# Service difficulty reports: N39081, cancelled Jan 17, 2003

A list on [N39081, cancelled Jan 17, 2003](https://openairdocs.org/deregistered/N39081-2003-01-17.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 · 87 reports

- [SDR CALA0100826](https://openairdocs.org/sdr/CALA0100826.md): Restrictor Valve · failed · Aug 31, 2001 · N39081 · Doug DC1030 · Landing Gear Retraction/Extension System
  > THE LT MLG WOULD NOT RETRACT AFTER TAKEOFF FROM NRT. A VISUAL CHECK CONFIRMED THE GEAR WAS DOWN. THE AIRCRAFT WAS RETURNED TO NRT WHERE IT LANDED WITHOUT INCIDENT. THE LT MLG RETRACT CYLINDER WAS REMOVED AND REPLACED, BUT THE PROBLEM REMAINED. MAINTENANCE
- [SDR CALA0100457](https://openairdocs.org/sdr/CALA0100457.md): Bottle · discharged · May 13, 2001 · N39081 · Doug DC1030 · Service Doors
  > DOOR R-4 WAS HARD TO OPERATE. THE R-4 DOOR N2 BOTTLE WAS RESERVICED IAW MM 52-12-16.
- [SDR CALA0001692](https://openairdocs.org/sdr/CALA0001692.md): Duct · blown · Nov 2, 2000 · N39081 · Doug DC1030 · Pneumatic Distribution System
  > THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED DURING TAKEOFF FROM IAH. THE NR 1 NACELLE TEMP WENT TO 300 DEGREES AND THE NR 1 THRUST REVERSER VALVE OPEN LIGHT CAME ON. POWER WAS REDUCED TO JUST ABOVE IDLE AND THE FIRE WARNING LIGHT EXTINGUISHED. FUE
- [SDR CALA0001407](https://openairdocs.org/sdr/CALA0001407.md): Spar Cap · corroded · Sep 8, 2000 · N39081 · Doug DC1030 · Wing Spar
  > INSPECTION FOUND CORROSION ON CENTER WING FORWARD LOWER SPAR CAP AT XCW 0.0. THE SPAR CAP WAS REPAIRED IAW ECRA 5311-01104 AND FLS DRAWING 90-53-1071.
- [SDR CALA0001372](https://openairdocs.org/sdr/CALA0001372.md): Longeron · corroded · Sep 3, 2000 · N39081 · Doug DC1030 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 48L CORRODED AROUND FASTENERS IN CENTER CARGO BAY AT STA 1521. THE END CAP WAS REMOVED AND A NEW END CAP WAS INSTALLED IAW SRM 51-00-01.
- [SDR CALA0001371](https://openairdocs.org/sdr/CALA0001371.md): Shear Tie · corroded · Sep 3, 2000 · N39081 · Doug DC1030 · Fuselage Main, Structure
  > INSPECTION FOUND SHEAR CLIPS CORRODED AT FRAME STA 1903 FROM L48R-49R, 50R-51R, AND 50L-52L. THE SHEAR CLIPS WERE REMOVED AND REPLACED IAW SRM 53-30-00.
- [SDR CALA0001370](https://openairdocs.org/sdr/CALA0001370.md): Angle · corroded · Sep 3, 2000 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND STIFFENER ANGLES CORRODED AT FRAME STA 1997 ABOVE L49L TO L49R. THE STIFFENER ANGLES WERE REPLACED IAW SRM 51-00-01.
- [SDR CALA0001369](https://openairdocs.org/sdr/CALA0001369.md): Shear Tie · corroded · Sep 3, 2000 · N39081 · Doug DC1030 · Fuselage Main, Structure
  > INSPECTION FOUND SHEAR CLIPS CORRODED AT FRAME STA 1941 L49R - 52L, STA 1959 L50L - L52L, AND STA 1975 L50L - L50R. THE SHEAR CLIPS WERE REPLACED IAW SRM 53-30-00, 53-00-01, AND 51-21-02.
- [SDR CALA0001298](https://openairdocs.org/sdr/CALA0001298.md): Beam · corroded · Aug 22, 2000 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND G1A -G5 LT SUPPORT BEAM CORRODED AT STA 800. THE SUPPORT BEAM WAS REPLACED IAW GMM 10-900-01.
- [SDR CALA0001286](https://openairdocs.org/sdr/CALA0001286.md): Beam · corroded · Aug 21, 2000 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT BEAM BENEATH LAV D CORRODED AT STA 836 - 880. THE INNER SUPPORT BEAM WAS REPLACED IAW GMM 10-900-01.
- [SDR CALA0001285](https://openairdocs.org/sdr/CALA0001285.md): Beam · corroded · Aug 21, 2000 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT SUPPORT BEAM CORRODED AT STA 840. THE BEAM WAS REPLACED IAW SRM 53-70-00 AND GMM 10-900-01.
- [SDR CALA0001284](https://openairdocs.org/sdr/CALA0001284.md): Floorbeam · corroded · Aug 21, 2000 · N39081 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND O/B FLOORBEAM CORRODED AT GALLEY 2. THE FLOORBEAM WAS REPLACED IAW SRM 53-00-00 AND GMM 10-900-01.
- [SDR CALA0001283](https://openairdocs.org/sdr/CALA0001283.md): Floor Support · corroded · Aug 21, 2000 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 392 ADJACENT TO R-1 DOOR. THE FLOOR SUPPORT BEAM WAS REPLACED IAW SRM 53-00-00 AND GMM 10-900-01.
- [SDR CALA0001282](https://openairdocs.org/sdr/CALA0001282.md): Floor Support · corroded · Aug 21, 2000 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT ADJACENT TO GALLEY G-1 CORRODED. REPAIRED IAW SRM 53-00-00 AND GMM 10-900-01.
- [SDR CALA0001266](https://openairdocs.org/sdr/CALA0001266.md): Floor Support · corroded · Aug 14, 2000 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED AT STA 836 AND 804, X42 TO X-42. THE CORRODED SECTIONS OF FLOOR SUPPORT BEAM WERE REPLACED IAW GMM 10-900-01.
- [SDR CALA0000572](https://openairdocs.org/sdr/CALA0000572.md): Engine · failed · Apr 25, 2000 · N39081 · Doug DC1030 · Turbine Section
  > NUMBER ONE ENGINE FAILED (UNCONTAINED) AT TAKEOFF. ENGINE BEING REMOVED AND FORWARDED TO SHOP FOR FAILURE ANALYSIS. THIS SDR TO REMAIN OPEN PENDING TEARDOWN AND ANALYSIS.
- [SDR CALA9901085](https://openairdocs.org/sdr/CALA9901085.md): Wire · damaged · Aug 24, 1999 · N39081 · Doug DC1030 · Light System Wiring
  > THE EXIT IDENTIFIER AT LAV C FAILED TO ILLUMINATE. INSPECTION FOUND CABLES DAMAGED. THE CABLES WERE REPAIRED AND OPERATION CHECKED IAW MM 33-50-00.
- [SDR CALA9901084](https://openairdocs.org/sdr/CALA9901084.md): Wire · chafed · Aug 24, 1999 · N39081 · Doug DC1030 · Light System Wiring
  > INSPECTION FOUND THE EMERGENCY PATH LIGHTING SYSTEM BATTERY POWER SUPPLY BLOWING FUSES AT L-3 DOOR. MAINTENANCE FOUND CHAFED WIRE AT SIDEWALL FORWARD OF LT OVERWING EXIT. REPAIRED IAW MM 20-00-00 AND OPERATION CHECKED GOOD IAW MM 33-50-00.
- [SDR CALA9901083](https://openairdocs.org/sdr/CALA9901083.md): Charger · inop · Aug 24, 1999 · N39081 · Doug DC1030 · Emergency Lighting
  > INSPECTION FOUND L-2 DOOR EMERGENCY LIGHTS BATTERY CHARGER UNIT BATTERY DISCONNECT PLUG CABLE BROKEN AT PLUG. THE CHARGER UNIT WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.
- [SDR CALA9901082](https://openairdocs.org/sdr/CALA9901082.md): Skin · corroded · Aug 23, 1999 · N39081 · Doug DC1030 · Leading Edge Devices
  > INSPECTION FOUND LT WING NR 8 SLAT CORRODED ON LEADING EDGE AT TRACK. THE NR 8 SLAT WAS REMOVED AND REPLACED IAW MM 27-80-01.
- [SDR CALA9901079](https://openairdocs.org/sdr/CALA9901079.md): End Cap · corroded · Aug 23, 1999 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD CARGO BAY STRINGER 44R END CAP CORRODED AT STA 889. THE END CAP WAS REPAIRED IAW SRM 53-30-00.
- [SDR CALA9901071](https://openairdocs.org/sdr/CALA9901071.md): Floor · delaminated · Aug 19, 1999 · N39081 · Doug DC1030 · Fuselage Floor Panel
  > INSPECTION FOUND FLOOR PANEL 283KF DELAMINATED WITH CORRODED FERRULES. A NEW FLOOR PANEL WAS INSTALLED IAW GMM 10-100-01.
- [SDR CALA9901052](https://openairdocs.org/sdr/CALA9901052.md): Support · corroded · Aug 14, 1999 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED AT STA Y= 1838-1873, X= 3R. THE CORRODED SECTION OF SUPPORT BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW GMM 10-100-01.
- [SDR CALA9901051](https://openairdocs.org/sdr/CALA9901051.md): Support · corroded · Aug 14, 1999 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND THE LONGITUDINAL FLOOR SUPPORT BEAM CORRODED AT STA Y= 1990-1996, X= 22R. REPAIRED IAW SRM 53-70-00, FIGURE 13 AND 14.
- [SDR CALA9901050](https://openairdocs.org/sdr/CALA9901050.md): Support · corroded · Aug 14, 1999 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT Y= 1887, X= 3R TO 70R AND AT Y= 1887, X= 3L TO 70L, J CAPPING STRIP. THE CORRODED SECTIONS OF CAPPING STRIP WERE REMOVED. NEW SECTIONS OF CAPPING STRIP WERE INSTALLED IAW GMM 10-100-01.
- [SDR CALA9801233](https://openairdocs.org/sdr/CALA9801233.md): Light · inoperative · Jul 10, 1998 · N39081 · Doug DC1030 · Emergency Lighting
  > INSPECTION FOUND EMERGENCY FLASHLIGHT IN CABIN INOPERATIVE. THE FLASHLIGHT WAS REMOVED AND REPLACED.
- [SDR CALA9800387](https://openairdocs.org/sdr/CALA9800387.md): Filter Case · broken · Mar 5, 1998 · N39081 · Doug DC1030 · Hydraulic System, Main
  > THE NR 3 HYDRAULIC SYSTEM LOST FLUID ACCOMPANIED BY ILLUMINATION OF THE HYDRAULIC SYSTEM ELEVATOR OFF LIGHT WHILE EN ROUTE FROM FCO TO EWR. FUEL WAS DUMPED AND THE AIRCRAFT WAS DIVERTED TO CDG WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGI
- [SDR CALA9701791](https://openairdocs.org/sdr/CALA9701791.md): Actuator · inoperative · Dec 22, 1997 · N39081 · Doug DC1030 · Landing Gear Door Actuator
  > THE LT MLG WOULD NOT RETRACT AFTER TAKEOFF FROM LGW. APPROPRIATE CHECKLISTS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT GEAR DOOR ACTUATOR SLOW TO OPERATE AND THE GEAR CONTACTED THE OUTER DOO
- [SDR CALA9701228](https://openairdocs.org/sdr/CALA9701228.md): Bulkhead · buckled · Aug 11, 1997 · N39081 · Doug DC1030 · Fuselage Main, Bulkhead
  > INSPECTION FOUND TAIL CONE BULKHEAD AT FS 2163, STRINGER 51L BUCKLED. THE BUCKLED AREA WAS REMOVED AND A REPAIR WAS INSTALLED USING DOUBLER AND FILLER IAW SRM 53-00-1 FIGURE 4 SHEET 2.
- [SDR CALA9701088](https://openairdocs.org/sdr/CALA9701088.md): Floor Panel · corroded · Jun 20, 1997 · N39081 · Doug DC1030 · Fuselage Floor Panel
  > INSPECTION FOUND FLOOR PANELS 291AF, 291EF, 292BF, 292DF, 292EF, 293BF, 293CF, AND 293DF CORRODED. REPLACEMENT FLOOR PANELS WERE FABRICATED AND INSTALLED IAW SRM 51-30-00, 53-21-00, AND 53-60-00.
- [SDR CALA9701087](https://openairdocs.org/sdr/CALA9701087.md): Floor Panel · corroded · Jun 20, 1997 · N39081 · Doug DC1030 · Fuselage Floor Panel
  > INSPECTION FOUND FLOOR PANELS 241EF, 241FF, 242BF, 242FF, AND 261BF CORRODED. REPLACEMENT FLOOR PANELS WERE FABRICATED AND INSTALLED IAW SRM 51-30-00, 53-60-00, AND 53-21-00.
- [SDR CALA9701085](https://openairdocs.org/sdr/CALA9701085.md): Floorboard · corroded · Jun 19, 1997 · N39081 · Doug DC1030 · Fuselage Floor Panel
  > INSPECTION FOUND FLOORBOARD PANEL 227AF CORRODED. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-60-00.
- [SDR CALA9701074](https://openairdocs.org/sdr/CALA9701074.md): Support · corroded · Jun 19, 1997 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT AND MOUNT FITTING CORRODED AT STA 459 TO 501, RBL 14. THE MOUNT FITTING WAS REMOVED AND REPLACED IAW SRM 51-31-01. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01 AND 53-00-01.
- [SDR CALA9701075](https://openairdocs.org/sdr/CALA9701075.md): Skin · corroded · Jun 17, 1997 · N39081 · Doug DC1030 · Trailing Edge Flaps
  > INSPECTION FOUND LT WING INBOARD FLAP CORRODED. THE LT INBOARD TRAILING EDGE FLAP SKIN WAS REMOVED AND NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 57-52-01.
- [SDR CALA9701020](https://openairdocs.org/sdr/CALA9701020.md): Support · corroded · Jun 17, 1997 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 475, RBL 38. THE UPPER FLANGE OF FLOOR SUPPORT WAS TRIMMED OFF AND REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 5310-03505.
- [SDR CALA9701017](https://openairdocs.org/sdr/CALA9701017.md): Skin · dented · Jun 13, 1997 · N39081 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A DENT AND CREASE IN LT AFT FUSELAGE SKIN AT STA 1841 BETWEEN LONGERON 40L AND 41L. THE DENT AND CREASE WERE REWORKED IAW SRM 53-20-00, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-20-00 AND ECRA 5330-02532.
- [SDR CALA9701016](https://openairdocs.org/sdr/CALA9701016.md): Skin · corroded · Jun 13, 1997 · N39081 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1501, BL 0. THE CORROSION WAS REMOVED IAW SRM 51-21-01, A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5330-02524.
- [SDR CALA9701084](https://openairdocs.org/sdr/CALA9701084.md): Web · elongated holes · Jun 5, 1997 · N39081 · Doug DC1030 · Nacelle/Pylon Structure
  > INSPECTION FOUND SEVERAL ELONGATED FASTENER HOLES IN NR 3 PYLON FRONT SPAR WEB. THE WEB WAS REMOVED, A NEW WEB WAS FABRICATED AND INSTALLED IAW EA 5410-01109 AND SRM 51-30-00.
- [SDR CALA9701082](https://openairdocs.org/sdr/CALA9701082.md): Angle · corroded · Jun 4, 1997 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION ATTACH CHANNEL CORRODED AT STA 595, LONGERON 45L. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 53-12-01.
- [SDR CALA9701070](https://openairdocs.org/sdr/CALA9701070.md): Floor · cracked · Jun 3, 1997 · N39081 · Doug DC1030 · Fuselage Floor Panel
  > INSPECTION FOUND AN 8 INCH CRACK AT LIGHTENING HOLE OF FLOOR UNDER FLIGHT ENGINEER'S SEAT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-11-01 AND 51-31-01.
- [SDR CALA9701069](https://openairdocs.org/sdr/CALA9701069.md): Support · corroded · Jun 3, 1997 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 1901 TO 2007, LBL 57. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-31-01, AND 51-21-01.
- [SDR CALA9701086](https://openairdocs.org/sdr/CALA9701086.md): Floor Panel · corroded · Jun 2, 1997 · N39081 · Doug DC1030 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN FLOOR PANELS 231CF, 232AF, 232CF, 233AF, AND 233CF CORRODED. REPLACEMENT FLOOR PANELS WERE FABRICATED AND INSTALLED IAW SRM 51-30-00, 53-60-00, AND 53-21-00.
- [SDR CALA9701081](https://openairdocs.org/sdr/CALA9701081.md): Angle · corroded · Jun 2, 1997 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CENTER CARGO AFT BILGE FORWARD FRAME WEB SUMP PANEL ATTACH ANGLE CORRODED AT STA 1781, RBL 1 TO RBL 12. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, 51-31-01, AND 53-15-01.
- [SDR CALA9701073](https://openairdocs.org/sdr/CALA9701073.md): Skin · gouged · May 31, 1997 · N39081 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT FUSELAGE SKIN GOUGED AT STA 735, LONGERON 28R. THE GOUGED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 53-20-00.
- [SDR CALA9701018](https://openairdocs.org/sdr/CALA9701018.md): Floor Panel · corroded · May 29, 1997 · N39081 · Doug DC1030 · Fuselage Floor Panel
  > INSPECTION FOUND FLOOR PANEL CORRODED AT STA 840-899, RBL 72. THE PANEL WAS REMOVED AND REPLACED IAW SRM 53-00-01.
- [SDR CALA9701083](https://openairdocs.org/sdr/CALA9701083.md): Web · cracked · May 27, 1997 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.125 INCH CRACK AT CORNER ACCESS HOLE WEB FRAME STA 1256, LONGERON 27R. A 1 INCH CRACK WAS FOUND ON LT SIDE AS WELL, AT LONGERON 27L. THE CRACKS WERE STOP DRILLED, REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 4,
- [SDR CALA9701080](https://openairdocs.org/sdr/CALA9701080.md): Support · corroded · May 27, 1997 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1884, LBL 28 TO 33. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-21-01, AND 51-31-01.
- [SDR CALA9701076](https://openairdocs.org/sdr/CALA9701076.md): Frame · cracked · May 27, 1997 · N39081 · Doug DC1030 · Fuselage Main, Frame
  > INSPECTION FOUND A.075 INCH CRACK IN FRAME AT FORWARD LOWER CORNER OF ACCESS HOLE WEB, STA 1305, LONGERON 27L. A.5 INCH CRACK WAS FOUND ON THE RT SIDE AT LONGERON 27R. THE CRACKS WERE STOP DRILLED, DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-0
- [SDR CALA9701071](https://openairdocs.org/sdr/CALA9701071.md): Support · corroded · May 27, 1997 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1884, RBL 4 TO 21. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 53-16-01.
- [SDR CALA9701067](https://openairdocs.org/sdr/CALA9701067.md): Support · corroded · May 27, 1997 · N39081 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 840 TO 899. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-13-01, 51-21-01, AND 51-30-01.

Next page: https://openairdocs.org/deregistered/N39081-2003-01-17/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 = 'N39081' AND deregistration_id = 'N39081-2003-01-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N39081-2003-01-17/reports

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