# Service difficulty reports: N638AS, cancelled Jul 14, 2015

A list on [N638AS, cancelled Jul 14, 2015](https://openairdocs.org/deregistered/N638AS-2015-07-14.md).

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

- [SDR ASOA03185](https://openairdocs.org/sdr/ASOA03185.md): Lamp · burned out · Apr 26, 2003 · N638AS · Emb EMB120ER · Emergency Lighting
  > DURING 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)
- [SDR ASOA02458](https://openairdocs.org/sdr/ASOA02458.md): Battery Pack · discharged · Aug 21, 2002 · N638AS · Emb EMB120ER · Emergency Lighting
  > DURING 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)
- [SDR ASOA02448](https://openairdocs.org/sdr/ASOA02448.md): Regulator Valve · leaking · Aug 12, 2002 · N638AS · Emb EMB120ER · Pneumatic Distribution System
  > WHILE 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,
- [SDR ASOA02101](https://openairdocs.org/sdr/ASOA02101.md): Light · burned out · Feb 17, 2002 · N638AS · Emb EMB120ER · Emergency Lighting
  > DURING 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)
- [SDR ASOA020258](https://openairdocs.org/sdr/ASOA020258.md): Seat Track · corroded · Jan 24, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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 T
- [SDR ASOA02058](https://openairdocs.org/sdr/ASOA02058.md): Seat Track · corroded · Jan 24, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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 T
- [SDR ASOA02057](https://openairdocs.org/sdr/ASOA02057.md): Seat Track · corroded · Jan 24, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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
- [SDR ASOA02056](https://openairdocs.org/sdr/ASOA02056.md): Seat Track · corroded · Jan 24, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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
- [SDR ASOA02055](https://openairdocs.org/sdr/ASOA02055.md): Strap · corroded · Jan 24, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous Structure
  > DURING 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)
- [SDR ASOA02053](https://openairdocs.org/sdr/ASOA02053.md): Stringer · corroded · Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Main, Longeron/Stringer
  > DURING 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)
- [SDR ASOA02052](https://openairdocs.org/sdr/ASOA02052.md): Seat Track · corroded · Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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, A
- [SDR ASOA020251](https://openairdocs.org/sdr/ASOA020251.md): Sill · corroded · Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous Structure
  > DURING 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)
- [SDR ASOA02050](https://openairdocs.org/sdr/ASOA02050.md): Sill · corroded · Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous Structure
  > DURING 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 5
- [SDR ASOA02049](https://openairdocs.org/sdr/ASOA02049.md): Buttstrap · corroded · Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous Structure
  > DURING 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)
- [SDR ASOA02048](https://openairdocs.org/sdr/ASOA02048.md): Crossbeam · corroded · Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous Structure
  > DURING 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)
- [SDR ASOA02047](https://openairdocs.org/sdr/ASOA02047.md): Crossbeam · corroded · Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous Structure
  > DURING 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)
- [SDR ASOA02046](https://openairdocs.org/sdr/ASOA02046.md): Floorbeam · corroded · Jan 22, 2002 · N638AS · Emb EMB120ER · Fuselage Main, Floor Beam
  > DURING 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)
- [SDR ASOA02037](https://openairdocs.org/sdr/ASOA02037.md): Crossbeam · corroded · Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous Structure
  > DURING 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)
- [SDR ASOA02038](https://openairdocs.org/sdr/ASOA02038.md): Seat Track · corroded · Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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)
- [SDR ASOA02039](https://openairdocs.org/sdr/ASOA02039.md): Seat Track · corroded · Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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)
- [SDR ASOA02040](https://openairdocs.org/sdr/ASOA02040.md): Seat Track · corroded · Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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)
- [SDR ASOA02041](https://openairdocs.org/sdr/ASOA02041.md): Seat Track · corroded · Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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)
- [SDR ASOA02042](https://openairdocs.org/sdr/ASOA02042.md): Sill · corroded · Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous Structure
  > DURING 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)
- [SDR ASOA02034](https://openairdocs.org/sdr/ASOA02034.md): Crossbeam · corroded · Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous Structure
  > DURING 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)
- [SDR ASOA02033](https://openairdocs.org/sdr/ASOA02033.md): Stringer · corroded · Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Main, Longeron/Stringer
  > DURING 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)
- [SDR ASOA02032](https://openairdocs.org/sdr/ASOA02032.md): Buttstrap · corroded · Jan 18, 2002 · N638AS · Emb EMB120ER · Fuselage Miscellaneous Structure
  > DURING 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)
- [SDR ASOA01173](https://openairdocs.org/sdr/ASOA01173.md): Light · inoperative · Sep 17, 2001 · N638AS · Emb EMB120ER · Emergency Lighting
  > DURING 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)
- [SDR ASOA01135](https://openairdocs.org/sdr/ASOA01135.md): Battery Pack · weak · Aug 11, 2001 · N638AS · Emb EMB120ER · Emergency Lighting
  > DURNIG 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)
- [SDR ASOA00084](https://openairdocs.org/sdr/ASOA00084.md): Landing Gear · failed · Jul 22, 2000 · N638AS · Emb EMB120ER · Nose/Tail Landing Gear
  > FLT 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 WARN
- [SDR 20000516SH028](https://openairdocs.org/sdr/20000516SH028.md): Frame · cracked · Apr 24, 2000 · N638AS · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > FLUORESCENT 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)
- [SDR 20000516SH027](https://openairdocs.org/sdr/20000516SH027.md): Frame · cracked · Apr 24, 2000 · N638AS · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > FLUORESCENT 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)
- [SDR ASOA99046](https://openairdocs.org/sdr/ASOA99046.md): Acm · vibrates · May 18, 1999 · N638AS · Emb EMB120ER · Cabin Cooling System
  > SMELL 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)
- [SDR 98ZZZX4362](https://openairdocs.org/sdr/98ZZZX4362.md): Blade · damaged · Jun 18, 1998 · N638AS · Emb EMB120ER · Propeller Blade Section
  > DISCONTINUITY - NR 2 RIGHT BLADE FILLET FAILED INSPECTION. DAMAGE TO THE FILLET AREA, BLADE FACE SIDE. THE BLADE IS SCRAP. CUSTOMER: ATLANTIC SOUTHEAST AIRLINES.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N638AS-2015-07-14/reports

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