# Service difficulty reports: N244US, cancelled Oct 1, 2002

A list on [N244US, cancelled Oct 1, 2002](https://openairdocs.org/deregistered/N244US-2002-10-01.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 · 84 reports

- [SDR USAASB01232](https://openairdocs.org/sdr/USAASB01232.md): Light · inoperative · Aug 16, 2001 · N244US · Boeing 737201 · Emergency Lighting
  > ALB - PILOT REPORTED THAT THE COCKPIT EVACUATION LIGHT WOULD NOT ILLUMINATE WITH COCKPIT SWITCH IN THE ON POSITION. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB01084](https://openairdocs.org/sdr/USAASB01084.md): Harness · failed · Mar 22, 2001 · N244US · Boeing 737201 · AC Generation System
  > BOS - FLT 2993 - ON CLIMB-OUT FROM BOS, EN ROUTE TO FLL, THE NR 1 GENERATOR BUS OFF LIGHT ILLUMINATED. CREW TRIED TO RESET GENERATOR WITH NO HELP. THE APU WAS ALREADY ON MEL SO THE FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHR INCIDENT. NO EMERG
- [SDR USAA000954](https://openairdocs.org/sdr/USAA000954.md): Floorbeam · corroded · Jul 6, 2000 · N244US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 2 INCHES, BS 986.5, LBL 38. INSTALLED NEW FLOOR SUPPORT PER SRM 51-10-1. (M)
- [SDR USAA000953](https://openairdocs.org/sdr/USAA000953.md): Tie Clip · cracked · Jul 6, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 787, STRINGER 20R. INSTALLED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA000950](https://openairdocs.org/sdr/USAA000950.md): Floorbeam · corroded · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 3 INCHES BY 3 INCHES AND 2 INCHES BY 2 INCHES, BS 986.5 4 INCHES, RBL AND 4 INCHES THROUGH 12 INCHES LBL. FABRICATED NEW T-CAP AND ANGLE DOUBLER PER TR 53-60-01. (M)
- [SDR USAA000949](https://openairdocs.org/sdr/USAA000949.md): Strap · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRAP CRACKED.750 INCH, S-5A STRAP STATION 1138 LT SIDE. INSTALLED INTERIM REPAIR PER EA 67518 AND SRM 53-00-01 FIG 221. (M)
- [SDR USAA000948](https://openairdocs.org/sdr/USAA000948.md): Stringer · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CRACKED 3 INCHES, STATION 1006 TO 1009, STRINGER 27R. REPAIRED PER BOEING DWG 65-46558. (M)
- [SDR USAA000947](https://openairdocs.org/sdr/USAA000947.md): Skin · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND AFT SKIN CRACKED.350 INCH, BS 951 AFT GALLEY DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 53-30-3. (M)
- [SDR USAA000946](https://openairdocs.org/sdr/USAA000946.md): Skin · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED.3 INCHES, STATION 948 SKIN UPPER END SERVICE DOOR HINGE CUTOUT. INSTALLED DOUBLER PER SRM 53-30-3. (M)
- [SDR USAA000945](https://openairdocs.org/sdr/USAA000945.md): Frame · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND FRAME.125 INCH CRACKED, STATION 887, STRINGER 19L. REMOVED AND INSTALLED DOUBLER PER SRM 53-10-4 FIG 9. (M)
- [SDR USAA000944](https://openairdocs.org/sdr/USAA000944.md): Tie Clip · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.5 INCH, STATION 787, STRINGER 3R. INSTALED NEW TIE CLIP PER EO 5393G227. (M)
- [SDR USAA000943](https://openairdocs.org/sdr/USAA000943.md): Skin · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED.5 INCH, BS 764.5 AT STRINGER 19L. INSTALLED FILLER AND DOUBLER PER 53-30-3 FIG 6. (M)
- [SDR USAA000942](https://openairdocs.org/sdr/USAA000942.md): Skin · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED.5 INCH, BS 727A PLUS 17 INCHES STRINGER 19L. REPAIRED DOUBLER PER SRM 53-30-3. (M)
- [SDR USAA000941](https://openairdocs.org/sdr/USAA000941.md): Skin · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1.5 INCH, BS 727A PLUS 8 INCHES STRINGER 19L. REPAIRED DOUBLER PER SRM 53-30-3. (M)
- [SDR USAA000940](https://openairdocs.org/sdr/USAA000940.md): Stringer Clip · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.250 INCH, BS 706, STRINGER 3R. REMOVED AND REPLACED PER SRM 51-10-1. (M)
- [SDR USAA000939](https://openairdocs.org/sdr/USAA000939.md): Floorbeam · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND 2 CRACKS IN FLOORBEAM.100 INCH, BS 663, WL 208 UPPER T-CAP. INSTALLED REPAIR PER TR 57-10-04. (M)
- [SDR USAA000938](https://openairdocs.org/sdr/USAA000938.md): Floorbeam · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CRACKED.250 INCH, STATION 520, RBL 45 UPPER CHORD RADIUS. INSTALLED REPAIR PER EA 67455. (M)
- [SDR USAA000937](https://openairdocs.org/sdr/USAA000937.md): Floorbeam · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND BEAM CRACKED 3 INCHES, BS 520, RBL 24, WL 208. INSTALLED REPAIR ANGLE PER EA 67455. (M)
- [SDR USAA000936](https://openairdocs.org/sdr/USAA000936.md): Floorbeam · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CRACKED, BS 520, LBL 45 UPPER CHORD AFT RADIUS. INSTALLED DOUBLER PER EA 67455. (M)
- [SDR USAA000935](https://openairdocs.org/sdr/USAA000935.md): Floorbeam · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CRACKED.500 INCH, BS 520, LBL 24 UPPER CHORD AFT RADIUS. REPAIRED PER EA 67455. (M)
- [SDR USAA000934](https://openairdocs.org/sdr/USAA000934.md): Stringer Clip · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRINGER TIE CLIP CRACKED.25 INCH, BS 520, STRINGER 19L. INSTALLED DOUBLER PER SRM 51-40-03. (M)
- [SDR USAA000933](https://openairdocs.org/sdr/USAA000933.md): Web · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED.5 INCH, STRINGER 10L SUPPORT WEB BS 350. REPLACED WEB PER SRM 51-10-02. (M)
- [SDR USAA000932](https://openairdocs.org/sdr/USAA000932.md): Angle · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND ANGLE CRACKED 1.5 INCHES, BS 350, STRINGER 16L. REPLACED SUPPORT ANGLE PER SRM 51-10-2. (M)
- [SDR USAA000931](https://openairdocs.org/sdr/USAA000931.md): Angle · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND ANGLE CRACKED 2 INCHES, BS 350, STRINGER 15L. REMOVED AND REPLACED ANGLE PER SRM 51-10-2 AND SRM 51-40-02. (M)
- [SDR USAA000930](https://openairdocs.org/sdr/USAA000930.md): Frame · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED 1.5 INCH, BS 350, AT STRINGER 15L DOOR STOP FITTING. REPAIRED PER SRM 51-10-2. (M)
- [SDR USAA000929](https://openairdocs.org/sdr/USAA000929.md): Skin · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND OUTER SKIN CRACKED 3 INCHES, AFT ENTRY DOOR CUTOUT LOWER FORWARD CORNER STATION 947. INSTALLED EXTERNAL SKIN TRIPLER PER SRM 53-30-3. (M)
- [SDR USAA000928](https://openairdocs.org/sdr/USAA000928.md): Skin · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND INNER SKIN PLATE CRACKED 1 INCH, AFT SERVICE DOOR FUSE. CUTOUT TORQUE BOX INBOARD SIDE. INSTALLED DOUBLER AND FILLER PER TR 53-30-07A. (M)
- [SDR USAA000927](https://openairdocs.org/sdr/USAA000927.md): Support Fitting · cracked · Jul 3, 2000 · N244US · Boeing 737201 · Wing, Attach Fittings
  > CLT - FOUND SUPPORT FITTING CRACKED.200 INCH, RT WING LANDING GEAR BEAM. ACCOMPLISHED PART A PER TR 57-40-10. (M)
- [SDR USAA000951](https://openairdocs.org/sdr/USAA000951.md): Angle · corroded · Jul 3, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND Z-ANGLE CORRODED 24 INCHES BY 1 INCH, AFT SERVICE DOOR BS 947 TO BS 986 RT. INSTALLED NEW Z-ANGLE PER SRM 51-10-02. (M)
- [SDR USAA000879](https://openairdocs.org/sdr/USAA000879.md): Angle · corroded · Jun 20, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND Z-ANGLE CORRODED 1 INCH BY 1 INCH, AFT ENTRY DOOR SILL Z-ANGLE. INSTALLED NEW Z-ANGLE PER SRM 51-10-1 AND 51-30-0. CORROSION LEVEL 1. (M)
- [SDR USAA000873](https://openairdocs.org/sdr/USAA000873.md): Stringer · corroded · Jun 19, 2000 · N244US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CORRODED 2 INCHES, STATION 947 STRINGER 27L. REMOVED AND REPLACED PER SRM 53-10-03. (M)
- [SDR USAA000872](https://openairdocs.org/sdr/USAA000872.md): Fitting · cracked · Jun 19, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND BULKHEAD FITTING CRACKED.750 AND.375 INCH, BS 663.75 BULKHEAD FITTING RT SIDE WL 191.5 POCKET. REMOVED AND REPLACED BULKHEAD FITTING PER EA 67452, 67457 AND 67412. (M)
- [SDR USAA000854](https://openairdocs.org/sdr/USAA000854.md): Floorbeam · corroded · Jun 15, 2000 · N244US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 12 INCHES BY 1 INCH, 3 AREAS AT STATION 344, LBL 8 THROUGH LBL 18. REPAIRED T-CAP PER TR 53-10-13. CORROSION LEVEL 2. (M)
- [SDR USAA000852](https://openairdocs.org/sdr/USAA000852.md): Frame · corroded · Jun 15, 2000 · N244US · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND FRAME CORRODED 2.5 INCHES, BS 967, STRINGER 26R AT SKIN ATTACH POINT. INSTALLED DOUBLER FRAME REPAIR PER SRM 53-10-4. CORROSION LEVEL 2, C53-208-01. (M)
- [SDR USAA000836](https://openairdocs.org/sdr/USAA000836.md): Web · cracked · Jun 13, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB/STIFFENER CRACKED 6 INCHES, STATION 727, LBL 13 BETWEEN VERT SUPPORT BEAMS. REPLACED PART PER SRM 51-10-1. (M)
- [SDR USAA000837](https://openairdocs.org/sdr/USAA000837.md): Angle · cracked · Jun 13, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND ANGLE CRACKED 4 INCHES, STATION 727B LBL 40. REPLACED PER SRM 51-10-1. (M)
- [SDR USAA000839](https://openairdocs.org/sdr/USAA000839.md): Stringer · cracked · Jun 13, 2000 · N244US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND SEVERAL CRACKS.125 INCH OR LESS, INSIDE CHANNEL STRINGER 15L, BETWEEN STATION 520 AND 540. INSTALLED STRINGER REPAIR SECTION PER SRM 53-10-3. (M)
- [SDR USAA000813](https://openairdocs.org/sdr/USAA000813.md): Tie Clip · cracked · Jun 12, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, BS 706, STRINGER 5R. REMOVED AND REPLACED PER SRM 51-10-1. (M)
- [SDR USAA000808](https://openairdocs.org/sdr/USAA000808.md): Tie Clip · cracked · Jun 8, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.5 INCH, STATION 787 STRINGER 7R. REPLACED TIE CLIP PER SRM 51-10-1. (M)
- [SDR USAA000804](https://openairdocs.org/sdr/USAA000804.md): Intercostal · cracked · Jun 8, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND INTERCOSTAL CRACKED 1 INCH AND 2 INCHES, FLOOR SUPPORT BETWEEN STATION 380 TO 400 BL 0. REPAIRED PER SRM 51-10-01. (M)
- [SDR USAA000797](https://openairdocs.org/sdr/USAA000797.md): Tie Clip · cracked · Jun 5, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.5 INCH, STATION 767, STRINGER 11R. FABRICATED NEW CLIP PER SRM 51-10-1 AND DWG 6945156. (M)
- [SDR USAA000798](https://openairdocs.org/sdr/USAA000798.md): Tie Clip · cracked · Jun 5, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED 1 INCH, STATION 663, STRINGER 10L. REPAIRED PER EO 5393G227. (M)
- [SDR USAA000799](https://openairdocs.org/sdr/USAA000799.md): Tie Clip · cracked · Jun 5, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, BS 597, STRINGER 5R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-1. (M)
- [SDR USAA000800](https://openairdocs.org/sdr/USAA000800.md): Tie Clip · cracked · Jun 5, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED 1 INCH, STATION 706, STRINGER 3R. REPAIRED PER EO 5393G227. (M)
- [SDR USAA000775](https://openairdocs.org/sdr/USAA000775.md): Tie Clip · cracked · Jun 2, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, BS 685, STRINGER 4L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)
- [SDR USAA000776](https://openairdocs.org/sdr/USAA000776.md): Tie Clip · cracked · Jun 2, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, BS 727A, STRINGER 4L. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)
- [SDR USAA000777](https://openairdocs.org/sdr/USAA000777.md): Tie Clip · cracked · Jun 2, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, BS 787, STRINGER 3R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)
- [SDR USAA000778](https://openairdocs.org/sdr/USAA000778.md): Tie Clip · cracked · Jun 2, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, BS 787, STRINGER 5R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)
- [SDR USAA000779](https://openairdocs.org/sdr/USAA000779.md): Clip · cracked · Jun 2, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, BS 787, STRINGER 7R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)
- [SDR USAA991341](https://openairdocs.org/sdr/USAA991341.md): Keel Beam · corroded · Dec 6, 1999 · N244US · Boeing 737201 · Fuselage Main, Keel
  > TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND MINOR CORROSION 4 INCH BY 6 INCH BOTTOM KEEL BEAM STATION 727 STRINGER 26L. CORROSION LEVEL 1. INSTALLED DOUBLER PER SRM 53-30-3 FIG 28. (M)

Next page: https://openairdocs.org/deregistered/N244US-2002-10-01/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 = 'N244US' AND deregistration_id = 'N244US-2002-10-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N244US-2002-10-01/reports

---
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