# Service difficulty reports: N338US, cancelled Jan 9, 2004

A list on [N338US, cancelled Jan 9, 2004](https://openairdocs.org/deregistered/N338US-2004-01-09.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 · 60 reports

- [SDR USAA020383](https://openairdocs.org/sdr/USAA020383.md): Angle · cracked · Oct 3, 2002 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND Z-ANGLE CRACKED 2 INCHES, W/W FORWARD BULKHEAD LEFT CENTER VERTICAL Z-ANGLE. MANUFACTURED IAW EA 75003. (M)
- [SDR USAA020159](https://openairdocs.org/sdr/USAA020159.md): Skin · cracked · Mar 28, 2002 · N338US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED TWO PLACES 2.25 INCH AND 1.25 INCH, STATION 730 STRINGER 23R AND 24R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)
- [SDR USAASB01197](https://openairdocs.org/sdr/USAASB01197.md): Battery · discharged · Jul 8, 2001 · N338US · Boeing 737301 · Emergency Lighting
  > DCA - FOUND MID-CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M)
- [SDR USAA001762](https://openairdocs.org/sdr/USAA001762.md): Gusset · cracked · Oct 16, 2000 · N338US · Boeing 737301 · Fuselage Main, Structure
  > CLT - GUSSET CRACKED 1 INCH AT BS 259, BBL ZERO TOP OF N/G WELL. INSTALLED NEW GUSSET PER DWG 65 45819. (X)
- [SDR USAA001761](https://openairdocs.org/sdr/USAA001761.md): Frame · cracked · Oct 16, 2000 · N338US · Boeing 737301 · Fuselage Main, Frame
  > CLT - CHORD CRACKED 1.5 INCHES AT BS 178, WL 207, LBL 26. FABRICATED NEW WEB PER SRM 51-10-02. (X)
- [SDR UAAA001709](https://openairdocs.org/sdr/UAAA001709.md): Bulkhead · cracked · Oct 10, 2000 · N338US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - WEB CRACKED,.50 INCH, BS 178, WL 207, LBL 26. FABRICATED AND INSTALLED NEW WEB PER SRM 51-10-02. (X)
- [SDR USAA001708](https://openairdocs.org/sdr/USAA001708.md): Intercostal · cracked · Oct 10, 2000 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DROP IN INTERCOSTAL CRACKED, 2 INCHES, BS 178, WL 195, LBL 24. REPAIRED PER SRM 53-10-08 FIG 207. (X)
- [SDR USAASB00269](https://openairdocs.org/sdr/USAASB00269.md): Lever · jammed · Sep 22, 2000 · N338US · Boeing 737301 · Engine Thrust Reverser
  > PHL - FLT 1820 - EN ROUTE FROM JAX TO PHL, CAPTAIN REPORTED THAT THE NR 1 ENGINE THRUST LEVER WAS JAMMED. THRUST LEVER COULD MOVE FORWARD BUT WOULD NOT RETARD THE LAST FOUR INCHES. CREW DISCONNECTED THE AUTOTHROTTLE AND PULLED THE CIRCUIT BREAKER AND RESET.
- [SDR USAASB00084](https://openairdocs.org/sdr/USAASB00084.md): Valve · failed · Mar 24, 2000 · N338US · Boeing 737301 · Brake Anti-Skid Section
  > CLT - FLT 1403 - EN ROUTE FROM TPA-LGA, THE ANTI-SKID INOPERATIVE LIGHT ILLUMINATED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT OUTBOARD MAIN LANDING GEAR ANTI-SKID VALVE HAD FAULTED. REMOVED AND REPLACED THE LEFT
- [SDR USAA990791](https://openairdocs.org/sdr/USAA990791.md): Stringer · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - DURING Q3 CHECK, FOUND.75 INCH CRACK AT BS 727 STRINGER 18A WEB S18AL. REPAIRED WITH REPLACEMENT REF SB 737-53-1170. (M)
- [SDR USAA990790](https://openairdocs.org/sdr/USAA990790.md): Frame · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q3 CHECK, FOUND VARIOUS 1 INCH AREAS OF CORROSION AT NUTPLATE HOLES IN FRAME/WEB AT BS 605 TO 845 STRINGER 25R TOP FLANGE. REPLACED WITH IDENTICAL PART NUMBER. (M)
- [SDR USAA990789](https://openairdocs.org/sdr/USAA990789.md): Intercostal · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT STATION 178, 195 INTERCOSTAL RT SIDE. REPLACED WITH IDENTICAL PART NUMBER. (M)
- [SDR USAA990788](https://openairdocs.org/sdr/USAA990788.md): Post · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT CAPTAINS UPPER O/B CORNER OF EXTERIOR WINDSHIELD (POST). INSTALLED EXTERNAL DOUBLER PER EA 64979. (M)
- [SDR USAA990787](https://openairdocs.org/sdr/USAA990787.md): Skin · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Leading Edge Devices
  > CLT - DURING Q3 CHECK, FOUND 3 CRACKS ONE 1.375 INCH, TWO.5 INCH ON SKIN AT NR 1 L/E SLAT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 57-50-01 REV 'H'. (M)
- [SDR USAA990786](https://openairdocs.org/sdr/USAA990786.md): Clip · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q3 CHECK, FOUND.25 INCH CRACK AT TIE CLIP AT STATION 663 S10L. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M)
- [SDR USAA990785](https://openairdocs.org/sdr/USAA990785.md): Skin · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - DURING Q-3 CHECK, FOUND.5 INCH CRACK E/E COOLING DUCT OUTLET INNER FUSELAGE FUSELAGE SKIN AT BS 380 BL 0. INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER 23 INCH BY 40 INCH PER TR 53-30-07 AND BOEING DWG NR 65C33930. (M)
- [SDR USAA990784](https://openairdocs.org/sdr/USAA990784.md): Angle · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT CREASE BEAM INNER CHORD ANGLE BS 294.5 RBL 45 WL 208. INSTALLED CHORD ANGLE PER SRM 51-10-02. (M)
- [SDR USAA990783](https://openairdocs.org/sdr/USAA990783.md): Splice · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q3 CHECK, FOUND.250 INCH CRACK AT BS 908 STRINGER SPLICE STRINGER 4LT. REPLACED STRINGER SPLICE WITH IDENTICAL PART. (M)
- [SDR USAA990782](https://openairdocs.org/sdr/USAA990782.md): Splice · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK, FOUND.250 INCH CRACK AT BS 908 STRINGER SPLICE STRINGER 4RT. REPLACED STRINGER SPLICE WITH IDENTICAL PART. (M)
- [SDR USAA990781](https://openairdocs.org/sdr/USAA990781.md): Frame · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q3 CHECK, FOUND.125 INCH CRACK IN FRAME AT STATION 616 RBL 64 WL 201 INBOARD CHORD ANGLE. INSTALLED REPAIR FILLER AND STIFFENING ANGLE PER EA 65007 TR 53-10-23 (737-200). (M)
- [SDR USAA990780](https://openairdocs.org/sdr/USAA990780.md): Frame · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DUIRNG Q-3 CHECK, FOUND.25 INCH CRACK IN FRAME AT BS 480 S9R. INSTALLED DOUBLER PER EA 65009. (M)
- [SDR USAA990779](https://openairdocs.org/sdr/USAA990779.md): Tie Clip · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q3 CHECK, FOUND TIE CLIP CRACKED IN HALF. ALSO, FOUND STRINGER CRACKED BELOW CLIP LOCATION, STATION 616, S-4L. INSTALLED STRINGER DOUBLER PER SRM 53-00-03 FIG 204 AND FABRICATED TIE CLIP AND INSTALLED PER SRM 51-10-1. (M)
- [SDR USAA990772](https://openairdocs.org/sdr/USAA990772.md): Stringer · corroded · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH AREA OF CORROSION AT STATION 727A PLUS 14 INCHES, STRINGER 26L. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. INSTALLED FABRICATED STRINGER REPAIR CHANNEL ANDRADIUS FILLERS PER SRM 53-00-03 FIG 201. (
- [SDR USAA990771](https://openairdocs.org/sdr/USAA990771.md): Angle · corroded · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 6 SQUARE INCH OF CORROSION MED Z-ANGLE UPPER SURFACE. CORROSION LEVEL 2. REPLACED Z-ANGLE PER SRM 51-10-02. (M)
- [SDR USAA990770](https://openairdocs.org/sdr/USAA990770.md): Stabilizer Link · corroded · Jul 29, 1999 · N338US · Boeing 737301 · Main Landing Gear
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION RIGHT GEAR STABILIZER LINK ATTACH POINTS. CORROSION LEVEL 2. REMOVED AND REPLACED STABILIZER LINK PER MM 32-32-93 AND 32-13-21. (M)
- [SDR USAA990769](https://openairdocs.org/sdr/USAA990769.md): Angle · corroded · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT BS 957 AND 987, LBL 45, WL 208 CREASEBEAM INNER CHORD ANGLE. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. INSTALLED NEW CHORD ANGLE PER SRM 51-40-02. (M)
- [SDR USAA990768](https://openairdocs.org/sdr/USAA990768.md): Tie Clip · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 616 STRINGER 6L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAA990729](https://openairdocs.org/sdr/USAA990729.md): Frame · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.50 INCH CRACK FRAME 312 AT STR 5L. CRACK TRIMMED OUT AND DOUBLER INSTALLED PER SRM 53-00-07 FIG 202 AND EA 65075. (X)
- [SDR USAA990728](https://openairdocs.org/sdr/USAA990728.md): Frame · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.500 INCH CRACK MAIN ENTRY DOORWAY UPPER HINGE H-STRAP DOORWAY FRAME. FABRICATED AND INSTALLED NEW H-STRAP PER SRM 51-10-02 AND BOEING DWG 90-7822. (X)
- [SDR USAA990727](https://openairdocs.org/sdr/USAA990727.md): Angle · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.75 INCH CRACK AT AFT END STA 360 STR 14L SHEARBEAM OUTBOARD CHORD ANGLE. REPAIRED PER BOEING DWG NR 69-48985/51-10-02. (X)
- [SDR USAA990726](https://openairdocs.org/sdr/USAA990726.md): Frame · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AFT ENTRY DOOR CUT-OUT FRAME UPPER FORWARD SECTION AT BOTTOM HOLE FORWARD EDGE FRAME. INSTALLED DOUBLER PER SRM 51-70-11. (X)
- [SDR USAA990725](https://openairdocs.org/sdr/USAA990725.md): Tie Clip · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STA 639 STR 4L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X)
- [SDR USAA990724](https://openairdocs.org/sdr/USAA990724.md): Tie Clip · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 639 STRINGER 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAA990723](https://openairdocs.org/sdr/USAA990723.md): Tie Clip · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURIGN Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 616 STRINGER 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAA990722](https://openairdocs.org/sdr/USAA990722.md): Skin · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Nacelle/Pylon, Plate/Skin
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.75 INCH CRACK AT NR 1 ENGINE PYLON SKIN AT ACCESS PANEL NR 5727 CUTOUT LOWER AFT CORNER. INSTALLED DOUBLER PER TR 54-30-07. (M)
- [SDR USAA990721](https://openairdocs.org/sdr/USAA990721.md): Tie Clip · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK AT STATION 520 STRINGER 7R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAA990719](https://openairdocs.org/sdr/USAA990719.md): Tie Clip · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK AT STA 500C STR 7R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X)
- [SDR USAA990718](https://openairdocs.org/sdr/USAA990718.md): Tie Clip · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK AT STA 600 STR 8L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X)
- [SDR USAA990717](https://openairdocs.org/sdr/USAA990717.md): Longeron · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.75 INCH LONGERON CRACK AT FORWARD L/B CORNER STATION 277 STRINGER 14R. FABRICATED NEW LONGERON WEB AND INSTALLED PER SRM 51-30-2. (M)
- [SDR USAA990716](https://openairdocs.org/sdr/USAA990716.md): Stringer · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.50 INCH CRACK IN STRINGER AT STA 306 STR 4L. FABRICATED NEW WEB AND INSTALLED PER SRM 53-10-15. (X)
- [SDR USAA990715](https://openairdocs.org/sdr/USAA990715.md): Frame · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.50 INCH CRACK IN FRAME AT STA 727D, RBL 2. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-00-07 AND EA 65131 PAGES 1 AND 2. (X)
- [SDR USAA990685](https://openairdocs.org/sdr/USAA990685.md): Angle · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK AT BS 480 STRINGER 9L BAG BIN ATTACH ANGLE. FABRICATED NEW REPAIR DOUBLER PER SRM 53-00-07 AND EA 650009. (M)
- [SDR USAA990684](https://openairdocs.org/sdr/USAA990684.md): Bulkhead · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND.50 INCH CRACK AT STA 178 BULKHEAD LBL 5 W/L 195 SKIN. INSTALLED DOUBLER PER TR 53-10-07. (X)
- [SDR USAA990683](https://openairdocs.org/sdr/USAA990683.md): Bulkhead · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT STA 178 BULKHEAD LBL 5 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER TR 53-10-07. (X)
- [SDR USAA990682](https://openairdocs.org/sdr/USAA990682.md): Bulkhead · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND.50 INCH CRACK AT STA 178 BULKHEAD RBL1 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-10-08 FIG 203. (X)
- [SDR USAA990681](https://openairdocs.org/sdr/USAA990681.md): Bulkhead · cracked · Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - DURING A Q-3 CHECK VISUAL INSPECTION FOUND.50 INCH CRACK AT STA 178 BULKHEAD LBL1 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-10-08 FIG 203. (X)
- [SDR USAA990680](https://openairdocs.org/sdr/USAA990680.md): Angle · corroded · Jul 29, 1999 · N338US · Boeing 737301 · Service Doors
  > CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AFT RT Z-ANGLE AT AFT SERV DOOR. CORROSION LEVEL 2. REPLACED PER SRM 51-10-02. (M)
- [SDR USAASB99015](https://openairdocs.org/sdr/USAASB99015.md): Battery Charger · failed · Jan 20, 1999 · N338US · Boeing 737301 · Emergency Lighting
  > LGA - PILOT REPORTED THAT THE INTERIOR EMERGNECY FLOOR LIGHTING FROM SEAT ROWS 5 THROUGH 10 AND THE LEFT EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT ROW 10ABC WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER FOR THE INTERIOR EMERGENCY FLOOR LI
- [SDR 99ZZZM158](https://openairdocs.org/sdr/99ZZZM158.md): Light · inoperative · Jan 20, 1999 · N338US · Boeing 737301 · Emergency Lighting
  > LGA - PILOT REPORTED THAT THE INTERIOR EMERGNECY FLOOR LIGHTING FROM SEAT ROWS 5 THROUGH 10 AND THE LEFT EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT ROW 10ABC WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER FOR THE INTERIOR EMERGENCY FLOOR LI
- [SDR USAASB98278](https://openairdocs.org/sdr/USAASB98278.md): Switch · contaminated · Oct 21, 1998 · N338US · Boeing 737301 · Landing Gear Position and Warning
  > PIT - FLT 345 - DURING LANDING GEAR EXTENSION, GEAR CAME DOWN WITH 3 GREEN AND 3 RED LIGHTS. HYDRAULIC PRESSURE WAS NORMAL. CREW RECYCLED GEAR AND RECEIVED 3 GREEN LIGHTS WITH RED LIGHTS EXTINGUISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CLE

Next page: https://openairdocs.org/deregistered/N338US-2004-01-09/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 = 'N338US' AND deregistration_id = 'N338US-2004-01-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N338US-2004-01-09/reports

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