# Service difficulty reports: N349US, cancelled Nov 8, 2004

A list on [N349US, cancelled Nov 8, 2004](https://openairdocs.org/deregistered/N349US-2004-11-08.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR USA2001F00007](https://openairdocs.org/sdr/USA2001F00007.md): Socket · defective · Dec 12, 2001 · N349US · Boeing 737301 · Emergency Lighting
  > PIT MAINTENANCE FOUND THE FORWARD SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD.
- [SDR USAASB00204](https://openairdocs.org/sdr/USAASB00204.md): Duct · severed · Aug 1, 2000 · N349US · Boeing 737301 · Air Distribution System
  > BOS - FLT 6507 - FLIGHT RETURNED TO FIELD AT BOS DUE TO AN ELECTRICAL SMELL THROUGHOUT THE CABIN. CAPTAIN ELECTED TO RETURN TO BOS AFTER NUMEROUS COMPLAINTS FROM THE FLIGHT ATTENDANTS AND PASSENGERS. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT LANDED WITHOU
- [SDR USAASB00187](https://openairdocs.org/sdr/USAASB00187.md): Sensor · failed · Jul 9, 2000 · N349US · Boeing 737301 · Landing Gear Retraction/Extension System
  > BOS - FLT 6527 - AFTER TAKEOFF, THE LANDING GEAR LEVER WOULD NOT MOVE UP TO THE RETRACT POSITION. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTEN
- [SDR USAA991031](https://openairdocs.org/sdr/USAA991031.md): Angle · corroded · Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 59 INCH AREA OF CORROSION AT STATION 285-344, WL 208.1 Z-ANGLE. CORROSION LEVEL 2. REMOVED AND REPLACED Z-ANGLE EPR SRM 51-10-02. (M)
- [SDR USAA991032](https://openairdocs.org/sdr/USAA991032.md): Floorbeam · corroded · Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ALONG UPPER T-CAP AT NUTPLATE HOLES 10 INCH AT BS 294.5, LBL 22 TO RBL 22, BEAM CAP. CORROSION LEVEL 2. INSTALLED T-CAP PER SRM 53-10-51. (M)
- [SDR USAA991022](https://openairdocs.org/sdr/USAA991022.md): Floorbeam · corroded · Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION FLOORBEAM UPPER CHORD STATION 986 FROM BL 3.5 TO RBL 9.5, CORROSION LEVEL 1. INSTALLED DOUBLER PER TR 53-10-05. (M)
- [SDR USAA991023](https://openairdocs.org/sdr/USAA991023.md): Floorbeam · corroded · Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION FLOORBEAM BETWEEN STATION 986.5 BY 1016 DIAGONALLY FROM RBL 19 TO RBL 5. CORROSION LEVEL 1. REPAIRED WITH IDENTICAL PART PER SRM 51-10-02. (M)
- [SDR USAA991002](https://openairdocs.org/sdr/USAA991002.md): Floorbeam · corroded · Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURNG Q-4 CHECK VISUAL INSPECTION, FOUND A.5 INCH AREA OF CORROSION FLOORBEAM 967 UPPER CHORD AT LBL 27.5, CORROSION LEVEL 1. REPAIRED DOUBLER PER SRM 53-00-51. (M)
- [SDR USAA991102](https://openairdocs.org/sdr/USAA991102.md): Angle · cracked · Oct 13, 1999 · N349US · Boeing 737301 · Horizontal Stabilizer Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT HORIZONTAL STAB CENTER SECTION THRUST BEAM ATTACH ANGLE. REPLACED ANGLE PER REPAIR DOCUMENT 51-10-02. (M)
- [SDR USAA991090](https://openairdocs.org/sdr/USAA991090.md): Skin · cracked · Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 EACH.50 INCH CRACKS AT BS 5332, RBBL 60, WL 21.5 SKIN ASSEMBLY. INSTALLED REPAIR PLATES PER SRM 53-10-01 FIG 202. (X)
- [SDR USAA991081](https://openairdocs.org/sdr/USAA991081.md): Fitting · cracked · Oct 13, 1999 · N349US · Boeing 737301 · Service Doors
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK AT FORWARD SERVICE DOOR LOWER AFT DOOR STOP FITTING ASSEMBLY. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (X)
- [SDR USAA991057](https://openairdocs.org/sdr/USAA991057.md): Keel Beam · corroded · Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Keel
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CORRODED AREA KEEL BEAM AT BS 500C PLUS 9.5 INCH LBL 5. CORROSION LEVEL 2. INSTALLED REPAIR DOUBLER PER EA 65730. (M)
- [SDR USAA991047](https://openairdocs.org/sdr/USAA991047.md): Keel Beam · corroded · Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Keel
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION.75 INCH BY 5 INCH AT STATIN 532, RLB 6.5 STRINGER 28R KEEL BEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. INSTALLED REPAIR STRAP AND ANGLE PER EA 65811. (M)
- [SDR USAA991029](https://openairdocs.org/sdr/USAA991029.md): Tie Clip · cracked · Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.3750 INCH CRACK AT BS 907, STR 9L STRINGER TIE CLIP. REPAIRED WITH IDENTICAL PART PER SRM 51-10-2. (X)
- [SDR USAA991021](https://openairdocs.org/sdr/USAA991021.md): Frame · cracked · Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.50 INCH CRACK AT BS 480, BETWEEN STR 8L AND STR 9L FRAME. INSTALLED DOUBLER ANGLE PER EA 65618 AND SRM 53-00-07 FIG 202. (X)
- [SDR USAA991020](https://openairdocs.org/sdr/USAA991020.md): Frame · cracked · Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.50 INCH CRACK AT BS 887, BETWEEN STR 8L AND STR 9L FRAME. INTALLED DOUBLER ANGLE PER EA 65618. (X)
- [SDR USAA990795](https://openairdocs.org/sdr/USAA990795.md): Stringer · cracked · Aug 12, 1999 · N349US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - ON PARKED, OUT OF TIME AIRCRAFT, FOUND 1.5 INCH CRACK AT STR 22R, STA 809. INSTALLED DOUBLER PER SRM 53-00-01. (X)
- [SDR USAASB99169](https://openairdocs.org/sdr/USAASB99169.md): Battery Pack · discharged · Jul 9, 1999 · N349US · Boeing 737301 · Emergency Lighting
  > IAH - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)
- [SDR USAASB97286](https://openairdocs.org/sdr/USAASB97286.md): Battery Pack · discharged · Oct 18, 1997 · N349US · Boeing 737301 · Emergency Lighting
  > PIT - EMERGENCY EXIT SIGN ROW 10 BROKEN AND BATTERY PACK ABOVE ROW 9D INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY (10-1262-3), NO HELP. FOUND BROKEN WIRE UNDER SEAT AND REPAIRED. THE BATTERY CHARGER (2012-1) WAS REPLACED ABOVE ROW 9D. OPERATIONAL CHEC
- [SDR USAASB97192](https://openairdocs.org/sdr/USAASB97192.md): Position Ind · failed · Jul 15, 1997 · N349US · Boeing 737301 · Trailing Flap Position Indicating System
  > PHL - FL2191 - IN THE PROCESS OF CONFIGURING THE A/C FOR LANDING. CAPTAIN DID NOT RECEIVE LEADING OR TRAILING EDGE FLAP INDICATION. ADVISED PHL TOWER OF THE PROBLEM AND HIS INTENTION TO GO AROUND. AFTER GO AROUND, FLIGHT LANDED SAFELY WITHOUT FURTHER INCIDE
- [SDR USAA951034](https://openairdocs.org/sdr/USAA951034.md): Skin · mis mfg · Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - VISUALLY INSPECTED EXISTING REPAIR, LARGE RIVET IN SKIN BAY LOCATED AT STATION 390 ABOVE STRINGER 11L. INSTALLED PROTRUDING HEAD RIVET 211TT3. (M)
- [SDR USAA951033](https://openairdocs.org/sdr/USAA951033.md): Doubler · damaged · Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - PREVIOUS 14 INCH BY 10 INCH REPAIR (EXT DOUBLER) INSTALLED LOCATED STATION 867 BETWEEN STRINGER 21R AND STRINGER 22R. VISUALLY INSPECTED. PREVIOUS REPAIR DOUBLER INSTALLED. (M)
- [SDR USAA951032](https://openairdocs.org/sdr/USAA951032.md): Doubler · damaged · Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 8 INCH BY 8 INCH REPAIR INSTALLED LOCATED AT STATION 430 STRINGER 10L. PREVIOUS REPAIR DOUBLER INSTALLED. (M)
- [SDR USAA951031](https://openairdocs.org/sdr/USAA951031.md): Doubler · damaged · Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING A Q3-CHECK INSPECTION, A 16 INCH BY 10 INCH REPAIR INSTALLED LOCATED AT STATION 365, STRINGER 11L WAS VISUALLY FOUND. EXISTING REPAIR DOUBLER INSTALLED. (M)
- [SDR USAA951030](https://openairdocs.org/sdr/USAA951030.md): Doubler · damaged · Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1 INCH HOLE REPAIR LOCATED AT STATION 344, STRINGER 18L. EXISTING REPAIR, DOUBLER INSTALLED. (M)

## 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 = 'N349US' AND deregistration_id = 'N349US-2004-11-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N349US-2004-11-08/reports

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