# Service difficulty reports: N252AU, cancelled Jul 18, 2002

A list on [N252AU, cancelled Jul 18, 2002](https://openairdocs.org/deregistered/N252AU-2002-07-18.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 · 83 reports

- [SDR USAASB01108](https://openairdocs.org/sdr/USAASB01108.md): Charger · inoperative · Apr 25, 2001 · N252AU · Boeing 737201 · Emergency Lighting
  > MCO - THE FORWARD SECTION OF LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY/CHARGER. (M)
- [SDR USAASB00361](https://openairdocs.org/sdr/USAASB00361.md): Charger · discharged · Dec 27, 2000 · N252AU · Boeing 737201 · Emergency Lighting
  > LGA - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY PATH LIGHTS FROM SEAT ROWS 1 THROUGH 7 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 9008-3-5A) AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)
- [SDR USAASB00353](https://openairdocs.org/sdr/USAASB00353.md): Seal · failed · Dec 21, 2000 · N252AU · Boeing 737201 · Passenger/Crew Doors
  > BWI - FLT 2637 - ON CLIMB-OUT FROM BWI, AT FL230, A LOUD SQUEAL BEGAN COMING FROM THE FORWARD MAIN ENTRY DOOR. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FORWARD MAIN
- [SDR USAA001925](https://openairdocs.org/sdr/USAA001925.md): Skin · cracked · Nov 13, 2000 · N252AU · Boeing 737201 · Horizontal Stabilizer, Plate/Skin
  > CLT - FOUND SKIN CRACKED.5 INCH, UNDER STRINGER 5L, STATION 1138 LEFT STAB. INSTALLED DOUBLER PER EA 68315. (M)
- [SDR USAA001959](https://openairdocs.org/sdr/USAA001959.md): Web · cracked · Nov 13, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CRACKS UPPER RT & LT RADAR MOUNT BRACKET RBL 05 WL 198CORRECTIVE ACTION: DOUBLERS INSTALLED PER EA 68266
- [SDR USAA002118](https://openairdocs.org/sdr/USAA002118.md): Skin · cracked · Nov 11, 2000 · N252AU · Boeing 737201 · Service Doors
  > PIT - FOUND SKIN CRACKED.5 INCH, AFT ENTRY DOOR BELOW LOWER HINGE AREA. INSTALLED DOUBLER PER SRM 52-00-3. (M)
- [SDR USAA001917](https://openairdocs.org/sdr/USAA001917.md): Angle · cracked · Nov 9, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND ANGLE 1 INCH, RT STA 597 BELOW FLOOR LEVEL. REPLACED ANGLE PER SRM 51-10-1. (M)
- [SDR USAA001887](https://openairdocs.org/sdr/USAA001887.md): Intercostal · corroded · Nov 7, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND INTERCOSTAL CORRODED 1 INCH BY 1 INCH, STATION 990, LBL 17 FLOORBEAM INTERCOSTAL. INSTALLED DOUBLER PER SRM 53-10-09 AND TR 53-60-02. CORROSION LEVEL 1 C53-107-02. (M)
- [SDR USAA001892](https://openairdocs.org/sdr/USAA001892.md): Frame · cracked · Nov 7, 2000 · N252AU · Boeing 737201 · Fuselage Main, Frame
  > CRACK STA 490, STR 23R. SPLICED IN FRAME SECTION PER SRM 51-40-3 FIG 1
- [SDR USAA001891](https://openairdocs.org/sdr/USAA001891.md): Frame · cracked · Nov 7, 2000 · N252AU · Boeing 737201 · Fuselage Main, Frame
  > CRACK STA 597, R/W LWR SIDE OF FRAME. REPLACED WEB/FRAME PER SRM 51-10-01
- [SDR USAA001890](https://openairdocs.org/sdr/USAA001890.md): Floorbeam · corroded · Nov 7, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CORROSION LEVEL 1 C 53-107-02 FLOORBEAM INTERCOASTAL STRAP STA 1016, LBL 17.5INSTALLED FLOORBEAM REPAIR ANGLE PER SRM 51-10-1
- [SDR USAA001889](https://openairdocs.org/sdr/USAA001889.md): Intercostal · corroded · Nov 7, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CORROSION LEVEL 1 C 53-107-02 FLOORBEAM INTERCOASTAL STRAP STA 1016, RBL 2.5.INSTALLED DOUBLER PER SRM 531009 & 536002
- [SDR USAA001888](https://openairdocs.org/sdr/USAA001888.md): Floorbeam · corroded · Nov 7, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED. INSTALLED DOUBLER PER SRM 53-10-09 & TR 53-60-02.
- [SDR USAA001877](https://openairdocs.org/sdr/USAA001877.md): Floorbeam · corroded · Nov 3, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 2 INCHES AND 1 FT BY 2 INCHES, STATION 1006 TO 1016, LBL 5.5 TO 9. REMOVED AND REPLACED PER SRM 51-30-00. (M)
- [SDR USAA001859](https://openairdocs.org/sdr/USAA001859.md): Frame · cracked · Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND CHORD CRACKED 2 INCH, BS 178, WL 195, LBL 24. INSTALLED NEW CHORD ANGLE. (M)
- [SDR USAA001858](https://openairdocs.org/sdr/USAA001858.md): Web · cracked · Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED, BS 178, RBL 5, WL 198. INSTALLED DOUBLER PER EA 68266. (M)
- [SDR USAA001857](https://openairdocs.org/sdr/USAA001857.md): Web · cracked · Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED.5 INCH IN TWO PLACES, BS 178, LBL 5 AND 6 UPPER RADAR MOUNT BRACKET. INSTALLED DOUBLER PER EA 68266. (M)
- [SDR USAA001856](https://openairdocs.org/sdr/USAA001856.md): Frame · cracked · Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND SIDE CHORD CRACKED 1 INCH, BS 178, WL 207, LBL 26. INSTALLED NEW CHORD ANGLE PER EA 68295. (M)
- [SDR USAA001855](https://openairdocs.org/sdr/USAA001855.md): Web · cracked · Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED 1 INCH, BS 178, WL 207, LBL 27. INSTALLED NEW CHORD ANGLE PER EA 68295. (M)
- [SDR USAA001854](https://openairdocs.org/sdr/USAA001854.md): Web · cracked · Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED.250 INCH, BS 178, LBL.05, WL 197-201. INSTALLED DOUBLER PER EA 68266. (M)
- [SDR USAA001853](https://openairdocs.org/sdr/USAA001853.md): Floorbeam · corroded · Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH IN SIX AREAS, UPPER T-CAP FLOORBEAM STATION 1006, LBL 9, 11, 15, 28.5. INSTALLED NEW T-CAP SECTION PER SRM 53-10-9 FIG 2. (M)
- [SDR USAA001842](https://openairdocs.org/sdr/USAA001842.md): Web · cracked · Nov 1, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED 1 INCH, BS 676, RBL 25. INSTALLED DOUBLER AND V CHANNEL PER EO 5791G632. (M)
- [SDR USAA001841](https://openairdocs.org/sdr/USAA001841.md): Floorbeam · cracked · Nov 1, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CRACKED.250 INCH, BS 668 - BS 680, LBL 23.5. REMOVED AND REPLACED BEAM PER DWG 65-45410. (M)
- [SDR USAA001840](https://openairdocs.org/sdr/USAA001840.md): Stiffener · cracked · Nov 1, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND VERTICAL CHORD CRACKED.25 INCH, BS 178, AFT SIDE LBL 5-7, WL 184. FOUND DOUBLER STRAP/REPAIR ANGLES PER SRM 53-10-11. (M)
- [SDR USAA001839](https://openairdocs.org/sdr/USAA001839.md): Stiffener · cracked · Nov 1, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND VERTICAL CHORD (STIFFENER) CRACKED.25 INCH, BS 178, AFT SIDE RBL 5-7, WL 184. FOUND DOUBLER STRAP/REPAIR ANGLES PER SRM 53-10-11. (M)
- [SDR USAA001835](https://openairdocs.org/sdr/USAA001835.md): Tie Clip · cracked · Oct 31, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRINGER TIE CLIP CRACKED.25 INCH, STATION 578 STRINGER 5L. REPLACED TIE CLIP PER EO 5393G227 REV A. (M)
- [SDR USAA001833](https://openairdocs.org/sdr/USAA001833.md): Web · cracked · Oct 27, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED.250 INCH, BS 706-710, LBL 24. INSTALLED NEW WEB PER EA 68267. (M)
- [SDR USAA001832](https://openairdocs.org/sdr/USAA001832.md): Floorbeam · corroded · Oct 27, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3 INCHES, LOWER SURFACE CREASEBEAM WEB AFT SERVICE DOOR. INSTALLED DOUBLER AND REPAIR ANGLE PER SRM 51-10-1. CORROSION LEVEL 1 C53-107-02. (M)
- [SDR USAA001826](https://openairdocs.org/sdr/USAA001826.md): Stringer · corroded · Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CORRODED 1 INCH BY 1 INCH AREA, BS 948 STRINGER 27L. CORROSION LEVEL 1. INSTALLED NEW SECTION PER SRM 53-10-3. (M)
- [SDR USAA001825](https://openairdocs.org/sdr/USAA001825.md): Floorbeam · corroded · Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH IN FOUR PLACES, STATION 947.5 RBL 4, 5, 10.5 AND LBL 5. CORROSION LEVEL 1. SPLICED T-CAP PER SRM 53-10-2. (M)
- [SDR USAA001824](https://openairdocs.org/sdr/USAA001824.md): Angle · corroded · Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TRANSITION ANGLE CORRODED 32 INCHES BY 1 INCH, STATION 344 TO 312. INSTALLED NEW Z-ANGLE PER SRM 51-10-2 AND 51-30-3. (M)
- [SDR USAA001823](https://openairdocs.org/sdr/USAA001823.md): Floorbeam · corroded · Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOOBEAM CORRODED 12 INCHES BY 5 INCHES, STATION 344, BL 0 TO BL 12L. CORROSION LEVEL 1. REPLACED PER TR 53-10-13. (M)
- [SDR USAA001822](https://openairdocs.org/sdr/USAA001822.md): Web · cracked · Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED.250 INCH, BS 715. REPAIRED PER TR 57-10-05. (M)
- [SDR USAA001821](https://openairdocs.org/sdr/USAA001821.md): Web · cracked · Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND LONGITUDINAL WEB CRACKED 1 INCH, BS 706-710, RBL 24. INSTALLED DOUBLER AND WEB PER EA 67997-A, EA 68267 AND TR 57-10-05. (M)
- [SDR USAA001820](https://openairdocs.org/sdr/USAA001820.md): Intercostal · cracked · Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND INTERCOSTAL CRACKED 2 INCHES, BS 178, WL 195, RBL 24. REPAIRED PER EO 5300V152. (M)
- [SDR USAA001819](https://openairdocs.org/sdr/USAA001819.md): Intercostal · cracked · Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND INTERCOSTAL CRACKED 2 INCHES, BS 178 WL 195, LBL 24. INSTALLED NEW INTERCOSTAL PER SRM 51-10-1. (M)
- [SDR USAA001818](https://openairdocs.org/sdr/USAA001818.md): Beam · cracked · Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND LONGITUDINAL BEAM 2 INCH CRACK, BS 663, OBL. INSTALLED DOUBLER, NEW WEB PER TR 57-10-04 AND EA 68369. (M)
- [SDR USAA001817](https://openairdocs.org/sdr/USAA001817.md): Tie Clip · cracked · Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP.5 INCH, STATION 400 STRINGER 28L. REPAIRED PER SRM 51-10-1. (M)
- [SDR USAA001816](https://openairdocs.org/sdr/USAA001816.md): Stringer Clip · cracked · Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRINGER TIE CRACKED.5 INCH, BS 360, STRINGER 16L. REPAIRED PER SRM 51-30-2. (M)
- [SDR USAA001815](https://openairdocs.org/sdr/USAA001815.md): Angle · cracked · Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND INTERCOSTAL ANGLE CRACKED 2 INCHES, BS 178, WL 195 LBL 25. INSTALLED DOUBLER PER SRM 51-40-4. (M)
- [SDR USAA001797](https://openairdocs.org/sdr/USAA001797.md): Skin · cracked · Oct 23, 2000 · N252AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND FUSELAGE SKIN CRACKED 2 INCHES, STATION 957 FORWARD LOWER CORNER AFT RIGHT SERVICE DOOR CUTOUT. INSTALLED 3 DOUBLERS AND FILLERS PER SRM 53-30-3. (M)
- [SDR USAA001798](https://openairdocs.org/sdr/USAA001798.md): Skin · corroded · Oct 23, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CORROSION ON SKIN 8 INCHES BY 3 INCHES, STATION 767-787. CORROSION LEVEL 1. INSTALLED DOUBLER AND FILLER PER SRM 53-30-3. (M)
- [SDR USAA001778](https://openairdocs.org/sdr/USAA001778.md): Frame · cracked · Oct 19, 2000 · N252AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED 3 INCHES, LOWER END OF FORWARD SERVICE DOOR FORWARD FRAME WL 209. FABRICATED REPAIR PARTS PER SRM 51-40-03. (M)
- [SDR USAA001779](https://openairdocs.org/sdr/USAA001779.md): Floorbeam · corroded · Oct 19, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM 38 INCHES, STATION 328, BL 12L TO BL 50L. CORROSION LEVEL 1. REPLACED FLOORBEAM PER SRM 53-10-9. (M)
- [SDR USAA001772](https://openairdocs.org/sdr/USAA001772.md): Floorbeam · corroded · Oct 18, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH BY 1 INCH EACH, STATION 987, LBL 5, 6, 16, 17, 39.5 AND RBL 5, 14.5, 23.5. INSTALLED NEW T-CAP PER TR 53-60-01 REV A. (M)
- [SDR USAA001771](https://openairdocs.org/sdr/USAA001771.md): Floorbeam · cracked · Oct 18, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM ANGLE CRACKED 1 INCH, BS 520, RBL 45. REPLACED ANGLE PER REPAIR DOCUMENT 51-10-02. (M)
- [SDR USAA001759](https://openairdocs.org/sdr/USAA001759.md): Floor Support · cracked · Oct 16, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND FLOOR SUPPORT CRACKED 1 INCH, BS 727, LBL 46. FABRICATED ANGLE PER SRM 51-10-03. (M)
- [SDR USAA001758](https://openairdocs.org/sdr/USAA001758.md): Bulkhead · cracked · Oct 16, 2000 · N252AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB CRACKED, BS 178, RBL 10.5, WL 234. INSTALLED DOUBLER PER SRM 53-10-11. (M)
- [SDR USAA001757](https://openairdocs.org/sdr/USAA001757.md): Bulkhead · cracked · Oct 16, 2000 · N252AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB CRACKED.25 INCH IN TEN PLACES, BS 178, WL 234 BETWEEN LT AND RBL 7 TO 12 AFT SIDE. INSTALLED DOUBLER PER SRM 53-10-11. (M)
- [SDR USAA001707](https://openairdocs.org/sdr/USAA001707.md): Splice · cracked · Oct 10, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRINGER SPLICE CRACKED.375 INCH, STATION 908, STRINGER 4L CIRCUMFERENTIAL SPLICE. REPAIRED PER SRM 51-10-01. (M)

Next page: https://openairdocs.org/deregistered/N252AU-2002-07-18/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 = 'N252AU' AND deregistration_id = 'N252AU-2002-07-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N252AU-2002-07-18/reports

---
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