# Service difficulty reports: N251AU, cancelled Aug 13, 2003

A list on [N251AU, cancelled Aug 13, 2003](https://openairdocs.org/deregistered/N251AU-2003-08-13.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 3 · 107 reports

- [SDR USAA011361](https://openairdocs.org/sdr/USAA011361.md): Skin · cracked · Nov 7, 2001 · N251AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED.20, FUSELAGE SKIN BETWEEN FRAME 727A AND 727B STRINGER 16R. INSTALLED DOUBLER AND REPAIR ANGLE PER EA 72869 AND SRM 53-30-3. (M)
- [SDR USAASB01294](https://openairdocs.org/sdr/USAASB01294.md): Battery Pack · discharged · Oct 13, 2001 · N251AU · Boeing 737201 · Emergency Lighting
  > BWI - THE RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M)
- [SDR USAASB01233](https://openairdocs.org/sdr/USAASB01233.md): Light · not seated · Aug 15, 2001 · N251AU · Boeing 737201 · Emergency Lighting
  > BWI - PILOT REPORTED THE THE EMERGENCY EXIT LIGHT AT THE FORWARD ENTRY DOOR WAS ILLUMINATED. MAINTENANCE RESEATED THE LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. (M)
- [SDR USAA010300](https://openairdocs.org/sdr/USAA010300.md): Bulkhead · cracked · Mar 20, 2001 · N251AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND HORIZ WEB CRACKED 1 INCH, BS 178 BULKHEAD, WL 207, RBL 29. REMOVED AND REPLACED WEB PER EO 5300V157. (M)
- [SDR USAA010267](https://openairdocs.org/sdr/USAA010267.md): Skin · cracked · Feb 28, 2001 · N251AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - FOUND SKIN CRACKED 2.5 INCHES, STATION 951, STRINGER 20L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M)
- [SDR USAA010221](https://openairdocs.org/sdr/USAA010221.md): Intercostal · cracked · Feb 20, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND INTERCOSTAL CRACKED 1 INCH, 178 BULKHEAD, RBL 26, WL 195. MODIFIED PART INSTALLED PER EA 68934. (M)
- [SDR USAA010247](https://openairdocs.org/sdr/USAA010247.md): Floorbeam · corroded · Feb 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOOR FRAME CORRODED 4 SQUARE INCHES, STATION 987.5 LBL 14, RBL 15, RBL 24. REPLACED T-CAP FROM LEFT AND RIGHT EXTREMITIES PER TYP REP 53-60-01. CORROSION LEVEL 1, TASK NR C53-107-02. (M)
- [SDR USAA010246](https://openairdocs.org/sdr/USAA010246.md): Floorbeam · corroded · Feb 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOOR FRAME CORRODED 12 SQUARE INCHES, BS 947.5 LBL 30 - RBL 49. FABRICATED T-CAP AND SPLICE PARTS PER 53-10-9. CORROSION LEVEL 1, TASK NR C53-107-02. (M)
- [SDR USAA010249](https://openairdocs.org/sdr/USAA010249.md): Angle · cracked · Feb 14, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CHORD ANGLE CRACKED.5 INCH, STATION 663 RBL 24, WL 201.5. INSTALLED REPAIR ANGLES PER DRW 65C37732, EA 68973. (M)
- [SDR USAA010136](https://openairdocs.org/sdr/USAA010136.md): Skin · cracked · Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1 INCH, FS 785 AT STRINGER 19L. INSTALLED DOUBLER PER EA 69066. (M)
- [SDR USAA010135](https://openairdocs.org/sdr/USAA010135.md): Tie Clip · cracked · Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.125 INCH, STATION 685 STRINGER 4L. REPLACED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA010134](https://openairdocs.org/sdr/USAA010134.md): Tie Clip · cracked · Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 727G, STRINGER 8R. REPLACED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA010133](https://openairdocs.org/sdr/USAA010133.md): Tie Clip · cracked · Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.125 INCH, STATION 616, STRINGER 2L. INSTALLED NEW TIE CLIP PE EO 5393G227. (M)
- [SDR USAA010132](https://openairdocs.org/sdr/USAA010132.md): Tie Clip · cracked · Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.125 INCH, STATION 616, STRINGER 6L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)
- [SDR USAA010155](https://openairdocs.org/sdr/USAA010155.md): Frame · cracked · Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND SIDE CHORD CRACKED 1 INCH, STATION 178, WL 207 AND 195 RIGHT SIDE. SPLICED IN NEW SIDE CORD PER EO 5300V157. (M)
- [SDR USAA010154](https://openairdocs.org/sdr/USAA010154.md): Frame · cracked · Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND SIDE CHORD CRACKED 1 INCH, TWO PLACES, STATION 178, WL 207, AND WL 195, LEFT SIDE. SPLICED IN NEW SIDE CHORD PER EO 5300V157. (M)
- [SDR USAA010137](https://openairdocs.org/sdr/USAA010137.md): Bulkhead · cracked · Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND BULKHEAD CRACKED.125 INCH, TWO PLACES, BS 1016 AT APPROX STRINGER 3L. INSTALLED DOUBLER PER EA 69021. (M)
- [SDR USAA010151](https://openairdocs.org/sdr/USAA010151.md): Skin · cracked · Feb 12, 2001 · N251AU · Boeing 737201 · Service Doors
  > CLT - FOUND SKIN CRACKED 1.60 INCH, RIGHT AFT SERVICE DOOR BEAR STRAP. INSTALLED TRIPLER PER SRM 53-30-3. (M)
- [SDR USAA010150](https://openairdocs.org/sdr/USAA010150.md): Frame · cracked · Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH, STATION 767, STRINGER 13L. INSTALLED DOUBLER PER SRM 53-10-4 FIG 1. (M)
- [SDR USAA010149](https://openairdocs.org/sdr/USAA010149.md): Web · cracked · Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED.25 INCH, STATION 767 WEB CRACKED STRINGER 13R. INSTALLED RADIUS BLOCK PER EA 69053. (M)
- [SDR USAA010125](https://openairdocs.org/sdr/USAA010125.md): Bulkhead · cracked · Feb 6, 2001 · N251AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND BULKHEAD CRACKED.125 INCH, BS 1016, STRINGER 6L. INSTALLED DOUBLER AND TRIPLER PER SRM 53-10-4 FIG 15. (M)
- [SDR USAA01024](https://openairdocs.org/sdr/USAA01024.md): Angle · cracked · Feb 6, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND UPPER CHORD ANGLE CRACKED.5 INCH, STATION 663, RBL 24, WL 201.5. INSTALLED REPAIR ANGLES PER EA 68973. (M)
- [SDR USAA010123](https://openairdocs.org/sdr/USAA010123.md): Frame · cracked · Feb 6, 2001 · N251AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND CHORD FRAME CRACKED.75 INCH, STATION 639, WL 210. REMOVED AND REPLACED PER REPAIR DOCUMENT 51-30-2. (M)
- [SDR USAA010112A](https://openairdocs.org/sdr/USAA010112A.md): Web · cracked · Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED.25 INCH, STATION 334 STRINGER 8R AT FORWARD SERVICE DOOR. REPLACED SHEAR WEB PER DRAWING 65C33288. (M)
- [SDR USAA010122](https://openairdocs.org/sdr/USAA010122.md): Shear Tie · cracked · Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND SHEAR TIE CRACKED.75 INCH, FS 1040 BETWEEN STRINGER 2/3 RT. INSTALLED SHEAR TIE PER DWG 65-46569. (M)
- [SDR USAA010121](https://openairdocs.org/sdr/USAA010121.md): Shear Tie · cracked · Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND SHEAR TIE CRACKED 1 INCH, STATION 1040 STRINGER 2L AND 3L. INSTALLED REPAIR PER DWG 65 46569. (M)
- [SDR USAA010120](https://openairdocs.org/sdr/USAA010120.md): Skin · cracked · Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 2.5 INCH, STATION 727B PLUS 2 AND 727A PLUS 8 STRINGER 18L. INSTALLED REPAIR DOUBLER PER SRM 53-30-3. (M)
- [SDR USAA010119](https://openairdocs.org/sdr/USAA010119.md): Floorbeam · cracked · Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM WEB CRACKED 1 INCH, STATION 727, RBL 24.5. FABRICATED REPAIR AND INSTALLED PER EA 68992A. (M)
- [SDR USAA010118](https://openairdocs.org/sdr/USAA010118.md): Floorbeam · cracked · Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM WEB CRACKED 1 INCH, STATION 706, LBL 24.5. FABRICATED REPAIR AND INSTALLED PER EA 69008 AND 69031. (M)
- [SDR USAA010117](https://openairdocs.org/sdr/USAA010117.md): Floorbeam · cracked · Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CRACKED 1 INCH, STATION 695 LBL 45.5. INSTALLED DOUBLER PER SRM 51-40-4. (M)
- [SDR USAA010116](https://openairdocs.org/sdr/USAA010116.md): Floor Support · cracked · Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND FLOOR SUPPORT CRACKED 1 INCH, STATION 540. REPLACED FLOOR SUPPORT PER SRM 51-10-01. (M)
- [SDR USAA010115](https://openairdocs.org/sdr/USAA010115.md): Web · cracked · Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED 6 INCHES, STATION 520, RBL 24.5. REPAIRED PER SRM 51-10-10. (M)
- [SDR USAA010114](https://openairdocs.org/sdr/USAA010114.md): Doubler · cracked · Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND PRODUCTION DOUBLER CRACKED 1 INCH, 4 PLACES, BL 0, STATION 370 TO 380. INSTALLED DOUBLER PER EA 69056. (M)
- [SDR USAA010113](https://openairdocs.org/sdr/USAA010113.md): Bulkhead · cracked · Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND BULKHEAD CRACKED.250 INCH, STATION 178 BULKHEAD, WL 224, RBL 2. INSTALLED TRIPLER PER EA 68961 AND EO 5300V153. (M)
- [SDR USAA010248](https://openairdocs.org/sdr/USAA010248.md): Intercostal · corroded · Feb 3, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND INTERCOSTAL CORRODED 2 SQUARE INCHES, BS 987.9, LBL 20 TO STATION 1016, LBL 6. FABRICATED NEW INTERCOSTAL PER 51-30-0 AND 51-10-1. CORROSION LEVEL1, TASK NR C53-107-02. (M)
- [SDR USAA010099](https://openairdocs.org/sdr/USAA010099.md): Web · cracked · Jan 30, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED 3 INCHES, STATION 663.7, BL 0. INSTALLED DOUBLER PER TR 57-10-04. (M)
- [SDR USAA010098](https://openairdocs.org/sdr/USAA010098.md): Floorbeam · cracked · Jan 30, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND T-CAP CRACKED 4 INCHES, STATION 663, BL 0. INSTALLED REPAIR ANGLES PER TR 57-10-04 AND EA 69046. (M)
- [SDR USAA010097](https://openairdocs.org/sdr/USAA010097.md): Clip · cracked · Jan 30, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CLIP CRACKED.75 INCH, INTERCOSTAL FUSELAGE FRAME ATTACHED CLIP. INSTALLED DOUBLER PER SRM 51-40-3. (M)
- [SDR USAA010096](https://openairdocs.org/sdr/USAA010096.md): Stiffener · cracked · Jan 30, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND STIFFENER CRACKED 2 INCHES, STRINGER 10L 294. INSTALLED STIFFENER PER EA 68991. (M)
- [SDR USAA010095](https://openairdocs.org/sdr/USAA010095.md): Skin · cracked · Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 14 INCHES BY 8 INCHES, STRINGER 17R TO 19R, STATION 727A. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)
- [SDR USAA010094](https://openairdocs.org/sdr/USAA010094.md): Skin · cracked · Jan 29, 2001 · N251AU · Boeing 737201 · Passenger/Crew Doors
  > CLT - FOUND SKIN CRACKED 2.5 INCHES, LEFT AFT ENTRY DOOR OUTER SKIN STRINGER 17L PLUS 960. INSTALLED DOUBLER PER SRM 53-30-3. (M)
- [SDR USAA010093](https://openairdocs.org/sdr/USAA010093.md): Frame · cracked · Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.25 INCH, STATION 747 FRAME PLUS STRINGER 13L. INSTALLED DOUBLER PER SRM 53-10-4. (M)
- [SDR USAA010092](https://openairdocs.org/sdr/USAA010092.md): Angle · cracked · Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CHORD ANGLE CRACKED.75 INCH, STATION 663, LBL 23, WL 201.5. INSTALLED DOUBLER PER EA 68798. (M)
- [SDR USAA010091](https://openairdocs.org/sdr/USAA010091.md): Floorbeam · cracked · Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CRACKED 1 INCH, STATION 663, LBL 0.0. INSTALLED DOUBLER AND ANGLES PER SRM 53-10-9. (M)
- [SDR USAA010090](https://openairdocs.org/sdr/USAA010090.md): Beam · cracked · Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND BEAM CRACKED 1.8 INCH, STATION 520, RBL 45.5. REPAIRED DOUBLER PER SB 737-53-1120. (M)
- [SDR USAA010089](https://openairdocs.org/sdr/USAA010089.md): Beam · cracked · Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND BEAM CRACKED 1.3 INCH, STATION 520-540, LBL 45.5. REPAIRED DOUBLER PER SB 737-53-1120. (M)
- [SDR USAA010088](https://openairdocs.org/sdr/USAA010088.md): Beam · cracked · Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND BEAM CRACKED 1.5 INCH, STATION 520, LBL 24. REPAIRED DOUBLER PER SB 737-53-1120. (M)
- [SDR USAA010087](https://openairdocs.org/sdr/USAA010087.md): Tie Clip · cracked · Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED 1 INCH, BS 520, STRINGER 19R. INSTALLED REPAIR PER SRM 51-40-3. (M)
- [SDR USAA010086](https://openairdocs.org/sdr/USAA010086.md): Structure · cracked · Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND INNER CHORD CRACKED 3 INCHES, STATION 294, WL 208. REPLACED CHORD PER SRM 51-10-01. (M)
- [SDR USAA010085](https://openairdocs.org/sdr/USAA010085.md): Bulkhead · cracked · Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND BULKHEAD CRACKED.5 INCH, WL 234, RBL 10. INSTALLED DOUBLER PER SRM 53-10-08. (M)

Next page: https://openairdocs.org/deregistered/N251AU-2003-08-13/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 = 'N251AU' AND deregistration_id = 'N251AU-2003-08-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N251AU-2003-08-13/reports

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