N27512

Service difficulty reports · 57

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N27512' AND registry_match = 'registration'
  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 C2XA07RI047Plug · damagedFLT 2189 - EWR - CREW REPORTED ENG 1 PRODUCING WHITE/LIGHT GRAY SMOKE AFTER ENGINE SHUT DOWN. LARGE QUANTITY COMING OUT FROM FRONT AND BACK. OIL, HYD, FUEL INDICATIONS ARE NORMAL. THIS IS A REPEAT WRITE UP. EWR MX PERFORMED TROUBLESHOOTING AND FOUND AFT SUJun 16, 2007 · N27512 · Emb EMB135ER · Engine (Turbine/Turboprop)SDR C2XA07RI028Smoke Detector · defectiveFLT 2214 - EWR - CREW REPORTED GATE RETURN FOR A SECOND TIME DUE TO LAV SMOKE FALSE ALARM. FIRST TIME SYSTEM WAS RESET. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB 135 AMM 26-14-01. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED May 6, 2007 · N27512 · Emb EMB135ER · Smoke DetectionSDR C2XA07RI021Warning System · malfunctionedFLT 2979 - BDL - CREW REPORTED LAV SMOKE IND ON EICAS WITH NO SMOKE. CREW RESET SYSTEM AND MESSAGE WAS CLEARED.Apr 30, 2007 · N27512 · Emb EMB135ER · Smoke DetectionSDR C2XA07SH003Floor Support · corrodedSHV - DURING C-CHECK LEFT OMEGA BEAM LOWER FLANGE WAS FOUND WITH CORROSION BETWEEN FRAME 23 AND 32. MAINTENANCE REPAIRED LT OMEGA BEAM AT LOWER FLANGE IAW EMB 145 SRM 53-00-10 & CPM 51-21-07. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jan 4, 2007 · N27512 · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA07SH002Floor Support · corrodedSHV - DURING C-CHECK LEFT OMEGA BEAM LOWER FLANGE WAS FOUND WITH CORROSION BETWEEN FRAMES 32 AND 36. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 33 IAW EMB 135 SRM 53-00-10 FIG 202, CPM 51-21-07 AND EMB 135 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SJan 4, 2007 · N27512 · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA07SH001Firewall · crackedSHV - DURING C-CHECK THE APU FIREWALL WAS FOUND CRACKED AT FIVE RIVETS NEAR STRINGER 12R. MAINTENANCE REPAIRED THE CRACKED APU FIREWALL IAW IC2006-145/10117. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jan 4, 2007 · N27512 · Emb EMB135LR · Fuselage Main, BulkheadSDR C2XA06CL032Switch · faultyCLE FLIGHT 2501 THE CREW REPORTED A VERY LOUD NOISE FROM THE FORWARD SECTION OF THE AIRCRAFT. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS WOULD NOT CLOSE AFTER GEAR RETRACTION. THE NOSE GEAR DOOR SEQUENCE PROXIMITY SWITCH WAS REPLACED. OPERATIONAL CMar 13, 2006 · N27512 · Emb EMB135ER · Landing Gear Door Retract SectionSDR C2XA04TY141Selector · defectiveCLE - UPON GEAR RETRACTION OF FLIGHT 2127 THE LANDING GEAR AURAL WARNING INDICATION CAME ON. REMOVED AND REPLACED THE FLAP SELECTOR LEVER IAW EMB 135/145 AMM 27-51-03. OPS CHECKS WERE GOOD OF THE FLAPS AND LANDING WARNING SYSTEM IAW EMB AMM 27-50-00 AND 32-6Jul 23, 2004 · N27512 · Emb EMB135LR · Trailing Edge Flap Control SystemSDR C2XA04CL055Bulb · inoperativeDURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT AT ROW 9BC (IN PSU) WAS FOUND INOPERATIVE. MAINTENANCE REPLACED LIGHT BULB. OPERATIONAL CHECKS WERE GOOD.May 14, 2004 · N27512 · Emb EMB135ER · Emergency LightingSDR C2XA04CL054Liner · misalignedDURING ROUTINE MAINTENANCE THE LT OVERWING EMERGENCY EXIT WOULD NOT OPEN. MAINTENANCE INSPECTED AND FOUND THE LT OVERWING INNER DOOR LINER TO BE MISALIGNED. MAINTENANCE REALIGNED LINER AND OPERATIONAL CHECKS WERE GOOD.May 14, 2004 · N27512 · Emb EMB135ER · Emergency ExitsSDR C2XA04SH265Sill · corrodedSHV-DURING C CHECK THE LEFT SILL WAS FOUND TO BE CORRODED AFT OF FRAME 23 AND FORWARD OF FRAME 25. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 4, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH264Strap · corrodedSHV-DURING C CHECK THE AFT DIGITAL STRAP AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 4, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH263Angle · corrodedSHV-DURING C CHECK THE RIGHT RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 4, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH260Floorbeam · corrodedSHV-DURING C CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 3, 2004 · N27512 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA04SH259Buttstrap · corrodedSHV-DURING C CHECK THE CENTER OMEGA BEAM BUTTSTRAP BETWEEN FRAME 18 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 3, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH256Sill · corrodedSHV-DURING C CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 30, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH255Doubler · corrodedSHV-DURING C CHECK THE DOUBLER ON THE RIGHT OMEGA BEAM AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 30, 2004 · N27512 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA04SH254Strap · corrodedSHV-DURING C CHECK THE FORWARD DIGITAL STRAP BETWEEN FRAMES 14 AND 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 29, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH252Sill · corrodedSHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 29, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH249Doubler · corrodedSHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 27, 2004 · N27512 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA04SH248Sill · corrodedSHV - DURING C-CHECK THE LEFT HAND SILL WAS FOUND TO BE CORRODED FROM FRAME 19 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 27, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH247Buttstrap · corrodedSHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 18 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 27, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH246Sill · corrodedSHV- DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 27, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH244Sill · corrodedSHV- DURING C-CHECK THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 65 AND 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 24, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH243Floorbeam · corrodedSHV- DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 24, 2004 · N27512 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA04SH242Firewall · crackedSHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP OF THE RIGHT VERTICAL STIFFENER. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 23, 2004 · N27512 · Emb EMB135ER · APU Cowling/ContainmentSDR C2XA04SH241Floorbeam · corrodedSHV- DURING C-CHECK THE CENTER FLOORBEAM AT FRAME 18 TO 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 23, 2004 · N27512 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA04SH240Bracket · corrodedSHV- DURING C-CHECK THE PASSENGER DOOR THRESHOLD AFT BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 23, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH239Bracket · corrodedSHV- DURING C-CHECK THE PASSENGER DOOR FORWARD THRESHOLD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 23, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH238Structure · gougedSHV- DURING C-CHECK THE STRINGER REINFORCEMENT ON STRINGER 19 RIGHT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5310-01260. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 23, 2004 · N27512 · Emb EMB135ER · Fuselage Main, Longeron/StringerSDR C2XA04CL033Drag Strut · seizedCLE FLIGHT 2127 THE CREW REPORTED ON APPROACH THE NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. THE CREW FOLLOWED THE QRH AND ACCOMPLISHED LANDING GEAR EXTENSION. ALL GEAR INDICATED DOWN AND LOCKED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCEApr 8, 2004 · N27512 · Emb EMB135ER · Nose/Tail Landing GearSDR C2XA03CL202Access Door · stickingCLE FLIGHT 2438 THE CREW REPORTED, COULD NOT OPEN THE LANDING GEAR EMERGENCY EXTENSION ACCESS DOOR LOCATED IN THE COCKPIT. MAINTENANCE INSPECTED AND LUBED AND UNSTUCK THE ACCESS DOOR. OPERATIONAL CHECKS WERE GOOD.Dec 19, 2003 · N27512 · Emb EMB135ER · Accessory Compartment DoorsSDR C2XA03TY192Engine · failedAIRCRAFT AIR-RETURNED TO CLE, EMERGENCY DECLARED, THE LEFT ENGINE FAILED IN FLIGHT, ITT SPIKED AT 1100 DEG C, WITH A LOUD BANG. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE, OPS AND LEAK CHECKED GOOD IAW EMB135-MM-71-00-00 AND TASK CARD 6271001. AIRCRAFTNov 7, 2003 · N27512 · Emb EMB135ER · Engine (Turbine/Turboprop)SDR C2XA03BT061Battery · inoperativeCREW (DURING WALKAROUND) NOTICED THE EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERIES AND OPS CHECKED SYSTEM GOOD.May 24, 2003 · N27512 · Emb EMB135ER · Emergency LightingSDR C2XA03CL030Connector · looseCLE FLIGHT 2083 THE CREW REPORTED A EXTINGUISHING BOTTLE -B- ENGINE 1/2 MESSAGE INTERMITTENTLY IN FLIGHT. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CLEANED CANNON PLUG ON EXTINGUISHING BOTTLE -B- AND SECURED LOOSE BFeb 4, 2003 · N27512 · Emb EMB135ER · Fire Bottle, FixedSDR C2XA02CL229Light · inoperativeTHE CREW REPORTED A FLOOR EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FLOOR EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.Nov 3, 2002 · N27512 · Emb EMB135ER · Emergency LightingSDR C2XA02CL214Charger · burnedCMH FLIGHT 3961 THE CREW REPORTED A BURNED PLASTIC ODOR COMING FROM THE REAR OF THE CABIN. THEY REPORTED THE ODOR SEEMED TO BE ASSOCIATED WITH THE APU AND THE NR 2 PACK.THE AIRCRAFT WAS RELEASED IAW MEL 21-51-00/1. MAINTENANCE INSPECTED AND PERFORMED OPERATIOct 29, 2002 · N27512 · Emb EMB135ER · Emergency EquipmentSDR C2XA02CL099Nozzle · cokedCLE FLIGHT 3085 THE CREW REPORTED A STRONG BURNING ODOR DURING ICE TEST AND WHEN NR 2 PACK IS ON. MAINTENANCE REPLACED THE NR 2 ENGINE FUEL NOZZLES. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Apr 11, 2002 · N27512 · Emb EMB135ER · Fuel Injector NozzleSDR C2XA02CL094Bulb · inoperativeDURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY LIGHT.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.Apr 8, 2002 · N27512 · Emb EMB135ER · Emergency LightingSDR C2XA02CL093Switch · inoperativeCLE FLIGHT 4141 THE CREW REPORTED A SMOKE SMELL WHEN IN ICE CONDITIONS AND WHEN THE ICE TEST WAS DONE. MAINTENANCE INSPECTED AND REPLACED NR 2 PACK SETDOWN SWITCH. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Apr 8, 2002 · N27512 · Emb EMB135ER · Cabin Cooling SystemSDR C2XA02CL092Odor · detectedCLE FLIGHT 3193 THE CREW REPORTED NR 2 PACK HAD A BURNING SMELL. THE SMELL WENT AWAY AFTER THE PACK WAS TURNED OFF. MAINTENANCE INSPECTED NR 2 PACK AND PERFORMED SYSTEM CHECKS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.Apr 7, 2002 · N27512 · Emb EMB135ER · Air Distribution SystemSDR C2XA02CL084Generator · contaminatedCLE FLIGHT# 3194 THE CREW REPORTED ALL 4 GENERATORS FELL OFF LINE AFTER GEAR RETRACTION.THE #4 GENERATOR DID COME BACK ONLINE. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND ALL FOUR GENERATORS TO BE CONTMar 26, 2002 · N27512 · Emb EMB135ER · DC Generating SystemSDR C2XA01TY202Bypass Jacket · corrodedTYS DURING A SCHEDULE INSPECTION, BETWEEN THE FAN CASE AND THE OUTER BYPASS, OXIDATION WAS FOUND ON NR 1 AND NR 2 ENGINE. MAINTENANCE REMOVED THE OXIDATION, PERFORMED TOUCHUP OF PERMANENT RESIN COATING ON ACCESS, GEAR BOX MOUNTS, PLACED A CHEMICAL-FILM COATIDec 15, 2001 · N27512 · Emb EMB135ER · Turbine Engine Bypass SectionSDR C2XA01TY204Skin · dentedTYS DURING A SCHEDULE INSPECTION THE FUSELAGE WAS DAMAGED BEHIND FRAME 31 BETWEEN STRINGER 12 AND 13R. REMOVED DAMAGED AREA. FABRICATED A DOUBLER, ALODINED AND INSTALLED, SEALED, PRIMED AND PAINTED IAW EMB 135 SRM 51-40-02 AND 51-22-01 AND CPM 51-21-05. ALLDec 15, 2001 · N27512 · Emb EMB135ER · Fuselage Main, Plate/SkinSDR C2XA01TY203Bypass Jacket · corrodedTYS DURING A SCHEDULE INSPECTION, BETWEEN THE FAN CASE AND THE OUTER BYPASS, OXIDATION WAS FOUND ON NR 1 ENGINE. MAINTENANCE REMOVED THE OXIDATION, PERFORMED TOUCH UP OF PERMANENT RESIN COATING ON ACCESS, GEAR BOX MOUNTS, PLACED A CHEMICAL-FILM COATING FOR MDec 15, 2001 · N27512 · Emb EMB135ER · Turbine Engine Bypass SectionSDR C2XA01TY201Attach Fitting · damagedTYS DURING A SCHEDULED INSPECTION THE LEFT HAND COCKPIT PARTITION WALL ATTACHMENT POINTS WERE FOUND TO BE DAMAGED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR AND PERFORMED A DYE PENETRANT INSPECTION IAW EMBRAER GST 3877/01, EMB-135 CPM 51-21-04, 51-21-05 ADec 14, 2001 · N27512 · Emb EMB135ER · Passenger Compartment EquipmentSDR C2XA01TY200Floor Support · corrodedTYS DURING A SCHEDULED INSPECTION THE FLOOR SUPPORT ANGLES LOCATED BELOW THE THRESHOLD STRIP AT THE MAIN ENTRY DOOR WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB-135 SRM 51-20-03, 51-40-02 AND CPM 51-21-04,Dec 14, 2001 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA01TY199Inlet · damagedTYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ENGINE AIR INLET WAS FOUND TO HAVE TWO NICKS ON THE ACOUSTIC PERFORATED INNER SKIN. MAINTENANCE REWORKED THE NICKS (BLEND-OUT) IAW EMB-135 SRM 54-20-01 AND EMBRAER GST 3879/01, THE REPAIR WAS FOUND TO BE SATIDec 14, 2001 · N27512 · Emb EMB135ER · Turbine Engine Air Inlet SectionSDR C2XA01TY198Limiter · gougedTYS DURING A SCHEDULED INSPECTION THE LEFT HAND ELEVATOR INBOARD LIMITER TUBE WAS FOUND TO BE GOUGED. MAINTENANCE ACCOMPLISHED THE BLEND-OUT REPAIR AND PERFORMED A DYE PENETRANT INSPECTION IAW EMBRAER GST-3934/01, THE REPAIR AND INSPECTION WERE SATISFACTORY.Dec 13, 2001 · N27512 · Emb EMB135ER · Elevator Control SystemSDR C2XA01TY197Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE LOCATED BELOW THE FLOORING AND JUST AFT OF THE COCKPIT ENTRANCE WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE FORWARD DIGITAL IAW EMB-135 SRM 51-40-02, THE REPADec 13, 2001 · N27512 · Emb EMB135ER · Fuselage Main, Floor Beam
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