N638AS, cancelled Jul 14, 2015

Service difficulty reports · 33

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 = 'N638AS' AND deregistration_id = 'N638AS-2015-07-14'
  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 ASOA03185Lamp · burned outDURING A GROUND INSPECTION IN ATL, THE RIGHT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Apr 26, 2003 · N638AS · Emb EMB120ER · Emergency LightingSDR ASOA02458Battery Pack · dischargedDURING HANGAR MAINTENANCE IN TXK, TRACK EMERGENCY LIGHTING AT GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Aug 21, 2002 · N638AS · Emb EMB120ER · Emergency LightingSDR ASOA02448Regulator Valve · leakingWHILE PERFORMING A GO AROUND PROCEDURE, CLIMBING TO 4000 FEET, THE FLIGHT CREW RECEIVED A DUCT LEAK WARNING FOR THE RT ENGINE. THE APPROPRIATE CHECKLIST WAS COMPLIED WITH, BUT THE LIGHT DID NOT EXTINGUISH. IAW THE CHECKLIST THE CAPTAIN SECURED THE RT ENGINE,Aug 12, 2002 · N638AS · Emb EMB120ER · Pneumatic Distribution SystemSDR ASOA02101Light · burned outDURING SCHEDULED INSPECTION IN MCN, THE FORWARD MOST WHITE FLOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT BULB ON THE FLOOR EMERGENCY LIGHT TRACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Feb 17, 2002 · N638AS · Emb EMB120ER · Emergency LightingSDR ASOA020258Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT WALL SEAT TRACK, FORWARD SECTION, WAS FOUND WITH CORROSION BETWEEN FRAMES 16 AND 31. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK USING SRM 51-40-02, SRM 51-25-00, SRM 51-21-02, ASA EO 120-25-0007, AND TJan 24, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02058Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT WALL SEAT TRACK, FORWARD SECTION, WAS FOUND WITH CORROSION BETWEEN FRAMES 16 AND 31. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK USING SRM 51-40-02, SRM 51-25-00, SRM 51-21-02, ASA EO 120-25-0007, AND TJan 24, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02057Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT FLOOR SEAT TRACK, FORWARD SECTION , WAS FOUND WITH CORROSION BETWEEN FRAMES 17 AND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK USING SRM 51-40-02, SRM 51-25-00, SRM 51-21-01, ASA EO 120-25-0007, AND Jan 24, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02056Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE AFT RIGHT SEAT TRACK HAD CORROSION FROM FRAME 34 TO 40. MAINTENANCE REMOVED THE RIGHT AFT SEAT TRACK FROM FRAMES 34 TO 40 IAW SRM 51-40-02. A NEW TRACK WAS FABRICATED AND MADE READY FOR INSTALLATION IAW SRM 51-25-00 AND Jan 24, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02055Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 16 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF BUTT STRAP IAW SRM 51-40-02 AND ASA EO 120-53-0173. (M)Jan 24, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02053Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON STRINGER 18 LEFT BETWEEN FRAME STATION 4214 AND 4992. MAINTENANCE REMOVED AND REPLACED THE DAMAGED PART OF THE STRINGER IAW SRM 53-00-03, 51-25-00, AND 51-40-02. (M)Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Main, Longeron/StringerSDR ASOA02052Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE AFT, LEFT INBOARD SEAT TRACK, BETWEEN FRAMES 34 AND 40 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. A NEW SEAT TRACK WAS FABRICATED IAW SRM 51-25-00, 51-21-02, AJan 22, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA020251Sill · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SILL WAS FOUND CORRODED FROM FRAMES 44 TO 47. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR SILL IAW SRM 51-40-02. (M)Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02050Sill · corrodedDURING C-CHECK INSPECTION IN BNA, THE SILL PLATE AT FRAME 13, RUNNING LEFT TO RIGHT, WAS CORRODED FROM THE CENTER TO THE RIGHT SIDE. MAINTENANCE CUT AWAY THE DAMAGED PORTION OF THE SILL PLATE. A NEW REPLACEMENT PART AND SPLICE PLATE WERE FABRICATED IAW SRM 5Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02049Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE CENTER BUTT STRAP AT FRAMES 13 TO 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED CENTER BUTT STRAP IAW SRM 51-40-02. (M)Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02048Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT CROSSBEAM AT FRAME 20 WAS FOUND CORRODED BETWEEN THE FLOOR SILL AND THE LEFT BUTT STRAP. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRM 51-40-02. M)Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02047Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, ALL CROSSBEAMS AT FRAME 16 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAMS IAW SRM 51-40-02. (M)Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02046Floorbeam · corrodedDURING C-CHECK INSPECTION IN BNA, FOUND CORROSION ON THE CENTER OMEGA BEAM BETWEEN FRAME STATION 5518-5533. MX REPAIRED THE CORRODED OMEGA BEAM IAW ASA EO120-53-0173. (M)Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Main, Floor BeamSDR ASOA02037Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, A CROSS FRAME WAS FOUND CORRODED AT FRAME 23 BETWEEN THE RIGHT AND CENTER BUTT STRAPS. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS FRAME IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02038Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE FORWARD SECTION OF THE LEFT WALL SEAT TRACK WAS FOUND CORRODED BETWEEN FRAMES 17 AND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02039Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SEAT TRACK, FORWARD SECTION, WAS FOUND TO BE CORRODED BETWEEN FRAMES 16 AND 31. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02040Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, FOUND CORROSION ON THE AFT SECTION OF THE LEFT WALL SEAT TRACK BETWEEN FRAMES 32 AND 39. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02041Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT AFT SECTION OF WALL SEAT TRACK WAS FOUND CORRODED BETWEEN FRAMES 34 AND 38. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02042Sill · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT SILL PLATE BETWEEN FRAMES 38 AND 44. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02034Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD CROSS FRAME WAS FOUND TO BE CORRODED AT FRAME 26. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS FRAME IAW SRM 51-30-01 AND 51-30-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02033Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 19 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 13A AND 15A. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 53-00-03 AND 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Main, Longeron/StringerSDR ASOA02032Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 25 AND 30. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM 51-40-02. (M)Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA01173Light · inoperativeDURING HANGAR MAINTENANCE IN MCN, THE FLOOR TRACK LIGHTING WAS FOUND WITH ONE RED LIGHT INOPERATIVE AT ROW 8. MAINTENANCE REMOVED AND REPLACED BURNED OUT LAMP ON THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 8. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Sep 17, 2001 · N638AS · Emb EMB120ER · Emergency LightingSDR ASOA01135Battery Pack · weakDURNIG SCHEDULED MAINTENANCE IN MCN, EMERGENCY LIGHTS ON FLOOR AT ROWS 3 AND 4 HAD WEAK ILLUMINATION. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)Aug 11, 2001 · N638AS · Emb EMB120ER · Emergency LightingSDR ASOA00084Landing Gear · failedFLT 4893 - DURNIG GEAR RETRACTION AFTER TAKEOFF, THE NOSE GEAR FAILED TO RETRACT AND A AND B RED AND GREEN LIGHTS ILLUMINATED. CREW LEVELED AIRCRAFT AT 5000 AND ENTERED APPROACH TO LAND. CREW WAS PERFORMING A QRH CHECKLIST WHEN THEY RECEIVED A HYDRAULIC WARNJul 22, 2000 · N638AS · Emb EMB120ER · Nose/Tail Landing GearSDR 20000516SH028Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED A CRACK IN THE RIGHT NACELLE FORWARD FRAME NR 1. POSSIBLE CAUSE IS STILL UNDETERMINED. SUSPECT ENGINE TORQUE AND VIBRATION TO BE POSSIBLE CONTRIBUTING FACTORS. SB 120-54-0036 IS BEING INCORPORATED. (X)Apr 24, 2000 · N638AS · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR 20000516SH027Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED A CRACK IN THE LEFT NACELLE FORWARD FRAME NR 1. POSSIBLE CAUSE IS STILL UNDETERMINED. SUSPECT ENGINE TORQUE AND VIBRATION TO BE POSSIBLE CONTRIBUTING FACTORS. SB 120-54-0036 IS BEING INCORPORATED. (X)Apr 24, 2000 · N638AS · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR ASOA99046Acm · vibratesSMELL OF SOMETHING HOT IN CABIN AND LIGHT HAZE SEEN BY FLIGHT ATTENDANT. BELIEVED LEFT PACK OVERHEAT. MAINTENANCE FOUND THE LEFT PACK TO OPERATE NORMALLY. RIGHT PACK VIBRATES AND DOES NOT COOL WELL. REMOVED AND REPLACED RIGHT ACM. (M)May 18, 1999 · N638AS · Emb EMB120ER · Cabin Cooling SystemSDR 98ZZZX4362Blade · damagedDISCONTINUITY - NR 2 RIGHT BLADE FILLET FAILED INSPECTION. DAMAGE TO THE FILLET AREA, BLADE FACE SIDE. THE BLADE IS SCRAP. CUSTOMER: ATLANTIC SOUTHEAST AIRLINES.Jun 18, 1998 · N638AS · Emb EMB120ER · Propeller Blade Section
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