GE CF34-10E5A1

Service difficulty reports · 476

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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 = 'CF3410E5A1'
  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 BAGA2026042700005Oil System · low pressureDURING FLIGHT ENGINE OIL 2 PRESSURE DECREASED WENT TO APPROX 20 RED INDICATION, RAN QRH AND SHUT ENGINE DOWN. NO FURTHER INCIDENT.Apr 24, 2026 · N120BZ · Emb ERJ190100IGW · Engine Oil Indicating SystemSDR BAGA2024082800662Engine · vibrationENGINE 2 VIBRATION ON HIGH PASS DURRING TAXI, AND THERE WAS A SLIGHT HAZE AND UNUSUAL SMELL. NO FIRE INDICATIONS NOR SMOKE IN THE COCKPIT OCCURED. AIRCRAFT RETURNED TO THE GATE. ENGINE R/R IN PROCESS FOR CORRECTIVE ACTION.Aug 28, 2024 · N126BZ · Emb ERJ190100IGW · Engine (Turbine/Turboprop)SDR BAGA2024073000004Bleed Valve · failedENGINE 1 BLEED ON MEL, ENGINE 2 BLEED FAULED. BLEED 2 FAIL EICAS ENROUTE JUST AFTER ICING CONDITIONS EICAS MESSAGE APPEARED. PERFORMED QRH. BLEED 2 FAIL MESSAGE CONTINUED. MOC NOTIFIED. REMOVED AND REPLACED NAPROV PER AMM 36-11-03/400, LEAK CHECK GOOD. PERFORMJul 29, 2024 · N145BZ · Emb ERJ190200IGW · Compressor Bleed ValveSDR CA190812014Engine · power loss(CAN) AFTER DEPARTURE THROUGH 15000 FEET CREW NOTICED SMALL DROP IN N1 AND HAD SHUTTERING AND VIBRATIONS FROM NUMBER 2 ENGINE. AFTER LOSING POWER ON THE NUMBER 2,FLIGHT CREW BROUGHT THROTTLES BACK TO IDLE THAT STOPPED THE CONTINUOUS VIBRATIONS. THEY DECLARED AAug 4, 2019 · Emb ERJ190100IGW · Engine (Turbine/Turboprop)SDR CA190605001Control Panel · failed(CAN) FLIGHT DECLARED `MAYDAY` DUE INSTRUMENTATION FAILURE. FLIGHT DIVERTING. RESOLUTION GUIDANCE PANEL REPLACED IAW AMM 22-11-01. OPS CHK SERVICEABLE. (TC# 20190605001)Jun 4, 2019 · Emb ERJ190100IGW · Autopilot ComputerSDR CA190527023Proximity Sensor · failed(CAN) SHORTLY AFTER DEPARTURE THE CREW REPORTED A WEIGHT ON WHEELS FAIL MESSAGE. THE FLIGHT RETURNED AND LANDED APPROXIMATELY 400KG OVERWEIGHT. NO EMERGENCY WAS DECLARED. RESOLUTION CARRIED OUT THE WIRING CHECK TO ASCB TERMINATORS AS PER FIM 31-42-00-815-A. May 25, 2019 · Emb ERJ190100IGW · Landing Gear Position and WarningSDR CA190523005Processor · failed(CAN) DECLARED A PAN PAN WITH ATC DUE TO A MAU 1 FAILURE. POSSIBLE LOSS OF SPOILERS, NOSEWHEEL STEERING. AIRCRAFT WAS ABLE TO CLEAR THE RWY WITHOUT A TOW. RESOLUTION CMC INTERROGATED, AVNX MAU 1A FAIL MSG + F.C. 45452143CMC. REPLACED MAU1 + NIC1 PROC MODULEMay 22, 2019 · Emb ERJ190100IGW · Central ComputersSDR CA190510002Processing Unit · failed(CAN) AIRCRAFT RECEIVED ANVX MAU 2B FAULT MESSAGE. DUE TO THIS SYSTEM AFFECTING THE BRAKES THE CREW DECLARED A PAN PAN TO HAVE FIRE TRUCKS TO DO A BRAKE INSPECTION ON ARRIVAL. FLIGHT TAXIED INTO GATE SHORTLY AFTER LANDING. RESOLUTION REF FIM 45-45-00-810-942May 9, 2019 · Emb ERJ190100IGW · Central ComputersSDR CA190429010Trans Rectifier · arced(CAN) UPON ARRIVAL AIRCRAFT EICAS MESSAGES AC STBY BUS OFF, FL CTRL NO DISPATCH AND ELECTRONIC CB`S EMRG FAN EBAY MID AND EMRG FAN EBAY FWD ARE POPPED OUT, WITH FWD EBAY FANS FAIL AND CENTER EBAY FANS FAIL EICAS MESSAGES. RESOLUTION TRU #1 REPLACED AS PER Apr 29, 2019 · Emb ERJ190100IGW · DC Rectifier/ConverterSDR CA190425010Processor · failed(CAN) CREW GOT AN AVIONICS MAU 1A FAIL. ALONG WITH THIS MESSAGE, THE QRH STATES THAT THEY MAY HAVE PRESSURE ISSUES THAT MAY AFFECT NOSE WHEEL STEERING, OUTBOARD BRAKING. WE HAVE CONFIRMED WITH THE CREW THAT THEY WILL NOT DECLARE A PAN PAN OR MAYDAY, BUT CREW AApr 22, 2019 · Emb ERJ190100IGW · Central ComputersSDR CA190304003Bleed Valve · failed(CAN) LEFT WITH ONE BLEED AIR SYSTEM UNDER MEL. ENROUTE, THE OTHER BLEED AIR SYSTEM FAILED. MTC SUGGESTED THAT THE AIRCRAFT SHOULD RETURN RESOLUTION REPLACED NAPRSOV AS PER AMM 36-11-03-000-801-A ON LEAK CHK FOUND LOWER SEALS LEAKING INSTALLED NEW SEALS. REPLMar 1, 2019 · Emb ERJ190100IGW · Pneumatic Distribution SystemSDR CA190225007Motor · failed(CAN) CREW CONTACTED MOC CONCERNING A WIPER PROBLEM. MOC GAVE CREW CB RESET AND CREW DID THE RESET AND TRIED THE WIPERS AGAIN. THE MOTOR STARTED BUT THE WIPERS DID NOT MOVE. THE CAPTAIN SAID HE SMELLED AN ODOUR AS DID THE F/O. THE FIRST OFFICER SAID THAT HE SAFeb 24, 2019 · Emb ERJ190100IGW · Windshield/Door Rain/Ice RemovalSDR CA190225009Flight Dir · failed(CAN) FLIGHT REJECTED TAKE-OFF AT 20KTS DUE TO AN AUTO THROTTLE FAIL/FLIGHT DIRECTOR FAIL MESSAGE. RESOLUTION AFTER CONSULTING MOC AND RE-ENGAGING AT SYSTEM THE SYSTEM WORKED CORRECTLY. (EICAS HAD CLEARED AFTER T/O REJECTED). (TC# 20190225009)Feb 24, 2019 · Emb ERJ190100IGW · Flight Management Computing Hardware SystemSDR 7AHR2018092500000Nut · crackedREPLACED CRACKED NUT ON NR 2 PYLON PER AMM 54-50-00-000-803-A. OPENED NR 2 RT PYLON ACCESS PANEL. INSTALLED NR 2 RT PYLON PANEL.Sep 25, 2018 · Emb ERJ190100IGW · Nacelle/Pylon Miscellaneous StructureSDR CA180223004Sensor · failed(CAN) IN CRUISE CREW HAD FLAP LOW RATE ON EICAS. RESOLUTION CMC INTERROGATED & FOUND FAULT CODE 27534019ACE AND 27512009ACE C/O FIM TASK 27-53-00-810-840-A. REPLACED LT WING OUTBOARD FLAP SKEW SENSOR (POS NR 4) IAW AMM 27-53-06/401. FLAP LOW RATE MSG CLEAREFeb 22, 2018 · Emb ERJ190100IGW · Trailing Flap Position Indicating SystemSDR CA160317007Skin · cracked(CAN) DURING SURFACE PREPARATION FOR TREATMENT, A CRACK WAS FOUND ON RT WING LOWER TRAILING EDGE SKIN INBOARD OF RIB 4 AFT OF SPAR II.Mar 16, 2016 · Emb ERJ190100IGW · Wing, Plate/SkinSDR CA160310010Sensor · failed(CAN) CREW REPORTED THEY HAD A SLAT FAIL ON APPROACH. RESOLUTION FIM TASK 27-83-00-810-814-A CARRIED OUT. FOUND SLAT SKEW SENSOR (OUTBOARD) 2/3 RESISTANCE OUT OF LIMIT. REPLACED IAW AMM 27-83-01 PB 401. SLAT SYSTEM CHECK SERVICEABLE.Mar 10, 2016 · Emb ERJ190100IGW · Leading Edge Slat Position Indicating SystemSDR CA160229002Actuator · failed(CAN) DECLARED A PAN PAN DUE TO A FLAP ISSUE. RT I/B FLAP ACTUATORS 1R AND 2R FOUND TRIPPED. RESET OPERATED WITH NO FAULTS. MOC REQUEST TO REPLACE BOTH ACTUATORS. RT I/B CANOE REMOVED FLAP DRIVE 2R REPLACED IAW AMM 27-51-01 PB 401 AND ADJUSTED IAW AMM 27-50-0Feb 27, 2016 · Emb ERJ190100IGW · Trailing Edge Flap ActuatorSDR CA160120020Warning System · false activation(CAN) DURING DEPARTURE CREW RECEIVED ENGINE VIBRATION WARNING IN CLIMB. IN CRUISE THE WARNING CONTINUED. AFTER CONSULTATION WITH MOC AND DISPATCH IT WAS DECIDED TO DIVERT. NR 2 ENGINE GND RUN TO T/O POWER ENGINE VIBRATION TEST COMPLETED IAW EMM 72-00-00-760-1Jan 20, 2016 · Emb ERJ190100IGW · Engine Vibration AnalyzerSDR CA160119019Window · cracked(CAN) AFTER DEPARTURE CREW REPORTED FIRST OFFICERS WINDOW HAD CRACKED. THE CREW ELECTED TO RETURN TO DEPARTURE AIRPORT. NO EMERGENCY WAS DECLARED TO ATC. FLIGHT LANDED WITHOUT FURTHER INCIDENT. RESOLUTION RT WINDSHIELD REPLACED ON J/C IAW 39-56-01-00-001AC-02Jan 19, 2016 · Emb ERJ190100IGW · Flight Compartment WindowsSDR CA160118007Uplock · failed(CAN) AFTER GEAR RETRACTION THE CREW REPORTED A BANGING NOISE FROM THE NOSE GEAR AREA AND THE GEAR WOULD MOMENTARILY INDICATE IN TRANSIT. THE CREW DID NOT DECLARE ANY LEVEL OF EMERGENCY BUT REQUESTED THE FIRE TRUCKS ATTEND AS A PRECAUTION. AIRCRAFT WAS APPROXIJan 17, 2016 · Emb ERJ190100IGW · Landing Gear Retraction/Extension SystemSDR CA160118006Oxygen Mask · unwanted deploy(CAN) WHILE IN CRUISE, BOTH F/A OXYGEN MASKS DEPLOYED WITH A FAULT LIGHT ON THE F/A PANEL. NO PRESSURIZATION ISSUES OR TURBULENCE REPORTED AT THE TIME. RESOLUTION RESEATED&STOWED F/A`S L2&R2 MASK.OP`S OK PER AMM 35-20-07.Jan 16, 2016 · Emb ERJ190100IGW · Passenger Oxygen SystemSDR CA160111002Heat Exchanger · contaminated(CAN) FLIGHT DEPARTED, AT 1500FT CABIN AND COCKPIT HAD A STRONG SMOKE ODOUR IN THE FORM OF A WHITE POWDER COME THROUGH THE VENTS. PASSENGERS AND CREW EXPERIENCED EYE AND THROAT IRRITATION. COCKPIT CREW DONNED OXYGEN MASKS AND DECLARED A MAYDAY WITH ATC. FLIGHTJan 9, 2016 · Emb ERJ190100IGW · Cabin Cooling SystemSDR CA151210003Sensor · failed(CAN) ON APPROACH CREW HAD A SLAT FAIL. FLIGHT DECLARED A PAN PAN WITH ATC FLIGHT LANDED AND WAS MET BY CFR. FLIGHT TAXIED TO GATE WITH NO FURTHER INCIDENT. RESOLUTION C/O FIM 27-80-00-810-802-A AND FIM 27-83-00-810-814-A. REPLACED RT SLAT POSITION SENSOR UNIDec 10, 2015 · Emb ERJ190100IGW · Leading Edge Slat Position Indicating SystemSDR CA151214009Link · worn(CAN) FORWARD MOUNT LINK SPHERICAL BEARING FOUND WORN DURING ENGINE CHANGE.Dec 8, 2015 · Emb ERJ190100IGW · Engine Mount SectionSDR CA151214005Link · worn(CAN) FORWARD MOUNT LINK SPHERICAL BEARING FOUND WORN DURING ENGINE CHANGE.Dec 6, 2015 · Emb ERJ190100IGW · Engine Mount SectionSDR CA151127013Proximity Sensor · failed(CAN) AFTER DEPARTURE THE FLIGHT CREW WERE UNABLE TO RAISE THE LANDING GEAR. THE FLIGHT CREW RETURNED AND THERE WAS NIL ADVERSE PASSENGER REACTION. RESOLUTION FIM 32-61-00-810-840A CARRIED OUT. NLG WOFW PROX SENSOR P36 REPLACED PER AMM 32-61-01 PB401. LANDINGNov 27, 2015 · Emb ERJ190100IGW · Landing Gear Position and WarningSDR CA151118003Loop · failed(CAN) DEPARTING, CLIMBING THROUGH 8000`, THE CREW RECEIVED AN ALERT, BLEED 2 LEAK. WHILE PERFORMING THE CHECKLIST FOR THAT FAILURE, THEY RECEIVED A SECOND ALERT, WING ANTI ICE FAIL THROUGH 13,000`. THE DECISION WAS MADE TO RETURN AS THEY WERE CLIMBING INTO ICINov 17, 2015 · Emb ERJ190100IGW · Pneumatic Indicating SystemSDR CA151116006Control Valve · failed(CAN) ON TAKEOFF AND LANDING THERE WAS A BURNING ODOR DETECTED BY THE CREW. NO SIGN OF VISIBLE SMOKE. A PAN PAN WAS DECLARED. LOCAL MTCE IS INVESTIGATING. RT PACK FLOW CONTROL VALVE, RT PACK BYPASS VALVE FILTERS REPLACED AS PER AMM 21-51-01 AND 21-51-00 RESPENov 14, 2015 · Emb ERJ190100IGW · Cabin Cooling SystemSDR CA151210007Mount · worn(CAN) FORWARD MOUNT LINK SPHERICAL BEARING FOUND WORN DURING ENGINE CHANGE.Oct 22, 2015 · Emb ERJ190100IGW · Engine Mount SectionSDR CA151022003Deflector · failed(CAN) SHORTLY AFTER TAKEOFF THE CREW CREW REPORTED A BANG AND SOME VIBRATION FELT THROUGH THE AIRCRAFT. THE FLIGHT CONTINUED AT 10000FT AS A PRECAUTION AGAINST A POSSIBLE DOOR/PRESSURIZATION ISSUE. FORWARD PASSENGER DOOR DEFLECTOR REPLACED IAW AMM 52-11-28.Oct 21, 2015 · Emb ERJ190100IGW · Passenger/Crew DoorsSDR CA151001009Sensor · failed(CAN) LANDING GEAR WILL NOT GO UP. RETURNING TO DEPARTURE AIRPORT. RESOLUTION T/S IAW FIM TASK 32-61-00-810-840-A AND REPLACED STEERING FEEDBACK SENSOR IAW AMM 32-00-01-000-801B AND PROXIMITY SENSOR IAW AMM 32-62-01-400-801A. OPS CHECK NORMAL . OK FOR SERVICEOct 1, 2015 · Emb ERJ190100IGW · Landing Gear Steering SystemSDR CA150925011Module · failed(CAN) ON APPROACH TO RWY AT 700 AGL AIRCRAFT HAD MULTIPLE AMBER WARNINGS SPOILER FAULT STICK SHAKER ANTICIPATED AOA FAIL RESOLUTION GENERIC I/O MODULE MAU NR 1 SLOT 11/12 REPLACED IAW AMM 31-41-06 PS401.Sep 25, 2015 · Emb ERJ190100IGW · Central ComputersSDR CA150909008Indicator · malfunctioned(CAN) AIRCRAFT WAS INTERCEPTING FINAL AND HAD SELECTED FLAPS 0 TO 1 AT WHICH POINT THE CREW GOT A SLAT FAIL MESSAGE. THE CREW USED THEIR QRH AND CLEARED THE FAULT WHILE THEY LEVELED OFF. ONCE FAULT WAS CLEARED THEY CAME AROUND AND DID THE VISUAL TO RWY 14R. RSep 7, 2015 · Emb ERJ190100IGW · Leading Edge Slat Position Indicating SystemSDR CA150821007Wire Harness · loose(CAN) ON DEPARTURE THE GEAR FAILED TO RETRACT. THE CREW CONSULTED WITH MTCE AND ELECTED TO RETURN. AN UNEVENTFUL LANDING WAS CONDUCTED. FOUND NLG PROX HARNESS P41 IN WHEEL WELL LOOSE. RETIGHTENED CANON PLUG. PROX SENSORS CHECKED IAW 32-62-01-820-801-A & AIR/Aug 21, 2015 · Emb ERJ190100IGW · Landing Gear System WiringSDR CA150819001Unknown · odor(CAN) SHORTLY AFTER DEPARTURE BACK END CREW REPORT AN ELECTRICAL ODOR, CAPT ELECTED TO DIVERT AND LANDED WITHOUT FURTHER INCIDENT...NO EMERGENCY DECLARED WITH ATC. TAXIED TO THE GATE UNDER OWN POWER. RESOLUTION NO ODOUR OF SMOKE OR ABNORMAL SMELL IN CABIN UPAug 18, 2015 · Emb ERJ190100IGW · Air Distribution SystemSDR CA150819003Flap System · malfunctioned(CAN) ON FINAL FOR RWY CREW EXPERIENCED A FLAP ISSUE AND INITIATED A GO AROUND, CREW CARRIED OUT QRH CHECKLIST AND ISSUE WAS RESOLVED. CAME BACK AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED WITH ATC. FIM22-31-00-810-806A(AT-INVALID DATA-FLAPAug 18, 2015 · Emb ERJ190100IGW · Trailing Edge Flap Control SystemSDR CA150814003Motor · failed(CAN) PAN PAN DECLARED WITH ATC DUE TO FLAP FAIL. FAULT CODE 27512014ACE RETRIVED FROM CMC FIM PROCEEDURE 27-51-00 COMPLETED TO BOX NR 8 NIL FAULTS R/H FPDU MOTOR REPLACED AS PER AMM 27-53-03 SYST OPS OK NORMAL.Aug 13, 2015 · Emb ERJ190100IGW · Trailing Edge Flap ActuatorSDR CA150805006Pump · failed(CAN) AIR RETURN DUE TO HYDRAULIC 2 SHOWING 0 QTY,NO PRESSURIZATION., REQUIRING TOW OFF,PAN PAN DECLARED. NR 2 ENG EDP REPLACED AS PER AMM 29-11-01-401. NR 2 SYSTEM MANIFOLD PRESSURE AND CASE DRAIN FILTERS REPLACED AS PER AMM 29-11-05-401 OPS CHECK AND LEAK CAug 5, 2015 · Emb ERJ190100IGW · Hydraulic Pump (Electric/Engine), MainSDR CA150806003Processor · failed(CAN) DUEL BLEED FAILURE ENROUTE, MADE AN EMERGENCY DESCENT TO F200,DIVERTING MASKS DID DROP AT CABIN ALTITUDE 14400FT. AMS CONTROLLER PROCESSOR MODULE SLOT 25 FROM SPDA2 REPLACED IAW 21-00-01-000/400-801-A TESTED NFF.Aug 5, 2015 · Emb ERJ190100IGW · Cabin Pressure Control SystemSDR CA150805002Processor · failed(CAN) STEERING FAIL ON APPROACH. GO-AROUND INITIATED. IAW FC- 45452145CMC AND FIM 45-45-00-810-941-A. FAULT ISOLATION PROCEDURE C/OUT. NIC + PROCESSOR MODULE NR 3 (MAU NR 2, NIC NR 1) REPLACED IAW AMM TASK- 31-41-04-000/400-801-A.Aug 4, 2015 · Emb ERJ190100IGW · Central ComputersSDR CA150803003Pump · failed(CAN) AT APPROX 2315Z AC PATCHED THROUGH TO MOC VIA DISPATCH REGARDING LOSS OF THEIR NR 2 HYDRAULICS, WILL CONTINUE BUT WILL DECLARE AN EMERGENCY THROUGH ATC FOR THE ARRIVAL...TOWER CONTACTED AND STATION ORGANIZED A TOW TO GET AIRCRAFT OFF THE RUNWAY. NR 2 HYAug 2, 2015 · Emb ERJ190100IGW · Hydraulic Pump (Electric/Engine), MainSDR CA150731008Pump · failed(CAN) AT CRUISE AIRCRAFT EXPERIENCED HYDRAULIC SYSTEM 1 FAILURE MESSAGE, ALONG WITH A LOW PRESSURE AND LOW QUANTITY INDICATION. DECLARED PAN PAN WITH ATC, AFTER LANDING AIRCRAFT TAXIED TO THE GATE UNDER OWN POWER. CRF WAS ADVISED AND PRESENT. EDP REMOVED PER Jul 31, 2015 · Emb ERJ190100IGW · Hydraulic Pump (Electric/Engine), MainSDR CA150720011Windshield · cracked(CAN) DURING CRUISE THE CAPTAINS WINDSCREEN CRACKED. THE FLIGHT RETURNED. CAPT WINDSHIELD REPLACED IAW TASK CARD 39-56-01-00-001AC-01.Jul 19, 2015 · Emb ERJ190100IGW · Flight Compartment WindowsSDR CA150716001Io Card · failed(CAN) FLIGHT TAXIED TO GATE. WHILE ENGS WERE OFF AT GATE, CREW OBSERVED A 3S FIRE INDICATION. THIS OCCURRED 3 TIMES, DURING 3RD EVENT, CREW WAS PREPARED TO FIRE THE BOTTLE. CREW OBSERVED NO PHYSICAL SMOKE OR FIRE FROM NR 1 ENG, NO BOTTLE WAS FIRED. PAX DISJul 16, 2015 · Emb ERJ190100IGW · Central ComputersSDR CA150714002Shutoff Valve · failed(CAN) FLIGHT DEPARTED WITH LT ENG BLEED INOPERATIVE. AFTER DEPARTURE THE RT ENG BLEED FAILED, ATTEMPTS TO RESET WERE UNSUCCESSFUL. FLIGHT DIVERTED FOR MX. LANDING WEIGHT WAS BELOW MAXIMUM LANDING WEIGHT. RESOLUTION NR 2 ENG PRSOV REPLACED IAW AMM 36-11-01 Jul 11, 2015 · Emb ERJ190100IGW · Pneumatic Distribution SystemSDR CA150702001Control Lever · failed(CAN) ON DEPARTURE THE CREW WAS UNABLE TO SELECT GEAR UP. THEY WERE UNABLE TO MOVE THE LANDING GEAR LEVER. AFTER COMPLETING THEIR QRH AND CONSULTING WITH MTCE THE CREW ELECTED TO RETURN. THE AIRCRAFT WAS 200KGS ABOVE MAX LANDING WEIGHT AND LANDED WITHOUT FURTHJun 30, 2015 · Emb ERJ190100IGW · Landing Gear SelectorSDR CA150702002Valve · failed(CAN) DURING CRUISE THE PARKING BRAKE ON LIGHT ILLUMINATED. AFTER CONSULTATION WITH MTCE THE LIGHT WENT OUT. AS A PRECAUTION THE CREW ELECTED TO DECLARE A PAN PAN AND HAVE CFR ON STAND BY FOR THEIR ARRIVAL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. RESOLUTIJun 30, 2015 · Emb ERJ190100IGW · Landing Gear Brake SystemSDR CA150629020Actuator · failed(CAN) ON APPROACH TO AIRPORT THE CREW DID A GO AROUND DUE TO A SLAT FAIL. THE CREW COMPLETED THE CHECKLIST & CONDUCTED AN UNEVENTFUL LANDING. RESOLUTION COMPLIED WITH FIM TASK 27-81-00-810-802-A. FOUND RT NR 8 SLAT ACTUATOR TORQUE LIMITER INDICATOR TRIPPED.Jun 28, 2015 · Emb ERJ190100IGW · Leading Edge Slat ActuatorSDR CA150623010Controller · failed(CAN) AFTER TAKEOFF CREW REPORTED A WINDSHIELD HEAT FAILURE. DUE TO CONVECTIVE ACTIVITY EN ROUTE & FORECAST THE FLIGHT IS RETURNING. LANDING WEIGHT WILL BE BELOW MAXIMUM. RESOLUTION IAW FAULT CODE 30420030AI1, WINDSHIELD HEATER CONTROL REPLACED IAW AMM 30-4Jun 23, 2015 · Emb ERJ190100IGW · Windshield/Door Rain/Ice Removal
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