# Service difficulty reports: N261AU, cancelled Jun 6, 2002

A list on [N261AU, cancelled Jun 6, 2002](https://openairdocs.org/deregistered/N261AU-2002-06-06.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 · 73 reports

- [SDR USAASB01181](https://openairdocs.org/sdr/USAASB01181.md): Battery · discharged · Jun 20, 2001 · N261AU · Boeing 737201 · Emergency Lighting
  > BOS - THE PASSENGER CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAASB01102](https://openairdocs.org/sdr/USAASB01102.md): Power Supply · inoperative · Apr 17, 2001 · N261AU · Boeing 737201 · Emergency Lighting
  > MCO - THE CENTER OVERHEAD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE CENTER OVERHEAD EMERGENCY EXIT LIGHT POWER SUPPLY. (M)
- [SDR USAASB01107](https://openairdocs.org/sdr/USAASB01107.md): Power Supply · failed · Apr 4, 2001 · N261AU · Boeing 737201 · Emergency Lighting
  > LGA - THE CENTER EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT POWER SUPPLY. (M)
- [SDR USAA010201](https://openairdocs.org/sdr/USAA010201.md): Skin · cracked · Feb 9, 2001 · N261AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > BOS - FOUND SKIN CRACKED.75 INCH, BETWEEN STATION 787/807 STRINGER 19L. INSTALLED DOUBLER INCORPORATED PREVIOUS PATCH PER SRM 53-30-3 FIG 1. (M)
- [SDR USAASB00293](https://openairdocs.org/sdr/USAASB00293.md): Accessory Unit · faulty · Oct 16, 2000 · N261AU · Boeing 737201 · Landing Gear Position and Warning
  > BDL - FLT 2708 - ON FINAL APPROACH TO BDL FROM MCO, CREW RECEIVED THREE GREEN GEAR DOWN LIGHTS AND THREE RED GEAR UNSAFE LIGHTS WHEN GEAR WAS EXTENDED. CREW RECYCLED GEAR SEVERAL TIMES AND RED LIGHTS EXTINGUISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAI
- [SDR USAA001728](https://openairdocs.org/sdr/USAA001728.md): Stringer · cracked · Oct 12, 2000 · N261AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CRACKED.250 INCHES, BS 360, STRINGER 15L. INSTALLED NEW PART PER SRM 51-10-01. (M)
- [SDR USAA001729](https://openairdocs.org/sdr/USAA001729.md): Wedge · cracked · Oct 12, 2000 · N261AU · Boeing 737201 · Leading Edge Devices
  > CLT - FOUND SLAT TRAILING EDGE WEDGE CRACKED 12.5 INCHES, ENTIRE WIDTH OF THE WEDGE. REMOVED DAMAGED CORE PER EA 68081 AND SRM 51-40-10 AND 51-70-10. (M)
- [SDR USAA001698](https://openairdocs.org/sdr/USAA001698.md): Angle · cracked · Oct 9, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CHORD ANGLE CRACKED 2 INCHES, STATION 695 AT RBL 48. REPAIRED PER EA 68082. (M)
- [SDR USAA001697](https://openairdocs.org/sdr/USAA001697.md): Angle · cracked · Oct 9, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CHORD ANGLE CRACKED 2 INCHES, STATION 695 AT LBL 48. REPAIRED PER EA 68082. (M)
- [SDR USAA001696](https://openairdocs.org/sdr/USAA001696.md): Tie Clip · cracked · Oct 9, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.500 INCH, STRINGER TIE CLIP FS 500B, STRINGER 22L. INSTALLED TIE CLIP PER SRM 51-10-1 AND 51-30-3. (M)
- [SDR USAA001648](https://openairdocs.org/sdr/USAA001648.md): Floorbeam · cracked · Oct 2, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND CHORD ANGLE CRACKED 1 INCH, AT FLOORBEAM CHORD BS 344, RBL 12. REPLACED ANGLE PER SRM 51-10-2. (M)
- [SDR USAA001649](https://openairdocs.org/sdr/USAA001649.md): Floorbeam · cracked · Oct 2, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CHORD CRACKED 1 INCH, AT SEAT TRACK BS 344, WL 208. REPLACED BEAM PER TR 53-10-13. (M)
- [SDR USAA001650](https://openairdocs.org/sdr/USAA001650.md): Attach Angle · cracked · Oct 2, 2000 · N261AU · Boeing 737201 · Fuselage Main, Attach Fittings
  > CLT - FOUND ATTACH ANGLE CRACKED 1 INCH, STATION 350, STRINGER 15L, WL 221. REPLACED ANGLE PER SRM 51-10-01. (M)
- [SDR USAA001651](https://openairdocs.org/sdr/USAA001651.md): Stringer · cracked · Oct 2, 2000 · N261AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CRACKED.75 INCH, STRINGER 16L CRACKED AT FS 787. INSTALLED DOUBLER PER SRM 53-10-3. (M)
- [SDR USAA001631](https://openairdocs.org/sdr/USAA001631.md): Floorbeam · corroded · Sep 29, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 967, RBL 44 - LBL 12. CORROSION LEVEL 1 C 53-107-02. REPAIRED PER T-CAP SPLICE PER SRM 53-10-9. (M)
- [SDR USAA001630](https://openairdocs.org/sdr/USAA001630.md): Floorbeam · corroded · Sep 29, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 947, RBL 50 - LBL 44. REPAIRED T-CAP PER SRM 53-10-09. (M)
- [SDR USAA001629](https://openairdocs.org/sdr/USAA001629.md): Angle · cracked · Sep 29, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND ANGLE CRACKED 1.5 INCH, FORWARD SERVICE DOOR Z-ANGLE STATION 296.5, WL 208. FABRICATED NEW ANGLE PER DWG 65-45807. (M)
- [SDR USAA001628](https://openairdocs.org/sdr/USAA001628.md): Tie Clip · cracked · Sep 29, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 827, STRINGER 9R. REPAIRED PER EO 5393G227. (M)
- [SDR USAA001627](https://openairdocs.org/sdr/USAA001627.md): Tie Clip · cracked · Sep 29, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 663.75, STRINGER 10R. REPAIRED PER EO 5393G227. (M)
- [SDR USAA001626](https://openairdocs.org/sdr/USAA001626.md): Angle · cracked · Sep 29, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND ANGLE CRACKED.25 INCH, AFT LOWER CORNER ANGLE ASSEMBLY THRESHOLD. REPAIRED PER SRM 51-30-02. (M)
- [SDR USAA001613](https://openairdocs.org/sdr/USAA001613.md): Bulkhead · cracked · Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND THE BULKHEAD WEB CRACKED.5 INCH, STATION 178 RBL 6.75, WL 198. ENLARGED CUTOUT OF DAMAGE (3 INCHES BY 5 INCHES) AND INSTALLED DOUBLERS PER SRM 53-10-11 FIG 1. (M)
- [SDR USAA001619](https://openairdocs.org/sdr/USAA001619.md): Tie Clip · cracked · Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CARCKED.25 INCH, AT FS 727B-582. MODIFIED PART INSTALLED PER EO 5393G227. (M)
- [SDR USAA001618](https://openairdocs.org/sdr/USAA001618.md): Tie Clip · cracked · Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED,.572 INCH BS 663-510L. MODIFIED PART INSTALLED PER EO 5393G227. (M)
- [SDR USAA001617](https://openairdocs.org/sdr/USAA001617.md): Tie Clip · cracked · Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRINGER TIE CLIP CRACKED.25, STRINGER 10L B STATION 500A. REPLACED CLIP PER EO 5393G227. (M)
- [SDR USAA001622](https://openairdocs.org/sdr/USAA001622.md): Web · cracked · Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED.25 INCH, AT FORWARD END OF STRINGER 14R AT STATION 277. ROUTED OUT CRACK PER 51-10-1 FIG 1. (M)
- [SDR USAA001621](https://openairdocs.org/sdr/USAA001621.md): Stiffener · cracked · Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND VERTICAL STIFFENER CRACKED 1 INCH, INBOARD FLANGE LBL 5.7 VERT STIFFENER STATION 178 WL 184. INSTALLED 1/2 HARD SS ANGLES PER SRM 53-10-11. (M)
- [SDR USAA001620](https://openairdocs.org/sdr/USAA001620.md): Tie Clip · cracked · Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.5 INCH, STATION 597 STRINGER 9R. MODIFIED PART INSTALLED PER EO 53936227. (M)
- [SDR USAA001616](https://openairdocs.org/sdr/USAA001616.md): Tie Clip · cracked · Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRINGER TIE CLIP CRACKED, FS 727B-S7L. MODIFIED PART INSTALLED PER EO 5393G227. (M)
- [SDR USAA001615](https://openairdocs.org/sdr/USAA001615.md): Tie Clip · cracked · Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.5 INCH, STATION 639 STRINGER 2R. MODIFIED PART INSTALLED PER EO 5393G227. (M)
- [SDR USAA001614](https://openairdocs.org/sdr/USAA001614.md): Splice · cracked · Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRINGER END SPLICE CRACKED.5 INCH, STATION 360 STRINGER 14L. REPLACED SPLICE PER SRM 51-10-01. (M)
- [SDR USAA001610](https://openairdocs.org/sdr/USAA001610.md): Skin · cracked · Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND DOOR CUTOUT CRACKED 3 INCHES, LEFT AFT ENTRY DOOR LOWER FORWARD CORNER. INSTALLED DOUBLER PER SRM 53-30-03 AND EA 68158. (M)
- [SDR USAA001609](https://openairdocs.org/sdr/USAA001609.md): Bulkhead · cracked · Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND AFT NOSE W/W BULKHEAD CRACKED 1.5 INCHES, ACT SUPPORT BEAM WEB STATION 228, WL 185.5, BL 0. INSTALLED FILLER AND DOUBLER PER SRM 51-40-2. (M)
- [SDR USAA001599](https://openairdocs.org/sdr/USAA001599.md): Angle · cracked · Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND VERTICAL ANGLE CRACKED.25 INCH, AFT SIDE STATION 727, BULKHEAD RBL 6.5. REPLACED ANGLE PER SRM 51-10-01 AND EA 68132. (M)
- [SDR USAA001570](https://openairdocs.org/sdr/USAA001570.md): Skin · cracked · Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED.25 INCH, BS 339, STRINGER 17LT. REPAIRED PER DWG 65C27257 AND 65C27297. (M)
- [SDR USAA001569](https://openairdocs.org/sdr/USAA001569.md): Frame · cracked · Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND SIDE CHORD CRACKED 2 INCHES, BS 178, WL 207, LBL 25. INSTALLED REPAIR ANGLE PER SRM 53-10-11 AND EA 68032. (M)
- [SDR USAA001598](https://openairdocs.org/sdr/USAA001598.md): Bulkhead · cracked · Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB CRACKED.5 INCH, STATION 178 BULKHEAD WEB LBL 6.75 WL 201. ENLARGED CUT OUT OF DAMAGE (3 INCHES BY 5 INCHES) AND INSTALLED DOUBLERS. (M)
- [SDR USAA001575](https://openairdocs.org/sdr/USAA001575.md): Floorbeam · corroded · Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 986, RBL 46, LBL 12. CORROSION LEVEL 1, C53-107-02. INSTALLED FABRICATED T-CAP AND SPLICE DOUBLER PER TR 53-60-01 REV A. (M)
- [SDR USAA001574](https://openairdocs.org/sdr/USAA001574.md): Web · cracked · Sep 27, 2000 · N261AU · Boeing 737201 · Wing Miscellaneous Structure
  > CLT - FOUND WEB CRACKED TWO PLACES.25 INCH EACH, 2 INCHES AND 3 INCHES AFT OF BS 706 AT BL 0. INSTALLED FILLER, DOUBLER AND TRIPLER PER TR 57-10-05. (M)
- [SDR USAA001573](https://openairdocs.org/sdr/USAA001573.md): Angle · cracked · Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CHORD ANGLE CRACKED 1 INCH, STATION 663, RBL 25, WL 201.5 ON L/B SIDE. INSTALLED REPAIR ANGLE AND SPLICES PER EA 68031. (M)
- [SDR USAA001572](https://openairdocs.org/sdr/USAA001572.md): Torque Box · cracked · Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, Structure
  > CLT - FOUND TORQUE BOX CRACKED.5 INCH, FS 947 PLUS 1, STRINGER 10L. INSTALLED FILLER AND REPAIR STRAP PER TR 53-30-07A. (M)
- [SDR USAA001571](https://openairdocs.org/sdr/USAA001571.md): Web · cracked · Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED 3 INCHES, IN RADIUS OF NLG ACT BEAM WEB. REPLACED WEB PER SRM 51-10-02. (M)
- [SDR USAA001565](https://openairdocs.org/sdr/USAA001565.md): Skin · cracked · Sep 26, 2000 · N261AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 3 INCHES, BS 962, STRINGER 17 LEFT. INSTALLED DOUBLER PER SRM 53-30-3 FIG 24. (M)
- [SDR USAA001544](https://openairdocs.org/sdr/USAA001544.md): Floorbeam · corroded · Sep 25, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM 2 INCHES BY 10 INCHES, BS 1016, LBL 5 - LBL 15. CORROSION LEVEL 1. REPAIRED T-CAP PER TR 53-60-02. (M)
- [SDR SAA001543](https://openairdocs.org/sdr/SAA001543.md): Tie Clip · cracked · Sep 25, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 827, STRINGER 9RT. REPAIRED PER EO 5393G227. (M)
- [SDR USAA001539](https://openairdocs.org/sdr/USAA001539.md): Bulkhead · cracked · Sep 25, 2000 · N261AU · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND BULKHEAD CRACKED 3 INCHES, STATION 178, LBL 5.7, WL 211-214. INSTALLED DOUBLER PER SRM 53-10-11. (M)
- [SDR USAA001538](https://openairdocs.org/sdr/USAA001538.md): Frame · cracked · Sep 25, 2000 · N261AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND CHORD ANGLE CRACKED 1 INCH, STATION 663, LBL 25, WL 201.5 ON L/B SIDE. INSTALLED DOUBLER PER EA 68031. (M)
- [SDR USAA001507](https://openairdocs.org/sdr/USAA001507.md): Intercostal · cracked · Sep 12, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND INTERCOSTAL CRACKED 2 INCHES, BS 178, WL 195, RBL 24. INSTALLED NEW INTERCOSTAL PER TR 53-10-15. (M)
- [SDR USAA001506](https://openairdocs.org/sdr/USAA001506.md): Intercostal · cracked · Sep 12, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND INTERCOSTAL CRACKED 2 INCHES, BS 178, WL 195, LBL 24. INSTALLED NEW INTERCOSTAL PER TR 53-10-15. (M)
- [SDR USAA001505](https://openairdocs.org/sdr/USAA001505.md): Floorbeam · corroded · Sep 12, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND T-CAP CORRODED 6 PLACES 1 INCH BY 1 INCH EACH, BS 344 LBL 24 TO RBL 24, WL 208. CORROSION LEVEL 1 C53-46-53501C. INSTALLED T-CAP PER TR 53-10-13. (M)
- [SDR USAA001504](https://openairdocs.org/sdr/USAA001504.md): Strap · cracked · Sep 12, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND STABILIZER STRAP CRACKED.5 INCH, BS 328 AT RBL 33. INSTALLED DOUBLER PER SRM 53-10-9 FIG 4. (M)

Next page: https://openairdocs.org/deregistered/N261AU-2002-06-06/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 = 'N261AU' AND deregistration_id = 'N261AU-2002-06-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N261AU-2002-06-06/reports

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