL. PAN PAN DECLARED WITH ATC, RETRACTED FLAPS AND INITIATED GO-AROUND FOUND RT FAILURE OF SKEW SENSOR S2/3. RT SKEW SENSOR REPLACED. AMM 27-83-01/401, GROUND CHECKED SERVICEABLE.Mar 9, 2011 · Emb ERJ190100IGWSDR CA110307001Slat System · malfunctioned(CAN) AFTER TAKEOFF SLATS FAILED BETWEEN 0-1. FLIGHT RETURNED TO POINT OF DEPARTURE AND DECLARED AN EMERGENCY WITH ATC. FLIGHT LANDED WITH NO ISSUE BUT MET ON RWY BY EMERGENCY VEHICLES SFCC NR 1 AND NR 2 WTB RESET, SFCC NR 1 AND NR 2 TEST COMPLETED AND REMar 6, 2011 · Airbus A320211SDR IPXA1165075Slat System · bindingSLATS SYS 1 & 2 FAULT CYCLED SLATS 4 TIMES LANDED WITH FLAPS 40 DEGREES; NO SLATS. ACCOMPLISHED SFCC BITE CHECK IAW TSM 27-50-00 SYS NR1 SHOWED SLATS ARE JAMMED. ACOMPLISHED TSM PROCEDURE 278002. FOUND NR4 RT TORQUE LIMITER ACTIVATED. FOUND OIL LEVEL IN SCREMar 2, 2011 · N139UP · Airbus A300F4622RSDR FDEA201103010804Switch · failedAFTER TAKEOFF LEADING EDGE FLAPS FAILED TO INDICATE RETRACTED. FE PANEL SHOWED NR 2 LED NOT RETRACTED. FOUND SWITCH S203 FROZEN AND VERY HARD TO MOVE. REPLACE SWITCH 203 REF WDM27-81-02 AND MM 27-82-001-4. OPS CHECK NORMAL ACFT OK FOR SERVICE.Mar 1, 2011 · N288FE · Boeing 7272D4SDR IPXA1164916Slat System · inoperativeSLATS 1/2 ON APPROACH. CYCLED HANDLE. FLAPS 40 SLATS STAYED AT 0. EMERGENCY DECLARED NRC336455, SUPPLEMENTAL SDR. C/W ALERT T149038 AND WAN 1726288. ACCOMPLISH BOW TS2560/998. PERFORM SFCC BITE CHECK IAW AMM 27-51-05. BITE TEST GOOD.Feb 23, 2011 · N153UP · Airbus A300F4622RSDR AALA20110223MIA01Fseu · faultedMIA - CREW REPORTED ON APPROACH LEADING EDGE SLAT DISAGREE AT HANDLE POSITION 25. FLIGHT LANDED MIA WITHOUT INCIDENT. REPLACED FLAP/SLAT ELECTRONICS UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.Feb 23, 2011 · N7375A · Boeing 767323SDR ASOA201100225Slat System · failedSLATS FAIL CAUTION MESSAGE ON APPROACH. SYSTEM RESET IAW FIM 27-81-00. OPS CHECK GOOD IAW AMM 27-50-00.Feb 7, 2011 · N605QX · Cndair CL6002C10SDR UALA2011020700664Slat System · malfunctionedECAM FLT CONTROL SLAT SYS 2 FAULT APPEARED AT FLAP RET AT 2000 FT ON CLIMBOUT. REF LOG 1 AND 2 SLAT LOCK OUT. CHECKED ALL SLAT DRIVE OVERLOAD INDICATORS LT AND RT ALL OK. ACCMP'D INSP OF SLAT WING TIP BRAKES. FOUND RT WING TIP BRAKE 0036CU VERY STIFF AND CHFeb 6, 2011 · N432UA · Airbus A320232SDR REXA201100079Indicator · trippedSLATS FAIL CAUTION IN FLIGHT SLATS STUCK AT 0 DEG, RAN QRH SITUATION AND MESSAGE PERSISTED. FOUND SFECUS REPORTED "MECHANICAL JAM" CODES TO MDC. T/S PER FIM 27-81-09, FOUND RT O/B SLAT I/B ACTUATOR & LT O/B SLAT O/B ACTUATOR TRIP INDICATORS FLIPPED. RESET IJan 30, 2011 · N200PA · Cndair CL6002D24SDR IPXA11664484Warning Light · illuminatedDIVERSION - EICAS MSG FLAP/SLAT ELEC DISPLAYED AFTER TAKEOFF. T/S C/O IAW FIM 29-51-00, FIG 114, SH 1 BLOCK 1 & 21. NO FAULTS NOTED, SYS OK. FIM REV 48.Jan 27, 2011 · N330UP · Boeing 76734AFSDR CA110125020Control Panel · malfunctioned(CAN) SLAT FLAP SLOW TO DEPLOY ON ARRIVING ,LANDED SAFELY NO OTHER ISSUES AROSE.MAINTENANCE ADVISED. MSG AUTO CLEARED FAULT UNABLE TO DUPLICATE ON GROUND OPERATIONAL TEST AS PER AMM 27-54-00-710-002 CHECKED SERVICEJan 21, 2011 · Airbus A319114SDR UALA2011012100351Fseu · illuminatedL/E SLAT ASSY EICAS, RTFL. TROUBLE SHOT, DIRECTED BY FIM TO L/E SLAT PROX SENSOR HEALTH CHECK, HEALTH CHECK FOUND SENSOR S298 WITH HIGH RESISTANCE. INSPECTED FOUND SENSOR SPLICES DAMAGED. REMOVED SENSOR AND RESPLICED. REPEATED HEALTH CHECK ALL CHECKS OK. DUEJan 21, 2011 · N662UA · Boeing 767322SDR AALA20110113TUL01Fseu · failedMSP - CREW REPORTED ON APPROACH LEADING EDGE DEVICES WOULD NOT EXTEND WHEN SELECTING FLAPS 1. EMERGENCY DECLARED FLIGHT LANDED MSP WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.Jan 12, 2011 · N946AN · Boeing 737823SDR AALA20110108LAX01Button · malfunctionedLAX - CREW REPORTED LEADING EDGE SLAT STUCK AND ONLY ABLE TO LAND FLAPS 20. EMERGENCY DECLARED FLIGHT LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RESET TORQUE LIMITER OVERLOAD BUTTON THAT HAD BEEN EXTENDED. SYSTEM GROUND CHECK NORMAL OPERATJan 8, 2011 · N691AA · Boeing 757223SDR QXEA2011011200022Slat System · malfunctionedSLATS FAIL, CAUTION MESSAGE CAME ON WHEN FLAPS WERE SELECTED. MDC SHOWS MECHANICAL JAM. LANDING UNEVENTFUL. CLEARED CAUTION IAW FIM TASK 27-81-00-810-802-A01, INTERGRATED MDC FAULT SLAT ACTUATOR SYS / MECHANICAL JAM, PERFORMED OPS TEST OF FLAPS AND SLATS IAWJan 8, 2011 · N616QX · Cndair CL6002C10SDR 9JLA20110107001Position Switch · shortedTHE FLIGHT CREW DISCOVERED DURING THE PREFLIGHT CHECKS A SSU/FLAP FAULT INDICATION. MX TROUBLESHOT THE FAULT AND FOUND BOTH THE RT INBD/OTBD FLAP POSITION FLAP SWITCHES SHORTED TO GROUND AND THE F5 3AMP FUSE FOR THE NR2 SSU WAS OPEN. BOTH FLAP POSITION SWITCHJan 7, 2011 · N800FL · Raythn HAWKER800SDR R61A20100590Slat · malfunctionedCREW REPORTED SLAT FAIL ON DESCENT, EMERGENCY VEHICLES WERE ROLLED, AC LANDED WITHOUT INCIDENT. MX CLEARED INHIBITS PER FIM, OPS CK GOOD.Jan 6, 2011 · N871RW · Emb ERJ170100SUSDR R61A20100589Unknown · malfunctionedCREW REPORTED SLAT FAIL ON APPROACH AND DECLARED EMERGENCY, CABIN WAS NOT PREPARED. A/C LANDED WITHOUT INCIDENT, MX RESET PER FIM, MESSAGE CLEARED OPS CHECK GOOD.Jan 4, 2011 · N125HQ · Emb ERJ170200LRSDR C77A353088Slat System · intermittentSLAT FAIL ON FINAL APPROACH. CLEARED SLAT FAIL MESSAGE IAW FIM TASK 27-81-00-810-803A. OPS TEST OF FLAP AND SLAT, GOOD, ACFT OK FOR SERVICE. IAW COMPANY REQUEST R & R LT SLAT, 3/4 HARNESS PN 171-10231-401, SN FO33911661, LT HARNESS SLAT 2/3 PN 171-00187-40Jan 3, 2011 · N615CZ · Emb ERJ170200LRSDR IPXA11563987Module · leakingBOTH FLAP POINTER ARE ON .5 WITH FLAP LEVER IN UP POSITION L/E SLAT DISAGREE DISPLAYED. DISAGREE MSG TEMPORARILY WENT OUT WITH SELECTION OF L/E ALT SWITCH BUT RETURNED. T/S C/O IAW FIM 27-51-00, FIG 104, A SHT 1. BITE TEST ON FSEU NR1, NO FAULTS SHOWN. ROTADec 29, 2010 · N446UP · Boeing 75724APFSDR IPXA11563986Fseu · inoperativeL/E SLAT DISAGREE LT ON CLEANUP. BOTH FLAP POINTERS ON .5 WITH FLAP LEVER IN UP L/E SLAT DISAGREE DISPLAYED. ATB T/S CARRIED IAW FIM 27-81-00. PERFORMED BITE ON ALL FSEU. NR1 FSEU FAILED MSG DISPLAYED. R & R NR1 FSEU IAW AMM 27-51-01. OPS TEST ON SLAT Dec 29, 2010 · N446UP · Boeing 75724APFSDR IPXA11563985Slat System · malfunctionedEMERGENCY DECLARED - "L/E SLAT DISAGREE" DISPLAYED WITH THE FLAP LEVER IN 1. BOTH FLAP POINTERS INDICATE 1/2. BITE TEST FSEU 1, 2 & 3, NO FAULT NOTED FIM 27-51-00. RESET C/B'S FSEU 1, 2 & 3. OPS CHECK SEVERAL TIMES, FOUND SATIS. ACFT OK TO CONTINUE.Dec 28, 2010 · N446UP · Boeing 75724APFSDR CA110103002Slat System · binding(CAN) ON APPROACH, FLIGHT DECLARED AN EMERGENCY WITH THEIR SLATS FAILED AT 0 DEGREES. FLIGHT LANDED WITHOUT ISSUE ON RUNWAY 33R. PASSENGERS WERE NOTIFIED OF THE IRREGULAR CONFIGURATION FOR LANDING AND WERE INFORMED ABOUT THE EMERGENCY VEHICLES. AFTER LANDING Dec 27, 2010 · Airbus A320211SDR FDEA201012234745Slat System · malfunctionedON APPROACH SPEED 230KTS, SLAT SYS 1 & 2 FAULT WHEN SLATS EXTENDED. MOMENTARY WENT OUT. UNTIL FLAP 15 SELECTED, THEN CAME BACK ON. PERFORMED GO-AROUND THEN PERFORMED CYCLE. SLATS EXTENDED OK WITHOUT FAULT. FOUND SFCC1 AND SFCC2 WITH THE SAME 4 FAULT BALLS Dec 23, 2010 · N435FE · Airbus A310203SDR FDEA201012224736Valve · malfunctionedAFTER T/O ECAM INDICATED SLATS SYS 2 FAULT AND OVER-HEAD INDICATED SLATS SYS 2 FAULT LIGHT ILLUMINATED. CREW CYCLED SLATS TWICE - SLATS AND FLAPS WERE NORMAL AFTER SECOND CYCLE - LIGHT REMAINED ILLUMINATED. NR 2 SFCC FAULTED HIGH SPEED VALVE. REPLACED SLAT Dec 22, 2010 · N726FD · Airbus A300B4622RSDR UALA2010122204689Controller · faultedFLAP-SLAT CONTROL 2 HIGH LIFT CONTROL LANE NR2 HAS A FAULT. FAULT MSG 27-20412. MAINTENANCE VERIFIED ALTN FLAPS OPERATE NORMALLY PER MEL 2703A. WORKING WITH FIM 27-52 TASK 804 PG213, FOUND RESISTANCE BETWEEN PINS 4 AND 14 READING 146.5 OHMS INSTEAD OF 56.5 Dec 21, 2010 · N224UA · Boeing 777222SDR CA101221002Sensor · failed(CAN) ON APPROACH, SLAT FAILURE THEN WING ANTI-ICE FAILURE DESCENDING THROUGH CLOUDS. BROKE OFF THE APPOACH, RESETS, DECLARED PAN PAN LANDED WITHOUT INCIDENT WITH 0 SLAT AND 0 FLAP ACCORDING TO CREW. T/S C/O TSM 27-83-00-810-814 AND CHANGING R/H SLAT 2-3 SKEDec 20, 2010 · Emb ERJ190100IGWSDR AALA20101216MIA01Fseu · malfunctionedMIA - CREW REPORTED DURING APPROACH FLAT SLAT ASSYMETRY. EMERGENCY DECLARED LANDED MIA WITHOUT INCIDENT. ACCOMPLISHED BITE OF FLAP SLAT ELECTRONICS UNIT AND FOUND FAULT CODE M548 AND M603. RESET SYSTEM AND OPERATED FLAPS SEVERAL TIMES AND NO FAULTS NOTED. Dec 16, 2010 · N327AA · Boeing 767223SDR ASOA201001913Slat System · failedSLAT FAIL CAUTION MSG ON APPROACH INTO ATL COMPLIED W/QRH (EMERGENCY DECLARED). RESET AND OPS CHECKED GOOD IAW FIM 27-81-00 810-801 A01. (CLOSED)Dec 9, 2010 · N135EV · Cndair CL6002D24SDR IPXA10563790Switch · inoperativeATB - L/E SLAT DISAGREE. FOUND SWITCH S10339 ON RT WING OTBD INOPERATIVE. S10339 REMOVED/INSTALLED S10339 STARTING AT STEP 3 TO THE END OF M/M 27-81-42-4. ALSO REF WDM 27-81-31. SYS OPS CKS NORMAL. ACFT OK FOR CONT SVC.Dec 5, 2010 · N452UP · Boeing 75724APFSDR UALA2010120304446Warning Light · illuminatedL/E FLAP DISAGREE EICAS ON FLAP EXTENSION. AFTER COMPLETION OF TEST FLIGHT, INSPECTED ALL LEADING EDGE SLAT DRIVE ROTARY ACTUATOR OVERLOAD INDICATORS FOR A TRIPPED CONDITION. ACCOMPLISHED CHECK FOR OVERLOAD. NO TRIPPED ROTARY ACTUATORS FOUND. CREW STATED SDec 3, 2010 · N519UA · Boeing 757222SDR ASMF201012004Sensor · damagedACFT RETURNED OF FLIGHT DUE TO DURING CRUISE AT 38,000 FEET, THE L/E FLAPS TRANSIT LIGHT AND L/E DEVICES LIGHT TURNED ON, SO THE FLIGHT CREW PERFORMED THE QRH 9.12 PROCEDURE LANDING WITH NO ADDITIONAL PROBLEMS. ACFT WAS SENT TO THE HANGAR AND DURING MX REVISIODec 1, 2010 · N855AM · Boeing 737705SDR CA101129001Drive Shaft · disconnectedSHORTLY AFTER TAKEOFF THE CREW REPORTED A SLAT FAIL MESSAGE. DUE TO ALTITUDE AND SPEED LIMITATIONS WITH SLAT EXTENDED THE FLIGHT WAS UNABLE TO CONTINUE TO DESTINATION AND MADE A DIVERSION. FOUND DRIVE SHAFT DISCONNECTED AT NR 1 LT SLAT ACTUATOR. SHAFT RECONNov 27, 2010 · Emb ERJ190100IGWSDR AALA20101127ORD01Fseu · inoperativeORD - CREW REPORTED EICAS MESSAGE LEADING EDGE SLAT ASSYMETRY. EMERGENCY DECLARED LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH STALL WARNING CARDS (MPN 285T110423) AND FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECK NORMAL OPERANov 27, 2010 · N390AA · Boeing 767323SDR FDEA201011274497Flap System · malfunctionedAT FLAPS 2 POSITION THE AMBER L/E FLAPS LIGHT STAYS ILLUMINATED. L/E DIVICES POSITION INDICATOR SHOWS NORMAL LED CONFIGURATION. RELEASED FOR SERVICE IAW MEL: 27-06-C CATEGORY: C EXPIRATION: 07DEC10 "MEL 27-06-C: AMBER L/E FLAPS LIGHT ON THE FWD INSTRUMENTNov 27, 2010 · N466FE · Boeing 727225SDR FDEA201011264495Valve · malfunctionedDURING SLAT RETRACTION ECAM IND SLAT SYS 2 FAULT WITH OVERHEAD LIGHT ON. CYCLED HANDLE NO JOY. SPFI INDICATED SLATS UP. ZIPPER AND HOOK WORKED NORMALLY, CONSULTED QRH, DID NOT COVER FAULT WITH SLATS ACTUALLY UP. WITH BOTH VISUAL AND SPFI INDICATING FLAPSNov 26, 2010 · N726FD · Airbus A300B4622RSDR CA101125002Brake · failedON APPROACH TO YXE WHEN FLAP 1 SELECTED THE CREW RECEIVED A SLAT LOCK ECAM MESSAGE. NO OTHER DETAILS PROVIDED. T/S CARRIED OUT PER TSM 27-81-00-810-815 AND AMM 27-84-00-200-001. DVI OF SLAT TRANSMISSION SYSTEM CARRIED OUT. NO TORQUE LIMITER INDICATOR FOUNDNov 23, 2010 · Airbus A319114SDR FDEA201011194431Limiter · failedSLATS SYS 1 AND SLATS SYS 2 FLAPS, REPEAT ITEM, NO SLATS LANDING. PERFORMED LGAV, T/S SYS IAW FIM 27-80-02, FIG 101, SHEET 1. FOUND TORQUE LIMITER POPED. R AND R TORQUE LIMITER IAW MM 27-84-12-04. ALSO SERVICED LT WING SLATS, SCREW JACKS AND GEAR BOXES INov 19, 2010 · N801FD · Airbus A310324SDR CA101115017Slat System · failed(CAN) THE AIRCRAFT ENCOUNTERED A SLAT FAILURE DURING APPROACH. SF ACE 1 AND 2 INHIBITS CLEARED IAW AMM 45-45-00-970-805-A/200. OPS CHECK FOUND SATISFACTORY IAW 27-56-00-710-810-A/200.Nov 15, 2010 · Emb ERJ170200SUSDR CA101116001Slat System · failed(CAN) WHEN EXTENDING FLAPS 0 TO 1, EICAS MESSAGE "SLAT FAILURE". QRH ACTIONED, NIL FIX. UNEVENTFUL LANDING RWY 31 - NO HANDLING DIFFICULTIES NOTED. FLIGHT CONTROL SYSTEM RESET ALL FLIGHT CONTROL MESSAGES ON CMC CLEARED. NO CORRESPONDING MAINT FIM MESSAGES ONov 14, 2010 · Emb ERJ170200SU
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