# Service difficulty reports: N520AU, cancelled Nov 30, 2007

A list on [N520AU, cancelled Nov 30, 2007](https://openairdocs.org/deregistered/N520AU-2007-11-30.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 USAA061166](https://openairdocs.org/sdr/USAA061166.md): Angle · cracked · Sep 13, 2006 · N520AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND ANGLE CRACKED, STA 294 STR 12L. REMOVED DAMAGED PARTS AND INSTALLED FABRICATED PARTS IAW 65-17664, DEFECT SIZE: 1".
- [SDR SB05101](https://openairdocs.org/sdr/SB05101.md): Warning Light · false indication · Aug 29, 2005 · N520AU · Boeing 7373B7 · Landing Gear Position and Warning
  > CLT - UPON LOWERING LANDING GEAR, CREW RECEIVED A GEAR INDICATION OF 3 GREEN AND 3 RED. CREW ACCOMPLISHED A GO-AROUND, CYCLED THE GEAR AND RECEIVED A NORMAL GEAR INDICATION OF 3 GREEN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE JACKED AIRCRAFT AND
- [SDR SB05097](https://openairdocs.org/sdr/SB05097.md): Charger · inoperative · Aug 23, 2005 · N520AU · Boeing 7373B7 · Emergency Lighting
  > MAINTENANCE REPORTED THE BATTERY CHARGER FOR THE AFT ENTRY DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD.
- [SDR SB05083](https://openairdocs.org/sdr/SB05083.md): Battery Pack · discharged · Jul 21, 2005 · N520AU · Boeing 7373B7 · Emergency Lighting
  > PVD MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT OVER THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.
- [SDR USAA050309](https://openairdocs.org/sdr/USAA050309.md): Skin · chafed · Feb 18, 2005 · N520AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CHAFED.013 INCH BY.011 INCH DEEP BY 20 INCHES LONG, BS 867-887 LT/RT SIDE OF SKIN UNDER DORSAL FIN. CUT AREA OUT, INSTALLED FILLER, DOUBLER AND TRIPLER AND CHAFED STRAPS PER SRM 53-60-01 FIG 201 PAGE 241. (M)
- [SDR USAA050295](https://openairdocs.org/sdr/USAA050295.md): Stringer · cracked · Feb 18, 2005 · N520AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND STRINGER CRACKED 3 INCHES, BS 1138 S5A LEFT. TRIM OUT DAMAGE AND SPLICE IN NEW SECTION OF STRINGER PER TYPICAL REPAIR 53-80-04. (M)
- [SDR USAA050310](https://openairdocs.org/sdr/USAA050310.md): Support Angle · cracked · Feb 17, 2005 · N520AU · Boeing 7373B7 · Wing Miscellaneous Structure
  > PIT - FOUND SUPPORT ANGLE CRACKED 1 INCH, TRAILING EDGE OF SUPPORT PANEL, RT WING JUST ABOVE INBOARD EDGE OF NR 5 FLAP. FABRICATED AND INSTALLED NEW SUPPORT ANGLE PER BOEING DWG 69-47542 AND SRM 57-51-02. (M)
- [SDR USAA050314](https://openairdocs.org/sdr/USAA050314.md): Floor Support · corroded · Feb 16, 2005 · N520AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH AREA, FLOOR SUPPORT BEAM S-26R BS 787-867. CORROSION LEVEL 1, TASK C53-208-01. REMOVED AND REPLACED FLOOR SUPPORT BEAM WITH FABRICATED BEAM PER SRM 51-40-02. (M)
- [SDR USAA050311](https://openairdocs.org/sdr/USAA050311.md): Channel · cracked · Feb 16, 2005 · N520AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND U-CHANNEL WITH 1 INCH CRACK, BS 747-767. FABRICATED AND INSTALLED NEW U-CHANNEL SUPPORT. (M)
- [SDR USAA050296](https://openairdocs.org/sdr/USAA050296.md): Skin · cracked · Feb 13, 2005 · N520AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 1.5 INCH, FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER. INSTALLED DOUBLER PER SRM 53-10-01. (M)
- [SDR USAA050297](https://openairdocs.org/sdr/USAA050297.md): Support Angle · corroded · Feb 13, 2005 · N520AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND SUPPORT ANGLE CORRODED APPROX 24 INCHES, FORWARD SERVICE DOOR FLOOR THRESHOLD SUPPORT ANGLE. REPLACED SUPPORT PER SRM 53-10-15. (M)
- [SDR USAA050316](https://openairdocs.org/sdr/USAA050316.md): Skin · delaminated · Feb 11, 2005 · N520AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND EXT COMPOSITE SURFACE DELAMINATED 4 INCHES LONG BY.0625 INCHE WIDE SINGLE LAYER DAMAGE, RUDDER LEFT SIDE 38 INCHES FROM BOTTOM, 13.5 INCHES FROM T/E. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER SRM 51-70-17 AND EA 7
- [SDR USAA050315](https://openairdocs.org/sdr/USAA050315.md): Skin Panel · delaminated · Feb 11, 2005 · N520AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND COMPOSITE SKIN PANEL DELAMINATED.5 INCH BY.0625 INCH SINGLE LAYER DAMAGE, LT SIDE RUDDER 57 INCHES FROM BOTTOM, 34 INCHES FROM T/E. INSTALLED REPAIR PLYS PER SRM 51-70-17 AND EA 79999. (M)
- [SDR USAA050317](https://openairdocs.org/sdr/USAA050317.md): Skin · delaminated · Feb 11, 2005 · N520AU · Boeing 7373B7 · Rudder, Plate/Skin
  > FOUND EXT COMPOSITE SURF DELAMINATED.5 INCH LONG BY.0625 INCH WIDE SINGLE LAYER DAMAGE, RUDDER LEFT SIDE 66 INCHES FROM BOTTOM, 14 INCHES FROM T/E. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER SRM 51-70-17, EA 79999. (M)
- [SDR USAA050320](https://openairdocs.org/sdr/USAA050320.md): Skin · delaminated · Feb 11, 2005 · N520AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND EXT COMPOSITE SURF WITH 1 INCH SINGLE LAYER DAMAGE DELAMINATION, RUDDER RT SIDE 41 INCHES FROM BOTTOM, 8 INCH FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER BOEING SRM 51-70-17, EA 79999. (M)
- [SDR USAA050321](https://openairdocs.org/sdr/USAA050321.md): Skin · delaminated · Feb 11, 2005 · N520AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND EXIT COMPOSITE SURF, 2 INCHES LONG BY.125 INCH WIDE SINGLE LAYER DAMAGE, RUDDER RT SIDE 57 INCH FROM BOTTOM, 10 INCH FROM T/E. INSTALLED REPAIR PLYS, SEALED, REFINISHED PER SRM 51-70-17, EA 79999. (M)
- [SDR USAA050322](https://openairdocs.org/sdr/USAA050322.md): Skin · delaminated · Feb 11, 2005 · N520AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND EXT COMPOSITE SURF 4 INCH LONG BY.125 INCH SINGLE LAYER DAMAGE, RUDDER RT SIDE 64 INCHES FROM BOTTOM 34 INCHES FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER BOEING SRM 51-70-17, EA 79999. (M)
- [SDR USAA050323](https://openairdocs.org/sdr/USAA050323.md): Skin · delaminated · Feb 11, 2005 · N520AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND EXT COMPOSITE SURF WITH DELAMINATION 5 INCHES LONG BY.125 INCH WIDE SINGLE LAYER DAMAGE, RUDDER RT IDE 114 INCH FROM BOTTOM 7 INCH FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER SRM 51-70-17, EA 79999. (M)
- [SDR USAA050313](https://openairdocs.org/sdr/USAA050313.md): Attach Fitting · corroded · Feb 11, 2005 · N520AU · Boeing 7373B7 · Wing, Attach Fittings
  > PIT - FOUND ATTACH RING CORRODED 1 INCH BY 20 INCH AREA, ACCESS PANEL NR 7405. DEFECTIVE PART REPLACED WITH IDENT PART PER AMM 57-00-00. (M)
- [SDR USAA050318](https://openairdocs.org/sdr/USAA050318.md): Skin Panel · delaminated · Feb 11, 2005 · N520AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND COMPOSITE SKIN PANEL DELAMINATED.1875 INCH DIAMETER SINGER LAYER DAMAGE, RUDDER LT SIDE 70 INCHES FROM BOTTOM, 9 INCHES FROM T/E. INSTALLED REPAIR PLYS PER SRM 51-70-17, EA 79999. (M)
- [SDR USAA050319](https://openairdocs.org/sdr/USAA050319.md): Skin Panel · delaminated · Feb 11, 2005 · N520AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND COMPOSITE SKIN PANEL WITH DELAMINATION 3 INCH BY.0625 INCH SINGLE LAYER DAMAGE, 165 INCHES FROM BOTTOM, 13 INCHES FROM T/E RUDDER LT SIDE. INSTALLED REPAIR PLYS PER SRM 51-70-17, EA 79999. (M)
- [SDR USAA050298](https://openairdocs.org/sdr/USAA050298.md): Skin · chafed · Feb 11, 2005 · N520AU · Boeing 7373B7 · Leading Edge Devices
  > PIT - FOUND RIGHT OUTBOARD MID FLAP CHAFED.25 INCH BY 2 INCH BY.016 INCH, OUTBOARD 4 EDGE SURFACE. DOUBLER INSTALLED PER SRM 57-53-01 FIG 208. (M)
- [SDR USAA050235](https://openairdocs.org/sdr/USAA050235.md): Web · corroded · Feb 11, 2005 · N520AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND WEB CORRODED 8 INCH BY 30 INCH AREA, BS 794-828, CORROSION LEVEL 1, TASK NR C53-202-01. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-40-00. (M)
- [SDR USAA050233](https://openairdocs.org/sdr/USAA050233.md): Web · torn · Feb 10, 2005 · N520AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND WEB WITH.5 INCH SQUARE SECTION TORN OUT, BS 847 AT S24R. CUT OUT DAMAGE AND INSTALLED DOUBLER SPLICE AND NEW WEB PER SRM 51-70-13. (M)
- [SDR USAA050232](https://openairdocs.org/sdr/USAA050232.md): Frame · cracked · Feb 10, 2005 · N520AU · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.25, BS 440 BETWEEN S8R AND S9R. CUT OUT DAMAGE AND INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-10-20A. (M)
- [SDR USAA050312](https://openairdocs.org/sdr/USAA050312.md): Hinge Bracket · worn · Feb 9, 2005 · N520AU · Boeing 7373B7 · Vertical Stabilizer
  > PIT - FOUND HINGE PLATES WITH THREE WORN HOLES.25 INCH DIAMETER, RUDDER HINGE NR 7 PLATES ON VERTICAL STABILIZER. DEFECTIVE PART REPLACED WITH IDENT PART PER AMM 55-00-00. (M)
- [SDR USAA050300](https://openairdocs.org/sdr/USAA050300.md): Skin · dented · Feb 9, 2005 · N520AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN DENTED AND PUNCTURED, 1 INCH BY 1 INCH BY.125 INCH, BETWEEN S-26R AND S27R AND STA 500D PLUS 10 INCHES. REPAIR DOUBLER INSTALLED PER SRM 53-00-01 FIG 229 DETAIL XII. (M)
- [SDR USAA050234](https://openairdocs.org/sdr/USAA050234.md): Angle · chafed · Feb 9, 2005 · N520AU · Boeing 7373B7 · Vertical Stabilizer Miscellaneous Structure
  > PIT - FOUND SKATE ANGLE CHAFED, VERT STAB RT AND LT LOWER SKATE ANGLE. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-40-00 AND DWG 65-54842. (M)
- [SDR USAA050231](https://openairdocs.org/sdr/USAA050231.md): Frame · cracked · Feb 9, 2005 · N520AU · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.25 INCH, FS 887 S-9R. DOUBLER REPAIR INSTALLED PER 53-10-20A. (M)
- [SDR USAA050236](https://openairdocs.org/sdr/USAA050236.md): Stringer Splice · cracked · Feb 9, 2005 · N520AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND STRINGER SPLICE CRACKED 1 INCH IN TWO LOCATIONS, BS 908 S4L AND S4R. REMOVED TWO SPLICES, MANUFACTURED NEW AND INSTALLED PER SRM 51-40-02 AND DWG NR 65-51698. (M)
- [SDR USAA050299](https://openairdocs.org/sdr/USAA050299.md): Skin · cracked · Feb 8, 2005 · N520AU · Boeing 7373B7 · Leading Edge Devices
  > PIT - FOUND NR 5 SLAT SKIN CRACKED 1 INCH, OUTBOARD FORWARD EDGE ABOVE UPSTOP. INSTALLED DOUBLER PER SRM 57-43-01. (M)
- [SDR USAA050230](https://openairdocs.org/sdr/USAA050230.md): Frame · cracked · Feb 7, 2005 · N520AU · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.75 INCH, FS 616 S17R. INSTALLED DOUBLER PER TYPICAL REPAIR 53-62-01. (M)
- [SDR USAA050227](https://openairdocs.org/sdr/USAA050227.md): Frame · cracked · Feb 4, 2005 · N520AU · Boeing 7373B7 · Passenger/Crew Doors
  > PIT - FOUND FRAME CRACKED.125 INCH, BETWEEN 4TH DOOR STOP FORWARD SIDE. INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-11. (M)
- [SDR USAA050228](https://openairdocs.org/sdr/USAA050228.md): Door Frame · cracked · Feb 4, 2005 · N520AU · Boeing 7373B7 · Passenger/Crew Doors
  > PIT - FOUND FRAME CRACKED.125 INCH, FRAME FORWARD SIDE NR 3 DOOR STOP CUTOUT. INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-11. (M)
- [SDR USAA050229](https://openairdocs.org/sdr/USAA050229.md): Door Frame · cracked · Feb 3, 2005 · N520AU · Boeing 7373B7 · Passenger/Crew Doors
  > PIT - FOUND FORWARD ENTRY DOOR CRACKED.3750, FRAME AND INNER WEB AT STOPS NR 5 AND NR 6 CUTOUTS. REMOVED DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 51-10-16. (M)
- [SDR USAA040522](https://openairdocs.org/sdr/USAA040522.md): Skin · cracked · Sep 1, 2004 · N520AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 1.125 INCH LONG, STATION 727D PLUS 18 INCHES STRINGER 22L FUSELAGE SKIN. INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 229. (M)
- [SDR USAA040051](https://openairdocs.org/sdr/USAA040051.md): Skin · cracked · Feb 25, 2004 · N520AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN WITH 3 CRACKS, 2 INCHES, 2.5 INCHES AND.5 INCHES, BS 727D S23R-S24R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M)
- [SDR USAASB03190](https://openairdocs.org/sdr/USAASB03190.md): Charger · inoperative · Oct 17, 2003 · N520AU · Boeing 7373B7 · Emergency Lighting
  > FOUND L1 DOOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER. (M)
- [SDR USAASB03185](https://openairdocs.org/sdr/USAASB03185.md): Charger · failed · Oct 17, 2003 · N520AU · Boeing 7373B7 · Emergency Lighting
  > MAINTENANCE REPORTED THE AFT LEFT ENTRY DOOR EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK, P/N 2013-1A. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB03186](https://openairdocs.org/sdr/USAASB03186.md): Battery Pack · inoperative · Oct 17, 2003 · N520AU · Boeing 7373B7 · Emergency Lighting
  > MAINTENANCE REPORTED THE FORWARD ENTRY DOOR EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAASB03191](https://openairdocs.org/sdr/USAASB03191.md): Battery · inoperative · Oct 17, 2003 · N520AU · Boeing 7373B7 · Emergency Lighting
  > FOUND L2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACE THE BATTERY. (M)
- [SDR USAASA03168](https://openairdocs.org/sdr/USAASA03168.md): Socket · inoperative · Sep 16, 2003 · N520AU · Boeing 7373B7 · Emergency Lighting
  > MAINTENANCE REPORTED THE EMERGENCY EXIT ILGHT AT SEAT ROW 4, RIGHT SIDE, INOPERATIVE. MAINTENANCE REPLACED THE LIGHT SOCKET. (M)
- [SDR USAA030180](https://openairdocs.org/sdr/USAA030180.md): Angle · cracked · Sep 2, 2003 · N520AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND SEAL ANGLE CRACKED 10.5 INCHES, LEFT GEARWELL, TIRE O/D AT FILLET FAIRING. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)
- [SDR USAASB03133](https://openairdocs.org/sdr/USAASB03133.md): Control Module · faulty · Aug 8, 2003 · N520AU · Boeing 7373B7 · Overheat Detection
  > ORF - FLT 636 - EN ROUTE FROM CLT-PVD, AT FL330, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW REDUCED THE NR 1 ENGINE THROTTLE TO IDLE AND THE LIGHT EXTINGUISHED. CREW DECLARED AN EMERGENCY AND DIVERTED TO ORF. FLIGHT LANDED WITHOUT FURTHER INCIDENT. M
- [SDR USAASB01254](https://openairdocs.org/sdr/USAASB01254.md): Battery Pack · discharged · Sep 12, 2001 · N520AU · Boeing 7373B7 · Emergency Lighting
  > LGA - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA010801](https://openairdocs.org/sdr/USAA010801.md): Skin · cracked · Jul 3, 2001 · N520AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 1.125 INCH, RIGHT SIDE STATION 727E STRINGER 24 RIGHT. CUT OUT DAMAGE, INSTALLED EXT DOUBLER PER SRM 53-00-01 FIG 201. (M)
- [SDR USAASB01090](https://openairdocs.org/sdr/USAASB01090.md): Door · not closed · Mar 27, 2001 · N520AU · Boeing 7373B7 · Passenger/Crew Doors
  > PWM - FLT 2271 - ON CLIMB-OUT FROM PWM, THE A/C WOULD NOT PRESSURIZE. CREW ASSUMED IT WAS A MALFUNCTION OF THE PRESSURIZATION SYSTEM SINCE THERE WAS NO DOOR WARNING LIGHT INDICATION. AT 4,000 FEET, CAPTAIN ELECTED TO RETURN TO FIELD AT PWM. FLIGHT LANDED WI
- [SDR USAASB01074](https://openairdocs.org/sdr/USAASB01074.md): Door · not closed · Mar 6, 2001 · N520AU · Boeing 7373B7 · Passenger/Crew Doors
  > IAH - FLT 744 - ON CLIMB-OUT FROM IAH, CAPTAIN REPORTED THEY COULD NOT GET THE CABIN TO PRESSURIZE. AT 8,000 FEET, FLIGHT ATTENDANT ADVISED CAPTAIN THAT THE AFT SERVICE DOOR WAS NOT CLOSED. NO DOOR INDICATION WAS NOTED IN COCKPIT. FLIGHT RETURNED TO FIELD A
- [SDR USAASB01056](https://openairdocs.org/sdr/USAASB01056.md): Door · not closed · Feb 24, 2001 · N520AU · Boeing 7373B7 · Service Doors
  > PWM - FLT 1433 - ON CLIMB-OUT FROM PWM, EN ROUTE TO PIT, THE AIRCRAFT WOULD NOT PRESSURIZE. AT 5,000 FEET, THE CREW LEVELED OFF AND TRIED TO PRESSURIZE. AIRCRAFT WOULD NOT PRESSURIZE IN AUTO, STANDBY OR MANUAL MODES. FLIGHT RETURNED TO FIELD AT PWM AND LAND
- [SDR USAA010111](https://openairdocs.org/sdr/USAA010111.md): Floorbeam · corroded · Feb 5, 2001 · N520AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - FOUND T-CAP CORRODED 70 INCHES, RBL 46 TO LBL 48. REPLACED T-CAP PER SRM 53-10-51. (M)

Next page: https://openairdocs.org/deregistered/N520AU-2007-11-30/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 = 'N520AU' AND deregistration_id = 'N520AU-2007-11-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N520AU-2007-11-30/reports

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