GE CF34-8E5A1

Service difficulty reports · 194

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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 engine_model_key = 'CF348E5A1'
  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 CA120822002Oil System · low pressure(CAN) NR 2 ENGINE LOW OIL PRESSURE INDICATION. QRH FOLLOWED, AND ENGINE SHUTDOWN. RETURNING TO DEPARTURE AND LANDED.Aug 22, 2012 · Emb ERJ170200SU · Engine Oil Indicating SystemSDR CA120814002Pump · leaking(CAN) APPROXIMATELY 5 MINUTES BEFORE TOP OF DESCENT, THE CREW RECEIVED A HYDRAULIC SYS 2 LOW QTY INDICATION FOLLOWED BY A HYD 2 FAILURE. AN EMERGENCY WAS DECLARED WITH ATC AND THE QRH WAS FOLLOWED. THE FLIGHT LANDED SAFETLY ON R23 WITH HYDRAULIC FLUID OBSERVAug 14, 2012 · Emb ERJ170200SU · Hydraulic Pump (Electric/Engine), MainSDR CA120906014Pump · leaking(CAN) APPROXIMATELY 5 MINUTES BEFORE TOP OF DESCENT, THE CREW RECEIVED A HYDRAULIC SYS 2 LOW QTY INDICATION FOLLOWED BY A HYD 2 FAILURE. AN EMERGENCY WAS DECLARED WITH ATC AND THE QRH WAS FOLLOWED. THE RT NR 2 ENGINE DRIVEN PUMP, EDP WAS FOUND LEAKING.Aug 14, 2012 · Emb ERJ170200SU · Hydraulic Pump (Electric/Engine), MainSDR CA120725004Processor · failed(CAN) FLIGHT HAD AVIONICS SYS FAULT MESSAGE, MAJOR FUNCTIONS OF ACFT ARE LIMITED SO DIVERSION WAS NECESSARY, DECLARED AN EMERGENCY. NIC PROC 5 REPLACED AND CHECKED SERVICEABLE IAW AMM 31-41-04 PB401.Jul 25, 2012 · Emb ERJ170200SU · Central ComputersSDR CA120720002Flap System · failed(CAN) ON DESCENT, FLIGHT REPORTED TO ATC THEY WERE UNABLE TO LOWER FLAPS FOR LANDING. AIRPORT EMERGENCY VEHICLES DISPATCHED. ACFT LANDED WITHOUT INCIDENT OTHER THAN HIGH BRAKE TEMPS WHICH WERE VISUALLY INSPECTED BY EMERGENCY VEHICLES PRIOR TO TAXI. FLAP FJul 19, 2012 · Emb ERJ170200SU · Trailing Edge Flap Control SystemSDR CA120718002Sensor · malfunctioned(CAN) INBOUND FLIGHT EXPERIENCED A FLAP FAIL EICAS. QRH WAS FOLLOWED AND A PAN WAS DECLARED AS A PRECAUTION. THE FLIGHT LANDED WITHOUT FURTHER EVENT. SFACE 1 & 2 PUT TO THIER ORIGINAL POSITION. SFACE 2 REPLACED AND CHECKED SERV IAW AMM 27-53-02. FLAP SKEW SEJul 18, 2012 · Emb ERJ170200SU · Trailing Flap Position Indicating SystemSDR CA120604016Indicator · failed(CAN) ON TAKEOFF AT APPROXIMATELY 105 KTS REJECTED T/O DUE LOSS OF V-SPEEDS ON PFD. RETURN TO THRESHOLD AND WAIT FOR BRAKES TO COOL. DVDR WAS DOWNLOADED, AND NO FAULT WAS FOUND.May 29, 2012 · Emb ERJ170200SU · Airspeed/Mach IndicatorSDR CA120511002Pump · failed(CAN) EMERGENCY DECLARED DUE TO HYDRAULIC 2 EDP FAIL. EICAS HYD 2 LOW QTY IN CRUISE . HYD FLUID UPLIFT CARRIED OUT AFTER HYD PUMP REPLACED.May 10, 2012 · Emb ERJ170200SU · Hydraulic Pump (Electric/Engine), MainSDR CA120509005Engine · shutdown(CAN) ENGINE SHUTDOWN CLIMBING THRU 14000 FT ON DEPARTURE, EMERGENCY DECLARED. ACFT IS RETURNED TO DEPARTURE. NR 2 ENGINE AUTO SHUTDOWN WITH FAULT ICON. IN CLIMB OUT RED OIL PRESSURE AFTER ABOUT 1 MIN NO RESTART ATTEMPTED. LIKELY HPT2 FAILURE.May 6, 2012 · Emb ERJ170200SU · Engine (Turbine/Turboprop)SDR CA120509002Module · failed(CAN) DURING THE CRUISE THE CREW REPORTED A WING LEAK/ANTI ICE FAULT. AFTER DISCUSSION WITH MAINTENANCE THE FLIGHT RETURNED DUE TO POSSIBLE ICING CONDITIONS AT DESTINATION LOOSE CONNECTOR PLUG ON SLAT 2 HARNESS FOUND AND RETIGHTENED. CUSTOM I/O MODULE 2, REMay 4, 2012 · Emb ERJ170200SU · Ice DetectionSDR CA120504005Module · failed(CAN) DURING THE CRUISE THE CREW REPORTED A WING LEAK, ANTI ICE FAULT. AFTER DISCUSSION WITH MAINTENANCE THE FLIGHT CONTINUED NORMALLY TO DESTINATION IN NON-ICING CONDITIONS. PREVIOUSLY SNAGGED ON APRIL 15TH, LT SLAT 2 OTBD TEMP SENSOR WAS REPLACED. DUE HISMay 3, 2012 · Emb ERJ170200SU · Ice DetectionSDR CA120423013Torque Tube · disconnected(CAN) ACFT ON APPROACH HAD SLAT FAIL, DECLARED PAN PAN. LANDED WITH NO ISSUES FOUND RT SLAT TORQUE TUBE DISCONNECTED AT SLAT DRIVE MOTOR. TORQUE TUBE RECONNECTED IAW AMM 27-81-03-400-801-A. SLAT CONTROL OPS TEST COMPLETED IAW 27-80-00-710-801A. NO FAULTS FApr 22, 2012 · Emb ERJ170200SU · Leading Edge Slat Control SystemSDR CA120423017Slat System · failed(CAN) DURING THE APPROACH TO LAND THE CREW REPORTED THEY HAD A, SLAT FAIL, MESSAGE, AFTER FOLLOWING THE QRH THE CREW LANDED WITH SLATS AT POSITION 3 AND FLAPS AT POSITION 2 SLAT SYS RESET CARRIED OUT IAW QUICK REFERENCE RESET GUIDE PAGE 123 AND FIM 27-80-00-8Apr 19, 2012 · Emb ERJ170200SU · Leading Edge Slat Control SystemSDR CA120416004Connector · failed(CAN) HOT BATTERY, DECLARED EMERGENCY, RETURNED FOUND WIRING DAMAGED BY BROKEN BACKSHELL AT CONNECTOR P0492. CONNECTOR BACKSHELL REPLACED AND WIRING RETERMINATED IAW SWPM 20-41-10 AND WDM 24036059 P1. BATTERY NR 2 OPS TEST CHECKS SERVICEABLE IAW AMM 24-36-00Apr 15, 2012 · Emb ERJ170200SU · Electrical Power System WiringSDR CA120404009Actuator · failed(CAN) AFTER DEPARTURE, THE CREW RECEIVED A LEFT MLG DISAGREE MESSAGE AND ELECTED TO RETURN. DOWNLOCK RELEASE ACTUATOR REPLACED IAW AMM 32-31-05. REPLACED LT MLG RETRACT ACTUATOR IAW 32-31-01 DOWNLOCK RELEASE ACT. PN: 190-71103-2103, SN: 1102735 MLG RETRACT Apr 3, 2012 · Emb ERJ170200SU · Landing Gear Retraction/Extension SystemSDR CA120301005Steering Sys · malfunctioned(CAN) AFTER NORMAL LANDING AND EXITING THE RUNWAY THE CREW REPORTED THE ACFT HAD A STEERING FAIL MESSAGE. THE ACFT TAXIED NORMALLY WITH DIFFERENTIAL BRAKING TO THE GATE. IAW QUICK REF RESET GUIDE, PROC CARRIED OUT, FIM 32-53-00-810-806-A, FAULT CLEARED.Feb 25, 2012 · Emb ERJ170200SU · Steering UnitSDR CA120217007Control Unit · malfunctioned(CAN) GO AROUND DUE TO A SLAT FAILURE ON APPROACH. SLAT FAIL ON EICAS. SLAT STUCK AT 3. WOULD NOT RETRACT OR EXTEND. AFTER GEAR DOWN AOA LIMIT FAIL. SPOILER FAULT. SHAKER ANTICIPATED. TROUBLESHOT IAW FIM TASK 27-81-00-810-807-A00. FOUND TRANSITORY CONDITIOFeb 17, 2012 · Emb ERJ170200SU · Leading Edge Slat Control SystemSDR CA120213001Wire Harness · failed(CAN) AFTER FLAP RETRACTION, HAD A SLAT FAILURE. RETURNED TO DEPARTURE AND DECLARED AN EMERGENCY. R & R OTBD SKEW SENSOR HARNESS IAW AMM 27-83-07. OPS CHK OK. ACFT SERVICEABLE.Feb 11, 2012 · Emb ERJ170200SU · Leading Edge Slat Position Indicating SystemSDR CA120111001Wire Harness · chafed(CAN) THE HARNESS WAS RUBBING ON A BRACKET, PN 170-31533-401, SRM 57-50-00, AT THE WING ROOT. THE 4 WIRES DAMAGED ARE W502-00178-24 GOES FROM P0589-P1249 THE LT OTBD FLAP SKEW SENSOR T4, W502-00046-24 GOES FROM P0589-P0915 GROUND SPOILER PROX SENSOR, W502-000Jan 10, 2012 · Emb ERJ170200SU · Wing System WiringSDR CA120105006Flap System · failed(CAN) ON APPROACH THE CREW REPORTED A FLAP SLAT FAIL, NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER COMPLICATIONS. CARRIED OUT FIM 27-81-00-810-807-A00. TRANSITORY CONDITION OF THE SLAT/FLAP ACE. SLAT OPERATION CHECK CARRIED OUT SERVICEABLE.Jan 3, 2012 · Emb ERJ170200SU · Trailing Edge Flap Control SystemSDR CA120107004Attach Bracket · cracked(CAN) LEFT NOSE WHEEL SPIN BRAKE BRACKET CRACKED. (TC# 20120107004)Jan 3, 2012 · Emb ERJ170200SU · Fuselage Main, Attach FittingsSDR CA111219015Slat System · failed(CAN) SLAT FAILURE STUCK IN NR 3,GO AROUND,LANDING NORMAL REF MAINTENACE ALERT 27-50-23, FLAP FAIL OR SLAT FAIL SLAT ACTUACTOR INSPECTION/CHECK CARRY OUT. NO ACTUACTOR FOUND ON TRIP POSITION. SLAT ACTUACTOR-INSPECTION/CHECK AIW AMM 27-81-01.Dec 11, 2011 · Emb ERJ170200SU · Leading Edge Slat Control SystemSDR CA111208016Slat System · malfunctioned(CAN) THE AIRCRAFT ENCOUNTERED A SLAT FAILURE AFTER DEPARTURE. THE FLIGHT DIVERTED BACK TO POINT OF DEPARTURE. MAINTENENCE HAS BEEN ADVISED. COMPLIED WITH FIM 27-81-00-810-807. NO FAULTS FOUND. RESET SLAT INHIBITS ACE1 AND ACE2 COMPIED WITH OPERATION TEST REDec 8, 2011 · Emb ERJ170200SU · Leading Edge Slat Control SystemSDR CA111123004Fan · failed(CAN) CREW REPORTED EXPERIENCING FUMES IN CABIN AND FLIGHT DECK, RETURNING TO POINT OF DEPARTURE. CHANGED RECIRCULATION FILTER IAW TASK 21-24-02-400-801A . OPERATION OF AIR CIRCULATION CARRIED OUT, NO STRONG ODOR.Nov 23, 2011 · Emb ERJ170200SU · Air Distribution FanSDR CA120107002Attach Bracket · cracked(CAN) RIGHT NOSEWHEEL SPINBRAKE ATTACH BRACKET CRACKING AT LOWER INBOARD HILITE FASTENER. IAW SRM 53-10-18, FIG. 15, ITEM 100.Oct 23, 2011 · Emb ERJ170200SU · Fuselage Main, Attach FittingsSDR CA111024003Actuator · failed(CAN) AFTER T/O, FLAP FAIL FAULT MESSAGE CHECKLIST CARRIED OUT, FLAPS RETURNED TO ZERO. NORMAL APPR AND LANDING WITH FLAP 5, AFTER LANDING FLAP FAIL FAULT MESSAGE. SLATS, GREEN ZERO, FLAPS AMBER DASHES, FIX: FLAP ACTUATOR 2R REMOVED AND INSTALLED IAW AMM 27Oct 21, 2011 · Emb ERJ170200SU · Trailing Edge Flap ActuatorSDR CA111004004Duct · cracked(CAN) CRACKED, ENGINE PRECOOLER TEE DUCT ASSY, BELOW PER-COOLER. THIS COULD LEAD TO PYLON OVERHEAT WARNINGS & PHYSICAL DAMAGE TO WIRING HARNESS COMPONENTS ON ENGINE PYLON.Oct 3, 2011 · Emb ERJ170200SU · Pneumatic Distribution SystemSDR CA110822002Deflector · failed(CAN) FLIGHT RETURNED DUE TO A LOUD SQUEAL COMING FROM SERVICE DOOR. FOUND R1 DOOR DEFLECTOR "SOFT". REPLACED R1 DEFLECTOR IAW AMM 52-41-28.Aug 19, 2011 · Emb ERJ170200SU · Service DoorsSDR CA110822004Oven · odor(CAN) WHILE HOLDING SHORT OF DEPARTURE RUNWAY THE SERVICE DIRECTOR OPENED THE OVEN TO CHECK THE STATUS OF J-CLASS SNACKS AND GREY BLUE SMOKE AND BURNING SMELL FROM AN UNDETERMINED SOURCE SPREAD FORWARD THROUGH THE CABIN. SMOKE CLEARED AND FLIGHT CONTINUED. Aug 18, 2011 · Emb ERJ170200SU · Buffet/GalleysSDR CA110808002Warning Message · false activationON CLIMB OUT, HAD DOUBLE BLEED FAULT AND AUTO THROTTLE DISCONNECT. BLEED AND PACKS NOW OPERATING NORMALLY, THROTTLES STAGGERED BY AN INCH, ENROUTE AT F140 TO DESTINATION. DEFECT REPORTED BY THE CREW: 3 PERCENT DIFF N1 50 DEG ITT TO 3 RSV. A/T DISENGAGE IN CAug 6, 2011 · Emb ERJ170200SU · Central WarningSDR CA110729006Sensor · failed(CAN) DURING THE CRUISE PORTION OF THE FLIGHT, THE SLATS BECAME "FROZEN" IN THE NR 3 POSITION. A "PANPAN" MESSAGE WAS GIVEN TO ATC AS A PRECAUTION. THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. CFR WAS ON STANDBY AS A PRECAUTION. OTBD SLAT SKEWJul 29, 2011 · Emb ERJ170200SU · Leading Edge Slat Position Indicating SystemSDR CA110728002Sensor · failedSLAT FAIL, PLANNING F200 AT 210KTS SLAT FAIL ON T/O, SLAT REMAINED IN POS 1- ON LANDING, FLAP 3 SELECTION ON LANDING SHOWED. FLAP 5 NORMAL CMC INTERROGATED. FAULT CODE FOUND 27811014ACE. FRM FIM 27-81-00-810-807-A00 C/O SERV RT OTBD SLAT SKEW SENSOR (S2-3)Jul 27, 2011 · Emb ERJ170200SU · Leading Edge Slat Position Indicating SystemSDR CA110728001Sensor · failedSLAT FAIL ON APPROACH, LANDED WITH OUT INCIDENT. EMERGENCY NOT DECLARED, "SLAT FAIL" EICAS MESSAGE ON APPROACH UPON SELECTING FLAP 2. QRH COMPLETED. MESSAGE DID NOT EXTINGUISH. LANDED WITH FLAP 2 SLAT 3 (AMBER). R & R LT WING INBD AND OTBD SLAT SKEW HARNEJul 25, 2011 · Emb ERJ170200SU · Leading Edge Slat Position Indicating SystemSDR CA110729003Brake · failedSIGNIFICANT TRAIL OF CARBON DUST DROPPING FROM RT MAIN L/G DURING PUSHBACK RTG ACTION: FOUND NR 4 BRAKE WITH EXCESSIVE CARBON PARTICLES. NR 4 BRAKE REPLACED IAW AMM 32-49-11.Jul 23, 2011 · Emb ERJ170200SU · BrakeSDR CA110729004Brake · failedON PUSHBACK, NR 3 MAIN WHEEL BRAKE WAS GRABBING & DISINTEGRATING ACTION: NR 3 BRAKE AND NR 3 MAINWHEEL REPLACED. AXLE INSPECTED, NIL FAULTS. COMMENTS: TIRE WAS SEIZED ON BRAKE, NECESSARY TO REMOVE THE WHEEL AND BRAKE AS A UNIT. REMOVED: 90000582WT, SN: JUN07-Jul 23, 2011 · Emb ERJ170200SU · BrakeSDR CA110722003Module · failedIN THE CLIMB THROUGH 11,000 FT, THE FLIGHT EXPERIENCE SIGNIFICANT DOOR SEAL VIBRATION FOLLOWED BY A NR 1 BLEED FAILURE THROUGH 16,000 FT. THE FLIGHT LEVELED OFF AND FOLLOWED THE QRH WHICH CLEARED THE BLEED FAILURE BUT THE CABIN PRESSURE CONTINUED TO CLIMB. TJul 21, 2011 · Emb ERJ170200SU · Electrical Power SystemSDR CA110712001Slat System · failedSLAT FAILURE INCIDENT DETAILS: AFTER DEPARTURE ON FLAP RETRACTION, THE FLAPS RETRACTED NORMALLY WITH THE SLATS REMAINING IN POSITION 3 FOLLOWED BY AN ICAS WARNING MESSAGE. SPEED WAS REDUCED, THE FLIGHT LEVELED OFF AT A70 AND ATC ADVISED. THE QRH WAS CARRIEDJul 8, 2011 · Emb ERJ170200SU · Leading Edge Slat Control SystemSDR CA110708004Sensor · failedEN ROUTE, 10 MINUTES INTO CRUISE, AUTOPILOT DISCONNECTED ASSOCIATED WITH WITH A SLAT FAIL AND SPOILER FAULT. ATC WAS ADVISED AND AN EMERGENCY WAS DECLARED. A ZERO FLAP/SLAT LANDING CARRIED OUT WITH THE ACFT REMAINING ON THE RUNWAY WITH ERS MEETING THE ACFT. Jul 6, 2011 · Emb ERJ170200SU · Leading Edge Slat Position Indicating SystemSDR CA110708007Sensor · malfunctionedDURING THE APPROACH, THE ACFT ENCOUNTERED A MILD WAKE TURBULENCE AND RECEIVED A FLAP FAIL MESSAGE AND SLAT FAIL MESSAGE AND AOA FAIL MESSAGE AS WELL AS A STICK SHAKER ANTICIPATED MESSAGE. ELECTED TO GO AROUND AND WAS UNABLE TO EXTEND THE FLAPS. THE FLIGHT DIJul 4, 2011 · Emb ERJ170200SU · Leading Edge Slat Position Indicating SystemSDR CA110707011Brake · failedBRAKE PARTS FOUND ON RAMP ON ARRIVAL. CREW MEMBERS AND RAMP FOUND PARTS ON WALK AROUND. ALSO THE PORT AUTHORITY FOUND PARTS NEAR TAXIWAY. BRAKES WILL NEED TO BE REPLACED. RT BRAKE HINGE BROKEN RT WHEEL INBD SIDE. R & R NR 3 MLG BRAKE ASSY IAW AMM 32-49-11.Jul 1, 2011 · Emb ERJ170200SU · BrakeSDR CA110607007Sensor · failed"SLAT FAIL" EICAS MSG AFTER T/O, BEFORE FLAP RETRACTION. QRH CARRIED OUT. MAX WEIGHTLANDING C/O. CONSTANT RT AILERON INPUT NECESSARY TO MAINTAIN WINGS LEVEL. NOT AN OVERWEIGHT LANDING. RT OTBD SLAT SKEW SENSORS PO990 AND PO992 REPLACED IAW FIM 27-81-00-81Jun 6, 2011 · Emb ERJ170200SU · Leading Edge Slat Position Indicating SystemSDR CA110525004Sensor · failedSLAT FAIL ON APPROACH TO RWY 05 AT 2000 FT, G/A INITIATED. PERFORMED QRH PROCEDURE, UNABLE TO CLEAR SLAT FAIL EICAS, SECOND APPROACH CONDUCTED TO RWY 05 IN SLAT 3/FLAP 2 MODE WITH 6000 FT. REQUIRED DISTANCE. CARRIED OUT FIM 27-81-00-810-807A. IAW AMM & SNL 1May 21, 2011 · Emb ERJ170200SU · Leading Edge Slat Position Indicating SystemSDR CA110520003Steering Unit · failedACFT LANDED AND LOST NLG STEERING. MAU 2 NIC PROCESSOR 3 FAULT ON PREVIOUS FAIL. ON RESET OF MAU 2 PROCESSOR 3 C/B FAULT CLEARED, NIC PROCESSOR 3 REPLACED IAW AMM 31-41-24-000/400-801. OP SOFTWARE AND FMS SOFTWARE LOADED. STEERING OPS CHECK CARRIED OUT WITHMay 19, 2011 · Emb ERJ170200SU · Steering UnitSDR CA110518004Connector · corrodedDURING A PLANNED APU CHANGE, CONNECTOR PN D38999-26FD97 SN ON HARNESS W314 WAS FOUND CORRODED.May 17, 2011 · Emb ERJ170200SU · APU System WiringSDR CA110518007Autothrottle Sys · malfunctionedCREW ADVISED FLIGHT DISPATCH OF A REJECTED TAKEOFF THAT EXCEEDED 100 KTS. THE ACFT WAS ON THE TAKEOFF ROLL. JUST AS THE ACFT ACCELERATED THROUGH 100 KTS, CREW OBSERVED AN EICAS "THROTTLE LEVER NOT TOGA". THE ACFT WAS STOPPED ON THE RUNWAY. OPS CHECK OF AUTMay 17, 2011 · Emb ERJ170200SU · Auto Throttle SystemSDR CA110516003Sensor · out of toleranceSLAT FAIL ON APPROACH, GO-AROUND INITIATED AT 2000 FT, FOLLOWED QRH PROCEDURE THEN RETURNED TO LAND. REF FIM TASK 27-81-00-810-805 A BOTH LT OTBD SKEW SENSORS OUT OF TOLERERANCE AND REPLACED IAW AMM 27-83-01. OPS TEST CARRIED OUT. REMOVED: LIB POSITION: PN 17May 13, 2011 · Emb ERJ170200SU · Leading Edge Slat Position Indicating SystemSDR CA110510001Trunnion · corroded(CAN) DURING INSPECTION OF THE RT TRUNNION FITTING IN THE NLG BAY, PITTING CORROSION WAS FOUND AT THE TOP OF THE BORE. AFTER REVIEW OF THE E175 SRM AND AMM, NO REPAIRS OR ALLOWABLE DAMAGE LIMITS COULD BE FOUND FOR THE SUBJECT FITTING. INFORMATION WILL BE UPDAMay 8, 2011 · Emb ERJ170200SU · Fuselage, Landing Gear Attach FittingsSDR CA110509007Wire Harness · failed(CAN) ON DEPARTURE CREW RECEIVED SLATS/FLAP FAIL MESSAGE. FLIGHT CONTINUED AND LANDED IAW QRH. EMERGENCY DECLARED AS PRECAUTION. SLAT HARNESS LT WING OTBD NR 4 W512 REPLACED IAW AMM 27-83-07-000-801-A. NO MESSAGE ALL OTHER FAULTS, NO FAULTS NOW. SERVICEABMay 7, 2011 · Emb ERJ170200SU · Flight Control System WiringSDR CA110509006Indicator · failed(CAN) ATC ADVISED FLIGHT DISPATCH THAT THE FLIGHT WAS INBD WITH A FLAP/SLAT FAIL. CREW CALLED TO REPORT THAT ON FINAL FOR RWY 24R, DURING NORMAL FLAP SELECTION, EICAS MSG. CREW ELECTED TO GO-AROUND, QRH COMPLETED, AND RETURNED TO LAND. NO OTHER ABNORMAL REPORMay 7, 2011 · Emb ERJ170200SU · Leading Edge Slat Position Indicating SystemSDR CA110510005Engine · overtemp(CAN) LEFT ENGINE INFLIGHT SHUTDOWN DUE TO EGT INDICATION IN THE RED. THE EGT INCREASE IN THE RED ZONE IN CRUISE, THEY MOVE THE THROTTLE TO IDLE POSITION AND THE EGT REMAINS IN THE RED AREA, THEY DECIDED TO SHUTDOWN THE ENGINE. THE ACFT LANDED.May 4, 2011 · Cndair CL600* · Engine (Turbine/Turboprop)
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