# Service difficulty reports: N264AU, cancelled Apr 28, 2003

A list on [N264AU, cancelled Apr 28, 2003](https://openairdocs.org/deregistered/N264AU-2003-04-28.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 · 89 reports

- [SDR USAASB01261](https://openairdocs.org/sdr/USAASB01261.md): Powerpack · failed · Sep 19, 2001 · N264AU · Boeing 737201 · Emergency Lighting
  > BWI - THE FORWARD RIGHT EMERGENCY EVACUATION SLIDE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)
- [SDR USAA011207](https://openairdocs.org/sdr/USAA011207.md): Stringer · cracked · Sep 5, 2001 · N264AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CRACKED.5 INCH, BS 360 STRINGER 11L. INSTALLED REPAIR DOUBLER PER SRM 53-1-2. (M)
- [SDR USAA011206](https://openairdocs.org/sdr/USAA011206.md): Stringer · cracked · Sep 5, 2001 · N264AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER SHELF 18A CRACKED.375 INCH, BS 727 AT STRINGER 18R. INSTALLED NON SHELF PER EA 85230. INSTALLED NON SHELF PER EA 85230. (M)
- [SDR USAA011205](https://openairdocs.org/sdr/USAA011205.md): Keelbeam · chafed · Sep 5, 2001 · N264AU · Boeing 737201 · Fuselage Main, Keel
  > CLT - FOUND KEEL BEAM CHAFED 1 INCH BY 27 INCHES, LEFT KEEL BEAM BS 700-727 LOWER CHORD. INSTALLED REPAIR WASHERS AND REPAIR STRAP PER EA 85306A. (M)
- [SDR USAA011204](https://openairdocs.org/sdr/USAA011204.md): Keelbeam · chafed · Sep 5, 2001 · N264AU · Boeing 737201 · Fuselage Main, Keel
  > CLT - FOUND KEEL BEAM CHAFED 1 INCH BY 64 INCHES, RT KEEL BEAM, BS 663-727. INSTALLED REPAIR WASHERS AND REPAIR STRAP PER EA 85306A. (M)
- [SDR USAA011203](https://openairdocs.org/sdr/USAA011203.md): Bulkhead · damaged · Sep 4, 2001 · N264AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB SKIN DAMAGED 10 SQUARE INCHES, BS 178, WL 196 TO WL 205, LBL 10.5 TO RBL 10.5. C/O DAMAGE VERIF, NO DAMAGE AT PERIM INSU CUT.100 MORE, INSTALLED DOUBLER PER EO 5300V153, EA 69902, SRM 531008. (M)
- [SDR USAA011202](https://openairdocs.org/sdr/USAA011202.md): Frame · corroded · Sep 4, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND FRAME CORRODED 5 INCHES, BS 415 STRINGER 25R. REMOVED DAMAGED SECTION OF STRINGER 25R, ADD STRINGER SPLICE J CHANNEL DOUBLER AND CENTER U-CHANNEL EA 85157, SRM 53-10-3. (M)
- [SDR USAA011201](https://openairdocs.org/sdr/USAA011201.md): Fitting · corroded · Sep 4, 2001 · N264AU · Boeing 737201 · Horizontal Stabilizer Structure
  > CLT - FOUND CORROSION ON CLEVIS LUG.019 INCH BY 2 INCH, LEFT HORIZONTAL CENTER, UP REAR SPAR AFT LUG, AFT FACE. SPOT FACED AFFECTED AREA AND INSTALLED NEW BUSHINGS PER EA NR 85229. (M)
- [SDR USAA011200](https://openairdocs.org/sdr/USAA011200.md): Fitting · corroded · Sep 4, 2001 · N264AU · Boeing 737201 · Horizontal Stabilizer Structure
  > CLT - FOUND CORROSION ON CLEVIS LUG.020 INCH BY 2 INCH, LEFT HORIZONTAL, STAB CENTER SECTION UP REAR SPAR FORWARD LUG. SPOT FACED AFFECTED AREA AND INSTALLED NEW BUSHINGS PER EA NR 85229. (M)
- [SDR USAA011196](https://openairdocs.org/sdr/USAA011196.md): Skin · corroded · Sep 4, 2001 · N264AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CORRODED 1 INCH BY 2 INCH, BS 1016. CORROSION LEVEL 2. INSTALLED DOUBLER PER EA 85159 AND EA 85231. (M)
- [SDR USAA011189](https://openairdocs.org/sdr/USAA011189.md): Bear Strap · corroded · Aug 31, 2001 · N264AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND DOOR C/O BEARSTRAP CORRODED 3 INCHES BY 5 INCHES, BS 485 AND BS 440 AND BS 420. INSTALLED FILLER AND DOUBLER AND 2 TRIPLERS PER EA NR 85292. (M)
- [SDR USAA011188](https://openairdocs.org/sdr/USAA011188.md): Frame · cracked · Aug 31, 2001 · N264AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND CHORD ANGLE CRACKED 1 INCH, BS 178 BULKHEAD RIGHT SIDE RADIUS WL 195. REMOVED AND REPLACED CHORD SECTION, INSTALLED INT DOUBLER ANGLE AND EX DOUBLER STRAP PER EO 5300V157AND EA 85332. (M)
- [SDR USAA011171](https://openairdocs.org/sdr/USAA011171.md): Floorbeam · cracked · Aug 30, 2001 · N264AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CRACKED 3 INCH, BS 663 BL 0. INSTALLED DOUBLER, SPLICE PLATES AND STIFFENERS, PER T/R 57-10-04 AND EA 69909. (M)
- [SDR USAA011170](https://openairdocs.org/sdr/USAA011170.md): Floorbeam · cracked · Aug 30, 2001 · N264AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM WEB CRACKED.5 INCH, BS 663 BL0. INSTALLED DOUBLER SPLICE PLATES AND STIFFENERS, PER TT 57-10-04 AND EA 69909. (M)
- [SDR USAA011169](https://openairdocs.org/sdr/USAA011169.md): Frame · corroded · Aug 29, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND FRAME CORRODED, BS 807 STRINGER 17R TO STRINGER 27R, CORROSION LEVEL 1 TASK NR C53-100-01. (M)
- [SDR USAA011157](https://openairdocs.org/sdr/USAA011157.md): Stringer · cracked · Aug 28, 2001 · N264AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND SHELF WEB CRACKED 3 INCHES, RIGHT 18A SHELF. REPLACED WITH NEW PART PER SRM 51-10-1 AND EO 85230. (M)
- [SDR USAA011156](https://openairdocs.org/sdr/USAA011156.md): Frame · corroded · Aug 28, 2001 · N264AU · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND FRAME CORRODED 2 INCHES BY 5 INCHES, BS 500 BL0. CORROSION LEVEL 1, TASK NR 90-25-01. CUT OUT DAMAGE ON FRM, HFEC INSPECTION FMD PARTS, HT TREAT/INSTALLED PER SRM 53-10-4/51-10-6/53-30-1. (M)
- [SDR USAA011152](https://openairdocs.org/sdr/USAA011152.md): Bulkhead · cracked · Aug 24, 2001 · N264AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB SKIN CRACKED.500 INCH, BS 178 BULKHEAD, LBL 1,WL 206. REMOVED DAMAGE, HFEC INSPECTION. CUT.100 MORE, INSTALLED DOUBLER PER EO 5300V153, EA 69902, SRM 53-10-08. (M)
- [SDR USAA011150](https://openairdocs.org/sdr/USAA011150.md): Bulkhead · cracked · Aug 24, 2001 · N264AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB SKIN CRACKED.500 INCH, BS 178 BULKHEAD, RBL 1, WL 206. REMOVED DAMAGED HFEC INSPECTION, CUT.100 MORE, INSTALLED DOUBLER PER EO 5300V153 EA 69902, SRM 53-10-08. (M)
- [SDR USAA011149](https://openairdocs.org/sdr/USAA011149.md): Web · cracked · Aug 24, 2001 · N264AU · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND WEB CRACKED 1 INCH, BS 178 BULKHEAD AT WL 207.5 AT RBL 1 TO 2. INSTALLED DOUBLER DAMAGE. REMOVED HFEC DONE. PER EO 5300V153 EA 69902, SRM 53-10-08 FIG 211. (M)
- [SDR USAA011142](https://openairdocs.org/sdr/USAA011142.md): Bulkhead · gouged · Aug 22, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND PRESSURE AFT BULKHEAD WITH 3 GOUGES APPROXIMATELY.125 INCH, LBL 3 BS 1016. INSTALLED DOUBLER, TRIPLER, FILLER OF REPAIR PER EA 85254. (M)
- [SDR USAA011141](https://openairdocs.org/sdr/USAA011141.md): Floorbeam · corroded · Aug 22, 2001 · N264AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND INTERCOSTAL CORRODED 2 INCHES BY 2.5 INCHES, BS 312, FLOORBEAM LBL 8.5 TO RBL 11 UPPER SURFACE. CORROSION TASK NR C53-107-01. REMOVED AND REPLACED FLOORBEAM UPPER CHORD WITH PART NR 65-45834-523 PER SRM 51-10-1. (M)
- [SDR USAA011140](https://openairdocs.org/sdr/USAA011140.md): Frame · cracked · Aug 22, 2001 · N264AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND CHORD ANGLE CRACKED 1 INCH, RIGHT SIDE CHORD BS 178 AT WL 207. INSTALLED REPAIR, SIDE CHORD, PER EO 5300V157. (M)
- [SDR USAA011139](https://openairdocs.org/sdr/USAA011139.md): Frame · cracked · Aug 22, 2001 · N264AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND CHORD ANGLE CRACKED 1 INCH, BS 178 SIDE CHORD AT WL 207, LEFT SIDE. INSTALLED REPAIR SIDE CHORD PER EO 5300V157. (M)
- [SDR USA011106](https://openairdocs.org/sdr/USA011106.md): Skin · cracked · Aug 20, 2001 · N264AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED, AFT ENTRY DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 34. (M)
- [SDR USAA011104](https://openairdocs.org/sdr/USAA011104.md): Stringer · corroded · Aug 20, 2001 · N264AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER AND TIE CLIP CORRODED 1 INCH, BS 538, S26R. REMOVED AND REPLACED PART PER SRM 53-10-03. (M)
- [SDR USAA011103](https://openairdocs.org/sdr/USAA011103.md): Tie Clip · Aug 20, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND TIE CLIP WITH WRONG TYPE CLIP INSTALLED, BS 596-S9L. INSTALLED NEW TIE CLIP PER EO NR 5393G227. (M)
- [SDR USAA011102](https://openairdocs.org/sdr/USAA011102.md): Frame · cracked · Aug 20, 2001 · N264AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND FRAME OUTER CHORD CRACKED 1 INCH, BS 597, 6 INCHES BELOW S17L ON FORWARD SIDE OF FRAME. REMOVED AND REPLACED WITH PART NR 65-46538-33 PER SRM 51-30-2. (M)
- [SDR USA011101](https://openairdocs.org/sdr/USA011101.md): Floorbeam · unknown · Aug 20, 2001 · N264AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM NO CRACKS PER NDT, BS 520 RBL 45. INSTALLED DOUBLER PER EA 85214. (M)
- [SDR USAA011100](https://openairdocs.org/sdr/USAA011100.md): Web · corroded · Aug 20, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND FLOORBEAM WEB CORRODED, BS 344 FLOORBEAM, LBL 14.5 TO 21.5. CORROSION LEVEL 1, TASK NR C53-107-01. BLENDED OUT CORROSION, INSTALLED DOUBLER AND TRIPLER PER EA 85198. (M)
- [SDR USAA011099](https://openairdocs.org/sdr/USAA011099.md): Frame · cracked · Aug 20, 2001 · N264AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND CHORD CRACKED.250 INCH, BS 178, LBL 5.6, RBL 5.7, WL 184. INSTALLED REPAIR ANGLES PER EO 5300 US155 PER JC MC-90-93857. (M)
- [SDR USAA011098](https://openairdocs.org/sdr/USAA011098.md): Frame · cracked · Aug 20, 2001 · N264AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND FRAME OUTER CHORD 1 INCH, BS 597, 6 INCHES BELOW 17L ON AFT SIDE OF FRAME. REMOVED AND REPLACED PART WITH PART NR 1126923 PER SRM 51-30-2. (M)
- [SDR USAA011097](https://openairdocs.org/sdr/USAA011097.md): Frame · cracked · Aug 20, 2001 · N264AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND CHORD CRACKED 1 INCH, BS 178, LBL 5.8, WL 184. INSTALLED REPAIR ANGLES PER EO 5300V155 PER M2-90-93857. (M)
- [SDR USAA011089](https://openairdocs.org/sdr/USAA011089.md): Skin · dented · Aug 14, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND SKIN DENTED AND GOUGED 1 INCH BY.070 INCH, BS 309 JUST BELOW BS 24R. FABRICATED AND INSTALLED FILLERS AND REPAIR DOUBLERS PER SRM 53-30-3 FIG 42. (M)
- [SDR USAA011088](https://openairdocs.org/sdr/USAA011088.md): Floorbeam · corroded · Aug 14, 2001 · N264AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 3 SQUARE INCHES, BS 1006 LBL 10. CORROSION LEVEL 1. REPLACED T-CAP PER SRM 53-10-9. (M)
- [SDR USAA011087](https://openairdocs.org/sdr/USAA011087.md): Floorbeam · cracked · Aug 14, 2001 · N264AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CRACKED 1.5 INCH, BS 520 LBL 45. INSTALLED DOUBLER PER EA 85214. (M)
- [SDR USAA011086](https://openairdocs.org/sdr/USAA011086.md): Angle · cracked · Aug 14, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND ANGLE CRACKED.5 INCH, BS 328 FLOORBEAM RBL 31.5 TO INTERCOSTAL. FABRICATED REPAIR DOUBLER PER SRM 53-10-02. (M)
- [SDR USAA011085](https://openairdocs.org/sdr/USAA011085.md): Stringer · cracked · Aug 14, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND STRINGER CRACKED.5 INCH, BS 359 S11L. REMOVED AND REPLACED PART WITH PART NR 1126212 PER 51-10-1. (M)
- [SDR USAA011093](https://openairdocs.org/sdr/USAA011093.md): Web · corroded · Aug 14, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND CREASE BEAM WEB CORRODED 10 SQUARE INCHES, LEFT SIDE BS 927-947. FABRICATED NEW WEB PER DRAWING 65-52878 AND INSTALLED PER SRM 51-30-2. (M)
- [SDR USAA011092](https://openairdocs.org/sdr/USAA011092.md): Floorbeam · cracked · Aug 14, 2001 · N264AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CRACKED.5 INCHES, BS 520 TO RBL 24 AND LBL 24. INSTALLED DOUBLER PER EA 85215. (M)
- [SDR USAA011064](https://openairdocs.org/sdr/USAA011064.md): Angle · bent · Aug 13, 2001 · N264AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND DRAG ANGLE BENT, RIGHT AFT VERTICAL STABILIZER MOUNT AREA. FABRICATED AND INSTALLED REPAIR STRAPS AND FILLERS PER EA 85186. (M)
- [SDR USAA01061](https://openairdocs.org/sdr/USAA01061.md): Intercostal · cracked · Aug 13, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND INTERCOSTAL CRACKED.75 INCH, BS 300.5 TO BS 301.5 S10L. INSTALLED NEW ANGLE PER SRM 51-10-1. (M)
- [SDR USAA011059](https://openairdocs.org/sdr/USAA011059.md): Web · cracked · Aug 13, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND WEB CRACKED TWO PLACES.060 INCH, BULKHEAD WEB AT ATTACH TO 1016 Y CHORD. INSTALLED DOUBLER PER SRM 53-10-4 AND SRM 51-30-5. (M)
- [SDR USAA011058](https://openairdocs.org/sdr/USAA011058.md): Frame · dented · Aug 13, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND FRAME DENTED.25 INCH, BS 827 AT S24L UPPER CHORD. INSTALLED FRAME DOUBLER PER SRM 53-10-4. (M)
- [SDR USAA011057](https://openairdocs.org/sdr/USAA011057.md): Stringer · cracked · Aug 13, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND STRINGER CRACKED.5 INCH, BS 359 S14L. REMOVED AND REPLACED WITH PART NR 1131272 PER SRM 51-10-01. (M)
- [SDR USAA011055](https://openairdocs.org/sdr/USAA011055.md): Frame · cracked · Aug 13, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND FRAME CRACKED.250 INCH, BS 380 STRINGER 26L. FABRICATED REPLACEMENT PART PER SRM 53-10-04. (M)
- [SDR USAA011056](https://openairdocs.org/sdr/USAA011056.md): Angle · corroded · Aug 13, 2001 · N264AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND Z-CHORD CORRODED 2 INCHES BY 10 INCHES, BS 947 TO BS 996. REMOVED AND REPLACED WITH NEW PART NR 1124774 PER SRM 51-10-1 AND SRM 51-30-02. (M)
- [SDR USAA011060](https://openairdocs.org/sdr/USAA011060.md): Floorbeam · corroded · Aug 13, 2001 · N264AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND TOP SURFACE OF T-CAP CORRODED, BS 947 RBL 22 THROUGH LBL 9. REPLACED T-CAP, INSTALLED PER EA 85177. (M)
- [SDR USAA011054](https://openairdocs.org/sdr/USAA011054.md): Skin · dented · Aug 10, 2001 · N264AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND SKIN DENTED 2 INCHES BY 8 INCHES BY.250 INCH, BS 827 STRINGER 27L. PREVIOUS REPAIR, FOUND AT S27L, REPORT STATES S27R, PER SRM 53-30-3. (M)
- [SDR USAA011053](https://openairdocs.org/sdr/USAA011053.md): Pressure Panel · damaged · Aug 10, 2001 · N264AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND BEADS MISSING IN PRESSURE WEB, BS 662 TO BS 673 WL 203. INSTALLED ANGLE STIFFENERS PER EA 85189 REF SB 737-57-1234. (M)

Next page: https://openairdocs.org/deregistered/N264AU-2003-04-28/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 = 'N264AU' AND deregistration_id = 'N264AU-2003-04-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N264AU-2003-04-28/reports

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