Embraer ERJ 190-200 LR

Service difficulty reports · 49

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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 aircraft_model_key = 'ERJ190200LR'
  ORDER BY difficulty_date DESC"

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SDR R61A2026062900182Power Supply · inoperativeCREW REPORTS 2 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED ELPU #2.Jun 29, 2026 · N748YX · Emb ERJ190200LR · Emergency LightingSDR R61A2026062700179Engine · faultedENG 2 FAIL AROUND 10,000 FT. N1 WENT TO 15.2. HIGH ENG VIB, ENG #2 ITT GAUGE TURNED RED. UPON LANDING ENG #2 EXCEEDANCE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENG #2.Jun 27, 2026 · N411YX · Emb ERJ190200LR · Engine (Turbine/Turboprop)SDR R61A2026062400171Engine · vibrationLOW PRESSURE VIBRATION NR 2 ENGINE AT ALTITUDE. RAN QRH, DESCENDED AND REDUCED SPEED, VIBRATIONS IN GREEN AT 3.0. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. INSPECTED ENG NR 2 FAN BLADES AND FOUND NO DEFECTS. PLACED ENGINE NR 2 ON NON-MEL DMI FOR FAN MX WIJun 24, 2026 · N111HQ · Emb ERJ190200LR · Engine (Turbine/Turboprop)SDR EE4Y2025110523420Rib · corrodedDURING THE ACCOMPLISHMENT OF TASK CARD 57-50-033-1295, AZORRA AVIATION IDENTIFIED CORROSION ON THE RH WING IINBOARD FLAP RIB 1 LOWER FLANGE. THIS CONDITION WAS REPORTED ANDREPAIRED IAW ETD2025-190-925075 DTD JUL 24 2025 AND DOCUMENTED BY COOPESA COO-EO-2025-22Nov 5, 2025 · N688DR · Emb ERJ190200LR · Wing, Rib/BulkheadSDR EE4Y2025110523419Rib · corrodedDURING THE ACCOMPLISHMENT OF TASK CARD 57-50-033-1295, AZORRA AVIATION IDENTIFIED CORROSION ON THE RH WING INBOARD FLAP RIB 1 LOWER FLANGE. THIS CONDITION WAS REPORTED AND REPAIRED IAWETD2025-190-925074 DTD JUL 24 2025 AND DOCUMENTED BY COOPESA COO-EO-2025-227Nov 5, 2025 · N688DR · Emb ERJ190200LR · Wing, Rib/BulkheadSDR EE4Y2025100623293Inlet · dentedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND P/N 341-1010-511A, S/N 1395001, AIR INLET MODULE WITH SEVERAL DENTS ON THE INNER BARREL UPPER AND LOWER ACOUSTIC PANELS. THE DENTS WERE EVALUATED AS PER SRM 71-61-01/AD53. MOST OF THE DENTS ARE BEYOND THE LIMITS FOct 6, 2025 · N688DR · Emb ERJ190200LR · Engine Air Intake SystemSDR EE4Y2025100623292Inlet · dentedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND P/N 341-1010-509F, S/N 1192001, AIR INLET MODULE WITH SEVERAL DENTS ON THE INNER BARREL UPPER AND LOWER ACOUSTIC PANEL. THE DENTS WERE EVALUATED AS PER REF. SRM 71-61-01/AD53. MOST OF THEM ARE BEYOND THE LIMITS FOOct 6, 2025 · N688DR · Emb ERJ190200LR · Engine Air Intake SystemSDR EE4Y2025100623291Skin · damagedAZORRA REPORTS THAT DURING THE STRUCTURE INSPECTION, WE FOUND THE CENTER FUSELAGE I – AT FR31+380MM, S-26R+30MM EXTERNAL SKIN WITH LIGHTNING STRIKE. THE DAMAGE WAS REMOVED BY DRILLING A HOLE (Ø4.0MM). THIS CONDITION WAS REPORTED AND REPAIRED IAW ETD2025-190-92Oct 6, 2025 · N688DR · Emb ERJ190200LR · Fuselage Main, Plate/SkinSDR EE4Y2025100623290Skin · damagedAZORRA REPORTS THAT DURING THE STRUCTURE INSPECTION, WAS FOUND THE CENTER FUSELAGE I – AT FR27+370MM, S-26R+60MM EXTERNAL SKIN WITH LIGHTNING STRIKE. THE DAMAGE WAS REMOVED BY DRILLING A HOLE (Ø4.0MM). DURING THE DOCUMENT CLOSING PROCESS, THE DAMAGE WAS LOCATEOct 6, 2025 · N688DR · Emb ERJ190200LR · Fuselage Main, Plate/SkinSDR EE4Y2025100623289Skin · damagedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND ON FORWARD FUSELAGE, AT FR18+18MM AND STGR-26R+85MM, EXTERNAL SKIN WITH A LIGHTNING STRIKE DAMAGE. EVALUATED THOUGH DAMAGE AND FOUND OUT OF LIMITS IAW ERJ190, PART II SRM 53-10-01, AD53, PARAGRAPH 4.B.(3): THE DISOct 6, 2025 · N688DR · Emb ERJ190200LR · Fuselage Main, Plate/SkinSDR EE4Y2025100623288Skin · damagedDURING THE MAINTENANCE ACTIVITIES AN EXISTING BLEND OUT WAS FOUND, IT IS LOCATED ON REAR FUSELAGE AT FR94+240MM, BTWN STRG 23R-25R. EVALUATED BLEND OUT WITH CLAD LAYER PENETRATED AND FOUND OUT LIMITS PER ERJ190 PART II SRM 53-30-01, AD 51, FIGURE 104, SHEET 4 Oct 6, 2025 · Emb ERJ190200LR · Fuselage Main, Plate/SkinSDR EE4Y2025100623287Skin · scratchedDURING THE STRUCTURAL INSPECTION IT WAS FOUND ON FORWARD FUSELAGE, RH-LATERAL SEAT TRACK FROM FR19 TO FR20 OTBD CROWN AREA WITH SCRATCH. EVALUATED BLEND OUT AREAS AND FOUND OUT OF LIMITS PER ERJ190, PART II SRM 53-10-10, AD51, PARAGRAPH 4.B. (NO DAMAGES AREA AOct 6, 2025 · N688DR · Emb ERJ190200LR · Fuselage Main, Plate/SkinSDR EE4Y2025091723170Skin · damagedDURING STRUCTURE INSPECTION, FOUND FWD FUSELAGE, FR 18+50MM, & S27L + 155MM (JUST 8.0MM FROM STR 28L FASTENER ROW), EXTERNAL SKIN WITH LIGHTNING STRIKE WITH EXISTING BLEND OUT. BLEND OUT WAS EVALUATED & CLASSIFIED AS NON-SIGNIFICANT IAW SRM 51-75-16. LIGHTNSep 17, 2025 · N688DR · Emb ERJ190200LR · Fuselage Main, Plate/SkinSDR EE4Y2025091723168Skin · damagedCENTER FUSELAGE I SKIN HAS A LIGHTNING STRIKE DAMAGE AT FRAME 30+290MM AND STRINGER 27R. SEE FIGURE 1. THE DAMAGE WAS REMOVED BY BLENDING AND WAS FOUND BEYOND LIMITS PER SRM 53-21-01/AD 51. SINCE THE DAMAGE IS LOCATED IN THE NOT ALLOWED REPAIR AREA (GREY AREA)Sep 17, 2025 · N688DR · Emb ERJ190200LR · Fuselage Main, Plate/SkinSDR EE4Y2025091723167Heat Shield · misrepairedDURING THE STRUCTURE INSPECTION, AN EXISTING REPAIR WAS FOUND INSTALLED WITHOUT RECORDS AT RH ENGINE PYLON HEAT SHIELD BAY #8. DUE TO THIS FACT, THE REPAIR WAS REMOVED. THIS CONDITION WAS REPORTED AND REPAIRED IAW ETD2025-190-926307 DTD AUG 08 2025 AND DOCUMENSep 17, 2025 · N688DR · Emb ERJ190200LR · Nacelle/Pylon, Main FrameSDR EE4Y2025091723166Seat · corruptedPER CUSTOMER REQUEST, PASSENGER CABIN SEATS DIAPHRAGMS 41191032-35, 41191032-36, 41191032-37, 41191032-38 WERE FOUND WITH CRACKS AND MUST BE REPAIRED.THE CONDITION REPORTED WAS REPAIRED IAW ETD2025-190-924987 REV. B, AND COOPESA COO-EO-2025-23053,Sep 17, 2025 · N688DR · Emb ERJ190200LR · Passenger Compartment EquipmentSDR EE4Y2022052315569Skin Panel · nickedLOWER CENTER FUSELAGE I, EXTERNAL SKIN WITH NICKS LOCATED FROM FR29 AND FR30 BETWEEN STRINGER 26LH AND STRINGER 27LH. NOTA: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER INSTRUCTIONS. ( FOR ADDITONAL DETAILS SEE COOPESA JOB: A1M007 SPECIAL ITEM: 21-48 ).May 23, 2022 · N140BZ · Emb ERJ190200LR · Fuselage Main, StructureSDR EE4Y2022052315568Fitting · crackedRH WING SPAR II, SPOILER #5 INBOARD SIDE FITTING CRACKED. NOTE: THE SPOILER FITTING WAS REPLACED AS PER EMBRAER INSTRUCTIONS. ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1M007 SPECIAL ITEM: 6-26 ).May 23, 2022 · N140BZ · Emb ERJ190200LR · SpoilersSDR EE4Y2022052315565Skin Panel · dentedUPPER FORWARD FUSELAGE EXTERNAL SKIN WITH DENT LOCATED AT FR20+10MM BETWEEN STRINGER 12LH AND STRINGER 13LH. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2022-190-012471 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2022-15334 INSTRUCTMay 23, 2022 · N140BZ · Emb ERJ190200LR · Fuselage Main, StructureSDR EE4Y2022052315567Skin Panel · dentedLOWER REAR FUSELAGE , EXTERNAL SKIN WITH DENT AND OIL CAN LOCATED AT FR95+310MM BETWEEN STRINGER 23LH AND STRINGER 25LH. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2022-190-014171 REV:B GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2May 23, 2022 · N140BZ · Emb ERJ190200LR · Fuselage Main, StructureSDR EE4Y2022051115564Skin Panel · dentedUPPER FORWARD FUSELAGE EXTERNAL SKIN WITH DENT AND CREASE LOCATED BETWEEN FR04 AND FR05, BETWEEN STRINGER 10LH AND STRINGER 12LH. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2022-190-014169 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EMay 11, 2022 · N140BZ · Emb ERJ190200LR · Fuselage Main, StructureSDR EE4Y202051115562Skin Panel · dentedUPPER FORWARD FUSELAGE EXTERNAL SKIN WITH DENT, LOCATED AT FR04+265MM, STRINGER 10RH+20MM. NOTE: THE FUSELAGE SKIN PANEL WAS REPAIRED AS PER EMBRAER ETD2022-190-013658 REV:A GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2022-15381 INSTRUCTIONS (May 11, 2022 · N140BZ · Emb ERJ190200LR · Fuselage Main, StructureSDR 3CEY20210817001Retaining Ring · deformedQUICK TURN HPC TOP CASE REPAIR IAW 72-00-00 SP001 AND 72-00-00 SP110 CONDUCTED. DURING THE AFFECTED HPC STG2 & 3 BLADES REMOVAL WE NOTED THE STG2 FWD BLADE RETAINER LUG WEAR AND TIGHT CONDITION. FURTER EXAMINATION REVEALED THAT BLADE RETAINER PN 2031M31G01 HASAug 13, 2021 · Emb ERJ190200LR · Turbine Engine Compressor SectionSDR R61A201909130959Rib · crackedMAJOR: FOUND LT HORIZONTAL RIB 12A CRACK. REMOVED AND REPLACED LT HORIZONTAL STAB RIB 12A PER SRM 51-40-08. APPLIED SURFACE PROTECTION PER SRM 51-23-05, 51-03-06. SEE WIPS FOR WORK PERFORMED. SEE W/O H6951 SN 691 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHSep 6, 2019 · N118HQ · Emb ERJ190200LR · Horizontal Stabilizer, Spar/RibSDR R61A201909130954Door Sill · corrodedWHILE PERFORMING L2 DOOR LOWER BEAM REWORK, CORROSION FOUND ON TOP OF SILL AT AFT GIRT BAR FITTING. REMOVED AND INSTALLED NEW L2 DOOR LOWER BEAM REF: SRM 51-40-08. SEE W/O H6951 SN 606 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.Aug 27, 2019 · N118HQ · Emb ERJ190200LR · Fuselage Miscellaneous StructureSDR R61A201901200090Beam · corrodedWHILE PERFORMING 2236:170EO-53-14-0002-170EO-53-14-0002 L1 DOOR LOWER BEAM REWORK FOUND CORROSION AROUND NUTCLIP FASTENER HOLE. REMOVED AND REPLACED L1 LOWER BEAM REF. SRM 51-40-08. RESTORED SURFACE PROTECTION REF. SRM 51-23-04, 51-23-05, AND 51-23-06. SEE W/Jan 2, 2019 · N216JQ · Emb ERJ190200LR · Fuselage Main, StructureSDR MASA2018101311443Battery · dischargedAFT FA FLASHLIGHT INOP. REPLACED BATTERY.Oct 13, 2018 · N85351 · Emb ERJ190200LR · Emergency EquipmentSDR MASA2018052713259Flashlight · inoperativeFWD FA FLASHLIGHT INOP. PLACED ON MEL.May 27, 2018 · N89357 · Emb ERJ190200LR · Emergency EquipmentSDR MASA2018052613257Battery Pack · dischargedFWD FA FLASHLIGHT RED LIGHT NOT BLINKING. REPLACED BATTERY PACK.May 26, 2018 · N86312 · Emb ERJ190200LR · Emergency EquipmentSDR R61A201804110489Doubler · corrodedLT FLOOR DOUBLER CORRODED AS MARKED FR 80. REMOVED AND REPLACED FR 80 STGR 26R - 28R REF SRM 51-40-08, SRM 51-40-02.Mar 20, 2018 · N880RW · Emb ERJ190200LR · Fuselage Miscellaneous StructureSDR R61A201802190286Splice · corrodedWHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, MAINTENANCE FOUND LEVEL 2 CORROSION AT AFT WET AREA LT OUTBD SPLICE PLATE AFT OF L2. THEY REMOVED AND REPLACED SPLICE IAW SRM 51-42-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.Feb 19, 2018 · N209JQ · Emb ERJ190200LR · Fuselage Miscellaneous StructureSDR R61A201711080820Rib · crackedMAJOR REPAIR FCBS 55-10-00-005, CRACKED RIBS ON RT HORIZONTAL STABILIZER BETWEEN FRONT SPAR AND MID SPAR. REMOVED AND REPLACED RIB 11 AND 12 ON RT HORIZONTAL STAB BETWEEN FRONT AND MID SPAR.Oct 19, 2017 · N125HQ · Emb ERJ190200LR · Horizontal Stabilizer, Spar/RibSDR R61A201702200145Floor Support · corrodedFLOOR SUPPORT AT FRAME 18 LBL 30 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01.Feb 6, 2017 · N867RW · Emb ERJ190200LR · Fuselage Miscellaneous StructureSDR SIMA20160524002Seal · defectiveMAIN DOOR HOLD OPEN LATCH INOPERATIVE. TRIMMED EXCESS MATERIAL FROM DUST SEAL AS REQUIRED. OPERATIONS CHECKED GOOD.May 24, 2016 · N233NN · Emb ERJ190200LR · Passenger/Crew DoorsSDR C77A20151120002Doubler · corrodedCORROSION ON SEVERAL AREAS OF FWD CABIN AFT LT FLOOR DOUBLER, PN 170-07311-001 AT FRAME 19, BETWEEN Y= -304 THRU - 850, X=5645. R & R LT AFT DOUBLER IAW SRM 51-41-01 & 51-43-01 ON WO 19451651E1 IAW EO E175-5300-128 REV IR WO 1980904.Nov 19, 2015 · N616CZ · Emb ERJ190200LR · Fuselage Miscellaneous StructureSDR C77A2015031200001Floor Support · corrodedAFT CABIN RT FLOOR SUPPORT HAS CORROSION AT FRAMES 86 - 89, Y 260.4. R & R THE FLOOR SUPPORT IAW SRM 51-41-02 & 51-43-01.Mar 12, 2015 · N603CZ · Emb ERJ190200LR · Fuselage Miscellaneous StructureSDR C77A201503050021Skin · corrodedCORROSION ON FUSELAGE SKIN INNER SURFACE AT AFT CARGO COMPARTMENT BETWEEN FRAME 80 & 81, STATION 21446 & OTBD SIDE OF STRINGER 28R. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 6213041M3 IAW 15-170-017453 & EA E175-53-485 REV IR WO 1834666Mar 2, 2015 · N602CZ · Emb ERJ190200LR · Fuselage Main, Plate/SkinSDR C77A20150305016Upper Sheet · corrodedAFT CABIN RT UPPER SHEET, PN 170-86101-001 HAS CORROSION BETWEEN FRAME 85 & 86, X= 23041 - 23453, Y=260.4. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 6213171J4 IAW ETD 015-170-016788 & EO E175-5300-100 REV IR WO 1834035.Mar 2, 2015 · N602CZ · Emb ERJ190200LR · Fuselage Miscellaneous StructureSDR C77A20150305005Door Sill · corrodedFORWARD CABIN RT FWD FLOOR SILL, PN 170-05663-003, HAS CORROSION BETWEEN FRAME 13 & 14, X=4011 - 4270, Y=939.8 TO Y=1244.6. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 14680921H1 IAW ETD 2015-170-016753A & EO E175-5300-101 REV IR WO 1834324.Mar 2, 2015 · N602CZ · Emb ERJ190200LR · Fuselage Miscellaneous StructureSDR C77A20140121013Panel Support · corrodedAFT CABIN FLOOR LT PANEL SUPPORT, PN 170-86139-005, IS CORRODED X 24868.0, Y -838. R & R LT PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WORK ORDER 737209-245 IAW EO E175-5300-097 REV IR WORK ORDER 906482.Jan 19, 2014 · N622CZ · Emb ERJ190200LR · Fuselage Miscellaneous StructureSDR C77A20140121003Panel Support · corrodedAFT CABIN FLOOR RT PANEL SUPPORT, PN 170-66797-001 FWD PANEL SUPPORT HAS CORROSION AT X 4000 Y 718. R & R RT PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WORK ORDER 737209-216 IAW EO E175-5300-097 REV IR WORK ORDER 906482.Jan 19, 2014 · N622CZ · Emb ERJ190200LR · Fuselage Miscellaneous StructureSDR R61A201307240659Rib · crackedDURING HEAVY CHECK, REPORTED SECOND INBD BRACKET ON LT HORIZONTAL STAB L/E CRACKED. MX REPAIRED RIB 5 ON LT HORZONTAL STAB L/E, PN 170-62334-001, RIB 5. ACFT REMAINS FOR COMPLETION OF HEAVY CHECK.Jul 24, 2013 · N111HQ · Emb ERJ190200LR · Horizontal Stabilizer, Spar/RibSDR R61A201304060403Skin · buckledWHILE PERFORMING MAINTENANCE IN HEAVY CHECK MAINTENANCE DAMAGED SKIN AFT LOWER FUSELAGE JACK PAD AREA. MAINTENANCE REPAIRED SKIN IAW EMB ETD 2013-170-006071 AND TI170-13-033. THIS WAS A MAJOR REPAIR. ITEMS REMOVED AND REPLACED WITH THE SKIN REPAIR ARE NON-FApr 6, 2013 · N134HQ · Emb ERJ190200LR · Fuselage Main, Plate/SkinSDR R61A201212090737Support · gougedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE NOSE LANDING GEAR ACTUATOR SUPPORT GOUGED FORWARD EDGE INBOARD SIDE. MAINTENANCE BLENDED OUT DAMAGE IAW EMB ETD 2012-170-018181 NOSE LANDING GEAR ACTUATOR SUPPORT FORWARD EDGE INBOARD SIDE. "MAJOR REPAIDec 9, 2012 · N102HQ · Emb ERJ190200LR · Landing Gear ActuatorSDR R61A20120001Service Panel · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND LAVATORY DUMP SERVICE BOX CORRODED. MAINTENANCE REMOVED AND REPLACED LAVATORY SERVICE BOX IAW EMB 175 SRM 51-40-02 AND 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.Dec 29, 2011 · N116HQ · Emb ERJ190200LR · Waste Disposal SystemSDR R61A20110353Door · lack of lubeCREW REPORTED L-2 DOOR DIFFICULT TO ARM/DISARM. MAINTENANCE LUBED AND PERFORMED OPS CHECK OF L-2 DOOR PER EMB AMM, OPS CHECK GOOD.Nov 7, 2011 · N164HQ · Emb ERJ190200LR · Passenger/Crew DoorsSDR R61A20110354Door · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND LAVATORY WASTE SERVICE DOOR CORRODED. MAINTENANCE REMOVED AND REPLACED LAVATORY WASTE SERVICE DOOR IAW EMB 170SRM 51-00-00. AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.Nov 6, 2011 · N118HQ · Emb ERJ190200LR · Service DoorsSDR CA090306002Floorbeam · corroded(CAN) AFT GALLEY FLOOR AREA WAS FOUND WITHOUT SEALANT BETWEEN THE FLOORBOARDS. WITH FLOORBOARDS REMOVED, CORROSION WAS DISCOVERED ON SEVERAL FLOORBEAMS, SEAT TRACKS AND SHEAR PLATES.Feb 27, 2009 · Emb ERJ190200LR · Fuselage Main, Floor BeamSDR R61A20090002Sensor · failedON CLIMBOUT CREW REPORTED, THEY RECEIVED SLAT/FLAP FAIL MESSAGE ON EICAS. CREW DECLARED EMERGENCY FOLLOWED QRH PROCEDURES AND RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO A/C TROUBLESHOT SYSTEM FOUND SLAT 2/3 SKEW SENSOR TO BE BAD. REPLAJan 19, 2009 · N125HQ · Emb ERJ190200LR · Leading Edge Slat Actuator
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