# Service difficulty reports: N325SW, cancelled Mar 28, 2012

A list on [N325SW, cancelled Mar 28, 2012](https://openairdocs.org/deregistered/N325SW-2012-03-28.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 7 · 344 reports

- [SDR SWAA117312](https://openairdocs.org/sdr/SWAA117312.md): Slide · out of position · Oct 22, 2011 · N325SW · Boeing 7373H4 · Escape Slide
  > R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CASE, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.
- [SDR SWAA116311](https://openairdocs.org/sdr/SWAA116311.md): Sign · loose · Sep 5, 2011 · N325SW · Boeing 7373H4 · Emergency Lighting
  > DURING SCHEDULED CV CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM.
- [SDR SWAA113869](https://openairdocs.org/sdr/SWAA113869.md): Light · inoperative · May 26, 2011 · N325SW · Boeing 7373H4 · Emergency Lighting
  > DURING SCHEDULED 24Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 13. RELAMPED LIGHT PER MM.
- [SDR SWAA113868](https://openairdocs.org/sdr/SWAA113868.md): Light · inoperative · May 26, 2011 · N325SW · Boeing 7373H4 · Emergency Lighting
  > DURING SCHEDULED 24Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 6. RELAMPED LIGHT PER MM.
- [SDR SWAA113844](https://openairdocs.org/sdr/SWAA113844.md): Attach Fitting · cracked · May 25, 2011 · N325SW · Boeing 7373H4 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED 24Y CHECK FOUND, STUB BEAM ATTACH CLIP ANGLE CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP PER EA.
- [SDR SWAA113843](https://openairdocs.org/sdr/SWAA113843.md): Floorbeam · cracked · May 25, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Floor Beam
  > DURING SCHEDULED 24Y CHECK FOUND, LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED AT BS 662, RBL 24. REPAIRED CHORD PER ER AND EA.
- [SDR SWAA113842](https://openairdocs.org/sdr/SWAA113842.md): Skin · cracked · May 25, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 500D+14, STR 15L. REPAIRED SKIN PER EA.
- [SDR SWAA113782](https://openairdocs.org/sdr/SWAA113782.md): Stringer · corroded · May 24, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED 24Y CHECK FOUND, STRINGER CORRODED BETWEEN BS 1006 TO BS 1014, STR 26R. REMOVED AND REPLACED STRINGER PER SRM.
- [SDR SWAA113781](https://openairdocs.org/sdr/SWAA113781.md): Skin · cracked · May 24, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 24Y CHECK FOUND, FUSELAGE SKIN CRACKED AT R1 DOOR UPPER AFT CORNER. REPAIRED SKIN PER ER.
- [SDR SWAA113780](https://openairdocs.org/sdr/SWAA113780.md): Shear Tie · corroded · May 24, 2011 · N325SW · Boeing 7373H4 · Fuselage Internal Mounting Structure
  > DURING SCHEDULED 24Y CHECK FOUND, SHEAR TIE CORRODED AT BS 967, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.
- [SDR SWAA113779](https://openairdocs.org/sdr/SWAA113779.md): Frame · cracked · May 24, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Frame
  > DURING SCHEDULED 24Y CHECK FOUND, FRAME WEB CRACKED AT BS 420, 1R. REPAIRED FRAME PER SRM.
- [SDR SWAA113778](https://openairdocs.org/sdr/SWAA113778.md): Skin · cracked · May 24, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 24Y CHECK FOUND, SKIN CRACKED AT BS 500D+18, STR 12R. REPAIRED SKIN PER ER.
- [SDR SWAA113777](https://openairdocs.org/sdr/SWAA113777.md): Skin · cracked · May 24, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 24Y CHECK FOUND, SKIN CRACKED AT BS 760, STR 19L. REPAIRED SKIN PER ER.
- [SDR SWAA113776](https://openairdocs.org/sdr/SWAA113776.md): Frame · cracked · May 24, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Frame
  > DURING SCHEDULED 24Y CHECK FOUND, FRAME CRACKED AT BS 727D, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SRM.
- [SDR SWAA113775](https://openairdocs.org/sdr/SWAA113775.md): Frame · cracked · May 24, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Frame
  > DURING SCHEDULED 24Y CHECK FOUND, FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER SRM.
- [SDR SWAA113774](https://openairdocs.org/sdr/SWAA113774.md): Shear Tie · corroded · May 24, 2011 · N325SW · Boeing 7373H4 · Fuselage Internal Mounting Structure
  > DURING SCHEDULED 24Y CHECK FOUND, SHEAR TIE CORRODED AT BS 947, BETWEEN STR 24L TO STR 26L. REPAIRED SHEAR TIE PER ER.
- [SDR SWAA113773](https://openairdocs.org/sdr/SWAA113773.md): Shear Tie · corroded · May 24, 2011 · N325SW · Boeing 7373H4 · Fuselage Internal Mounting Structure
  > DURING SCHEDULED 24Y CHECK FOUND, SHEAR TIE CORRODED AT BS 500, BETWEEN LBL 6 TO RBL 6. REPAIRED SHEAR TIE PER ER.
- [SDR SWAA113772](https://openairdocs.org/sdr/SWAA113772.md): Skin · cracked · May 24, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 24Y CHECK FOUND, SKIN CRACKED AT BS 308, STR 18R. REPAIRED SKIN PER SRM.
- [SDR SWAA113743](https://openairdocs.org/sdr/SWAA113743.md): Bulkhead · cracked · May 23, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Bulkhead
  > DURING SCHEDULED 24Y CHECK FOUND, PRESSURE DOME CRACKED AT BS 1016, STR 15L. REPAIRED DOME PER SRM.
- [SDR SWAA113742](https://openairdocs.org/sdr/SWAA113742.md): Floorbeam · cracked · May 23, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Floor Beam
  > DURING SCHEDULED 24Y CHECK FOUND, LONGITUIDNAL FLOORBEAM CRACKED BETWEEN BS 662 TO BS 665, LBL 24.5. REPAIRED BEAM PER EA.
- [SDR SWAA113631](https://openairdocs.org/sdr/SWAA113631.md): Frame · cracked · May 23, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Frame
  > DURING SCHEDULED 24Y CHECK FOUND, FRAME WEB CRACKED AT BS 947.5, STR 19L. REPAIRED WEB PER EA.
- [SDR SWAA113550](https://openairdocs.org/sdr/SWAA113550.md): Angle · cracked · May 23, 2011 · N325SW · Boeing 7373H4 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED 24Y CHECK FOUND, LT LONGITUDINAL BEAM L-ANGLE CRACKED, BS 694, BL 0. REMOVED AND REPLACED ANGLE PER SRM.
- [SDR SWAA113554](https://openairdocs.org/sdr/SWAA113554.md): Floorbeam · corroded · May 19, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Floor Beam
  > DURING SCHEDULED 24Y CHECK FOUND, FLOOR BEAM Z-CHORD CORRODED AT BS 270, LBL 10. REMOVED AND REPLACED Z-CHORD PER SRM.
- [SDR SWAA113553](https://openairdocs.org/sdr/SWAA113553.md): Stringer · corroded · May 19, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED 24Y CHECK FOUND, STRINGER CORRODED AT BS 989, STR 25L. REMOVED AND REPLACED STRINGER PER SRM.
- [SDR SWAA113468](https://openairdocs.org/sdr/SWAA113468.md): Stringer Clip · cracked · May 19, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 24Y CHECK FOUND, CRACKED STRINGER CLIP AT BS 520 STR 15L. REMOVED AND REPLACED CLIP PER SRM.
- [SDR SWAA113467](https://openairdocs.org/sdr/SWAA113467.md): Stringer Splice · corroded · May 19, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED 24Y CHECK FOUND, STRINGER SPLICE CORRODED AT BS 907, STR 26R. REPAIRED SPLICE PER SRM.
- [SDR SWAA113466](https://openairdocs.org/sdr/SWAA113466.md): Skin · cracked · May 19, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 24Y CHECK FOUND, SKIN CRACKED BS 920, STR 25R. REPAIRED SKIN PER SRM.
- [SDR SWAA113465](https://openairdocs.org/sdr/SWAA113465.md): Skin · cracked · May 19, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 24Y CHECK FOUND, SKIN CRACKED AT BS 842, STR 15L. REPAIRED SKIN PER ER.
- [SDR SWAA113463](https://openairdocs.org/sdr/SWAA113463.md): Attach Angle · cracked · May 19, 2011 · N325SW · Boeing 7373H4 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED 24Y CHECK FOUND, CREASE BEAM WEB ATTACH ANGLE CRACKED AT BS 615, RBL 64. REMOVED AND REPLACED CHANNEL PER SRM.
- [SDR SWAA113462](https://openairdocs.org/sdr/SWAA113462.md): Crease Beam · corroded · May 19, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Structure
  > DURING SCHEDULED 24Y CHECK FOUND, CREASE BEAM WEB CORRODED BETWEEN BS 907-927, STR 17L. REMOVED AND REPLACED WEB PER SRM.
- [SDR SWAA113461](https://openairdocs.org/sdr/SWAA113461.md): Skin · cracked · May 19, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 24Y CHECK FOUND, R2 DOOR FUSELAGE SKIN CRACKED AT LOWER CUTOUT. REPAIRED SKIN PER EA.
- [SDR SWAA113402](https://openairdocs.org/sdr/SWAA113402.md): Shear Tie · corroded · May 13, 2011 · N325SW · Boeing 7373H4 · Fuselage Internal Mounting Structure
  > DURING SCHEDULED 24Y CHECK FOUND, CORROSION ON SHEAR TIE AT BS 787 BETWEEN STR 19 AND 20 LEFT. REMOVED AND REPLACED SHEAR TIE PER SRM.
- [SDR SWAA113401](https://openairdocs.org/sdr/SWAA113401.md): Web · cracked · May 13, 2011 · N325SW · Boeing 7373H4 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED 24Y CHECK FOUND, WEB CRACKED AT BS 246 RBL 22. REPAIRED WEB PER ACO.
- [SDR SWAA113400](https://openairdocs.org/sdr/SWAA113400.md): Stringer Clip · cracked · May 13, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 24Y CHECK FOUND, STA 440 STR 16R STRINGER CLIP CRACKED. REMOVED AND REPLACED CLIP PER SRM.
- [SDR SWAA113399](https://openairdocs.org/sdr/SWAA113399.md): Fitting · loose · May 13, 2011 · N325SW · Boeing 7373H4 · Emergency Equipment
  > DURING SCHEDULED 24Y CHECK FOUND, R2 DOOR ESCAPE SLIDE ASSY-SLIDE GIRT BAR CLIPS LOOSE. REMOVED AND REPLACED CLIPS PER SOPM.
- [SDR SWAA113335A](https://openairdocs.org/sdr/SWAA113335A.md): Skin · cracked · May 12, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 24Y CHECK FOUND, SKIN CRACKED BS 967+12 BELOW STR 21L. REPAIRED SKIN PER ER.
- [SDR SWAA113334A](https://openairdocs.org/sdr/SWAA113334A.md): Shear Tie · corroded · May 12, 2011 · N325SW · Boeing 7373H4 · Fuselage Internal Mounting Structure
  > DURING SCHEDULED 24Y CHECK FOUND, CORRODED FWD BARGO BAY ON FRAME SHEAR TIE BS 480 BL 0 - STR 28L. REPAIRED SHEAR TIE PER ER.
- [SDR SWAA113333A](https://openairdocs.org/sdr/SWAA113333A.md): Beam · cracked · May 12, 2011 · N325SW · Boeing 7373H4 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED 24Y CHECK FOUND, VERTICAL FLANGE OF LONGITUDINAL BEAM FROM OVAL HOLE TO FASTENER HOLE BS 662 AND 665 RBL 24.5 WL 206, CRACKED. REPAIRED BEAM PER ER.
- [SDR SWAA113332A](https://openairdocs.org/sdr/SWAA113332A.md): Frame · cracked · May 12, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Frame
  > DURING SCHEDULED 24Y CHECK FOUND, FRAME BS 727B CRACKED AT LWER EDGEAT STRINGER 14R. REPAIRED FRAME PER EA.
- [SDR SWAA113331A](https://openairdocs.org/sdr/SWAA113331A.md): Skin · corroded · May 12, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 24Y CHECK FOUND, FUSELAGE EXTERIOR SKIN - LOWER LOBE - BS 971 JUST BELOW STR 20 AROUND STATIC PORT CUTOUT - SKIN SURFACE CORRODED. R&R PER EA.
- [SDR SWAA113334](https://openairdocs.org/sdr/SWAA113334.md): Door Frame · cracked · May 1, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Structure
  > DURING SCHEDULED 24Y CHECK, FOUND FWD SERVICE DOOR CUTOUT FWD SUB FRAME CRACK AT BS 294.5 ABOVE STR 8R. REPAIRED PER DOC.
- [SDR SWAA113335](https://openairdocs.org/sdr/SWAA113335.md): Stringer Clip · cracked · May 1, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 24Y CHECK, FOUND CRACKED STRINGER CLIP, BS 747, STR 19L. REMOVED AND REPLACED CLIP PER SRM.
- [SDR SWAA113230](https://openairdocs.org/sdr/SWAA113230.md): Stringer · cracked · Apr 29, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED 24Y CHECK, FOUND CRACKED STRINGER, BS 460+6 TO BS 460+8. REMOVED AND REPLACED STR PER DOC.
- [SDR SWAA113214](https://openairdocs.org/sdr/SWAA113214.md): Stringer Clip · cracked · Apr 28, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 24Y CHECK, FOUND CRACKED STR CLIP UPPER LOBE, BS 639, STR 4R. REMOVED AND REPLACED STR PER DOC.
- [SDR SWAA113166](https://openairdocs.org/sdr/SWAA113166.md): Skin · cracked · Apr 28, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 911.5, STR 20L. REPAIRED SKIN PER SRM.
- [SDR SWAA113233](https://openairdocs.org/sdr/SWAA113233.md): Stringer Clip · corroded · Apr 27, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 24Y CHECK, FOUND PILLOWING CORROSION ON STR CLIP, BS 987, BETWEEN SHEAR TIE AND FUSELAGE SKIN. REMOVED AND REPLACED STR PER SRM.
- [SDR SWAA113232](https://openairdocs.org/sdr/SWAA113232.md): Stringer Clip · cracked · Apr 27, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 24Y CHECK, FOUND CRACKED INTERIOR STR CLIP, BS 440, STR 16R-15R AT FASTENER HOLE. REMOVED AND REPLACED STR PER SRM.
- [SDR SWAA113231](https://openairdocs.org/sdr/SWAA113231.md): Stringer Clip · cracked · Apr 27, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 24Y CHECK, FOUND CRACKED INTERIOR STR CLIP, BS 420, STR 16R. REMOVED AND REPLACED STR PER SRM.
- [SDR SWAA113229](https://openairdocs.org/sdr/SWAA113229.md): Skin · cracked · Apr 27, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACK AT CHEM-MILL STEP, BS 931, STR 21R. REMOVED AND REPLACED STR PER DOC.
- [SDR SWAA113228](https://openairdocs.org/sdr/SWAA113228.md): Stringer Clip · cracked · Apr 27, 2011 · N325SW · Boeing 7373H4 · Fuselage Main, Attach Fittings
  > DURING SCHEDULED 24Y CHECK, FOUND CRACKED INTERIOR STR CLIP, BS 639, STR 3L. REMOVED AND REPLACED STR PER DOC.

Next page: https://openairdocs.org/deregistered/N325SW-2012-03-28/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 = 'N325SW' AND deregistration_id = 'N325SW-2012-03-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N325SW-2012-03-28/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.