# Service difficulty reports: N300AU, cancelled Sep 5, 2008

A list on [N300AU, cancelled Sep 5, 2008](https://openairdocs.org/deregistered/N300AU-2008-09-05.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 · 82 reports

- [SDR USAA051413](https://openairdocs.org/sdr/USAA051413.md): Skin · debonded · Nov 22, 2005 · N300AU · Boeing 737301 · Leading Edge Devices
  > NR 2 SLAT T/E WEDGE SS 246.4 - 241.9 DEBONDED. INSTALLED DOUBLER IAW EA 97124. DEFECT SIZE: 5 INCH X 4 INCH.
- [SDR USAA051199](https://openairdocs.org/sdr/USAA051199.md): Bulkhead · cracked · Oct 12, 2005 · N300AU · Boeing 737301 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED. REPAIRED AS REQUIRED, DOUBLER INSTALLED EA 96994, DEFECT SIZE 1 INCH.
- [SDR USAA200509002](https://openairdocs.org/sdr/USAA200509002.md): Skin · cracked · Sep 15, 2005 · N300AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > 2 INCH CRACK EXTENDING FROM UNDER A PREVIOUS REPAIR AT STA 727E - 747 STRINGER 23L. REMOVED REPAIR DOUBLER, FABRICATED NEW DOUBLER AND FILLERS AND INSTALLED REPAIR PER SRM 53-00-01 FIG 201.
- [SDR SB05108](https://openairdocs.org/sdr/SB05108.md): Pump · leaking · Sep 3, 2005 · N300AU · Boeing 737301 · Hydraulic Pump (Electric/Engine), Main
  > PHL - FLT803 - ON CLIMB-OUT FROM PHL, CREW REPORTED THE NR 1 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED ON GEAR RETRACTION. SYSTEM "A" HYDRAULIC QUANTITY DROPPED TO LESS THAN ONE-QUARTER. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER I
- [SDR USAA041111](https://openairdocs.org/sdr/USAA041111.md): Skin · cracked · Dec 28, 2004 · N300AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1.5 INCH, S-23R AT STATION 727D. INSTALLED DOUBLER IAW SRM 53-00-01. (M)
- [SDR USAA041110](https://openairdocs.org/sdr/USAA041110.md): Skin · cracked · Dec 28, 2004 · N300AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 3 INCHES, S-19R AT STATION 767. INSTALLED DOUBLER IAW SRM 53-00-01. (M)
- [SDR USA2004F00036](https://openairdocs.org/sdr/USA2004F00036.md): Charger · failed · May 13, 2004 · N300AU · Boeing 737301 · Emergency Lighting
  > MAINTENANCE REPORTED THE AFT SIX ROWS OF THE AISLE SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY CHARGER ASSY. ALSO, REPLACED THE BATTERY PACK. OPS CHECK GOOD.
- [SDR USA2004F00037](https://openairdocs.org/sdr/USA2004F00037.md): Battery Pack · discharged · May 8, 2004 · N300AU · Boeing 737301 · Emergency Lighting
  > MAINTENANCE REPORTED THE FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH FORWARD BATTERY PACKS. OPERATIONAL CHECK GOOD.
- [SDR USAA040191](https://openairdocs.org/sdr/USAA040191.md): Skin · cracked · May 7, 2004 · N300AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 4 INCHES, FORWARD SERVICE DOOR LOWER AFT CORNER STATION 328, APPROX STRINGER 16R. INSTALLED DOUBLER, TRIPLER AND FILLERS PER EA 78356. (M)
- [SDR USAA040055](https://openairdocs.org/sdr/USAA040055.md): Stringer · cracked · Mar 8, 2004 · N300AU · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CRACKED 1.25 INCH, AT STRINGER 23L BETWEEN BS 727E AND BS 747. INSTALLED DOUBLERS AFTER DAMAGE REMOVAL PER SRM 53-00-01 DETAIL XI FIG 229. (M)
- [SDR USAA040054](https://openairdocs.org/sdr/USAA040054.md): Stringer · cracked · Mar 8, 2004 · N300AU · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER CRACKED TWO PLACES 1.5 INCH AND 1.25 INCH, STRINGER 24L BETWEEN BS 727E AND BS 747. INSTALLED DOUBLERS AFTER DAMAGE REMOVED PER SRM 53-00-01 FIG 229 DETAIL XI. (M)
- [SDR USAASB03170](https://openairdocs.org/sdr/USAASB03170.md): Battery Pack · malfunctioned · Sep 18, 2003 · N300AU · Boeing 737301 · Emergency Lighting
  > MAINTENANCE REPORTED THE FORWARD SERVICE DOOR EMERGENCY LIGHT EXTINGUISHES AFTER APPROXIMATELY FIVE SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA030171](https://openairdocs.org/sdr/USAA030171.md): Skin · cracked · Aug 21, 2003 · N300AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED 1 INCH, AFT OF FS 727D BELOW S23R. INSTALLED DOUBLER PER EA 94615. (M)
- [SDR USAA030012](https://openairdocs.org/sdr/USAA030012.md): Skin · corroded · Jan 16, 2003 · N300AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CORRODED 2 INCHES BY 4 INCHES, BELOW CABIN FLOOR STATION 1016 AT BL 0 AFT PRESSURE BULKHEAD, CORROSION LEVEL 2, TASK NR C53-107-02. REMOVED CORRODED SECTION, INSTALLED DOUBLERS AND SPLICE PER SRM 53-80-08 AND 51-40-02, EA 75070. (M)
- [SDR USAASB02210](https://openairdocs.org/sdr/USAASB02210.md): Door · out of rig · Nov 24, 2002 · N300AU · Boeing 737301 · Passenger/Crew Doors
  > IND - FLT 338 - ON CLIMB-OUT FROM IND, EN ROUTE TO CLT, THE FORWARD MAIN ENTRY DOOR WARNING LIGHT ILLUMINATED. CREW REPORTED THE HANDLE COMES UP IN FLIGHT WHEN PRESSURIZED AND THE LIGHT WILL GO OFF AND ON AS HANDLE IS PRESSED DOWN TO CLOSED POSITION. FLIGHT
- [SDR USAA020417](https://openairdocs.org/sdr/USAA020417.md): Elevator · delaminated · Nov 7, 2002 · N300AU · Boeing 737301 · Elevator, Plate/Skin
  > PIT - FOUND LEFT ELEVATOR SPLINTERING AND DELAMINATED, STATION 95, 81, 100 INBOARD SIDE. ACCOMPLISHED SKIN AND CORE REPAIRS PER SRM 55-20-01, 51-70-17 AND EA 75277. (M)
- [SDR USAA020418](https://openairdocs.org/sdr/USAA020418.md): Stringer · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND SHELF CRACKED 1 INCH LONG, AFT END OF RIGHT 18A SHELF, FED OF STATION 727. REMOVED AND REPLACED SHELF PER SRM 51-10-02. (M)
- [SDR USAA020419](https://openairdocs.org/sdr/USAA020419.md): Frame · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.5 INCH DIAMETER, S27L AND STATION 336 IN FRAME OF EYE OPENING. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA020421](https://openairdocs.org/sdr/USAA020421.md): Intercostal · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND INTERCOSTAL CRACKED.75 INCH LONG, STATION 357 AND STRINGER 16L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA020422](https://openairdocs.org/sdr/USAA020422.md): Stringer · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND STRINGER CRACKED.375 INCH LONG, STRINGER 17R BETWEEN STATION 616-639. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA020423](https://openairdocs.org/sdr/USAA020423.md): Shear Tie · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, Structure
  > PIT - FOUND SHEAR TIE CRACKED.5 INCH LONG, SHEAR TIE S2L AT STATION 639. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA020424](https://openairdocs.org/sdr/USAA020424.md): Frame · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.375 INCH, STATION 663 AND STRINGER 2L. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE AND STRINGER SPLICES PER EA 74814. (M)
- [SDR USAA020425](https://openairdocs.org/sdr/USAA020425.md): Clip · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND CLIP CRACKED.5 INCH LONG, STATION 663 STRINGER 10L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA020426](https://openairdocs.org/sdr/USAA020426.md): Bracket · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND BRACKET CRACKED.5 INCH LONG, STATION 663 STRINGER 8L AND 9L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA020427](https://openairdocs.org/sdr/USAA020427.md): Stringer · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND STRINGER CRACKED.5 INCH LONG, FS 663 STRINGER 4L. REMOVED TIE CLIP, HFEC INSPECTION OF STRINGER AND CLIP PER SRM 51-40-02 AND NDT 0-4-53-10. (M)
- [SDR USAA020428](https://openairdocs.org/sdr/USAA020428.md): Frame · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.5 INCH LONG, FS 480 STRINGER 8L AND 9L. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES PER EA 74802-A. (M)
- [SDR USAA020429](https://openairdocs.org/sdr/USAA020429.md): Frame · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.125 INCH, STATION 480 STRINGER 8R AND 9R. REMOVED DAMAGED AND INSTALLED REPAIR ANGLES PER EA 74802-A. (M)
- [SDR USAA020432](https://openairdocs.org/sdr/USAA020432.md): Stringer · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND SHELF WITH 1 INCH LONG CRACK, AFT END OF LEFT 18A SHELF, FORWARD OF STATION 727. REMOVED AND REPLACED 18A SHELF PER SRM 51-10-02. (M)
- [SDR USAA020415](https://openairdocs.org/sdr/USAA020415.md): Skin · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Horizontal Stabilizer, Plate/Skin
  > PIT - FOUND LEADING EDGE REMOVABLE SKIN WITH CRACKS, 1 INCH BY 1 INCH AREA BEYOND 25 PERCENT MAXIMUM LIMITS, 14 EACH BLENDED AREAS, LEFT HORIZ STABILIZER LEADING EDGE STATION 86.66-151.75. BLENDED AND POLISHED PER SRM 55-10-01. (M)
- [SDR USAA020420](https://openairdocs.org/sdr/USAA020420.md): Intercostal · cracked · Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND INTERCOSTAL CRACKED.5 INCH BY 7 INCH AREA, STATION 303 AND 310 AT STRINGER 4L. FABRICATED WEB, STRAP AND T-FITTING PER SRM 53-02-04. (M)
- [SDR USAA020416](https://openairdocs.org/sdr/USAA020416.md): Support · corroded · Oct 2, 2002 · N300AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND SUPPORT CORRODED SEVERAL AREAS, BS 960 Z-ANGLE SUPPORT, AFT ENTRY THRESHOLD DOOR JAM. CORROSION, LEVEL 2, TASK NR C53-107-01. REPLACED Z-ANGLE PER BOEING DWG 65-52878. (M)
- [SDR USAA020369](https://openairdocs.org/sdr/USAA020369.md): Structure · chafed · Sep 27, 2002 · N300AU · Boeing 737301 · Wing, Control Surfaces
  > PIT - FOUND TRAILING EDGE HAS CHAFE, 59 INCHES INBOARD FROM INBOARD END. BURNISHED/BLENDED AND INSTALLED WEAR PAD PER TYPICAL REPAIR 57-50-17. (M)
- [SDR USAA020371](https://openairdocs.org/sdr/USAA020371.md): Mount · worn · Sep 25, 2002 · N300AU · Boeing 737301 · Engine Mount Section
  > PIT - FOUND ENGINE MOUNT CROSSBEAM WORN LUG, LUG BORE ON ENGINE MOUNT. MACHINE INSIDE DIAMETER OF LUG BORE TO OVERSIZE BEARING PER TYPICAL REPAIR 550-19 REV B. (M)
- [SDR USAA020414](https://openairdocs.org/sdr/USAA020414.md): Frame · cracked · Sep 20, 2002 · N300AU · Boeing 737301 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.5 INCH LONG, STATION 616 RIGHT SIDE FRAME LOWER INBOARD END. INSTALLED DOUBLER ANGLE PER TYPICAL REPAIR 53-61-01 AND EA 74856. (M)
- [SDR USAA020365](https://openairdocs.org/sdr/USAA020365.md): Frame · cracked · Sep 20, 2002 · N300AU · Boeing 737301 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED 1 INCH, STATION 616 RIGHT SIDE, FRAME LOWER INBOARD END CABIN FLOOR. INSTALLED DOUBLER ANGLE PER TYPICAL REPAIR 53-61-01 AND EA 74256. (M)
- [SDR USAA020364](https://openairdocs.org/sdr/USAA020364.md): Skin · delaminated · Sep 19, 2002 · N300AU · Boeing 737301 · Rudder, Plate/Skin
  > PIT - FOUND RUDDER DELAMINATED, LEFT SIDE, BOTTOM EDGE 19 INCHES AFT OF LEADING EDGE. RESIN AND OVERLAYED WITH TWO PLIES OF GRAPHITE FABRIC PER EA 74841, SRM 55-40-01, 51-70-17. (M)
- [SDR USAA020367](https://openairdocs.org/sdr/USAA020367.md): Skin · cracked · Sep 17, 2002 · N300AU · Boeing 737301 · Ailerons
  > RIGHT AILERON, CRACKED 2 LOCATIONS. LOWER SKIN FLANGE AT NR 3 HINGE AND NR 2 HINGE. REMOVED ALL DAMAGE PLUS COMPLETED WET LAYUP REPAIR IAW SRM AND EA.
- [SDR USAA020282](https://openairdocs.org/sdr/USAA020282.md): Mount · worn · Jul 23, 2002 · N300AU · Boeing 737301 · Engine Mount Section
  > PIT - FOUND ENGINE MOUNT STRUT WORN BEYOND LIMITS, ENGINE MOUNT MAIN SLEEVE REPAIR. REAMED, CHAMFERED, BLENDED AND ROTOPEENED THE FITTING BORE PER TYPICAL 54-50-10 REV A. (M)
- [SDR USA2002F00053](https://openairdocs.org/sdr/USA2002F00053.md): Sensor · failed · Jun 2, 2002 · N300AU · Boeing 737301 · Landing Gear Position and Warning
  > AFTER TAKEOFF, CREW WAS UNABLE TO MOVE THE LANDING GEAR SELECTOR HANDLE PAST THE OFF POSITION TO RETRACT THE GEAR. CREW ALSO TRIED THE GEAR OVER RIDE WITH NO HELP. DUE TO THE TAKEOFF WARNING HORN SOUNDING AFTER THE FLAPS WERE FULLY RETRACTED, CREW THINKS TH
- [SDR USAA020184](https://openairdocs.org/sdr/USAA020184.md): Rib · corroded · Apr 30, 2002 · N300AU · Boeing 737301 · Rudder, Spar/Rib
  > PIT - FOUND RUDDER CORRODED 3 INCHES BY 12 INCH AREA, COVER FACE OF RIB BEHIND BALANCE WEIGHTS ON BEAM. REPLACED RIB PER SRM 51-10-02, 51-20-01, 51-20-00 AND 51-40-02. (M)
- [SDR USAASB01349](https://openairdocs.org/sdr/USAASB01349.md): Wire · disconnected · Dec 23, 2001 · N300AU · Boeing 737301 · Light System Wiring
  > BWI - PILOT REPORTED THE WIRING FOR THE EMERGENCY EXIT LIGHTS UNDER SEAT 21C IS DISCONNECTED AND THE LIGHTS ARE INOPERATIVE. MAINTENANCE RECONNECTED AND SECURED WIRING. OPS CHECK OF LIGHTS GOOD. (M)
- [SDR USAA011393](https://openairdocs.org/sdr/USAA011393.md): Structure · damaged · Dec 17, 2001 · N300AU · Boeing 737301 · Rudder Structure
  > PIT - FOUND RUDDER DAMAGED, NR 7 HINGE AREA RSTA 225-235 LEADING EDGE. PER SRM 51-70-17 2 EXTRA PLIES WITH HALF OVERLAP PER EA 73066. (M)
- [SDR USAA011394](https://openairdocs.org/sdr/USAA011394.md): Structure · damaged · Dec 17, 2001 · N300AU · Boeing 737301 · Rudder Structure
  > PIT - FOUND RUDDER 8 INCH BY.750 INCH GOUGED, CLOSE TO T/E WEDGE BETWEEN R STA 121164 AND 174.12. REPAIRED PER SRM 51-70-17 WITH 2 EXTRA PILES WITH.5 OVERLAP PER EA 73065. (M)
- [SDR USAA011395](https://openairdocs.org/sdr/USAA011395.md): Skin · damaged · Dec 17, 2001 · N300AU · Boeing 737301 · Rudder, Plate/Skin
  > PIT - FOUND RUDDER SCREW PULLED THROUGH SKIN, LEFT SKIN PANEL AT R STATION 225 APPROXIMATELY. TWO EXTRA REPAIR PLIES WITH.5 INCH PER PLY OVERLAP PER EA 73064. (M)
- [SDR USAASB01083](https://openairdocs.org/sdr/USAASB01083.md): Door · not closed · Mar 20, 2001 · N300AU · Boeing 737301 · Passenger/Crew Doors
  > BWI - FLT 1568 - ON CLIMB-OUT FROM DCA, AT APPROXIMATELY 4,500 FEET, THE FLIGHT ATTENDANT ADVISED CREW OF A LOUD AIR NOISE COMING FROM THE FORWARD ENTRY DOOR. SIMULATANEOUSLY, THE CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT. FLIGHT DIVERTED TO BWI AND LANDED
- [SDR USAASB01009](https://openairdocs.org/sdr/USAASB01009.md): Wire Harness · out of position · Jan 18, 2001 · N300AU · Boeing 737301 · Light System Wiring
  > LGA - MAINTENANCE FOUND THE EMERGENCY EXIT PATH LIGHTING AT SEAT 16C INOPERATIVE. MAINTENANCE REPOSITIONED WIRING HARNESS FOR SEAT ROW 16ABC EMERGENCY EXIT PATH LIGHTING. OPS CHECK GOOD. (M)
- [SDR USAASB00223](https://openairdocs.org/sdr/USAASB00223.md): Charger · failed · Aug 19, 2000 · N300AU · Boeing 737301 · Emergency Lighting
  > CLT - PILOT REPOTED THAT THE EMERGENCY EXIT PATH LIGHTS FROM SEAT ROWS 5 TO 11 ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSY AND THE BATTERY PACK (P/N AD2013-1A). OPS CHECK GOOD. (M)
- [SDR USAASB00089](https://openairdocs.org/sdr/USAASB00089.md): Power Supply · failed · Mar 28, 2000 · N300AU · Boeing 737301 · Emergency Lighting
  > TPA - DURING ANNUAL OPERATIONAL CHECK OF THE AFT LEFT SERVICE DOOR ESCAPE SLIDE, THE SLIDE DEPLOYED NORMALLY BUT THE SLIDE MOUNTED EMERGENCY LIGHTS FAILED TO ILLUMINATE. SLIDE OPERATIONAL CHECK FAILED. MAINTENANCE FOUND THE POWER UNIT ASSY FOR THE ESCAPE SLI
- [SDR USAA991435](https://openairdocs.org/sdr/USAA991435.md): Skin · cracked · Dec 9, 1999 · N300AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > PIT - DURING RON VISIT, FOUND 1.0625 INCH LONG CRACK ON FUSELAGE SKIN AT RT SIDE, STATION 767 STRINGER 22 TO 23 RT. REMOVED CRACK WITH CUTOUT. INSTALLING EXTERNAL DOUBLER PER SRM 53-00-00-01, FIG 201, EA 53528. (M)
- [SDR USAASB99290](https://openairdocs.org/sdr/USAASB99290.md): Cabin Pressure · failed · Dec 8, 1999 · N300AU · Boeing 737301 · Cabin Pressure Control System
  > PIT - FLT 2380 - DURING CLIMB-OUT FROM PIT, THE AUTO PRESSURIZATION SYSTEM FAILED TO STANDBY. CREW WAS UNABLE TO CONTROL CABIN IN STANDBY OR MANUAL MODE. CABIN CONTINUED TO CLIMB WITH OUTFLOW VALVE CLOSED. DECISION WAS MADE TO RETURN TO FIELD AT PIT. FLIGH

Next page: https://openairdocs.org/deregistered/N300AU-2008-09-05/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 = 'N300AU' AND deregistration_id = 'N300AU-2008-09-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N300AU-2008-09-05/reports

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