# Service difficulty reports: N249US, cancelled Sep 26, 2003

A list on [N249US, cancelled Sep 26, 2003](https://openairdocs.org/deregistered/N249US-2003-09-26.md).

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

Page 1 of 2 · 78 reports

- [SDR USAASB01328](https://openairdocs.org/sdr/USAASB01328.md): Charger · failed · Nov 28, 2001 · N249US · Boeing 737201 · Emergency Lighting
  > LGA - THE MID CABIN AISLE EMERGENCY EXIT SIGN FLICKERED ON AND OFF. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN CHARGER. (M)
- [SDR USAA011027](https://openairdocs.org/sdr/USAA011027.md): Crease Beam · cracked · Aug 7, 2001 · N249US · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND CREASE BEAM CRACKED.750 INCH, BS 520 LBL 64. EXTRUDED SECTION REPAIR, SPLICE REPLACEMENT PER SRM 51-40-4 FIG 1. (M)
- [SDR USAA011026](https://openairdocs.org/sdr/USAA011026.md): Web · cracked · Aug 7, 2001 · N249US · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND WEB CRACKED.125 INCH, BS 178 BULKHEAD AT WL 234 AT RBL 10. INSTALLED DOUBLER PER SRM 53-10-11 FIG 1, 53-10-1. (M)
- [SDR USAA011029](https://openairdocs.org/sdr/USAA011029.md): Floorbeam · corroded · Aug 7, 2001 · N249US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3.5 INCHES, BS 294.5 LBL 1.5 TO RBL 1.5. CORROSION LEVEL 1, TASK NR C53-107-01. UPPER T-CHORD REPAIRED PER TR 53-10-04 B. (M)
- [SDR USAASB01149](https://openairdocs.org/sdr/USAASB01149.md): Light · inoperative · May 29, 2001 · N249US · Boeing 737201 · Emergency Lighting
  > IAD - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA010448](https://openairdocs.org/sdr/USAA010448.md): Tie Clip · cracked · Apr 25, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, BS 707, AFT SIDE OF STRINGER 11R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-01, INSTALLED FREEZE PLUG REPAIR PER EA 69175. (M)
- [SDR USAA010447](https://openairdocs.org/sdr/USAA010447.md): Pressure Panel · cracked · Apr 25, 2001 · N249US · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND PRESSURE DECK WEB 2 INCH, BS 663-676, RBL 20 TO RBL 50. INSTALLED DOUBLED, STIFFENERS, CHORD SEGMENT, FILLERS, WEB PER EA''S 69129, 69125, 69183. (M)
- [SDR USAA010354](https://openairdocs.org/sdr/USAA010354.md): Skin · cracked · Apr 4, 2001 · N249US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKS, TWO CRACKS.4 INCHES, TWO CRACKS AT.7 INCH, STATION 380 AND 397 BETWEEN STRINGER 19R AND 20R. INSTALLED DOUBLER PER EA 69250. (M)
- [SDR USAA010353](https://openairdocs.org/sdr/USAA010353.md): Support · damaged · Apr 4, 2001 · N249US · Boeing 737201 · Horizontal Stabilizer Structure
  > CLT - FOUND WEB SUPPORT WITH.5 INCH BULGE, HORIZ STAB JACKSCREW LOWER WEB SUPPORT, STATION 1088, LBL 4. INSTALLED WEB DOUBLER AND FILLER PER EA 69281. (M)
- [SDR USAA010352](https://openairdocs.org/sdr/USAA010352.md): Web · cracked · Apr 4, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED 2 INCHES, STATION 670-672 RBL 25 MWW CEILING. INSTALLED SPLICE PLATE, STIFFENERS, ANGLES WEB REPAIR PER EA 69183. (M)
- [SDR USAA010355](https://openairdocs.org/sdr/USAA010355.md): Frame · chafed · Apr 4, 2001 · N249US · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND FRAME CHAFED 2.5 INCH, STATIN 1040 FRAME CUTOUT OF APU DUCT STRINGER 22L-26L. INSTALLED DOUBLER, TRIPLER AND SHEAR TIES. INSTALLED DOUBLER, TRIPLER AND SHEAR TIES. (M)
- [SDR USAA010347](https://openairdocs.org/sdr/USAA010347.md): Skin · cracked · Mar 26, 2001 · N249US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 5 INCHES, STATION 727A PLUS 16 INCHES ABOVE STRINGER 17L. INSTALLED FILLER AND DOUBLER PER EA 69166. (M)
- [SDR USAA010299](https://openairdocs.org/sdr/USAA010299.md): Stiffener · corroded · Mar 20, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CORROSION ON CHANNEL STIFFENER 6 FEET, FORWARD LOWER SIDE AFT BULKHEAD AFT STATION 1016, BL 0. INSTALLED DOUBLER AND REPAIR ANGLES PER EA 69123. (M)
- [SDR USAA010298](https://openairdocs.org/sdr/USAA010298.md): Tie Clip · cracked · Mar 20, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.5 INCH, TIE CLIP STATION 663, STRINGER 10L. REPLACED WITH NEW PART PER SRM 51-10-1. (M)
- [SDR USAA010265](https://openairdocs.org/sdr/USAA010265.md): Bulkhead · cracked · Mar 7, 2001 · N249US · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND BULKHEAD CRACKED 1 INCH, BS 178, RBL 5.7. REMOVED CRACKED AREA, INSTALLED DOUBLER. (M)
- [SDR USAA010261](https://openairdocs.org/sdr/USAA010261.md): Bulkhead · cracked · Mar 5, 2001 · N249US · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND BULKHEAD WEB CRACKED.125 INCH, BS 178, RBL 5, WL 189, 190 AND 191.5. REMOVED DAMAGE INSTALLED DOUBLER PER EA 69132. (M)
- [SDR USAA010264](https://openairdocs.org/sdr/USAA010264.md): Bulkhead · cracked · Mar 2, 2001 · N249US · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND BULKHEAD CRACKED 1 INCH, STATION 178 LBL 7, WL 213.5. REMOVED DAMAGE, INSTALLED DOUBLER. (M)
- [SDR USAA010263](https://openairdocs.org/sdr/USAA010263.md): Bulkhead · cracked · Mar 2, 2001 · N249US · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND BULKHEAD CRACKED.25 INCH, STATION 178, RBL 10.5, WL 234. REMOVED DAMAGE, INSTALLED DOUBLER. (M)
- [SDR USAA010188](https://openairdocs.org/sdr/USAA010188.md): Web · cracked · Feb 28, 2001 · N249US · Boeing 737201 · Passenger/Crew Doors
  > CLT - FOUND DOOR WEB CRACKED.5 INCH, AFT SERVICE DOOR TORQUE BOX WEB BS 947 BELOW STRINGER 11R. INSTALLED DOUBLER PER TR 53-30-07A. (M)
- [SDR USAA010223](https://openairdocs.org/sdr/USAA010223.md): Frame · cracked · Feb 20, 2001 · N249US · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND VERTICAL CHORD CRACKED 1 INCH OUTBOARD RADIUS AND 1.8 INCH INBOARD, BS 178 BULKHEAD, LBL 5-7, WL 184. INSTALLED VERTICAL CHORD REPAIR PARTS PER EA 68935/EO 5300V155. (M)
- [SDR USAA010222](https://openairdocs.org/sdr/USAA010222.md): Frame · cracked · Feb 20, 2001 · N249US · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND CHORD VERTICAL CRACKED.9 INCH IN INBOARD RADIUS, RBL 5-7, WL 184, BS 178 BULKHEAD. INSTALLED VERTICAL CHORD REPAIR PARTS PER EA 68935/EO5300V155. (M)
- [SDR 20010426AP004](https://openairdocs.org/sdr/20010426AP004.md): Tie Clip · cracked · Feb 20, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRINGER AND TIE CLIP CRACKED.250 INCH, BS 520 STRINGER 19L. REMOVED AND REPLACED TIE CLIP AND INSTALLED STRINGER 18 INCH SECTION PER SRM 53-10-03, 51-10-01, 51-10-02. REF USAA010224. (M)
- [SDR USAA010224](https://openairdocs.org/sdr/USAA010224.md): Stringer · cracked · Feb 20, 2001 · N249US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER AND TIE CLIP CRACKED.250 INCH, BS 520 STRINGER 19L. REMOVED AND REPLACED TIE CLIP AND INSTALLED STRINGER 18 INCH SECTION PER SRM 53-10-03, 51-10-01, 51-10-02. (M)
- [SDR USAA010237](https://openairdocs.org/sdr/USAA010237.md): Skin · cracked · Feb 19, 2001 · N249US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1 INCH, BS 380 AT E/E EQUIPMENT COOLING DUCT OUTLET. INSTALLED INTERIOR SKIN DOUBLER PER T/R 53-30-04. (M)
- [SDR USAA010236](https://openairdocs.org/sdr/USAA010236.md): Frame · cracked · Feb 19, 2001 · N249US · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED 2 INCHES, FS 767 AT STRINGER 13L. INSTALLED REPAIR DOUBLERS PART 1 AND 2 IAW SRM 53-10-4. (M)
- [SDR USAA010235](https://openairdocs.org/sdr/USAA010235.md): Frame · cracked · Feb 19, 2001 · N249US · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.25 INCH, FRAME 807 STRINGER 13L. REMOVED DAMAGE AND INSTALLED DOUBLERS PART 1 AND 2 IAW SRM 53-10-4. (M)
- [SDR USAA010234](https://openairdocs.org/sdr/USAA010234.md): Skin · cracked · Feb 19, 2001 · N249US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN DOUBLER CRACKED 8 INCHES BY 11 INCHES, 727 PLUS 16 S 27R. INSTALLED DOUBLER PER SRM 53-30-03. (M)
- [SDR USAA010254](https://openairdocs.org/sdr/USAA010254.md): Clip · cracked · Feb 15, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CLIP CRACKED.125 INCH, STATION 616 STRINGER 3 LEFT. MODIFIED PART NR INSTALLED. (M)
- [SDR USAA010253](https://openairdocs.org/sdr/USAA010253.md): Tie Clip · cracked · Feb 15, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.125 INCH, BS 616 STRINGER 1. MODIFIED PART NR INSTALLED. (M)
- [SDR USAA010252](https://openairdocs.org/sdr/USAA010252.md): Shear Tie · cracked · Feb 15, 2001 · N249US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND SHEAR TIE CRACKED.5 INCH, BS 967 AT STRINGER 7L. FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM 53-10-4 FIG 8. (M)
- [SDR USAA010255](https://openairdocs.org/sdr/USAA010255.md): Stringer · cracked · Feb 14, 2001 · N249US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CRACKED.5 INCH, STRINGER 15L BS 520-540. REPLACED STRINGER SECTION IAW SRM 53-10-3. (M)
- [SDR USAA010157](https://openairdocs.org/sdr/USAA010157.md): Angle · cracked · Feb 13, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CREASEBEAM ANGLE.5 INCH, BS 630, RBL 45. FABRICATED NEW ANGLE PER SRM 51-10-1 AND DWG 65 47973. (M)
- [SDR USAA010156](https://openairdocs.org/sdr/USAA010156.md): Crease Beam · cracked · Feb 13, 2001 · N249US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND CREASEBEAM WEB CRACKED 1 INCH, AFT OUTBOARD CORNER AT STATION 638. SPLICED IN NEW SECTION PER SRM 51-10-1 AND 51-40-4. (M)
- [SDR USAA010152](https://openairdocs.org/sdr/USAA010152.md): Torque Box · cracked · Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TORQUE BOX WEB CRACKED.5 INCH, BS 947 JUST BELOW STRINGER 11L. REMOVED AND REPLACED DOUBLER AND FILLER PER TR 53-30-07 REV A. (M)
- [SDR USAA01043](https://openairdocs.org/sdr/USAA01043.md): Tie Clip · cracked · Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 707, STRINGER 10R. INSTALLED NEW TIE CLIP PER SRM 51-10-1 AND 51-30-2. (M)
- [SDR USAA010142](https://openairdocs.org/sdr/USAA010142.md): Tie Clip · cracked · Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.125 INCH, BS 706, STRINGER 6L. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)
- [SDR USAA010141](https://openairdocs.org/sdr/USAA010141.md): Clip · cracked · Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CLIP CRACKED.125 INCH, STATION 639, STRINGER 3L. INSTALLED NEW CLIP PER SRM 51-10-1. (M)
- [SDR USAA010140](https://openairdocs.org/sdr/USAA010140.md): Clip · cracked · Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CLIP CRACKED.125 INCH, STATION 616, STRINGER 2R. INSTALLED NEW CLIP PER SRM 51-10-1. (M)
- [SDR USAA010139](https://openairdocs.org/sdr/USAA010139.md): Clip · cracked · Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CLIP CRACKED.125 INCH, STATION 597, STRINGER 4R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)
- [SDR USAA010138](https://openairdocs.org/sdr/USAA010138.md): Floorbeam · corroded · Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 328, LBL 54. CORROSION LEVEL 1. INSTALLED UPPER SECTION PER TR 53-10-13 AND SRM 51-10-6. (M)
- [SDR USAA010148](https://openairdocs.org/sdr/USAA010148.md): Tie Clip · cracked · Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 807, STRINGER 11L. REPLACED TIE CLIP PER SRM 51-10-01 AND DWG 69-45156. (M)
- [SDR USAA010147](https://openairdocs.org/sdr/USAA010147.md): Tie Clip · cracked · Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.125 INCH, BS 807, STRINGER 10L. INSTALLED NEW CLIP PER SRM 51-10-1. (M)
- [SDR USAA010146](https://openairdocs.org/sdr/USAA010146.md): Tie Clip · cracked · Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 747, STRINGER 7R. INSTALLED NEW CLIP PER SRM 51-10-1. (M)
- [SDR USAA010145](https://openairdocs.org/sdr/USAA010145.md): Tie Clip · cracked · Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED, STATION 747, STRINGER 4R. INSTALLED NEW CLIP PER SRM 51-10-1. (M)
- [SDR USAA010144](https://openairdocs.org/sdr/USAA010144.md): Skin · cracked · Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED.5 INCH, FUSELAGE SKIN STATION 727A PLUS 8 JUST ABOVE STRINGER 18L. INSTALLED DOUBLER PER SRM 53-30-03. (M)
- [SDR USAA010262](https://openairdocs.org/sdr/USAA010262.md): Bulkhead · cracked · Feb 4, 2001 · N249US · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND PRESSURE BULKHEAD CRACKED 6.5 INCHES, BS 1016 PLUS 1 AT STRINGER 6L. INSTALLED FILLER, DOUBLER AND SHIMS. (M)
- [SDR USAA001393](https://openairdocs.org/sdr/USAA001393.md): Beam · corroded · Aug 30, 2000 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
  > TPA - FOUND BEAMS AND ANGLES CORRODED 12 INCHES, AFT LAV AREA FS 986 TO 1016. CORROSION LEVEL 1. REMOVED AND REPLACED BEAMS AND ANGLES PER SRM 51-10-1. (M)
- [SDR USAA000774](https://openairdocs.org/sdr/USAA000774.md): Skin · cracked · May 29, 2000 · N249US · Boeing 737201 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 1.5 INCHES, STATION 767, STRINGER 19L. PREVIOUS REPAIR TOO CLOSE TO DAMAGE. REMOVED IT AND INSTALLED LARGE REPAIR PER SRM 53-30-3 FIG 6. (M)
- [SDR USAASB00009](https://openairdocs.org/sdr/USAASB00009.md): Engine · failed · Jan 10, 2000 · N249US · Boeing 737201 · Engine (Turbine/Turboprop)
  > TPA - FLT 2746 - ON CLIMB-OUT FROM TPA, AT FL150, CREW REPORTED THE NR 1 ENGINE OIL PRESSURE WENT TO RED LINE WITH ENGINE TEMPERATURE FOLLOWING SHORTLY THEREAFTER. CREW SHUTDOWN THE NR 1 ENGINE, ADVISED AIR TRAFFIC CONTROL OF THE PROBLEM AND DECLARED AND EMER
- [SDR USAASB98154](https://openairdocs.org/sdr/USAASB98154.md): Battery Pack · discharged · Jun 24, 1998 · N249US · Boeing 737201 · Emergency Lighting
  > CMH - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)

Next page: https://openairdocs.org/deregistered/N249US-2003-09-26/reports.md?page=2

## 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 = 'N249US' AND deregistration_id = 'N249US-2003-09-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N249US-2003-09-26/reports

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