Embraer EMB-135KL

Service difficulty reports · 5,598

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'EMB135KL'
  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 SIMA200415401Battery Pack · inoperativeDLH - FLT 4465 - OPERATIONS REPORTED THE EMERGENCY LGIHTS ON THE AIRCRAFT ARE IN THE ON POSITION AND COULD NOT ACCESS THE COCKPIT. EMERGENCY BATTERY PACKS ARE LOW. REPLACED 4 BATTERY PACKS P/N 2013-1A S/N 73055, P/N 2013-1A S/N 69967, P/N 2013-1A S/N 73159, May 29, 2004 · N800AE · Emb EMB135KL · Emergency LightingSDR CHQA000498Wire · burnedRECEIVED A PITOT 3 INOP EICAS MSG IN THE PROCESS OF COMPLETING THE QRH CHECKLIST. WE SMELLED A DISTINCT ELECTRICAL BURNING SMELL. AT THAT POINT THE FLIGHT ATTENDANT NOTIFIED US OF SMOKE IN THE CABIN AREA. WE DECLARED AN EMERGENCY AND LANDED. MAINTENANCE INMay 23, 2004 · N371 · Emb EMB135KL · Ice/Rain Protection System WiringSDR SIMA200414401Drive Unit · inoperativeDURING LANDING, CREW DECLARED AN EMERGENCY DUE TO FLAP FAIL. FLAPS WERE AT 9 DEGREES AND NO INDICATION WAS SEEN IN COCKPIT. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT FOR FLAPS. OPERATIONAL CHECK WAMay 21, 2004 · N845AE · Emb EMB135KL · Trailing Edge Flap Control SystemSDR SIMA200414202Control Unit · inoperativeMAINTENANCE REPORTED A DUAL PITCH TRIM FAIL ON LANDING AND TWICE ENROUTE PITCH TRIM 1 AND 2 INOPERATIVE. MESSAGE APPEARED FOR 5 SECONDS EACH TIME, THEN WENT OUT. REPLACED HSCU IAW MFG MM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406973)May 19, 2004 · N807AE · Emb EMB135KL · Elevator Tab Control SystemSDR SIMA200413503Charger · inoperativeDISC-EMERGENCY LIGHTS AFT OF EMERGENCY EXIT ROW COME ON AFTER BATTERIES TURNED OFF WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECK GOOD, NO FURTHER DEFECTS. (SW21200406974)May 14, 2004 · N810AE · Emb EMB135KL · Emergency LightingSDR SIMA200413803Engine · vibrationBOS - FLT 4669 - UNUSUAL ABNORMAL VIBRATION AND NOISE FROM NR 1 ENGINE AT 40 PERCENT N1 AND BELOW, CAN BE FELT THROUGH FLOOR, YOKE AND RUDDER PEDALS. ALSO, IN CABIN AREA. ENGINE INSTRUMENTS READ NORMAL. REPLACED NR 1 ENGINE ASSEMBLY IAW W/C 72-000-00. LEAKMay 14, 2004 · N834AE · Emb EMB135KL · Engine (Turbine/Turboprop)SDR SIMA200413502Control Unit · malfunctionedBOS - FLT 4546 - MOMENTARY PITCH 1 AND 2 TRIM INOPERATIVE OCCURRING ON FINAL. FLAP AT 22 DEGREE, GEAR UP. LASTED APPROX 5 SECONDS. REPLACED HSCU. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)May 14, 2004 · N808AE · Emb EMB135KL · Stabilizer Control SystemSDR SIMA200413501Firewall · crackedSAW - FOUND CRACKS ALONG APU FIREWALL WHEN INSTALLING APU. REPLACED APU FIREWALL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)May 13, 2004 · N805AE · Emb EMB135KL · APU Cowling/ContainmentSDR CHQA000488Light · inoperativeLEFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LEFT OVERWING EXTERNAL EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-10. OPS CHECKS GOOD.May 11, 2004 · N378 · Emb EMB135KL · Emergency LightingSDR SIMA200413001Control Unit · inoperativeORD - FLT 4303 - DURING DESCENT, CREW REPORTED PITCH TRIM ONE AND TWO TO BE INOPERATIVE WITH NO EICAS MESSAGE. MAINTENANCE COMPLIED WITH ETN EB 27-022 AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT AND HSCU SHOCK MOUNTS. OPERAITONAL CHECK WAMay 5, 2004 · N814AE · Emb EMB135KL · Stabilizer Control SystemSDR SIMA200412501Control Unit · inoperativePITCH TRIM 1-2 INOPERATIVE ON EICAS AT 520 FT SHORTLY AFTER DISCONNECTING AUTO PILOT. REPLACED HSCU. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406976)May 1, 2004 · N802AE · Emb EMB135KL · Elevator Tab Control SystemSDR SIMA200412107Odor · detectedDURING LANDING, CREW REPORTED SMOKE AND ELECTRICAL ODOR IN COCKPIT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RAN ON GROUND WITH PACKS ON AND NO SMOKE REPORTED. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406986)Apr 29, 2004 · N840AE · Emb EMB135KL · Air Distribution SystemSDR SIMA200410703Pdu · malfunctionedDURING APPROACH WHEN FLAPS WERE SELECTED FROM 9 DEG TO 22 DEG, EICAS MESSAGE (SPS ADVANCED). FLAP POSITION INDICATOR BOX WENT AMBER WITH AMBER DASH WITH NO FLAP INDICATION, RMU PAGE SHOWING NO FLAP INDICATION BUT AMBER DASHES, EICAS DID NOT PRESENT A FLAP FAIApr 15, 2004 · N835AE · Emb EMB135KL · Trailing Edge Flap Control SystemSDR SIMA200409901Connector · looseEMERGENCY FLOOR LIGHTING STRIP INOPERATIVE AT SEAT 16A, ISSUED MEL 33-27. FOUND CONNECTION OF STRIP LIGHTING LOOSE. RE-SECURED AS REQUIRED IAW EMB AMM, MEL RESTORED. AIRCRAFT RETURNED TO SERVICE. (M)Apr 7, 2004 · N832AE · Emb EMB135KL · FastenersSDR CHQA000473Light · inoperativeRT WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT WING EMERGENCY LIGHT IAW EMB 140 MM CH 33-50-07. OPS CHECK GOOD. LAMP P/N GE1317.Apr 4, 2004 · N378 · Emb EMB135KL · Emergency LightingSDR SIMA200408603Control Unit · malfunctionedDFW - FLT 3574 - DURING LANDING ROLL CREW RECEIVED PITCH TRIM 1/2 INOPERATIVE MESSAGE AFTER A/P DISCONNECT. NO PROBLEMS WITH A/P SWITCH BEING STUCK. CREW DID NOT RESET C/B'S. MAINTENANCE REMOVED AND REPLACED THE HORIZ STABILIZER CONTROL UNIT IAW EMB MM AFTEMar 25, 2004 · N805AE · Emb EMB135KL · Stabilizer Control SystemSDR SIMA200408601Control Unit · malfunctionedYYZ- FLT 4904 - DURING APPROACH WHEN AUTO PILOT WAS DISCONNECTED, PITCH TRIM 1-2 INOPERATIVE MESSAGE CAME ON EICAS. STAYED ON FOR A FEW SECONDS THEN WENT OUT. BOTH PITCH TRIM SWITCHES WORKED. LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE COMPLIED WITH ETN EMar 22, 2004 · N813AE · Emb EMB135KL · Stabilizer Control SystemSDR SIMA200408202Control Unit · inoperativeORD - FLT 3972 - ON FINAL RECEIVED PITCH TRIM 1/2 INOPERATIVE WARNING ON EICAS WITH MASTER WARNING. PERFORMED TROUBLESHOOTING PITCH TRIM 1/2 INOPERATIVE IAW FAULT ISOLATION MANUAL AND ETN EB-27-022R1. REPLACED HSCU EMB AMM 27-40-01. OPS CHECK GOOD. A/C RETMar 21, 2004 · N811AE · Emb EMB135KL · Rudder Control SystemSDR SIMA200408201Control Unit · malfunctionedDFW - FLT 3486 - ON APPROACH INTO DFW GOT PITCH BACKUP WARNING AND PITCH MAIN WARNING. REPLACED HSCU IAW ETN EB-27-022. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Mar 20, 2004 · N854AE · Emb EMB135KL · Stabilizer Control SystemSDR SIMA200406805Module · failedNOTIFIED BY MAINTENANCE, EMERGENCY LIGHTS DO NOT TURN OFF AFTER F/A TESTS WITH BATTERIES ON AND EMERGENCY LIGHT ARMED ALSO SHOWING 'EMER LT NOT ARMED' ON EICAS. REPLACED EMERGENCY LIGHT OVERHEAD PANEL MODULE ASSEMBLY. OPS CHECK GOOD. (M)Mar 6, 2004 · N820AE · Emb EMB135KL · Emergency LightingSDR SIMA200406804Control Unit · inoperativeRECEIVED PITCH TRIM, .5 INOPERATIVE MESSAGE. CW ETN EB-27-0022R1 AND REPLACED HSCU OPS CHECKED GOOD. AC RETURNED TO SERVICE. (SW21200404959)Mar 6, 2004 · N811AE · Emb EMB135KL · Elevator Control SystemSDR SIMA200406803Indicator · malfunctionedCREW NOTED AFTER TAKEOFF THAT THE RT FUEL TANK WAS LOOSING ABOUT 300LB PER MINUTE, SO THEY RETURNED FOR MAINTENANCE. INSPECTED RT FUEL SYSTEM AND FOUND NO LEAKS. ALSO CALCULATED FUEL BURN OF LT AND RT ENGINES FOUND TO BE NORMAL. NO DEFECTS NOTED. AC RETURNMar 5, 2004 · N822AE · Emb EMB135KL · Fuel Quantity IndicatorSDR SIMA200405901Access Door · missingDURING POSTFLIGHT WALKAROUND, CREW REPORTED THE APU TAILCONE ACCESS DOOR TO BE MISSING. MAINTENANCE FOUND NO DAMAGE OTHER THAN MISSING PAINT AROUND ACCESS DOOR. THE DOOR WAS REPLACED IAW MM AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200404665)Feb 22, 2004 · N840AE · Emb EMB135KL · Auxiliary Power Unit (APU) DoorsSDR SIMA200405501Fuel Nozzle · brokenDISCOVERED FUMES IN CABIN AND COCKPIT SMELLS LIKE RAW JET FUEL. WALK AROUND INSPECTION REVEALED APU LEAKING FUEL. FOUND BROKEN FUEL NOZZLE. RAI APU FUEL NOZZLE IAW MFG MM. LEAK CHECKED APU, NO LEAKS NOTED AT THIS TIME. (SW21200404647)Feb 20, 2004 · N849AE · Emb EMB135KL · APU Core EngineSDR CHQA200500010Battery Pack · dischargedLEFT HAND OVERWING FORWARD EMERGENCY LIGHT IS INOP. AISLE EGRESS LIGHT AND CABIN FLOOD LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY EGRESS BATTERY PACK PER EMB 140 MM 33-50-04-5. OPS CHECK GOOD.Jan 21, 2004 · N295SK · Emb EMB135KL · Emergency LightingSDR CHQA000452Wire · brokenFLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRES. REPAIRED LIGHT STRIP IAW EMB145 WM 20-21-00 AND EMB145 AMM 33-56-12.Jan 14, 2004 · N378 · Emb EMB135KL · Light System WiringSDR CHQA000451Bulb · inoperativeRT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-10. OPS CHECK GOOD.Jan 13, 2004 · N378 · Emb EMB135KL · Emergency LightingSDR SIMA200402006Floorbeam · corrodedABI - DURING MBV INSPECTION, THE LEFT FLOORBEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF LEFT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONJan 1, 2004 · N825AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200402005Floorbeam · corrodedDURING AN MBV INSPECTION, THE CENTER FLOORBEAM BETWEEN FRAME 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGED SECTION OF THE CENTER FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DJan 1, 2004 · N825AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200335202Seat · inoperativeLAX - FLT 3161 - CAPTAIN REPORTED THE PILOTS SEAT WOULD NOT LOCK IN PLACE. MAINTENANCE REMOVED AND REPLACED THE PILOTS SEAT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Dec 18, 2003 · N822AE · Emb EMB135KL · Flight Compartment EquipmentSDR SIMA200335201Control Unit · inoperativeLAX - FLT 3159 - DURING CRUISE FLIGHT CREW REPORTED AN UNCOMMANDED DEPLOYMENT OF SPOILERS AT HIGH SPEED RESULTING IN A 15 DEGREE BANK TO THE RIGHT. MAINTENANCE REMOVED AND REPLACED THE SPOILER CONTROL UNIT IAW EMB MM. AIRCRAFT WAS RELEASED FOR AND PASSED A FDec 15, 2003 · N821AE · Emb EMB135KL · Drag Control SystemSDR SIMA200334501Control Unit · failedDFW - FLT 3544 - PITCH TRIM SYSTEM 1-2 INOPERATIVE ON EICAS. COMPLIED WITH ETN EB27-022 AND PERFORMED TROUBLESHOOTING IAW EMB FAULT ISOLATION MANUAL. REMOVED AND INSTALLED HSCU. OPERATIONAL CHECK GOOD IAW 27-40-01. AIRCRAFT RETURNED TO SERVICE. (M)Dec 10, 2003 · N810AE · Emb EMB135KL · Stabilizer Control SystemSDR SIMA200334101Control Unit · inoperativeORD - FLT 3967 - DURING CRUISE FLIGHT CREW REPORTED A MAIN AND BACKUP TRIM INOPERATIVE WARNING. MAIN SYSTEM WAS RESTORED BY RESETTING BREAKER. BACKUP TRIM WOULD NOT RESTORE. MAINTENANCE LUBRICATED THE BACKUP TRIM SWITCH AND DRAINED THE NR 1 AND 2 PITOT SYSTDec 4, 2003 · N835AE · Emb EMB135KL · Autopilot SystemSDR SIMA200333201Light · inoperativeCREW REPORTED THE ROW 11 EMERGENCY EXIT ILGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT ASSEMBLY IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Nov 25, 2003 · N823AE · Emb EMB135KL · Emergency LightingSDR SIMA200332705Smoke Detector · malfunctionedDURING CRUISE THE CREW REPORTED A BAGGAGE SMOKE WARNING. CREW FOLLOWED EMERGENCY PROCEDURES AND USED THE FIRE BOTTLES. SMOKE INDICATION THEN WENT OUT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE SMOKE DETECTOR WAS REMOVED AND REPLACED IAW EMB MM. OPS CHECKNov 21, 2003 · N834AE · Emb EMB135KL · Smoke DetectionSDR SIMA200332702Pressure Switch · inoperativeDURING CLIBM CREW REPORTED RUDDER SYSTEM 1/2 INOPERATIVE MESSAGE ON EICAS FOLLOWED BY A YAW DAMPNER FAIL. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 2 RUDDER PRESSURE SWITCH IAW EMB MM. OPERATIONAL CHECNov 20, 2003 · N827AE · Emb EMB135KL · Rudder Control SystemSDR CHQA0000429Controller · malfunctionedON DEPARTURE FROM DCA AT 8000 MSL RECEIVED THE PITCH TRIM 1-2 INOP ON THE EICAS. MAIN AND BACKUP TRIP CONFIRMED INOP BY TRIM SWITCHES. COMPLETED EMERGENCY CHECKLIST AND EMERGENCY WAS DECLARED INTO IAD. EMERGENCY EQUIPMENT WAS STANDING BY AND MADE UNEVENTFULNov 18, 2003 · N371 · Emb EMB135KL · Stabilizer Position IndicatingSDR SIMA200331402Odor · detectedDURING APU START, THE APU FAILED TO START. WHEN BATTERY SWITCHES WERE RETURNED TO AUTO CREW REPORTED A STRONG BURNING ELECTRICAL ODOR. MEL WAS ISSUED AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AN OPERATIONAL CHECK OF THE APU SYSTEM WAS COMPNov 6, 2003 · N821AE · Emb EMB135KL · Air Distribution SystemSDR SIMA200331001Battery Pack · inoperativeDURING TAXI IN CRWE NOTED FORWARD PORTION OF CABIN EMERGENCY LIGHTS INOPERATIVE. RAI NR 1 EMERGENCY BATTERY PACK P/N 20131A, S/N 67884, NR 2 BATTERY PACK P/N 20131A S/N 69700, AND NR 3 EMERGENCY BATTERY PACK P/N 20131A AND S/N 71003, OPS CHECK GOOD. (M)Nov 5, 2003 · N828AE · Emb EMB135KL · Emergency LightingSDR SIMA200330902Selector · inoperativeDURING APPROACH TO SNA CREW REPORTED A FLAP FAIL MESSAGE ON EICAS AND THE FLAPS STAYED AT 9 DEGREES. AIRCRAFT DIVERTED TO LAX. MAINTENANCE REMOVED AND REPLACED THE FLAP SELECTOR LEVER IAW EMB AMM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVNov 4, 2003 · N830AE · Emb EMB135KL · Trailing Edge Flap Control SystemSDR SIMA200330202Fcu · failedDURING FLIGHT CREW REPORTED A FLAPS FAIL MESSAGE ON EICAS AND FLAPS STUCK IN THE FIVE DEGREE POSITION. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 29, 2003 · N830AE · Emb EMB135KL · Trailing Edge Flap Control SystemSDR SIMA200330201Battery · inoperativeCREW REPORTED THE EMERGENCY LIGHTING BREAKER POPS OUT. DURING TROUBLESHOOTING MAINTENANCE FOUND THE NR 1 EMERGENCY BATTERY WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO Oct 28, 2003 · N821AE · Emb EMB135KL · Emergency LightingSDR SIMA200329702Power Supply · failedLAX - FLT 3160 - EMERGENCY LIGHTS CB POPPED WILL NOT RESET AND EXIT LIGHT FOR MAIN ENTRANCE DOOR WILL NOT GO OUT. RAI NR 1 EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW EMB 140 AMM 33-50-04. OPS CHECK GOOD. (M)Oct 23, 2003 · N821AE · Emb EMB135KL · Emergency LightingSDR SIMA200329701Seat Track · dirtyFIRST OFFICERS SEAT DIFFICULT TO LOCK IN PLACE. SEAT MOVED BACK IN FLIGHT. CLEANED DEBRIS FROM SEAT TRACK, OP CHECK GOOD. (M)Oct 21, 2003 · N830AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200329301Odor · detectedDURING CRUISE FLIGHT, THE CREW REPORTED A BURNING INSULATION ODOR. AIRCRAFT WAS DIVERTED TO LIT. (M)Oct 17, 2003 · N827AE · Emb EMB135KL · Air Distribution SystemSDR SIMA200330101Odor · detectedCREW REPORTED A BURNING INSULATION ODOR IN FLIGHT. AIRCRAFT WAS DIVERTED TO LIT AND LANDED WITH NO OTHER INCIDENT REPORTED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. BLEED SYSTEM WAS INSPECTED AND AN OPERATIONAL CHECK WAS COMPLIED WITH. NO ODOR WAS NOTEOct 17, 2003 · N827AE · Emb EMB135KL · Air Distribution SystemSDR SIMA200329303Floorbeam · corrodedDURING AN MBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED AN NDT INSPECTION. FABRICATED AN EXTERNAL ANGLE, FILLER, SHIMS AND PLATE. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 ROct 15, 2003 · N822AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200328807Seat Track · dirtyORD - WHILE TAXIING AIRCRAFT, CAPTAINS SEAT INTERMITTENTLY WOULD SLIDE BACK FROM A LOCKED POSITION. MAINTENANCE CLEANED DEBRIS FROM SLIDE TRACK. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 15, 2003 · N832AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200329302Stringer · chafedDURING AN MBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BEYOND SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3093A, EMB SRM SRM EMB-145/114Oct 12, 2003 · N822AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200327908Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS AT FRAME 20. BLENDED THE CORRODED AREA AND PERFORMED NDT INSPECTION. FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM EMB-145/Oct 4, 2003 · N824AE · Emb EMB135KL · Fuselage Main, Floor Beam
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