# Service difficulty reports: N260AU, cancelled Aug 16, 2004

A list on [N260AU, cancelled Aug 16, 2004](https://openairdocs.org/deregistered/N260AU-2004-08-16.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 · 93 reports

- [SDR USAASB01242](https://openairdocs.org/sdr/USAASB01242.md): Slide · inoperative · Aug 27, 2001 · N260AU · Boeing 737201 · Cabin Equipment/Furnishings
  > BOS - THE AFT RIGHT SERVICE DOOR EVACUATION SLIDE FAILED TO REMAIN INFLATED DURING TEST. MAINTENANCE REPLACED THE EVACUATION SLIDE. (M)
- [SDR USAASB00208](https://openairdocs.org/sdr/USAASB00208.md): Light · failed · Aug 5, 2000 · N260AU · Boeing 737201 · Emergency Lighting
  > PVD - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB00188](https://openairdocs.org/sdr/USAASB00188.md): Line · leaking · Jul 12, 2000 · N260AU · Boeing 737201 · Hydraulic System, Main
  > MCO - FLT 2670 - UPON APPROACH INTO MCO, AFTER SETTING FLAPS, FLIGHT ENCOUNTERED SYSTEM A HYDRAULIC FLUID LOSS. BOTH A PUMP LOW PRESSURE LIGHTS ILLUMINATED. CREW ACCOMPLISHED ALTERNATE FLAP EXTENSION AND MANUAL GEAR EXTENSION. FLIGHT LANDED WITHOUT FURTHER
- [SDR USAA000292](https://openairdocs.org/sdr/USAA000292.md): Stringer · corroded · Mar 1, 2000 · N260AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND 3 INCH BY 1 INCH OF CORROSION AT BS 980 TO 988, STRINGER 27L. INSTALLED NEW STRINGER PIECE PLU SPLICE PER SRM 53-10-3 FIG 1. CORROSION LEVEL 1. (M)
- [SDR USAA000287](https://openairdocs.org/sdr/USAA000287.md): Bracket · corroded · Feb 29, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - CORROSION LEVEL 1, ANTENNA BRACKET CORRODED BETWEEN BS 500 AND 500B STRINGER 28L AND 28R. INSTALLED NEW PARTS PER SRM 51-10-01. (M)
- [SDR USAA000288](https://openairdocs.org/sdr/USAA000288.md): Frame · cracked · Feb 29, 2000 · N260AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FRAME CRACKED AT BS 663.75 STRINGER 3L. INSTALLED DOUBLER PER SRM 53-10-4 FIG 14. (M)
- [SDR USAA000289](https://openairdocs.org/sdr/USAA000289.md): Frame · cracked · Feb 29, 2000 · N260AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FRAME CRACKED AT BS 663.75, STRINGER 2L. INSTALLED DOUBLER PER SRM 53-10-4 FIG 14. (M)
- [SDR USAA000290](https://openairdocs.org/sdr/USAA000290.md): Frame · cracked · Feb 29, 2000 · N260AU · Boeing 737201 · Fuselage Main, Frame
  > FRAME CRACKED AT 663.75 STRINGER 2R. INSTALLED DOUBLER PER SRM 53-10-4 FIG 14. (M)
- [SDR USAASB00056](https://openairdocs.org/sdr/USAASB00056.md): Packing · failed · Feb 28, 2000 · N260AU · Boeing 737201 · Hydraulic Filter, Main
  > CLT - FLT 7900 - WHILE ON TEST HOP, APPROACHING CLT, THE A HYDRAULIC SYSTEM LIGHT BEGAN FLICKERING. CAPTAIN SHUT DOWN PUMPS AND STARTED GETTING THE B HYDRAULIC SYSTEM LIGHT FLICKERING. CAPTAIN DECLARED AN EMERGENCY AND LANDED AT CLT WITHOUT FURTHER INCIDENT.
- [SDR USAA000275](https://openairdocs.org/sdr/USAA000275.md): Floorbeam · cracked · Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - FOUND CRACK IN T-CAP, 2 INCHES, BL 0 AT STATION 663. INSTALLED REPAIR STRAPS AND ANGLES PER TR 57-10-04. (M)
- [SDR USAA000276](https://openairdocs.org/sdr/USAA000276.md): Web · cracked · Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND 4 CRACKS,.5 INCH, LBL 25, STATION 710 TO 714. INSTALLED DOUBLER PER EA 66602. (M)
- [SDR USAA000277](https://openairdocs.org/sdr/USAA000277.md): Tie Clip · cracked · Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CRACK TIE CLIP.25 INCH, STATION 578, STRINGER 5L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)
- [SDR USAA000278](https://openairdocs.org/sdr/USAA000278.md): Frame · cracked · Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND 2 INCH CHORD ANGLE CRACK, STATION 1138, STRINGER 5AL. INSTALLED CHORD SECTION AND DOUBLER PER SRM 51-40-3 FIG 1. (M)
- [SDR USAA000279](https://openairdocs.org/sdr/USAA000279.md): Stringer · corroded · Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND CORROSION LEVEL 1, 6 INCHES, STATION 1006 STRINGER 24L. INSTALLED NEW PART PER SRM 51-10-1 FIG 1. (M)
- [SDR USAA000280](https://openairdocs.org/sdr/USAA000280.md): Fitting · corroded · Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CORROSION LEVEL 1,.5 INCH, INBOARD STAB FITTING ON GEAR BEAM INSIDE FLANGES. INSTALLED NEW PART PER SRM 20-10-19. (M)
- [SDR USAA000281](https://openairdocs.org/sdr/USAA000281.md): Frame · corroded · Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND CORROSION LEVEL 1, 1 INCH BY 2 INCH, STATION 500B ABOVE STRINGER 26R UNDER TRANSITION PANEL AND FRAME. INSTALLED REPAIR DOUBLER PER SRM 53-10-4. (M)
- [SDR USAA000260](https://openairdocs.org/sdr/USAA000260.md): Bulkhead · cracked · Feb 24, 2000 · N260AU · Boeing 737201 · Fuselage Main, Bulkhead
  > BULKHEAD HAS A.25 INCH CRACK AT BS 663, LBL 25. SPLICED IN DOUBLER PER EA 66610 AND SB 737-53-1184. (M)
- [SDR USAA000256](https://openairdocs.org/sdr/USAA000256.md): Web · cracked · Feb 22, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED 1 INCH, BS 950, STRINGER 10R. INSTALLED FILLER AND DOUBLER PER TR 53-30-07. (M)
- [SDR USAA000229](https://openairdocs.org/sdr/USAA000229.md): Skin · cracked · Feb 22, 2000 · N260AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - SKIN AT BS 947 BETWEEN STRINGER 11R AND 12R HAS A.125 INCH CRACK. INSTALLED DOUBLER PER SRM 53-30-3. (M)
- [SDR USAA000230](https://openairdocs.org/sdr/USAA000230.md): Stringer Clip · cracked · Feb 22, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - STRINGER CLIP CRACKED AT BS 727B STRINGER 7L. REPLACED TIE CLIP PER SRM 51-10-1. (M)
- [SDR USAA000231](https://openairdocs.org/sdr/USAA000231.md): Channel · cracked · Feb 22, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - CHANNEL HAS A 2 INCH CRACK AT BS 520 RBL 25 WL 206. INSTALLED PIVOT LINK PER SB 737-53-1120. (M)
- [SDR USAA000244](https://openairdocs.org/sdr/USAA000244.md): Angle · cracked · Feb 22, 2000 · N260AU · Boeing 737201 · Horizontal Stabilizer Structure
  > CLT - ANGLE CRACKED AT STATION 1138 ON HORIZ STABILIZER. REPAIRED PER SRM 51-40-3 FIG 1. (M)
- [SDR USAA000206](https://openairdocs.org/sdr/USAA000206.md): Stiffener · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - FOUND CRACK IN STIFFENER 1.75 INCHES, STATION 178, LBL 5.5 LOWER AFT SIDE VERTICAL STIFFENER. INSTALLED DOUBLER PER TR 53-10-17 AND SRM 20-40-04. (M)
- [SDR USAA0209](https://openairdocs.org/sdr/USAA0209.md): Stringer Clip · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 706, STRINGER 10L TIE CLIP. INSTALLED CLIP PER EO5393G227. (M)
- [SDR USAA0210](https://openairdocs.org/sdr/USAA0210.md): Web · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.750 INCH LONG CRACK AT BS 707 TO 710, RBL 25 WEB. INSTALLED DOUBLER PER EA 66602. (M)
- [SDR USAA0211](https://openairdocs.org/sdr/USAA0211.md): Stringer Clip · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.375 INCH CRACK AT STATION 616, STRINGER 5R CLIP. REPAIRED PER EO 5393G227. (M)
- [SDR USAA0212](https://openairdocs.org/sdr/USAA0212.md): Stringer Clip · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK AT STATION 727B, STRINGER 2L TIE CLIP. REPLACED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA0213](https://openairdocs.org/sdr/USAA0213.md): Stringer Clip · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.5 INCH CRACK AT STATION 747, STRINGER 4R TIE CLIP. REPLACED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA0214](https://openairdocs.org/sdr/USAA0214.md): Stringer Clip · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.375 INCH CRACK AT STATION 807, STRINGER 11R TIE CLIP. REPLACED TIE CLIP PER EO 5393G227. (M)
- [SDR USAA0215](https://openairdocs.org/sdr/USAA0215.md): Stringer Clip · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.375 INCH CRACK AT STATION 578, STRINGER 5L TIE CLIP. REPAIRED PER EO 5393G227. (M)
- [SDR USAA0216](https://openairdocs.org/sdr/USAA0216.md): Stringer Clip · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.5 INCH CRACK AT STATION 639, STRINGER 4L TIE CLIP. REPAIRED PER EO 5393G227. (M)
- [SDR USAA0217](https://openairdocs.org/sdr/USAA0217.md): Stringer Clip · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.375 INCH CRACK AT STATION 578, STRINGER 5L TIE CLIP. REPAIRED PER EO 5393G227. (M)
- [SDR USAA0218](https://openairdocs.org/sdr/USAA0218.md): Floorbeam · corroded · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT STATION 344, LBL 9 FLOORBEAM. CORROSION LEVEL 1. INSTALLED FILLER AND REPAIR ANGLE PER SRM 53-10-9. (M)
- [SDR USAA0219](https://openairdocs.org/sdr/USAA0219.md): Floorbeam · corroded · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND SCREW HOLES STATION 947.5 FROM LBL 17 - RBL 17 FLOORBEAM. CORROSION LEVEL 1. INSTALLED NEW T-CAP PER SRM 53-10-9, TR 53-10-05A, AND EA 66592. (M)
- [SDR USAA0220](https://openairdocs.org/sdr/USAA0220.md): Floorbeam · corroded · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION STATION 312, LBL 11 AND BL 0 FLOORBEAM T-CAP. CORROSION LEVEL 2. REPLACED T-CAP PER SRM 53-10-0 FIG 5 AND IAW 51-10-9 FIG 5. (M)
- [SDR USAA0221](https://openairdocs.org/sdr/USAA0221.md): Frame · corroded · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Main, Frame
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION STATION 500B ABOVE STRINGER 26R FRAME. CORROSION LEVEL 1. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-4. (M)
- [SDR USAA0222](https://openairdocs.org/sdr/USAA0222.md): Beam · corroded · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION BS 234, WL 190, RBL 6 ON NG TRAVERSE BEAM. CORROSION LEVEL 2. TASK NR C53-202-01. REPLACED PART PER SRM 51-10-1. (M)
- [SDR USAA0223](https://openairdocs.org/sdr/USAA0223.md): Stringer · corroded · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION STATION 1006, STRINGER 24R. CORROSION LEVEL 2. TASK NR C53-202-01. REPLACED PART PER SRM 51-10-1. (M)
- [SDR USAA0224](https://openairdocs.org/sdr/USAA0224.md): Angle · corroded · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 40 INCH AREA OF CORROSION STATION 957-1006, RBL 54 FLOOR LEVEL Z-ANGLE. CORROSION LEVEL 1. TASK NR C553-107-02. REPLACED PART PER BOEING DWG 65-45855 AND SRM 51-10-1. (M)
- [SDR USAA0225](https://openairdocs.org/sdr/USAA0225.md): Floorbeam · corroded · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 46 INCH AREA OF CORROSION FLOORBEAM 986.5 BETWEEN BBL 0 - RBL 46. CORROSION LEVEL 1. TASK NR C53-107-02. REPLACED T-CAP PER TR 53-60-01 REV A. (M)
- [SDR USAA0226](https://openairdocs.org/sdr/USAA0226.md): Floorbeam · corroded · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION FLOORBEAM 986.5 LBL 17. CORROSION LEVEL 1. TASK NR C53-107-02. REPLACED T-CAP PER TR 53-60-01 REV A. (M)
- [SDR USAA0227](https://openairdocs.org/sdr/USAA0227.md): Floorbeam · corroded · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND PATCHES OF CORROSION WITHIN 34 INCHES STATION 986.5 BETWEEN LBL 17 AND RBL 17 FLOORBEAM. CORROSION LEVEL 1. TASK NR C53-107-02. REPLACED T-CAP PER TR 53-60-01 REV A. (M)
- [SDR USAA0228](https://openairdocs.org/sdr/USAA0228.md): Angle · corroded · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 24 INCH AREA OF CORROSION LEFT AFT ENTRY Z-ANGLE. CORROSION LEVEL 1. TASK NR C53-107-02. FAB REPAIR DOUBLERS AND FILLER PER SRM 51-40-03 FIG 1. (M)
- [SDR USAA0208](https://openairdocs.org/sdr/USAA0208.md): Stringer Clip · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 727B, STR 5L TIE CLIP. REMOVED AND REPLACED CLIP PER EO 5393G227. (M)
- [SDR USAA000200](https://openairdocs.org/sdr/USAA000200.md): Skin · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND LOWER FORWARD CORNER OF AFT SERVICE DOOR CUTOUT SKIN HAS A 2 INCH CRACK. INSTALLED REPAIR PLATES PER SRM 53-30-3. (M)
- [SDR USAA000201](https://openairdocs.org/sdr/USAA000201.md): Stringer Clip · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - STRINGER CLIP HAS A.25 INCH CRACK AT BS 727B STRINGER 7L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-00. (M)
- [SDR USAA000202](https://openairdocs.org/sdr/USAA000202.md): Stringer · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - STRINGER 18A HAS A 1.5 INCH CRACK AT BS 727. REPAIRED PER SRM 51-10-01. (M)
- [SDR USAA0203](https://openairdocs.org/sdr/USAA0203.md): Gusset · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN RADIUS OF GUSSET AT BS 259, BBL 0, WL 193 TOP OF NG W/W. REPLACED GUSSET PER SRM 51-10-01. (M)
- [SDR USAA0204](https://openairdocs.org/sdr/USAA0204.md): Stringer Clip · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK AT STATION 727A STRINGER 5L TIE CLIP. REMOVED AND REPLACED CLIP PER EO 5393G227. (M)
- [SDR USAA0205](https://openairdocs.org/sdr/USAA0205.md): Floorbeam · cracked · Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SIX.5 INCH CRACKS BL 0 LONGITUDINAL FLOORBEAM WEB LOWER FASTENERS STATION 707 TO 715. REPAIRED NEW SECTION PER TR 57-10-05. (M)

Next page: https://openairdocs.org/deregistered/N260AU-2004-08-16/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 = 'N260AU' AND deregistration_id = 'N260AU-2004-08-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N260AU-2004-08-16/reports

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