N618AE

Service difficulty reports · 178

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 = 'N618AE' 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 SIMA200423910Skin · corrodedABI - DURING AN MBV INSPECTION, TORN SKIN WAS DISCOVERED ON THE LEFT ELEVATOR AT THE SERVO TAB ROD CUTOUT. PERFORMED A CUTOUT OF THE DAMAGED MATERIAL AND TREATED THE EDGES. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 26, CHAPTAug 21, 2004 · N618AE · Emb EMB145LR · Elevator, Plate/SkinSDR SIMA200423706Sill · corrodedDURING AN MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED CORRODED AREA AND PERFORMED NDT INSPECTION. FILLED BLENDED AREA WITH EPOXY RESIN EA 934NA AND SANDED SMOOTH. FABRICATED THREE DOUBLERS. REPAIR DONE IAW EMB SRM, SRM 14Aug 18, 2004 · N618AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200413802Window · malfunctionedORD - FLT 4233 - CREW REPORTED SMOKE SMELL IN COCKPIT WHEN USING CAPTAIN WINDOW HEAT. REPLACED CAPTAIN WINDOW IAW AMM 56-10-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)May 13, 2004 · N618AE · Emb EMB145LR · Flight Compartment WindowsSDR SIMA200328801Radome · bird strikeDURING TAKEOFF FROM BUF, CREW REPORTED A BIRD STRIKE TO THE NOSE AREA. MAINTENANCE REMOVED AND REPLACED FRAMES 3, 4, 5 AND 6, STRINGER 4R, RIGHT FORWARD NOSE TOP SKIN PANEL, RIGHT AFT NOSE TOP SKIN PANEL IAW EMB SRM 51-42-01 AND REPAIRED SKIN FORWARD OF RIGHTOct 10, 2003 · N618AE · Emb EMB145LR · Aerodynamic FairingsSDR SIMA200218403Frame · damagedABI - DURING AN IMBV MAINTENANCE, FOUND FRAME 72 DENTED AND BENT AT SPLICE JOINT ABOVE FLOOR ON LEFT SIDE OF CARGO. REMVOED FRAME 72 SPLICE CHANNEL. RECONTOURED DENT. PERFORMED NDT AND FOUND NO DEFECTS. FABRICATED TWO DOUBLER ANGLE, REPAIR DONE IAW EMB GSTJul 1, 2002 · N618AE · Emb EMB145LR · Fuselage Main, FrameSDR SIMA200218406Doubler · corrodedABI - MAINTENANCE FOUND CORROSION ON LEFT OMEGA BEAM PREVIOUS REPAIR AT FRAME 20. REMOVED PREVIOUS REPAIR, CORROSION LIMITED TO PREVIOUS REPAIR. FABRICATED DOUBLER, PLATE, AND SHIMS. REPAIR DONE IAW EMB 145 SRM 145/1142 CHAPTER 53, REV 18 53-21-01, AND STANJun 28, 2002 · N618AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200218405Floorbeam · corrodedABI - MAINTENANCE FOUND CORROSION ON FORWARD DIGITAL. REMOVED CORROSION BY CUT OUT. FABRICATED A REPLACEMENT STRAP AND TWO DOUBLERS. REPAIR DONE IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 18 53-21-10, AND STANDARD SRM PRACTICES. (M)Jun 28, 2002 · N618AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200218404Frame · dentedABI - DURING AN IMBV INSPECTION FOUND DENT ON FRAME 67 BETWEEN STRINGER 14R AND 15R. RECONTOURED DENT PERFORMED NDT AND FOUND NO DEFECTS. FABRICATED TWO DOUBLERS ANGLES, REPAIR DONE IAW EMB GST-2022/02-A ITEM 5, AND STANDARD SRM PRACTICES. (M)Jun 28, 2002 · N618AE · Emb EMB145LR · Fuselage Main, FrameSDR SIMA200218407Clip · crackedABI - DURING MBV INSPECTION, MAINTENANCE FOUND SHEAR CLIP CRACKED ON FRAME 81 AT THE 2 O'CLOCK POSITION. REMOVED DAMAGE SHEAR CLIP. INSTALLED SERVICEABLE CLIP IAW EMB GST-2022/02A, AND STANDARD SRM PRACTICES. (M)Jun 28, 2002 · N618AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200218409Sill · corrodedABI - MAINTENANCE FOUND CARGO DOOR LOWER SILL CORRODED. REMOVED CORRODED SILL BEAM. INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 145/1142, CHAPTER 51 REV 18 51-20-03, 51-40-02 AND STANDARD SRM PRACTICES. (M)Jun 28, 2002 · N618AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200218408Window Frame · corrodedABI - MAINTENANCE FOUND RIGHT WINDSHIELD CUT OUT STRUCTURE HAS 25 CORRODED HOLES. REMOVED CORROSION BY REAMING BOLT HOLES. FABRICATED FREEZE PLUGS. REPAIR DONE IAW EMB GST 2022/02, ITEM 9 AND STANDARD SRM PRACTICES. (M)Jun 28, 2002 · N618AE · Emb EMB145LR · Fuselage Main, StructureSDR SIMA200218402Floorbeam · corrodedABI - MAINTENANCE FOUND CORROSION ON GALLEY CENTER FLOORBEAM. REMOVED CORRODED GALLEY CENTER BEAM. INSTALLED SERVICEABLE BEAM IAW EMB 145 SRM 145/1142, CHAPTER 51, REV 18 51-40-02, AEA ETN EM-53-028 R1, AND STANDARD SRM PRACTICES. (M)Jun 28, 2002 · N618AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200218401Window Frame · corrodedABI - MAINTENANCE FOUND LEFT WINDSHIELD CUT OUT STRUCTURE HAS 15 CORRODED HOLES. REMOVED CORROSION BY REAMING/BOLT HOLES. FABRICATED FREEZE PLUGS. REPAIR DONE IAW EMB GST-2022/02, ITEM 9 AND STANDARD SRM PRACTICES. (M)Jun 28, 2002 · N618AE · Emb EMB145LR · Fuselage Main, StructureSDR SIMA200217308Gusset · corrodedTHIS IS A LEVEL 2 FINDING, LAVATORY CENTER BEAM GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)Jun 19, 2002 · N618AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200217314Structure · gougedABI - FOUND PASSENGER DOOR IS GOUGED IN TWO PLACES. PERFORMED NDT INSPECTION AND FOUND NO DEFECTS. REPAIR DONE IAW EMB GST-2005/02. (M)Jun 17, 2002 · N618AE · Emb EMB145LR · Passenger/Crew DoorsSDR SIMA200217313Skin · gougedABI - FOUND GOUGE WITH DENT AT FRAME 66 AND 67 BELOW CARGO DOOR AREA AND STRINGERS 18L AND 20L. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW EMB GST-1997/02, SURFACE PROTECTION RESTORED. (M)Jun 17, 2002 · N618AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA200217311Skin · gougedABI - FOUND GOUGE BETWEEN FRAMES 28/29 AND STRINGERS 17R/18R. BLENDED GOUGES, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW EMB GST-1999/02, SURFACE PROTECTION RESTORED. (M)Jun 17, 2002 · N618AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA200217312Skin · gougedABI - FOUND GOUGE AT FRAME 63/64 AND STRINGERS 19L AND 20L JUST BELOW AND FORWARD OF CARGO DOOR CUTOUT. BLENDED GOUGES, PERFORMED NDT, NO DEFECTS, ACCEPTED AS IS IAW EMB GST-1997/02, SURFACE PROTECTION RESTORED. (M)Jun 17, 2002 · N618AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA200217310Skin · dentedABI - FOUND ONE DENT AFT OF PASSENGER DOOR ON EMB PLACARD AT FRAME 19 AND 20 AND STRINGER 14L AND 15L. PERFORMED NDT, NO DEFECTS, DENT ACCEPTED AS IS IAW EMB GST-1999/02. (M)Jun 17, 2002 · N618AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA200217309Skin · dentedABI - FOUND ONE DENT MARKED NR 3 AFT OF PAX DOOR LOWER CORNER AT FRAMES 19 AND 20 AND STRINGER 15L AND 16L. ALSO FOUND CRACK. REMOVED DAMAGE BY CUT OUT, FABRICATED A REPAIR DOUBLER AND FILLER, REPAIR DONE IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 18 53-21-01Jun 17, 2002 · N618AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA200217304Structure · gougedABI - FOUND NUMEROUS SMALL GOUGES JUST INBOARD OF WASTE SERVICE ACCESS PANEL AT FRAMES 60 AND 61 AND STRINGERS 20R AND 21R. GOUGES BLENDED, PERFORMED NDT, NO DEFECTS, ACCEPTED AS IS IAW EMB GST-1999/02. SURFACE PROTECTION RESTORED. (M)Jun 17, 2002 · N618AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200217315Sill · corrodedABI - THIS IS A LEVEL 2 FINDING, RIGHT CENTER SILL HAS CORROSION. REMOVED CORROSION BY BLENDING, FILLED WITH EPOXY RESIN AND SANDED. FABRICATED A REPAIR DOUBLER, REPAIR DONE IAW ETN-53-036, FIG 5, AND STANDARD SRM PRACTICES. M)Jun 17, 2002 · N618AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200217307Floor Support · corrodedABI - THIS IS A LEVEL 2 FINDING. PASSENGER DOOR ENTRY FLOORBOARD SUPPORT HAS CORROSION. PERFORMED NDT, NO DEFECTS. FLOOR SUPPORTS FOUND TO BE WITHIN EMB 145-21-10 LIMITS. (M)Jun 17, 2002 · N618AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200217306Beam · corrodedABI - THIS IS A LEVEL 2 FINDING, RIGHT HAT BEAM IN GALLEY HAS CORROSION. REPAIRED HAT BEAM IAW ETN 53-036. (M)Jun 17, 2002 · N618AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200217305Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING. AFT DIGITAL HAS CORROSION. PERFORMED NDT INSPECTION AND FOUND NO DEFECTS. DIGITAL FOUND TO BE WITHIN EMB 145 SRM 53-21-10 LIMITS. (M)Jun 17, 2002 · N618AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR 20010607CW004Gearbox · making metalMETAL DEBRIS FOUND ON CHIP COLLECTOR DRAIN VALVE (GEARBOX, OIL TANK).May 16, 2001 · N618AE · Emb EMB145LR · Turbine Engine Accessory DriveSDR SIMA2112Light · inoperativeLBB - FLT 3892 - REAR FLOOR STRIP OF EMERGENCY LIGHTING SYSTEM INOPERATIVE, NOTIFIED CONTRACT MAINTENANCE ISSUED A FERRY PERMIT TO DFW FOR MAINTENANCE. FLOOR EMERGENCY LIGHT STRIP WAS REMOVED AND REPLACED. OPERATIONAL WAS GOOD AND AIRCRAFT WAS RETURNED TO SEJul 29, 2000 · N618AE · Emb EMB145LR · Emergency LightingSDR SIMA992953Bulb · failedORD - FLT 4389 - RIGHT FORWARD EXTERIOR EMERENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED RIGHT FORWARD EXTERIOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKED GOOD. (X)Oct 22, 1999 · N618AE · Emb EMB145LR · Emergency Lighting
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