# Service difficulty reports: N415US, cancelled Nov 4, 2003

A list on [N415US, cancelled Nov 4, 2003](https://openairdocs.org/deregistered/N415US-2003-11-04.md).

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

- [SDR USAA020283](https://openairdocs.org/sdr/USAA020283.md): Mount · worn · Jul 26, 2002 · N415US · Boeing 737401 · Engine Mount Section
  > PIT - FOUND ENGINE MOUNT WORN BEYOND LIMITS. MACHINED, CHAMFER, MPI, ROTOPEEN PER TYPICAL REP 50-50-08 REV B. (M)
- [SDR USAASB02004](https://openairdocs.org/sdr/USAASB02004.md): Battery Pack · discharged · Jan 6, 2002 · N415US · Boeing 737401 · Emergency Lighting
  > PIT - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHT DIMS DURING OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY ASSEMBLY PER MM 33-50-04. OPS CHECK GOOD. (M)
- [SDR USAASB01076](https://openairdocs.org/sdr/USAASB01076.md): Adc · failed · Mar 10, 2001 · N415US · Boeing 737401 · Air Data Computer
  > CLT - FLT 2138 - ON CLIMB-OUT FROM CLT, EN ROUTE TO IAH, CAPTAIN REPORTED THAT THE NR 2 AIR DATA COMPUTER HAD FAILED RESULTING IN LOSS OF THE FIRST OFFICERS ALTIMETER AND AIRSPEED INDICATIONS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDEN
- [SDR USAASB00143](https://openairdocs.org/sdr/USAASB00143.md): Circuit Board · failed · May 16, 2000 · N415US · Boeing 737401 · Landing Gear Position and Warning
  > PIT - FLT 710 - AFTER TAKEOFF AND GEAR RETRACTION FROM PIT, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED FOR APPROXIMATELY TWO MINUTES. CREW RECYCLED GEAR AND LGHT EXTINGUISHED. FLIGHT CONTINUED ON TO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE
- [SDR USAA990305](https://openairdocs.org/sdr/USAA990305.md): Frame · cracked · Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, Frame
  > CLT - DURING VISUAL CHECK INSPECTION, FOUND A 3 INCH CRACK ON FRAME STATION 870 BL 0 BOTTOM FLANGE. REMOVED CRACKED SKIN, FILLER AND REPAIRED PER SRM 53-00-07. (M)
- [SDR USAA990288](https://openairdocs.org/sdr/USAA990288.md): Skin · corroded · Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, Plate/Skin
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 4 INCH AREA OF CORROSION BS 757 BL 0 SKIN. INSTALLED DOUBLER PER SRM 53-00-01. (M)
- [SDR USAA990284](https://openairdocs.org/sdr/USAA990284.md): Support · corroded · Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.5 INCH BY.5 INCH AREA OF CORROSION AT BS 330, WL 208.10 AND RBBL 52 FLOOR SUPPORT. REPLACED FLOOR SUPPORT PER SRM 51-10-02. (M)
- [SDR USAA990283](https://openairdocs.org/sdr/USAA990283.md): Skin · corroded · Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, Plate/Skin
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.1 INCH BY.4 INCH AREA OF CORROSION AT BS 797 BL 0 SKIN. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)
- [SDR USAA990277](https://openairdocs.org/sdr/USAA990277.md): Floorbeam · corroded · Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, Floor Beam
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.5 INCH BY.5 INCH AREA OF CORROSION AROUND NUT PLATES BS 986 LBL 44 - RBL 30 'T' CAP OF FLOORBEAM. CORROSION TASK NR C53-107-02. REPAIRED PER TR 53-60-01. (M)
- [SDR USAA990255](https://openairdocs.org/sdr/USAA990255.md): Frame · cracked · Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.800 INCH CRACK AT FORWARD FRAME OF AFT CARGO DOOR 2 INCH ABOVE FORWARD LATCH ARM. INSTALLED DOUBLER PER SRM 52-30-02. (M)
- [SDR USAA990254](https://openairdocs.org/sdr/USAA990254.md): Frame · cracked · Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, Frame
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK AT BS 807 OBL FRAME. INSTALLED REPAIR PLATE AND FILLERS PER SRM 53-00-07. (M)
- [SDR USAA990234](https://openairdocs.org/sdr/USAA990234.md): Tie Clip · cracked · Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 277 STRINGER 24L TIE CLIP. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA990225](https://openairdocs.org/sdr/USAA990225.md): Floorbeam · corroded · Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, Floor Beam
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.5 INCH BY.5 INCH AREA OF CORROSION AT NUT PLATE HOLES BS 947 LBL 24 - RBL 24 FLOORBEAM, CORROSION TASK NR C53-107-02. INSTALLED REPAIR 'T' SECTION AND REPAIR ANGLE PER SRM 53-00-51. (M)
- [SDR USAA990217](https://openairdocs.org/sdr/USAA990217.md): Angle · cracked · Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK BS 294 WL 208.10 RBBL 55 ANGLE STIFFENER. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA990216](https://openairdocs.org/sdr/USAA990216.md): Frame · cracked · Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, Frame
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK BS 294, WL 208.10 RBBL 55 FRAME. INSTALLED DOUBLER PER SRM 51-70-11 EA 63977. (M)
- [SDR USAA950564](https://openairdocs.org/sdr/USAA950564.md): Floorbeam · corrosion · May 9, 1995 · N415US · Boeing 737401 · Fuselage Main, Floor Beam
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 10 INCHES CORRODED AREA ON FLOORBEAM AT STATION 967 RBL 9 TO RBL 36. REPAIRED PER EA 39247. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA950563](https://openairdocs.org/sdr/USAA950563.md): Intercostal · corrosion · May 3, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous Structure
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 12 INCHES CORRODED AREA ON INTERCOSTAL AT STATION 967 TO 986.5, LBL 17. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA950565](https://openairdocs.org/sdr/USAA950565.md): Angle · corrosion · May 2, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous Structure
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 36 INCHES OF CORROSION, AFT ENTRY THRESHOLD. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA950560](https://openairdocs.org/sdr/USAA950560.md): Support · corroded · May 2, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous Structure
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 20 INCH AREA CORRODED ON FLOOR SUPPORT AT STATION 947 TO STATION 967, LBL 50. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA950559](https://openairdocs.org/sdr/USAA950559.md): Floorbeam · corroded · Apr 28, 1995 · N415US · Boeing 737401 · Fuselage Main, Floor Beam
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1 INCH BY 5 INCH AREA ON FLOORBEAM, CORRODED AT STATION 947, LBL 12. REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA950558](https://openairdocs.org/sdr/USAA950558.md): Floorbeam · corrosion · Apr 28, 1995 · N415US · Boeing 737401 · Fuselage Main, Floor Beam
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROX 1 INCH BY 5 INCH CORROSION ON FLOORBEAM AT STATION 947, RBL 12. REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA950567](https://openairdocs.org/sdr/USAA950567.md): Door Sill · corroded · Apr 27, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous Structure
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH DIAMETER AND 3 INCH DIAMETER SPOTS OF CORROSION 40 TO 50 PERCENT LOSS TO.375 INCH DIAMETER 100 PERCENT LOSS 3 INCH BY 4 INCH CORROSION BS 807 TO BS 845 ON DOOR SILL BELOW AFT CARGO DOOR. REPAIRED PER SRM
- [SDR USAA950562](https://openairdocs.org/sdr/USAA950562.md): Intercostal · corrosion · Apr 26, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous Structure
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 7 INCH BY 1 INCH CORROSION ON INTERCOSTAL BETWEEN BS 947 AND BS 967 RBL 25 INCHES. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)
- [SDR USAA950561](https://openairdocs.org/sdr/USAA950561.md): Intercostal · corroded · Apr 25, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous Structure
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 6 INCH BY 1 INCH TOTAL CORROSION ON INTERCOSTAL, BETWEEN BS 967 AND BS 947 LBL 16 INCHES. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-10-02, CORROSION LEVEL 2. (M)
- [SDR USAA950566](https://openairdocs.org/sdr/USAA950566.md): Angle · corroded · Apr 24, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous Structure
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION 2 INCHES BY 30 INCHES 'Z' ANGLE IN THRESHOLD OF AFT SERVICE DOOR. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-2, CORROSION LEVEL 2. (M)
- [SDR USAA950557](https://openairdocs.org/sdr/USAA950557.md): Floorbeam · corroded · Apr 24, 1995 · N415US · Boeing 737401 · Fuselage Main, Floor Beam
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION (FULL WIDTH OF T-CAP) STATION 986.5 FLOORBEAM FROM 44 LBL TO 44 RBL. REPAIRED PER SRM 51-70-13 EA 39205. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (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 = 'N415US' AND deregistration_id = 'N415US-2003-11-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N415US-2003-11-04/reports

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