Embraer EMB-145

Service difficulty reports · 3,003

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 = 'EMB145'
  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 C2XA00IA104Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STAB DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01032, AND THE AIRCRAFTApr 17, 2000 · N12957 · Emb EMB145 · Vertical StabilizerSDR C2XA00IA103Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM BUTT STRAP WAS FOUD TO BE CORRODED FROM FRAME 15 TO FRAME 18. MAINTENANCE REPAIRED THE AFFECTED SECTION OF FLOOR BEAM IAW CONTINENTAL EXPRESS ENGINEEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01123, AND Apr 17, 2000 · N12957 · Emb EMB145 · Fuselage Miscellaneous StructureSDR RAIA0004010Engine · malfunctionedFLT 6258 - PHL, RT ENGINE OIL PRESSURE REACHED 116 PSI ON TAKEOFF ROLL. MAINTENENCE REPLACED RT ENGINE.Apr 12, 2000 · N804HK · Emb EMB145 · Turbine Engine Oil SystemSDR C2XA00BT017A/C Pack · odorEWR - FLT 3899 - CREW REPORTED NR 1 PACK FAULT AND BURNING ODOR IN COCKPIT. MAINTENANCE FOUND RAM AIR DOOR INLET AND PRECOOLER AREA FROZEN AND FILLED WITH ICE. CLEARED ICE AND OPERATIONALLY CHECKED SYSTEM GOOD. (M)Apr 9, 2000 · N16963 · Emb EMB145 · Cabin Cooling SystemSDR C2XA00BT016Duct · leakingEWR - FLT 4395 - CREW REPORTED NR 2 BLEED LEAK LIGHT INFLIGHT, ACCOMPANIED BY SMOKE IN COCKPIT AND CABIN, ODOR DISSIPATED QUICKLY. MAINTENANCE RESEALED ENGINE BLEED DUCT NR 2 AT RADIO ALTIMETER ACCESS PANEL. OPS CHECKED AND LEAK CHECKED GOOD. (M)Apr 9, 2000 · N14938 · Emb EMB145 · Pneumatic Distribution SystemSDR C2XA00IA087Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED UNDER THE CARBON FIBER FLOOR SUPPORT. MAINTENANCE REMOVED THE DAMAGED SECTION OF OMEGA BEAM AND INSTALLED A REPAIR DOUBLER IAW EMB 145 SRM 51-40-02 AND EMB FAX SST1274/99, AND THE AApr 4, 2000 · N13956 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA00IA088Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STAB DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01032, AND THE AIRCRAFT WApr 4, 2000 · N13956 · Emb EMB145 · Vertical StabilizerSDR C2XA00IA089Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STAB DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01032, AND THE AIRCRAFT Apr 4, 2000 · N13956 · Emb EMB145 · Vertical StabilizerSDR C2XA00IA090Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE INSTALLED A DOUBLER REPAIR TO THE DAMAGED SECTION OF OMEGA BEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01120, AND THE AIRCRAFApr 4, 2000 · N13956 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA00IA091Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE CENT BUTT STRAP FROM FRAME 15-18 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF BUTT STRAP IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01121, AND THE AIRCRApr 4, 2000 · N13956 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA00BT013Smoke Detector · inoperativeEWR - FLT 4025 - CREW REPORTED INTERMITTENT BAGGAGE SMOKE LIGHT ON GROUND. MAINTENANCE REMOVED AND REPLACED AFT BAGGAGE SMOKE DETECTOR. OPS CHECKED SATISFACTORY. (M)Apr 3, 2000 · N16944 · Emb EMB145 · Fire DetectionSDR C2XA00TY008Engine · malfunctionedTYS - THE RIGHT ENGINE WAS REMOVED AND REPLACED AFTER NUMEROUS ATTEMPTS TO TROUBLESHOOT AND CORRECT A HIGH OIL PRESSURE TREND. THE REMOVAL AND REPLACEMENT OF THE RIGHT ENGINE WAS ACCOMPLISHED IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAKApr 2, 2000 · N14974 · Emb EMB145 · Turbine Engine Oil SystemSDR C2XA00BT012Light · inoperativeBTV - FLT 4218 - DURING SERVICE CHECK, FOUND OVERHEAD EMERGENCY LIGHT ROW SEVEN INOPERATIVE. SECURED LOOSE CONNECTION ON OVERHEAD EMERGENCY LIGHT AT ROW SEVEN. OPS CHECKED GOOD. (M)Mar 30, 2000 · N13969 · Emb EMB145 · Emergency LightingSDR RAIA0003022Windshield · failed6261-BOS- AIRCRAFT SUSTAINED BIRD STRIKE ON CAPTAINS WINDSHIELD AT 24,000 FEET. MAINTENANCE INSPECTED AND REPLACED CAPTAINS FORWARD WINDSHIELD PANEL.Mar 30, 2000 · N806HK · Emb EMB145 · Flight Compartment WindowsSDR C2XA00TY007Engine · malfunctionedTYS - FLT 3867 - CREW REPORTED HIGH OIL PRESSURE ON THE LEFT ENGINE DURING THE TAKEOFF ROLL. THE AIRCRAFT WAS SUBSEQUENTLY MAINTENANCE FERRIED TO TYS WERE THE LEFT ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND Mar 27, 2000 · N7200 · Emb EMB145 · Engine (Turbine/Turboprop)SDR C2XA00IA075Skin · damagedBNA - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE PASSENGER DOOR SKIN WAS DAMAGED. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REPAIRED THE AFFECTED DOOR SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 22, 2000 · N13965 · Emb EMB145 · Passenger/Crew DoorsSDR C2XA00CL030Sensor · crackedCLE - FLT 4053 - THE CREW REPORTED THAT ON TAKEOFF ROLL, RECEIVED NR 1 THRUST REVERSER DISAGREE MESSAGE ALONG WITH A SPOILER OPEN MESSAGE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACEMar 21, 2000 · N14939 · Emb EMB145 · Landing Gear Position and WarningSDR C2XA00IA069Floorbeam · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT FLOORBEAM CORRODED AT FRAME 20 UNDER COMPOSITE FLOOR PANEL SUPPROT. MAINTENANCE REMOVED THE CORROSION, AND INSTALLED A REPAIRE DOUBLER ON THE FLOORBEAM. (M)Mar 20, 2000 · N12934 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA00IA068Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED AT FRAME 13 TO 18. MAINTENANCE REPAIRED THE AFFECTED BUTT STRAP. (M)Mar 20, 2000 · N13935 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA00IA067Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REPAIRED THE AFFECTED OMEGA BEAM. (M)Mar 20, 2000 · N13935 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA00IA066Floorbeam · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT FLOORBEAM AT FRAME TWENTY WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE DAMAGED SECTION OF FLOORBEAM. (M)Mar 20, 2000 · N15932 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA00IA065Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER AISLE OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE DAMAGED SECTION OF OMEGA BEAM WAS REMOVED AND REPLACED. (M)Mar 20, 2000 · N17928 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA00IA064Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER AISLE OMEGA BEAM WAS FOUND TO BE CORRODED JUST FORWARD OF FRAME 25 THE CORRODED SECTION OF OMEGA BEAM WAS REMOVED AND REPLACED AND PERFORMED A DOUBLER REPAIR. (M)Mar 20, 2000 · N17928 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA00IA063Beam · corrodedIAH - DURNG C-CHECK INSPECTION, CORROSION WAS FOUND BETWEEN THE COMPOSIT FLOOR CROSS BEAMS AND OMEGA BEAMS AT FRAMES 20 AND 25 THE DAMAGED SECTIONS OF OMEGA BEAM WERE REPAIRED. (M)Mar 20, 2000 · N15926 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA00IA062Support Bracket · corrodedIAH - REFERENCE CONTINENTAL EXPRESS SDR CONTROL NUMBER C2XA98IA472, DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM SUPPORT RAMP WAS FOUND TO BE CORRODED FROM FRAME 13 TO FRAME 18 AND WAS REMOVED AND REPLACED. (M)Mar 20, 2000 · N15926 · Emb EMB145 · Fuselage Miscellaneous StructureSDR RAIA0003010Switch · failed7604-STL -DURING CLIMB, RIGHT BLEED OVERHEAT EICAS MESSAGE CAME ON. MAINTENANCE REPLACED RIGHT ENGINE BLEED PRESSURE SWITCH.Mar 17, 2000 · N801HK · Emb EMB145 · Pneumatic Indicating SystemSDR SIMA0677Squat Switch · inoperativeLIT - FLT 3561 - CREW REPORTED ENGINE 1/2 REV DISAGREE AND AIR/GROUND INOPERATIVE MESSAGE ON EICAS. CREW DIVERTED TO LIT. UPON LANDING ALL FAULT MESSAGES WENT AWAY. REMOVED AND REPLACED NR 2 ENGINE WEIGHT ON WHEEL SWITCH IAW EMB145 AMM 32-63-02. OPS CHECK Mar 7, 2000 · N609AE · Emb EMB145 · Landing Gear Position and WarningSDR C2XA00CL028Bleed Valve · failedCLT - FLT 3882 - AFTER LANDING IN CLEVELAND, THE CREW REPORTED THE NR 1 ENGINE FLAMED OUT ON LANDING ROLL. THE AIRCRAFT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE 9TH STAGE BLEED VALVE TO BE BROKEN AND NOT FUNCTIONING. Mar 6, 2000 · N13958 · Emb EMB145 · Compressor Bleed ValveSDR RAIA0003002Seal · leaking7621 - XNA - EICAS NUMBER 2 BLEED LEAK MESSAGE APPEARED IN FLIGHT. CREW DIVERTED TO SGF. MAINTENANCE INSPECTED AND REPLACED RIGHT ENGINE BLEED LINE SEALS.Mar 3, 2000 · N802HK · Emb EMB145 · Pneumatic SystemSDR C2XA00TY004Smoke · detectedTYS - FLT 4301 - CREW REPORTED THAT AFTER TAKEOFF THEY OBSERVED SMOKE IN THE LAVATORY. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED SEVERAL ENGINE RUN OPERATIONAL CHECKS WITH NO DISCREPANCIES NOTEDMar 1, 2000 · N13968 · Emb EMB145 · Air Distribution SystemSDR C2XA00IA047Light · inoperativeIAH - DURING MAINTENANCE INSPECTION, THE LEFT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. (M)Feb 27, 2000 · N16927 · Emb EMB145 · Emergency LightingSDR C2XA00IA046Battery Pack · dischargedIAH - DURING MAINTENANCE INSPECTION, THE LEFT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 27, 2000 · N16927 · Emb EMB145 · Emergency LightingSDR RAIA0002020Rib · crackedMX - STL - DURING LEFT WING AILERON PCA MODIFICATION, FOUND LEFT WING RIB 21 CRACKED AT UPPER CENTER RIB FLANGE. MAINTENANCE REPAIRED LEFT WING UPPER CENTER RIB FLANGE IAW MANUFACTURERS REPAIR INSTRUCTIONS.Feb 22, 2000 · N802HK · Emb EMB145 · Wing, Rib/BulkheadSDR RAIA0002014Connector · shorted6237 - JFK - ON CLIMB-OUT, CREW REPORTED ELECTRICAL SMELL IN COCKPIT, NUMEROUS EICAS DE-ICE FAULTS ACTIVATED. MAINTENANCE INSPECTED AND FOUND WIRING CONNECTOR P/J-0837 SHORTED BELOW LEFT COCKPIT CREW SEAT. MAINTENANCE REPLACED CONNECTOR P/J-0837.Feb 22, 2000 · N806HK · Emb EMB145 · Pitot/Static Anti-Ice SystemSDR C2XAOOIA040Tank · crackedIAH- FLT 4276 - DURING POST FLT INSPECTION, THE CREW REPORTED THAT THE NUMBER TWO ENGINE WAS LEAKING OIL. MX INSPECTED THE NR 2 ENGINE AND FOUND THE OIL TANK TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED OIL TANK IAW EMB145 MM 79-1101, AND THEFeb 20, 2000 · N16961 · Emb EMB145 · Turbine Engine Oil SystemSDR SIMA0511Regulator · failedDFW - FLT 3619 - PILOT REPORTED VIBRATION IN CONTROL COLUMN WHEN PASSING THROUGH 24,000 FEET. INSPECTED AND FOUND ELEVATOR TENSION REGULATOR BAD CAUSING CONTROL CABLES TO SLACK AND BECOME FRAYED. REMOVED AND REPLACED ELEVATOR TENSION REGULATOR AND BOTH CONTRFeb 20, 2000 · N607AE · Emb EMB145 · Elevator Control SystemSDR 2000ZZZM262Regulator · failedDFW - FLT 3619 - PILOT REPORTED VIBRATION IN CONTROL COLUMN WHEN PASSING THROUGH 24,000 FEET. INSPECTED AND FOUND ELEVATOR TENSION REGULATOR BAD CAUSING CONTROL CABLES TO SLACK AND BECOME FRAYED. REMOVED AND REPLACED ELEVATOR TENSION REGULATOR AND BOTH CONTRFeb 20, 2000 · N607AE · Emb EMB145 · Elevator Control SystemSDR 2000ZZZM261Control Cable · frayedDFW - FLT 3619 - PILOT REPORTED VIBRATION IN CONTROL COLUMN WHEN PASSING THROUGH 24,000 FEET. INSPECTED AND FOUND ELEVATOR TENSION REGULATOR BAD CAUSING CONTROL CABLES TO SLACK AND BECOME FRAYED. REMOVED AND REPLACED ELEVATOR TENSION REGULATOR AND BOTH CONTRFeb 20, 2000 · N607AE · Emb EMB145 · Elevator Control SystemSDR C2XA00TY002Engine · malfunctionedTYS - DURING A SCHEDULED INSPECTION, THE LEFT ENGINE OIL PRESSURE WAS FOUND TO BE EXCEEDING MANUFACTURES LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIFeb 18, 2000 · N14938 · Emb EMB145 · Engine (Turbine/Turboprop)SDR RAIA0002012Computer · failed6304 - CLE - STALL PROTECTION SYSTEM EICAS FAIL MESSAGE CAME ON DURING TAXI. MAINTENANCE REPLACED THE STALL PROTECTION COMPUTER.Feb 17, 2000 · N805HK · Emb EMB145 · Stall Warning SystemSDR SIMA0434Ecu · failedDFW - FLT 3683 - AFTER TAKEOFF, HAD GROUND FAIL INDICATION AND LANDING GEAR CONTROL HANDLE FAIL TO OPERATE. AIRCRAFT RETURNED TO BASE. REMOVED AND REPLACED LGEU. PERFORMED OPERATIONAL CHECK OF LANDING GEAR SYSTEM OPS CHECK GOOD. (M)Feb 12, 2000 · N605RR · Emb EMB145 · Landing Gear Retraction/Extension SystemSDR C2XA00IA036Light · inoperativeIAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TOFeb 8, 2000 · N13935 · Emb EMB145 · Emergency LightingSDR C2XA00CL019Engine · failedCLE - FLT 4399 - AFTER TAKEOFF FROM CLEVELAND THE CREW RECEIVED A LAVATORY SMOKE WARNING INDICATION. SMOKE ENTERED THE AFT CABIN AREA. THE ARICRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND DETERMINED THAT THE NR 2 ENGINE 0 CFeb 7, 2000 · N13936 · Emb EMB145 · Engine (Turbine/Turboprop)SDR C2XA01BT006Unknown · smokeYUL - FLT 4009 - CREW REPORTED SMOKE IN AIRCRAFT AFTER TAKEOFF SUSPECT NR 1 PACK. MAINTENANCE DISPATCHED TO YUL, PERFORMED HARD/OVERWEIGHT LANDING INSPECTION AND RELEASED A/C IAW MEL NR 21-51-00 CATERGORY C PLACARD NR 003822. AIRCRAFT RETURNED TO SERVICE. OFeb 5, 2000 · N16927 · Emb EMB145 · Air Distribution SystemSDR C2XA00IA031Battery Pack · dischargedIAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY EXIT LIGHTS AT 11 ABC, 12 ABC, AND 14 ABC WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK IAW EMB145-LR MM 33-50-04, AND THE AIRCRAFT WAS APPROVED Feb 5, 2000 · N13964 · Emb EMB145 · Emergency LightingSDR C2XA00IA030Battery Pack · looseTYS - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE FORWARD SECTION OF EMERGENCY AISLE PATH LIGHTING TO BE INOPERATIVE. MAINTENANCE RESECURED THE BATTERY PACK ON THE AFFECTED POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 4, 2000 · N13964 · Emb EMB145 · Emergency LightingSDR RAIA0002003Thermostat · failed6309 - BOS - HORIZONTAL STABILIZER ANTI-ICE FAILED IN FLIGHT. MAINTENANCE REPLACED STABILIZER BLEED LEAK THERMOSTAT.Feb 3, 2000 · N805HK · Emb EMB145 · Airfoil Anti/De-ice SystemSDR C2XA01BT005Unknown · smokeYUL - FLT 4005 - AIR RETURNED DUE TO SMOKE FILLING CABIN AND COCKPIT. MAINTENANCE OPERATIONALLY CHECKED AIRCONDITIONING IN REF TO EMB145 MM 21-00-00. OPS CHECKED GOOD. SUBMITTER STATES, SUSPECT DE-ICING FLUID ON T/O RAN INTO APU INLET CAUSING SMOKE. (M)Feb 2, 2000 · N15932 · Emb EMB145 · Air Distribution SystemSDR C2XA00BT005Switch · contaminatedEWR - FLT 4164 - CREW REPORTED LANDING GEAR WOULD NOT RETRACT DURING GO AROUND. RETURNED TO THE FIELD AND LANDED UNEVENTFULLY. MAINTENANCE FOUND ICE ON ALL PROXIMITY SWITCHES. CLEANED SWITCHES AND OPERATIONALLY CHECKED GOOD ON TEST FLIGHT. (M)Jan 30, 2000 · N14942 · Emb EMB145 · Landing Gear Retraction/Extension SystemSDR RAIA0001026Switch · failed6315 - BOS - STABILIZER ANTI-ICE FAIL EICAS MESSAGE CAME ON, VALVE OPEN INDICATION ON ICE PROTECTION PANEL DID NOT ILLUMINATE. MAINTENANCE DEFERRED PER MEL. MAINTENANCE REPLACED ICE PROTECTION PANEL OPEN INDICATOR SWITCH.Jan 29, 2000 · N805HK · Emb EMB145 · Airfoil Anti/De-ice System
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