# Service difficulty reports: N560AU, cancelled Mar 8, 2007

A list on [N560AU, cancelled Mar 8, 2007](https://openairdocs.org/deregistered/N560AU-2007-03-08.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 · 70 reports

- [SDR USAA050589](https://openairdocs.org/sdr/USAA050589.md): Stiffener · cracked · May 3, 2005 · N560AU · Boeing 737301 · Nacelle/Pylon Miscellaneous Structure
  > CLT - FOUND STIFFENER CRACKED.4 INCH IN VERTICAL STIFFENER AT AFT SIDE OF PYLON LOWER SIDE OF WING. FABRICATED REPAIR PART AND INSTALLED SRM 51-10-02. (M)
- [SDR USAASB04010](https://openairdocs.org/sdr/USAASB04010.md): Charger · inoperative · Jan 21, 2004 · N560AU · Boeing 737301 · Emergency Lighting
  > PHL - MAINTENANCE REPORTED THE RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M)
- [SDR USAASB03221](https://openairdocs.org/sdr/USAASB03221.md): Fuse · inoperative · Dec 24, 2003 · N560AU · Boeing 737301 · Emergency Lighting
  > DCA- MAINTENANCE REPORTED THE EMERGENCY ESCAPE PATH SEAT MOUNTED LIGHTS ON SEAT ROWS 6, 7, 8, 9 AND 11 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BLOWN FUSE IN POWER SUPPLY ABOVE SEAT ROW 10 CEILING. OPERAITONAL CHECK GOOD. (M)
- [SDR USAA030194](https://openairdocs.org/sdr/USAA030194.md): Skin · cracked · Sep 10, 2003 · N560AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED 2.250 INCH, JUST BELOW S23R AT FS 730. INSTALLED DOUBLER/TRIPLER PER SRM 53-00-01, FIG 229, PROCEDURE V, DETAIL IV. (M)
- [SDR USAA030193](https://openairdocs.org/sdr/USAA030193.md): Skin · cracked · Sep 10, 2003 · N560AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED.750 INCH, FUSELAGE JUST ABOVE S24R FORWARD OF FS 727E. INSTALLED DOUBLR/TRIPLER PER SRM 53-00-01, FIG 229, PROCEDURE V, DETAIL IV. (M)
- [SDR USAA030187](https://openairdocs.org/sdr/USAA030187.md): Skin · cracked · Sep 8, 2003 · N560AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 2.5 INCHES, FUSELAGE SKIN JUST BELOW S19R AT FS 760. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)
- [SDR USAA030117](https://openairdocs.org/sdr/USAA030117.md): Skin · damaged · Jul 17, 2003 · N560AU · Boeing 737301 · Rudder, Plate/Skin
  > PIT - FOUND RUDDER WITH SKIN DAMAGE, 24 INCH OVAL ONE LAYER DAMAGE, LEFT SIDE OF RUDDER 107 INCH FROM BOTTOM 12 INCHES FROM TRAILING EDGE. WET LAY UP REPAIR PER SRM 51-70-17 AND EA 76292. (M)
- [SDR USAA030119](https://openairdocs.org/sdr/USAA030119.md): Floorbeam · cracked · Jul 17, 2003 · N560AU · Boeing 737301 · Fuselage Main, Floor Beam
  > PIT - FOUND FLOORBEAM CRACKED APPROX 1 INCH, BS 328 RBL 10.0. DOUBLER INSTALLED PER EA 76205. (M)
- [SDR USAA030118](https://openairdocs.org/sdr/USAA030118.md): Angle · cracked · Jul 11, 2003 · N560AU · Boeing 737301 · Wing Miscellaneous Structure
  > PIT - FOUND ANGLE HAS.375 INCH CRACK, NR 5 LE SLAT ACTUATOR ATTACH FITTING ANGLE. FABRICATED REPAIR ANGLE FROM 17-7 PH PER EA 76202. (M)
- [SDR USAA030116](https://openairdocs.org/sdr/USAA030116.md): Support Fitting · cracked · Jul 8, 2003 · N560AU · Boeing 737301 · Wing, Landing Gear Attach Fittings
  > PIT - FOUND MLG BEAM AFT SUPPORT FITTING HAS APPROX.5 INCH CRACK, UPPER OUTBOARD HOLD ON MLG BEAM AFT SUPPORT FITTING, RSS 224.14. OVERSIZED HOLE AND INSTALLED STRAP ACROSS UPPER REAR SPAR CHORD PER EA 76210. (M)
- [SDR USAA030089](https://openairdocs.org/sdr/USAA030089.md): Floorbeam · corroded · May 22, 2003 · N560AU · Boeing 737301 · Fuselage Main, Floor Beam
  > PIT - FOUND FLOORBEAM CORRODED APPROX 6 INCHES BY 1 INCH, FLOORBEAM BETWEEN STATION 344 AND 360 10 INCHES LBBL. MANUFACTURED AND INSTALLED T-CAP PER EA 76223 SRM CHAPTER 51. (M)
- [SDR USAA030060](https://openairdocs.org/sdr/USAA030060.md): Beltframe · cracked · May 22, 2003 · N560AU · Boeing 737301 · Fuselage Main, Structure
  > PIT - FOUND BELTFRAME CRACKED.1875 INCH, BELTFRAME CRACKED AT STATION 303.9 STRINGER 13L. DOUBLER INSTALLED PER EA 76233. (M)
- [SDR USAA030079](https://openairdocs.org/sdr/USAA030079.md): Angle · cracked · May 22, 2003 · N560AU · Boeing 737301 · Rudder Structure
  > PIT - FOUND RUDDER CRACKED.5 INCH, RUDDER LOWER FORWARD SEAL PLATE ANGLE. INSTALLED WET LAYUP REPAIR PER EA 76293, SRM 51-70-17 AND 51-60-00. (M)
- [SDR USAA030050](https://openairdocs.org/sdr/USAA030050.md): Skin · corroded · May 6, 2003 · N560AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND SKIN CORRODED 1 INCH AREA AND.5 INCH AREA, AROUND FASTENER, BL 0 STATION 1016 RADIAL STIFFENER. CORROSION LEVEL 1. REMOVED DAMAGED END OF STIFFENER, INSTALLED NEW SECTION AND SPLICE PER BOEING DRAWING 65C28106. (M)
- [SDR USAA030083](https://openairdocs.org/sdr/USAA030083.md): Bear Strap · cracked · May 5, 2003 · N560AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND BEAR STRAP CRACKED.1875 INCH, MED BEAR STRAP BS 304 UPPER AND LOEWR HINGE CUTOUT. INSTALLED DOUBLERS PER EA 76233. (M)
- [SDR USAA030147](https://openairdocs.org/sdr/USAA030147.md): Nut Plate · corroded · May 1, 2003 · N560AU · Boeing 737301 · Fasteners
  > PIT - FOUND NUTPLATE CORRODED.75 INCH BY 1 INCH AREA, FS 727A-727B 21 LT. INSTALLED DOUBLER PER SRM 53-00-3. CORROSION LEVEL 1, TASK NR C53-107-01. (M)
- [SDR USAA030096](https://openairdocs.org/sdr/USAA030096.md): Beltframe · cracked · Apr 30, 2003 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > PIT - FOUND BELTFRAME CRACKED.75 INCH LONG, AT RIVET FOR LOWER OVERHEAD BIN, BETWEEN S8L AND S9L, FS 440. PER TYPICAL REPAIR PER 53-10-20A. (M)
- [SDR USAA030082](https://openairdocs.org/sdr/USAA030082.md): Frame · cracked · Apr 27, 2003 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.1875 INCH, SMALL CRACK IN FRAME AT RIVET STATION 360 LEFT, BETWEEN 58-59. REMOVED DAMAGED AND INSTALLED DOUBLERS PER TR 53-10-20A. (M)
- [SDR USAA030059](https://openairdocs.org/sdr/USAA030059.md): Fitting · cracked · Apr 25, 2003 · N560AU · Boeing 737301 · Horizontal Stabilizer Structure
  > FOUND FITTING CRACKED 1.5 INCHES LONG, FITTING IN HORIZONTAL STABILIZER CENTER SECTION OF RIGHT THRUST BEAM. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)
- [SDR USAA020177](https://openairdocs.org/sdr/USAA020177.md): Skin · cracked · Apr 16, 2002 · N560AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN AND WEB PLATE CRACKED.625 INCH, BS 360-380, AT BL 10. SKIN DOUBLER ADDED PER TYPICAL REPAIR 53-30-07 AND EA 73800. (M)
- [SDR USAASB01346](https://openairdocs.org/sdr/USAASB01346.md): Light · inoperative · Dec 20, 2001 · N560AU · Boeing 737301 · Emergency Lighting
  > CLT - PILOT REPORTED THE FLOOR PATH EMERGENCY LIGHTING, AT SEAT ROW 13C, IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 13C. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB99278](https://openairdocs.org/sdr/USAASB99278.md): Indicator · failed · Nov 25, 1999 · N560AU · Boeing 737301 · Trailing Flap Position Indicating System
  > CLT - FLT 2202 - DURING CLIMB-OUT FROM CLT, THE FLAPS FAILED TO RETRACT AS FLAP INDICATOR FAILED AT 5 DEGREES FLAPS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FLAP PO
- [SDR USAA991218](https://openairdocs.org/sdr/USAA991218.md): Antenna Base · corroded · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 12 INCH AREA OF CORROSION BETWEEN STRINGER 28 LT AND RT AFT OF STATION 500 ANTENNA BASE, CORROSION LEVEL 2. REPLACED ANTENNA BASE PER SRM 51-10-02. (M)
- [SDR USAA991215](https://openairdocs.org/sdr/USAA991215.md): Shear Tie · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 420 STRINGER 4 LEFT SHEAR TIE. REMOVED AND REPLACED PER SRM 51-10-2. (M)
- [SDR USAA991214](https://openairdocs.org/sdr/USAA991214.md): Frame · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 500 RIGHT STRINGER 15 SHEAR TIE DAMAGE AT STRINGER AND FRAME. REMOVED AND REPLACED PER SRM 51-10-2. (M)
- [SDR USAA991213](https://openairdocs.org/sdr/USAA991213.md): Bulkhead · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - DURING Q-2 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK 178 BULKHEAD 5 INCH BELOW FLOOR LEVEL AT STIFFENER NR 2 WEB. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M)
- [SDR USAA991212](https://openairdocs.org/sdr/USAA991212.md): Bulkhead · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - DURING Q-2 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK 178 BULKHEAD 5 INCH BELOW FLOOR LEVEL AT STIFFENER NR 3 WEB. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M)
- [SDR USAA991211](https://openairdocs.org/sdr/USAA991211.md): Skin · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Nacelle/Pylon, Plate/Skin
  > CLT - DURIGN Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK ON NR 2 ENGINE PYLON AT ACCESS PANEL NR 5824R UPPER FORWARD CORNER SKIN. INSTALLED DOUBLER PER EA 65982 AND TR 54-50-04D. (M)
- [SDR USAA991210](https://openairdocs.org/sdr/USAA991210.md): Angle · corroded · Nov 11, 1999 · N560AU · Boeing 737301 · Passenger/Crew Doors
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 10 INCH AREA OF CORROSION AT AFT ENTRY DOOR FLOOR Z-ANGLE, CORROSION LEVEL 1. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-02. (M)
- [SDR USAA991208](https://openairdocs.org/sdr/USAA991208.md): T-Cap · corroded · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND TEN 1 INCH BY 1 INCH AREAS OF CORROSION ON UPPER CAP OF T-CAP STATION 967, CORROSION LEVEL 2. REPLACED T-CAP PER TR 53-10-05. (M)
- [SDR USAA991207](https://openairdocs.org/sdr/USAA991207.md): Angle · corroded · Nov 11, 1999 · N560AU · Boeing 737301 · Passenger/Crew Doors
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AT AFT ENTRY DOOR Z-ANGLE (CHANNEL), CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPLACED AFT ENTRY DOOR Z-ANGLE PER SRM 51-10-02. (M)
- [SDR USAA991206](https://openairdocs.org/sdr/USAA991206.md): Angle · corroded · Nov 11, 1999 · N560AU · Boeing 737301 · Service Doors
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 20 INCH AREA OF CORROSION AT RT AFT SERVICE DOOR Z-ANGLE (FLOOR), CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPLACED Z-ANGLE PER SRM 51-10-02. (M)
- [SDR USAA991205](https://openairdocs.org/sdr/USAA991205.md): Seat Track · corroded · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage, Seat/Cargo Attach Fittings
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION AT BS 727B-947 SEAT TRACK, CORROSION LEVEL 2. INSTALLED SEAT TRACK PER SRM 53-00-52. (M)
- [SDR USAA991204](https://openairdocs.org/sdr/USAA991204.md): Floorbeam · corroded · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH MULTIPLE AREA OF CORROSION AT BS 986.5, RBL 44 - LBL 45, FLOORBEAM T-CAP. CORROSION LEVEL 2. REPLACED FLOORBEAM T-CAP PER TR 53-60-01 AND SRM 53-00-51 FIG 202. (M)
- [SDR USAA991198](https://openairdocs.org/sdr/USAA991198.md): Frame · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK AT BS 908 STRINGER 9L BELT FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND SRM 53-00-07. (M)
- [SDR USAA991197](https://openairdocs.org/sdr/USAA991197.md): Frame · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK AT BS 727D STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND SRM 53-00-07. (M)
- [SDR USAA991196](https://openairdocs.org/sdr/USAA991196.md): Frame · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK AT BS 867 STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)
- [SDR USAA991195](https://openairdocs.org/sdr/USAA991195.md): Frame · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK AT RIVET BS 827 STRINGER 9L BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)
- [SDR USAA991194](https://openairdocs.org/sdr/USAA991194.md): Frame · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.2 5INCH CRACK AT BS 727D STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)
- [SDR USAA991193](https://openairdocs.org/sdr/USAA991193.md): Tie Clip · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK AT BS 663 STRINGER 10R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA991192](https://openairdocs.org/sdr/USAA991192.md): Frame · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK AT BS 480 BETWEEN STRINGER 8 AND 9L FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 65950. (M)
- [SDR USAA991191](https://openairdocs.org/sdr/USAA991191.md): Frame · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 727 STRINGER 14L OUTER CHORD ANGLE. REPAIRED DOUBLER AND TRIPLER PER EA 65952. (M)
- [SDR USAA991190](https://openairdocs.org/sdr/USAA991190.md): Frame · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.0625 INCH CRACK IN FUSE FRAME AT FASTENER HOLE BS 480 BETWEEN STRINGER 8 AND 9R. INSTALLED DOUBLER PER TR 53-10-14 AND EA 65950. (M)
- [SDR USAA991189](https://openairdocs.org/sdr/USAA991189.md): Bulkhead · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.250 INCH CRACKS IN 2 PLACES STATION 178 WEB A AND WEB B, LBL 1 AND RBL 1 SKIN. INSTALLED DOUBLER PER SRM 53-10-08. (M)
- [SDR USAA991188](https://openairdocs.org/sdr/USAA991188.md): Skin · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH CRACKS AT BS 663, LBL 32 CEILING PRESSURE DECK. INSTALLED DOUBLER PER TR 53-60-04 AND SRM 53-60-51. (M)
- [SDR USAA991187](https://openairdocs.org/sdr/USAA991187.md): Skin · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT RIGHT HORIZONTAL STABILIZER LOWER SURFACE STATION 111-166 SKIN. INSTALLED DOUBLER AND FILLER PER SRM 55-10-01 AND TR 55-10-07A. (M)
- [SDR USAA991186](https://openairdocs.org/sdr/USAA991186.md): Frame · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.5 INCH CRACK THROUGH RIVET HOLE BS 847, STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA991185](https://openairdocs.org/sdr/USAA991185.md): Tie Clip · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND.250 INCH CRACK AT BS 727B STRINGER 4L TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA991184](https://openairdocs.org/sdr/USAA991184.md): Frame · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK AT RIVET BS 807 STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)
- [SDR USAA991183](https://openairdocs.org/sdr/USAA991183.md): Frame · cracked · Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK AT RIVET BS 887 STRINGER 91 BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)

Next page: https://openairdocs.org/deregistered/N560AU-2007-03-08/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 = 'N560AU' AND deregistration_id = 'N560AU-2007-03-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N560AU-2007-03-08/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.