# Service difficulty reports: N354US, cancelled Aug 29, 2007

A list on [N354US, cancelled Aug 29, 2007](https://openairdocs.org/deregistered/N354US-2007-08-29.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 · 62 reports

- [SDR USAA050768](https://openairdocs.org/sdr/USAA050768.md): Skin · cracked · Jun 16, 2005 · N354US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 4 INCHES, STATION 727D, S23R. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 229 DETAIL XI. (M)
- [SDR USAA050767](https://openairdocs.org/sdr/USAA050767.md): Skin · punctured · Jun 16, 2005 · N354US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN PUNCTURED 1 INCH BY 2.5 INCH, BS 312-322 AT S23R. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. (M)
- [SDR USAA050221](https://openairdocs.org/sdr/USAA050221.md): Plate · cracked · Feb 1, 2005 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND HINGE DOUBLER PLATE CRACKED.3750, MED TOP FORWARD HINGE CUTOUT INSIDE BOTTOM FORWARD CORNER. INSTALLED WEB PER SRM 51-40-02 AND DWG 65-17684. (M)
- [SDR USAA040065](https://openairdocs.org/sdr/USAA040065.md): Floor Support · cracked · Mar 27, 2004 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > FOUND FLANGE CRACKED 1.5 INCH FLOOR SUPPORT STATION 937 BL 0. REMOVED TOP FLANGE OF FLOOR SUPPORT, REPLACED WITH NEW PART EPN 1138864 PER SRM 51-40-00. (M)
- [SDR USAA040064](https://openairdocs.org/sdr/USAA040064.md): Shear Web · corroded · Mar 27, 2004 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > FOUND SHEAR WEB CORRODED 3 INCHES BY 10 INCHES, TOP AND LOWER SURFACE OF FLOOR PAN AT AFT PRESS BULKHEAD, RBL 0-15. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-40-2. CORROSION LEVEL 1, TASK NR C53-107-02. (M)
- [SDR USAA040063](https://openairdocs.org/sdr/USAA040063.md): Floor Panel · gouged · Mar 27, 2004 · N354US · Boeing 737301 · Fuselage Floor Panel
  > FOUND FLOOR PANEL GOUGED 4 INCHES, STATION 992 RBL 39. MANUFACTURED OUT OF 2024 T3 020 PER SRM 51-40-02. (M)
- [SDR USAA040120](https://openairdocs.org/sdr/USAA040120.md): Keelbeam · corroded · Mar 24, 2004 · N354US · Boeing 737301 · Fuselage Main, Keel
  > FOUND KEELBEAM CORRODED AND PITTING 1 INCH BY 4 INCH AREA, RT KEELBEAM LOWER SURFACE STATION 663.75 TO 727. INSTALLED REPAIR STRAP PER EA 78097. LEVEL 1 TASK NR C53-212-01. (M)
- [SDR USAA040095](https://openairdocs.org/sdr/USAA040095.md): Skin · cracked · Jan 13, 2004 · N354US · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND SKIN WITH 3 INCH STRESS CRACK, FORWARD OF AFT BAGGAGE PIT DOOR BS 727E S18R. STRESS CRACK REPAIR PER SRM 53-00-01 FIG 201, AND OM-7 NR 27801. (M)
- [SDR USAA030169](https://openairdocs.org/sdr/USAA030169.md): Support · corroded · Jul 27, 2003 · N354US · Boeing 737301 · Landing Gear Retraction/Extension System
  > FOUND UPPER SUPPORT CORRODED.004 INCH TOP AND BOTTOM TOTAL OF.008 INCH, NLG UPPER SUPPORT. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA030152](https://openairdocs.org/sdr/USAA030152.md): Support · corroded · Jul 27, 2003 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > PHL - FOUND UPPER SUPPORT CORRODED TOP AND BOTTOM,.004 INCH TOP AND BOTTOM TOTAL OF.008 INCH. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAASB01288](https://openairdocs.org/sdr/USAASB01288.md): Indicator · faulty · Oct 8, 2001 · N354US · Boeing 737301 · Trailing Flap Position Indicating System
  > BUF - FLT 1157 - AFTER TAKEOFF FROM BUF, EN ROUTE TO CLT, CREW EXPERIENCED A FLAP ASYMMETRY PROBLEM DURING FLAP RETRACTION. ONE FLAP WAS IN THE 5 DEGREE POSITION AND THE OTHER WAS IN THE 2 DEGREE POSITION. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT
- [SDR USAASB00231](https://openairdocs.org/sdr/USAASB00231.md): Wire · broken · Aug 26, 2000 · N354US · Boeing 737301 · Light System Wiring
  > PIT - MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT BEHIND THE LEFT WING INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT SPLICE JUST ABOVE EMERGENCY LIGHT IN AFT CARGO BAY. INSTALLED NEW SPLICE. OPS CHECK GOOD. (M)
- [SDR USAA001122](https://openairdocs.org/sdr/USAA001122.md): Bushing · corroded · Aug 1, 2000 · N354US · Boeing 737301 · Horizontal Stabilizer Structure
  > CLT - FOUND LUG AND BUSHING CORRODED.25 INCH, LEFT HORIZONTAL STAB LOWER ATTACH BOLT FRONT SPAR. CORROSION LEVEL 1 C-53-701-02. REMOVED CORROSION PER SRM 55-10-10. (M)
- [SDR USAA001121](https://openairdocs.org/sdr/USAA001121.md): Bushing · corroded · Aug 1, 2000 · N354US · Boeing 737301 · Horizontal Stabilizer Structure
  > CLT - FOUND LUG AND BUSHING CORRODED.25 INCH, LEFT HORIZ STAB UPPER ATTACH BOLT FRONT SPAR. CORROSION LEVEL 1. REMOVED CORROSION PER SRM 55-10-10. (M)
- [SDR USAA001125](https://openairdocs.org/sdr/USAA001125.md): Pressure Panel · cracked · Aug 1, 2000 · N354US · Boeing 737301 · Fuselage Floor Panel
  > CLT - FOUND PRESSURE DECK WITH TWO CRACKS.5 INCH AND 1 INCH, PRESS DECK MLG WHEEL WELL STRINGER 663, LBL 30. REMOVED DAMAGE INSTALLED REPAIR DOUBLER AND FILLER PER TR 53-60-04. (M)
- [SDR USAA001124](https://openairdocs.org/sdr/USAA001124.md): Floorbeam · corroded · Aug 1, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM T-CAP CORRODED 2 INCHES, STATION 328, LBL 49. CORROSION LEVEL 1, C53-107-01. REMOVED CORROSION AND INSTALLED NEW T-CAP PER SRM 51-70-12 FIG 1. (M)
- [SDR USAA001123](https://openairdocs.org/sdr/USAA001123.md): Beam · cracked · Aug 1, 2000 · N354US · Boeing 737301 · Wing, Landing Gear Attach Fittings
  > CLT - FOUND SUPPORT BEAM CRACKED.375 INCH, LEFT MLG SUPPORT BEAM. ACCOMPLISHED INTERMIN REPAIR PER EA 67644 AND TR 57-40-13. (M)
- [SDR USAA001085](https://openairdocs.org/sdr/USAA001085.md): Floorbeam · corroded · Jul 31, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 2 INCH AREA, STATION 294.5, RBL 45. REMOVED AND INSTALLED FABRICATED ANGLE PER SRM 53-10-08 AND 51-40-02. (M)
- [SDR USAA001090](https://openairdocs.org/sdr/USAA001090.md): Splice · cracked · Jul 31, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRINGER SPLICE CRACKED.25 INCH, STRINGER 4R SPLICE STATION 907. REMOVED DAMAGE AND INSTALLED PER SRM 51-10-02. (M)
- [SDR USAA001089](https://openairdocs.org/sdr/USAA001089.md): Frame · cracked · Jul 31, 2000 · N354US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.025 INCH, AFT SIDE FRAME 847 AT TWO RIVETS JUST ABOVE STRINGER 9L. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 53-00-07 FIG 201 AND TR 53-10-14A. (M)
- [SDR USAA001088](https://openairdocs.org/sdr/USAA001088.md): Skin · cracked · Jul 31, 2000 · N354US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED.375 INCH, FUSE SKIN AT LOWER AFT CORNER OF DOOR CUTOUT. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 53-10-01 FIG 202. (M)
- [SDR USAA001087](https://openairdocs.org/sdr/USAA001087.md): Door Frame · cracked · Jul 31, 2000 · N354US · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND FRAME CRACKED.125 INCH, FORWARD SERVICE DOOR JAMB FORWARD FRAME AT LOWER OUTBOARD CORNER. REMOVED AND REPLACED PER SRM 51-40-02 AND BOEING DWG 65 45807. (M)
- [SDR USAA001086](https://openairdocs.org/sdr/USAA001086.md): Attach Angle · cracked · Jul 31, 2000 · N354US · Boeing 737301 · Horizontal Stabilizer Structure
  > CLT - FOUND ATTACH ANGLE CRACKED 1 INCH, HORIZ STAB CENTER BOX LOWER CHORD TO WEB. INSTALLED NEW ANGE PER TR 51-10-02. (M)
- [SDR USAA001010](https://openairdocs.org/sdr/USAA001010.md): Support Bracket · cracked · Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND DOOR SUPPORT CRACKED.25 INCH, STATION 294.5, FRAME AT STRINGER 14L. FABRICATED NEW WEB AND INSTALLED PER SRM 51-70-11. (M)
- [SDR USAA001009](https://openairdocs.org/sdr/USAA001009.md): Door Frame · cracked · Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND FRAME CRACKED.25 INCH, STATION 294.5, STRINGER 7L. REPAIRED PER SRM 53-10-15. (M)
- [SDR USAA001008](https://openairdocs.org/sdr/USAA001008.md): Door Frame · cracked · Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND FRAME CRACKED 2.5 INCHES, STATION 294.5, FORWARD SERVICE DOOR FRAME WL 208. REMOVED DAMAGED AREA INSTALLED REPAIR DOUBLER PER SRM 50-70-11. (M)
- [SDR USAA001007](https://openairdocs.org/sdr/USAA001007.md): Web · cracked · Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED.500 INCH, STRINGER 14R, WEB INNER CHORD ANGLE STATION 278. FABRICATED NEW WEB AND INSTALLED PER SRM 51-40-00 AND DWG 6 45807. (M)
- [SDR USAA001006](https://openairdocs.org/sdr/USAA001006.md): Bulkhead · cracked · Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB CRACKED TWO PLACES.25 INCH AND 1.5 INCH, STATION 178 BULKHEAD, WEB RBL 6.75, WL 201. FABRICATE REPAIR DOUBLER PER SRM 53-10-08 DETAIL 111. (M)
- [SDR USAA001005](https://openairdocs.org/sdr/USAA001005.md): Angle · cracked · Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND CHORD ANGLE CRACKED.5 INCH, LBL 5.7 VERT CHORD L/B FLANGE STATION 178, WL 184. INSTALLED REPAIR ANGLE AND STRAPS PER SRM 53-10-08. (M)
- [SDR USAA001004](https://openairdocs.org/sdr/USAA001004.md): Floorbeam · corroded · Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344, LBL 36. FABRICATED T-CAP PER REPAIR DOCUMENT 53-10-51. (M)
- [SDR USAA001003](https://openairdocs.org/sdr/USAA001003.md): Floorbeam · corroded · Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344, LBL 28. REMOVED AND REPLACED T-CAP PER SRM 53-10-51. CORROSION LEVEL 1. (M)
- [SDR USAA001002](https://openairdocs.org/sdr/USAA001002.md): Floorbeam · corroded · Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344, LBL 14. CORROSION LEVEL 1. FABRICATED T-CAP PER SRM 53-10-51. (M)
- [SDR USAA001001](https://openairdocs.org/sdr/USAA001001.md): Floorbeam · corroded · Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 312, LBL 12. REMOVED DAMAGED T-CAP PER SRM 53-10-51 FIG 205. (M)
- [SDR USAA001022](https://openairdocs.org/sdr/USAA001022.md): Floorbeam · corroded · Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 328, LBL 28. CORROSION LEVEL 1. FABRICATED NEW T-CAP AND INSTALLED PER REPAIR 51-70-12. (M)
- [SDR USAA001021](https://openairdocs.org/sdr/USAA001021.md): Floorbeam · corroded · Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 312, BL 0. CORROSION LEVEL 1. FABRICATED NEW T-CAP AND SPLICE ANGLE PER SRM 53-10-51. (M)
- [SDR USAA001020](https://openairdocs.org/sdr/USAA001020.md): Floorbeam · corroded · Jul 20, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 312, RBL 36. FABRICATED NEW T-CAP AND SPLICE ANGLE PER SRM 53-10-51. CORROSION LEVEL 1. (M)
- [SDR USAA000891](https://openairdocs.org/sdr/USAA000891.md): Tie Clip · cracked · Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.5 INCH, BS 344 STRINGER 11R. FABRICATED CLIP PER BOEING DWG 6938939. (M)
- [SDR USAA000892](https://openairdocs.org/sdr/USAA000892.md): Tie Clip · cracked · Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STRINGER 1 BS 380. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAA000893](https://openairdocs.org/sdr/USAA000893.md): Tie Clip · cracked · Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 380, STRINGER 2L. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAA000894](https://openairdocs.org/sdr/USAA000894.md): Tie Clip · cracked · Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.0625 INCH, BS 616, STRINGER 4L. INSTALLED NEW TIE CLIP PER SRM 51-10-2. (M)
- [SDR USAA000895](https://openairdocs.org/sdr/USAA000895.md): Tie Clip · cracked · Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CILP CRACKED.0625 INCH, BS 639, STRINGER 4L. INSTALLED CLIP PER SRM 51-10-2. (M)
- [SDR USAA000896](https://openairdocs.org/sdr/USAA000896.md): Tie Clip · cracked · Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.250 INCH, FORWARD SIDE FRAME 907, BELOW STRINGER 1. REPLACED TIE CLIP PER BOEING DWG 69-47869. (M)
- [SDR USAA000897](https://openairdocs.org/sdr/USAA000897.md): Tie Clip · cracked · Jul 3, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED TWO PLACES.5 INCH, FS 663, STRINGER 10L. INSTALLED CLIP PER SRM 51-10-2. (M)
- [SDR USAASB00142](https://openairdocs.org/sdr/USAASB00142.md): Light · failed · May 11, 2000 · N354US · Boeing 737301 · Emergency Lighting
  > PHL - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 12ABC INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 12ABC. OPERATIONAL CHECK GOOD. (X)
- [SDR USAASB99305](https://openairdocs.org/sdr/USAASB99305.md): Fire Loop · failed · Dec 27, 1999 · N354US · Boeing 737301 · Fire Detection
  > MCI - FLT 328 - AFTER TAKEOFF FROM MCI, THE RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. THREE MINUTES LATER, THE LEFT WING TO BODY OVERHEAT LIGHT ILLUMINATED AND A STRONG BURNING SMELL WAS PRESENT IN THE COCKPIT. FLIGHT RETURNED TO FIELD AT MCI AND LANDED
- [SDR USAASB99085](https://openairdocs.org/sdr/USAASB99085.md): Splice · defective · Apr 1, 1999 · N354US · Boeing 737301 · Emergency Lighting
  > ROC - WHOLE ACCOMPLISHING OVERNIGHT CHECK, MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHT ON SEAT ROW 16 END BAY INOPERATIVE. MAINTENANCE REPLACED DEFECTIVE WIRE SPLICES AND SECURED WIRING BENEATH SEAT ADJACENT TO END BAY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA980600](https://openairdocs.org/sdr/USAA980600.md): Skin · cracked · Nov 25, 1998 · N354US · Boeing 737301 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-1 CHECK VISUAL INSPECTION VERIFIED WITH HFEC FOUND A.125 INCH CRACK UPPER HINGE CUTOUT ON FORWARD SERVICE DOOR SKIN. FABRICATED DOUBLER AND INSTALLED PER SB 737-52-1096 FIG 6 AND EA 63034. (M)
- [SDR USAA980599](https://openairdocs.org/sdr/USAA980599.md): Skin · cracked · Nov 25, 1998 · N354US · Boeing 737301 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-1 CHECK VISUAL INSPECTION VERIFIED WITH HFEC, FOUND A.375 INCH CRACK LOWER HINGE CUTOUT ON FORWARD SERVICE DOOR SKIN. FABRICATED DOUBLER AND INSTALLED PER SB 737-52-1096 FIG 3 AND EA 63034. (M)
- [SDR USAA980598](https://openairdocs.org/sdr/USAA980598.md): Skin · cracked · Nov 25, 1998 · N354US · Boeing 737301 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-1 CHECK VISUAL INSPECTION VERIFIED WITH HFEC, FOUND A.375 INCH CRACK LOWER HINGE CUTOUT ON FORWARD ENTRY DOOR SKIN. FABRICATED DOUBLER AND INSTALLED PER SB 737-52-1096 FIG 3 AND EA 63034. (M)
- [SDR USAASB98233](https://openairdocs.org/sdr/USAASB98233.md): Transmitter · inoperative · Sep 6, 1998 · N354US · Boeing 737301 · Hydraulic Pressure Indicator
  > CLT - FLT 1080 - AT FL370, THE 'B' SYSTEM HYDRAULIC PRESSURE GAUGE WENT OT 750 PSI. SHORTLY THEREAFTER, THE 'B' SYSTEM HYDRAULIC QUANTITY RESERVOIR STARTED TO DECREASE. CREW DECIDED TO DIVERT TO CLT DUE TO POSSIBLE HYDRAULIC FLUID LOSS. FLIGHT LANDED WITHOUT

Next page: https://openairdocs.org/deregistered/N354US-2007-08-29/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 = 'N354US' AND deregistration_id = 'N354US-2007-08-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N354US-2007-08-29/reports

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