# Service difficulty reports: N246US, cancelled Mar 25, 2002

A list on [N246US, cancelled Mar 25, 2002](https://openairdocs.org/deregistered/N246US-2002-03-25.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 · 79 reports

- [SDR USAA010396](https://openairdocs.org/sdr/USAA010396.md): Skin · cracked · Apr 16, 2001 · N246US · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - FOUND SKIN CRACKED BS 727A PLUS 1 INCH BELOW STRINGER 17L, BS 727A PLUS 18 INCHES ABOVE STRINGER 18L. REMOVED EXISTING REPAIR, INSTALLED REPAIR DOUBLER AND TRIPLER, SRM 53-30-03 FIG 1. (M)
- [SDR USAA010394](https://openairdocs.org/sdr/USAA010394.md): Skin · cracked · Apr 16, 2001 · N246US · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - FOUND SKIN CRACKED 1.5 INCH, BS 727B PLUS 12 INCHES, STRINGER 17L. INSTALLED REPAIR DOUBLE, SRM 53-30-3, FIG 1. (M)
- [SDR USAASB01098](https://openairdocs.org/sdr/USAASB01098.md): Power Supply · inoperative · Apr 7, 2001 · N246US · Boeing 737201 · Emergency Lighting
  > CLE - THE AFT SERVICE DOOR AND AFT ENTRY DOOR EMERGENCY EXIT SIGNS AND ENTRY DOOR LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK. (M)
- [SDR USAA010395](https://openairdocs.org/sdr/USAA010395.md): Skin · cracked · Apr 1, 2001 · N246US · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - FOUND SKIN CRACKED 4 INCHES, BS 747 PLUS 3 INCHES, STRINGER 18R. INSTALLED REPAIR DOUBLER, SRM 53-30-3 FIG 1. (M)
- [SDR USAA010164](https://openairdocs.org/sdr/USAA010164.md): Skin · cracked · Jan 16, 2001 · N246US · Boeing 737201 · Fuselage Main, Plate/Skin
  > BOS - FOUND SKIN CRACKED 2 INCHES, BS 727A STRINGER 15L. INSTALLED DOUBLER PER SRM 53-30-3 PP 2E, FIG 1. (M)
- [SDR USAASB00260](https://openairdocs.org/sdr/USAASB00260.md): Control Unit · failed · Sep 17, 2000 · N246US · Boeing 737201 · Passenger Oxygen System
  > FLL - FLT 2995 - EN ROUTE FROM LGA-FLL, AT FL310, THE PASSENGERS OXYGEN DROPPED TO ZERO PSI. CREW ACCOMPLISHED PROCEDURES AND DESCENDED TO FL100. BEFORE LANDING, THE PASSENGER OXYGEN PRESSURE RETURNED TO NORMAL. MAINTENANCE REMOVED AND REPLACED THE PASSENGE
- [SDR USAA000736](https://openairdocs.org/sdr/USAA000736.md): Floorbeam · corroded · May 24, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 30 INCHES, STATION 328, LBL 28, AND RBL 20 - RBL 50. T-CAP REPLACEMENT PER SRM 53-10-2. (M)
- [SDR USAA000735](https://openairdocs.org/sdr/USAA000735.md): Floorbeam · corroded · May 24, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED, 1 INCH BY 8 INCH, BS 259 FLOORBEAM. INSTALLED DOUBLER AND NEW T-CAP PER TR 53-10-16 AND EA 67170. CORROSION LEVEL 2. (M)
- [SDR USAA000726](https://openairdocs.org/sdr/USAA000726.md): Floorbeam · corroded · May 23, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 344 UPPER CHORD LBL 15 TO LBL 50. REPAIRED T-CAP PER TR 53-10-13. (M)
- [SDR USAA000725](https://openairdocs.org/sdr/USAA000725.md): Fitting · cracked · May 23, 2000 · N246US · Boeing 737201 · Main Landing Gear Attach Section
  > CLT - FOUND.5 INCH CRACK IN FITTING, OUTBOARD SUPPORT FITTING MLG BEAM AT CUTOUT, REMOVED AND REPLACED. (M)
- [SDR USAA000715](https://openairdocs.org/sdr/USAA000715.md): Fitting · cracked · May 16, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, EXPANSION BEAM FITTING CRACKED 1.5 INCHES, BS 520, RBL 25. INSTALLED DOUBLER AND NEW CHANNEL PER EA 67143. (X)
- [SDR USAA000711](https://openairdocs.org/sdr/USAA000711.md): Beam · cracked · May 15, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, BEAM WEB HAD 2 EACH.75 INCH CRACKS, BL ZERO, STA 706 TO STA 713, WL 203 BEAM WEB. INSTALLED DOUBLER PER EA 67224. (X)
- [SDR USAA000710](https://openairdocs.org/sdr/USAA000710.md): Fitting · cracked · May 15, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, EXPANSION BEAM FITTING HAD.50 INCH CRACK, STA 520, LBL 25 EXPANSION BEAM FITTING. INSTALLED DOUBLER AND REPAIR ANGLES PER EA 67143. (X)
- [SDR USAA000704](https://openairdocs.org/sdr/USAA000704.md): Floorbeam · corroded · May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FLOORBEAM HAD LEVEL 2 CORROSION, 3 INCHES BY 15 INCHES, BS 986.5 LBL 14 TO RBL 16. INSTALLED T-CAP PER TR 53-60-1. (X)
- [SDR USAA000694](https://openairdocs.org/sdr/USAA000694.md): Beltframe · corroded · May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - BELT FRAME HAD LEVEL 2 CORROSION,.250 INCH BY.250 INCH, BS 727B, RBL 04. INSTALLED DOUBLER PER SRM 53-10-4. (X)
- [SDR USAA000692](https://openairdocs.org/sdr/USAA000692.md): Floorbeam · corroded · May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FLOORBEAM HAD LEVEL 2 CORROSION, 1 INCH BY 1 INCH, BS 986.5 LBL 43. INSTALLED T-CAP PER TR 53-60-01. (X)
- [SDR USAA000690](https://openairdocs.org/sdr/USAA000690.md): Floorbeam · corroded · May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FLOORBEAM HAD LEVEL 2 CORROSION, 1 INCH BY 6 INCH, AT BS 986.5, RBL 27, RBL 33. INSTALLED T-CAP PER TR 53-60-1. (X)
- [SDR USAA000688](https://openairdocs.org/sdr/USAA000688.md): Floorbeam · corroded · May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FLOORBEAM HAD LEVEL 2 CORROSION, 1 INCH BY 2 INCH, BS 986.5, RBL 40 TO RBL 42. INSTALLED T-CAP PER TR 53-60-1. (X)
- [SDR USAA000687](https://openairdocs.org/sdr/USAA000687.md): Skin · cracked · May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - SKIN CRACKED 2.7 INCHES, STR 19L, STA 726 - STA 765, STR 18L 765-780. REPAIRED FILLER AND DOUBLER PER SRM 53-30-03 FIGURE 17. (X)
- [SDR USAA000686](https://openairdocs.org/sdr/USAA000686.md): Floorbeam · cracked · May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FLOORBEAM CRACKED.50 INCH, UPPER FLANGE STA 520, LBL 45. INSTALLED DOUBLER AND PIVOT LINK PER EA 67143. (X)
- [SDR USAA000685](https://openairdocs.org/sdr/USAA000685.md): Attach Angle · cracked · May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Attach Fittings
  > CLT - ATTACH ANGLE CRACKED 1.50 INCHES, AT FRAME TO STRINGER ATTACH ANGLE STA 360, STR 20R. INSTALLED DOUBLER PER SRM 51-40-3. (X)
- [SDR USAA000684](https://openairdocs.org/sdr/USAA000684.md): Frame · cracked · May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Frame
  > CLT - FRAME HAD A 4 INCH CRACK AT STA 360, JUST ABOVE STR 20R. INSTALLED DOUBLER PER SRM 51-40-3. (X)
- [SDR USAA000683](https://openairdocs.org/sdr/USAA000683.md): Floorbeam · corroded · May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT- FLOORBEAM HAD LEVEL 1 CORROSION,.250 INCH BY.250 INCH, BS 312, LBL 08 TO RBL 08. INSTALLED NEW T-CAP PER TR 53-10-13. (X)
- [SDR USAA000682](https://openairdocs.org/sdr/USAA000682.md): Floorbeam · corroded · May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT- FLOORBEAM HAS LEVEL 1 CORROSION, 1 INCH BY 2 INCH, BS 986.5, RBL 37 TO RBL 45. INSTALLED T-CAP PER TR 53-60-1. (X)
- [SDR USAA000681](https://openairdocs.org/sdr/USAA000681.md): Floorbeam · corroded · May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FLOORBEAM HAD LEVEL 1 CORROSION, 1 INCH BY 1 INCH, BL 1006, LBL 19. REPAIRED ANGLE, INSTALLED PER EA67218 AND SRM 51-10-6. (X)
- [SDR USAA000679](https://openairdocs.org/sdr/USAA000679.md): Angle · cracked · May 9, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - WEB AND ANGLE HAD 6 EACH CRACKS, 4 EACH AT.50 INCH AND 2 EACH AT.1250 INCH, BL ZERO FROM BS 927 TO BS 947. FABRICATED AND INSTALLED NEW ANGLE PER DWG 6936656. (X)
- [SDR USAA000678](https://openairdocs.org/sdr/USAA000678.md): Floorbeam · corroded · May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FLOORBEAM HAD LEVEL 1 CORROSION, 1 INCH BY 1 INCH, BS 947, LBL 18. REPLACED T-CAP PER SRM 53-10-2. (X)
- [SDR USAA000677](https://openairdocs.org/sdr/USAA000677.md): Floorbeam · corroded · May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FLOORBEAM HAD LEVEL 1 CORROSION, 1 INCH BY 1 INCH, BS 947, LBL 14. REPLACED T-CAP PER SRM 53-10-2. (X)
- [SDR USAA000676](https://openairdocs.org/sdr/USAA000676.md): Floorbeam · corroded · May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FLOORBEAM HAD LEVEL 1 CORROSION, 2 INCHES BY 3 INCHES, BS 947, LBL 4.5, RBL 5. REPLACED T-CAP PER SRM 53-10-2. (X)
- [SDR USAA000675](https://openairdocs.org/sdr/USAA000675.md): Beam · cracked · May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - WEB CRACKED 1 INCH, AT LT SIDE CREASE BEAM, STA 663.75. (X)
- [SDR USAA000673](https://openairdocs.org/sdr/USAA000673.md): Tie Clip · cracked · May 8, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - TIE CLIP CRACKED 0.500 INCH, BS 986.5, STR 25R. INSTALLED TIE CLIP PER SRM 51-10-01. (X)
- [SDR USAA000672](https://openairdocs.org/sdr/USAA000672.md): Beam · cracked · May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - LEFT CREASE BEAM WEB HAD.50 INCH CRACK. REPLACED WEB PER TR 53-10-02. (X)
- [SDR USAA000671](https://openairdocs.org/sdr/USAA000671.md): Web · cracked · May 8, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - WEB CRACKED, 1 INCH, STR 25R, BS 847. INSTALLED NEW WEB PER SRM 51-10-02. (X)
- [SDR USAA000670](https://openairdocs.org/sdr/USAA000670.md): Floorbeam · cracked · May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FLOORBEAM CRACKED0.500 INCH BY 2 INCH, BS 967, RBL 17.5, CORROSION LEVEL 1. REPLACED ANGLE PER EA67156. (X)
- [SDR USAA000669](https://openairdocs.org/sdr/USAA000669.md): Skin · cracked · May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - SKIN CRACKED.250 INCH, FORWARD SERVICE DOOR CUT OUT AFT CORNER. REPAIRED FILLER AND DOUBLER PER SRM 53-30-3. (X)
- [SDR USAA000653](https://openairdocs.org/sdr/USAA000653.md): Tie Clip · cracked · May 1, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, BS 597, STRINGER 4L. INSTALLED NEW TIE CLIP PER EO5393G227. (M)
- [SDR USAA000652](https://openairdocs.org/sdr/USAA000652.md): Beam · cracked · May 1, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND BEAM WEB CRACKED.5 INCH, RIGHT CREASE BEAM WEB STATIN 647. REPLACED WEB PER TR 53-10-02. (M)
- [SDR USAA000651](https://openairdocs.org/sdr/USAA000651.md): Beam · cracked · May 1, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND BEAM WEB CRACKED.375 INCH, FRAME 663.75 RT CREASE BEAM FORWARD WEB. REPLACED WEB PER TR 53-10-02. (M)
- [SDR USAA000650](https://openairdocs.org/sdr/USAA000650.md): Beam · cracked · May 1, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND BEAM WEB CRACKED.5 INCH, STATION 616 RIGHT CREASE BEAM WEB. REPLACED NEW WEB PER TR 53-10-02. (M)
- [SDR USAA000641](https://openairdocs.org/sdr/USAA000641.md): Clip · cracked · Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TIE CLIP CRACKED.250 INCH, STATION 767, STRINGER 5 LEFT. REMOVED AND REPLACED PER EO 5393G227. (M)
- [SDR USAA000640](https://openairdocs.org/sdr/USAA000640.md): Clip · cracked · Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TIE CLIP CRACKED.250 INCH, BS 747, STRINGER 10 RIGHT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA000639](https://openairdocs.org/sdr/USAA000639.md): Clip · cracked · Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TIE CLIP CRACKED.250 INCH, BS 747, STRINGER 7 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA000638](https://openairdocs.org/sdr/USAA000638.md): Clip · cracked · Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TIE CLIP CRACKED.500 INCH, BS 747, STRINGER 5 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA000637](https://openairdocs.org/sdr/USAA000637.md): Clip · cracked · Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TIE CLIP CRACKED.500 INCH, BS 727B, STRINGER 5 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA000636](https://openairdocs.org/sdr/USAA000636.md): Clip · cracked · Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TIE CLIP CRACKED.250 INCH, BS 727B, STRINGER 8 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA000635](https://openairdocs.org/sdr/USAA000635.md): Clip · cracked · Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TIE CLIP CRACKED.50 INCH, BS 727B, STRINGER 6 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA000634](https://openairdocs.org/sdr/USAA000634.md): Clip · cracked · Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TIE CLIP CRACKED.250 INCH, BS 727A, STRINGER 5R. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA000633](https://openairdocs.org/sdr/USAA000633.md): Clip · cracked · Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TIE CLIP CRACKED, BS 706, STRINGER 10 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA000632](https://openairdocs.org/sdr/USAA000632.md): Clip · cracked · Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TIE CLIP CRACKED,.250 INCH, BS 706 STRINGER 3 RIGHT. REPAIRED PER EO 5393G227. (M)
- [SDR USAA000631](https://openairdocs.org/sdr/USAA000631.md): Clip · cracked · Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TIE CLIP CRACKED.250 INCH, BS 706, STRINGER 2 RIGHT. REPAIRED PER EO 5393G227. (M)

Next page: https://openairdocs.org/deregistered/N246US-2002-03-25/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 = 'N246US' AND deregistration_id = 'N246US-2002-03-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N246US-2002-03-25/reports

---
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