# Service difficulty reports: N488US, cancelled May 17, 2002

A list on [N488US, cancelled May 17, 2002](https://openairdocs.org/deregistered/N488US-2002-05-17.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 10 · 493 reports

- [SDR QXEA0200188](https://openairdocs.org/sdr/QXEA0200188.md): Stringer · corroded · Feb 10, 2002 · N488US · Fokker F28MK4000 · Wing, Longeron/Stringer
  > PDX - LT WING STRINGER 2.31 HAS TOOL MARK BECOMING CORRODED AT STATION 10990. REPAIRED IAW FOKKER SRM 51-10-4.
- [SDR QXEA0102165](https://openairdocs.org/sdr/QXEA0102165.md): Light · inoperative · Dec 27, 2001 · N488US · Fokker F28MK4000 · Emergency Lighting
  > PDX - PASSENGER EXIT LIGHT INOP AT NR 2 GALLEY CURTAIN, WHEN USING COCKPIT ARMING ON SWITCH. REPLACED EXIT LIGHT PANEL WITH SERVICEABLE UNIT.
- [SDR QXEA0102164](https://openairdocs.org/sdr/QXEA0102164.md): Door · out of rig · Dec 26, 2001 · N488US · Fokker F28MK4000 · Cargo/Baggage Doors
  > PDX - CENTER CARGO DOOR LEADING EDGE NOT FLUSH WITH AIRCRAFT SKIN WHEN AIRCRAFT IS PRESSURIZED. REPAIRED IAW HORIZON AIR EA 4-52-464.
- [SDR QXEA0102151](https://openairdocs.org/sdr/QXEA0102151.md): Frame · corroded · Dec 23, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - CORROSION UNDER FOUR NUT PLATES IN FRAME 14755 FROM CENTERLINE OUT TO 4 INCHES RIGHT OF CENTERLINE. REPAIRED IAW HORIZON AIR EA 4-53-1536, FOKKER SRM 51-31-01 AND SRM 51-31-05.
- [SDR QXEA0102150](https://openairdocs.org/sdr/QXEA0102150.md): Frame · corroded · Dec 23, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - CORROSION UNDER NUT PLATE ON FRAME 14755, 5 INCHES LEFT OF CENTERLINE. REPAIRED IAW HORIZON AIR EA 4-53-1536 AND FOKKER SRM 53-02-12.
- [SDR QXEA0102162](https://openairdocs.org/sdr/QXEA0102162.md): Structure · leaking · Dec 21, 2001 · N488US · Fokker F28MK4000 · Wing Main, Frame Structure
  > PDX - FUEL LEAK ON LT WING LOWER SKIN AT STATION 2635 AND STRINGER 2.9 JUST AFT AND OUTBOARD OF FUEL PANEL 71A. REPAIRED IAW FOKKER MM 28-11-06, PAGE 403.
- [SDR QXEA0102160](https://openairdocs.org/sdr/QXEA0102160.md): Panel · cracked · Dec 20, 2001 · N488US · Fokker F28MK4000 · Wing, Plate/Skin
  > PDX - CRACK IN SKIN OF RT STUBWING LOWER AFT PANEL. REPAIRED IAW FOKKER SRM 54-02-03, PAGE 4, FIGURE 2 AND SRM 51-31-05, PAGE 8, PARAGRAPH 7.
- [SDR QXEA0102158](https://openairdocs.org/sdr/QXEA0102158.md): Angle · cracked · Dec 20, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - REAR PRESSURE BULKHEAD FORWARD SIDE FRAME 17065 RT SIDE ANGLE TO FUSELAGE SKIN HAS CRACK IN RADIUS FROM STRINGER 54 TO 55. REPAIRED IAW HORIZON AIR EA 4-53-1150 AND FOKKER SRM 53-02-18.
- [SDR QXEA0102157](https://openairdocs.org/sdr/QXEA0102157.md): Beam · cracked · Dec 20, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - REAR PRESSURE BULKHEAD FORWARD SIDE FRAME 17065, BEAM 3 HAS TWO CRACKS IN RADIUS AT RT MOST OUTBOARD EDGE ON TOP SIDE. REPAIRED IAW FOKKER SRM 53-02-18, PAGE 38, FIGURE 13.
- [SDR QXEA0102149](https://openairdocs.org/sdr/QXEA0102149.md): Seat Track · corroded · Dec 19, 2001 · N488US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - CORROSION ON SEAT RAIL UPPER SURFACE ABOVE FRAME 4610, BL1127 RT. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205, SRM 53-02-15 AND SRM 53-31-01.
- [SDR QXEA0102148](https://openairdocs.org/sdr/QXEA0102148.md): Bracket · cracked · Dec 19, 2001 · N488US · Fokker F28MK4000 · Trailing Edge Flaps
  > PDX - INBOARD FLAP SHROUD DOOR ROLLER BRACKET ON OUTBOARD FLAP IS CRACKED IN RADIUS JUST BELOW MOUNT BOLTS. REPAIRED IAW FOKKER MM 27-50-6, PAGE 501-502, PARAGRAPH 3A.
- [SDR QXEA0102156](https://openairdocs.org/sdr/QXEA0102156.md): Frame · chafed · Dec 19, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - REAR PRESSURE BULKHEAD FORWARD SIDE FRAME 17065 HAS A.25 INCH CIRCULAR CHAFE INBOARD OF SKIN SPLICE AT BL LH425. REPAIRED IAW HORIZON AIR EA 4-53-154.
- [SDR QXEA0102127](https://openairdocs.org/sdr/QXEA0102127.md): Skin · corroded · Dec 18, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX - LOWER FORWARD VHF ANTENNA MOUNT AREA ON FUSELAGE SKIN CORRODED. REPAIRED IAW HORIZON AIR EA 4-53-1539 AND FOKKER SRM 53-10-4.
- [SDR QXEA0102159](https://openairdocs.org/sdr/QXEA0102159.md): Channel · cracked · Dec 18, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - LAVATORY AFT WALL VERTICAL SUPPORT CHANNEL THAT IS RIVETED TO REAR PRESSURE BULKHEAD FRAME 17065 IS CRACKED AROUND TWO RIVETS. REPAIRED IAW FOKKER SRM 53-01-00, PAGE 3, PARAGRAPH 3C AND SRM 51-31-01, PAGES 1 THRU 17.
- [SDR QXEA0102161](https://openairdocs.org/sdr/QXEA0102161.md): Skin · corroded · Dec 17, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX - CORROSION AT LOWER FORWARD VHF ANTENNA MOUNT AREA ON FUSELAGE SKIN. REPAIRED IAW HORIZON AIR EA 4-53-1539 AND FOKKER SRM 51-31-01.
- [SDR QXEA0102152](https://openairdocs.org/sdr/QXEA0102152.md): Structure · cracked · Dec 17, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - CRACK AT AFT SIDE OF NOSE WHEEL, 1 INCH FORWARD OF FRAME 4175 AND 2 INCHES ABOVE STRINGER 1. REPAIRED IAW HORIZON AIR EA 4-53-1544.
- [SDR QXEA0102126](https://openairdocs.org/sdr/QXEA0102126.md): Skin · dented · Dec 14, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX - ACCESS DOOR 21A OPENING STRUCTURE HAS DENTS AND SCRATCHES AT SLOTTED GUIDE PIN HOLE, STATION 1890 AND STRINGER 73. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 51-10-4.
- [SDR QXEA0102119](https://openairdocs.org/sdr/QXEA0102119.md): Seat Track · corroded · Dec 14, 2001 · N488US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - RT INBOARD SEAT TRACK CORRODED AT STATION 5060-5090. REPAIRED IAW FOKKER SRM 53-01-01 AND HORIZON AIR EA 4-53-1546.
- [SDR QXEA0102094](https://openairdocs.org/sdr/QXEA0102094.md): Bracket · cracked · Dec 14, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY.75 INCH IN LENGTH AT FRAME 17565 AND STRINGER 8. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-02-13.
- [SDR QXEA0102091](https://openairdocs.org/sdr/QXEA0102091.md): Bracket · cracked · Dec 14, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY.5 INCH IN LENGTH AT FRAME 50-2 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-10-05 AND SRM 51-31-01.
- [SDR QXEA0102090](https://openairdocs.org/sdr/QXEA0102090.md): Bracket · cracked · Dec 14, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY 1 INCH IN LENGTH AT FRAME 50-2 AND STRINGER 27. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 9.
- [SDR QXEA0102111](https://openairdocs.org/sdr/QXEA0102111.md): Fitting · damaged · Dec 14, 2001 · N488US · Fokker F28MK4000 · Horizontal Stabilizer Structure
  > PDX - HORIZONTAL STABILIZER JUNCTION FITTING, LT UPPER LUG HAS PITTING ON LUG. REPAIRED IAW HORIZON AIR EA 4-55-300 AND FOKKER SRM 55-01-01, PAGE 3, PARAGRAPH 3E, STEP 5.
- [SDR QXEA0102110](https://openairdocs.org/sdr/QXEA0102110.md): Fitting · damaged · Dec 14, 2001 · N488US · Fokker F28MK4000 · Horizontal Stabilizer Structure
  > PDX - HORIZONTAL STABILIZER JUNCTION FITTING, LT LOWER LUG HAS PITTING ON LUG. REPAIRED IAW HORIZON AIR EA 4-55-300 AND FOKKER SRM 55-01-01, PAGE 3, PARAGRAPH 3E, STEP 5.
- [SDR QXEA0102109](https://openairdocs.org/sdr/QXEA0102109.md): Fitting · damaged · Dec 14, 2001 · N488US · Fokker F28MK4000 · Horizontal Stabilizer Structure
  > PDX - HORIZONTAL STABILIZER JUNCTION FITTING, RT LUG HAS PITTING ON LUG. REPAIRED IAW HORIZON AIR EA 4-55-300 AND FOKKER SRM 55-01-01, PAGE 3, PARAGRAPH 3E STEP 5.
- [SDR QXEA0102108](https://openairdocs.org/sdr/QXEA0102108.md): Fitting · damaged · Dec 14, 2001 · N488US · Fokker F28MK4000 · Horizontal Stabilizer Structure
  > PDX - HORIZONTAL STABILIZER JUNCTION FITTING, RT LUG HAS PITTING ON LUG. REPAIRED IAW HORIZON AIR EA 4-55-300 AND FOKKER SRM 55-01-01, PAGE 3, PARAGRAPH 3E, STEP 5.
- [SDR QXEA0102103](https://openairdocs.org/sdr/QXEA0102103.md): Clip · cracked · Dec 14, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - FRAME CLIP CRACKED AT FRAME 7305 AND STRINGER 65. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4.
- [SDR QXEA0102080](https://openairdocs.org/sdr/QXEA0102080.md): Structure · cracked · Dec 14, 2001 · N488US · Fokker F28MK4000 · Wing Main, Frame Structure
  > PDX - SUSPECTED CRACK IN WING STRUCTURE RADIATING FROM LOWER SMALL BOLT LOCATED OUTBOARD OF RIGHT MAIN LANDING GEAR AFT TRUNNION POINT AT WS 117.165. REPAIRED IAW FOKKER SRM 51-35-02, PARAGRAPH 2 C (3), PAGE 2 AND SRM 57-02-09, PAGE 2, PARAGRAPH 3.
- [SDR QXEA0102147](https://openairdocs.org/sdr/QXEA0102147.md): Seat Track · corroded · Dec 13, 2001 · N488US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - RT OUTBOARD SEAT TRACK HAS FRETTING CORROSION BETWEEN STATION 4950 AND 4980. REPAIRED IAW HORIZON AIR EA 4-53-1541 AND FOKKER SRM 53-01-01.
- [SDR QXEA0102145](https://openairdocs.org/sdr/QXEA0102145.md): Skin · corroded · Dec 13, 2001 · N488US · Fokker F28MK4000 · Wing, Plate/Skin
  > PDX - RT FUEL PANEL 74E APERTURE HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-14-01, PAGE 16.
- [SDR QXEA0102144](https://openairdocs.org/sdr/QXEA0102144.md): Skin · corroded · Dec 13, 2001 · N488US · Fokker F28MK4000 · Wing, Plate/Skin
  > PDX - RT WING FUEL PANEL 74F APERTURE HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-14-01, PAGE 16, FIGURE 03.
- [SDR QXEA0102124](https://openairdocs.org/sdr/QXEA0102124.md): Stringer · corroded · Dec 13, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Longeron/Stringer
  > PDX - CORROSION ON STRINGER 73 BELOW FRAME 9305B. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 51-10-4.
- [SDR QXEA0102123](https://openairdocs.org/sdr/QXEA0102123.md): Frame · corroded · Dec 13, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - CORROSION AT NUT PLATES BELOW CROSS TIE AT FRAME 9305 AND STRINGER 74. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, SRM 51-32-02 AND SRM 51-10-4.
- [SDR QXEA0102120](https://openairdocs.org/sdr/QXEA0102120.md): Angle · cracked · Dec 13, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - ANGLE BRACKET AT CRACKED AT STATION 1700 ON AIRCRAFT STRUCTURE JUST UNDER INBOARD FLAP FAIRING DOOR. REPAIRED IAW FOKKER SRM 53-02-01 FIGURE 6.
- [SDR QXEA0102118](https://openairdocs.org/sdr/QXEA0102118.md): Seat Track · corroded · Dec 13, 2001 · N488US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - RT INBOARD SEAT TRACK PITTING CORROSION AT STATION 7805. REPAIRED IAW FOKKER SRM 53-01-01 AND HORIZON AIR EA 4-53-1542.
- [SDR QXEA0102168](https://openairdocs.org/sdr/QXEA0102168.md): Skin · corroded · Dec 13, 2001 · N488US · Fokker F28MK4000 · Wing, Plate/Skin
  > PDX - RT WING FUEL PANEL 74G APERTURE HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-01-01, PARAGRAPH 4B AND SRM 57-14-01, PAGE 16.
- [SDR QXEA0102097](https://openairdocs.org/sdr/QXEA0102097.md): Bracket · cracked · Dec 13, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY.5 INCH IN LENGTH AT FRAME 17565 AND BETWEEN STRINGER 52 AND 53. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5.
- [SDR QXEA0102096](https://openairdocs.org/sdr/QXEA0102096.md): Bracket · cracked · Dec 13, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY 0.5 INCH IN LENGTH AT FRAME 17565 AND STRINGER 51. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5.
- [SDR QXEA0102095](https://openairdocs.org/sdr/QXEA0102095.md): Bracket · cracked · Dec 13, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY 1.125 INCH AT FRAME 17565, BETWEEN STRINGER 22 AND 23. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B AND C, AND SRM 51-31-01.
- [SDR QXEA0102093](https://openairdocs.org/sdr/QXEA0102093.md): Bracket · cracked · Dec 13, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY.75 INCH IN LENGTH AT FRAME 32-2 AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND 53-10-5, PAGE 601.
- [SDR QXEA0102092](https://openairdocs.org/sdr/QXEA0102092.md): Bracket · cracked · Dec 13, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - FRAME TO SKIN CONNECTION ANGLE BRACKET CRACKED APPROXIMATELY.75 INCH IN LENGTH AT FRAME 32-2 AND STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-10-5, PAGE 601.
- [SDR QXEA0102106](https://openairdocs.org/sdr/QXEA0102106.md): Rivet · loose · Dec 13, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX - FORWARD FUSELAGE SKIN BETWEEN FRAMES 4175 AND 4610 ON STRINGER 68 HAS LOOSE RIVETS. REPAIRED IAW FOKKER SRM 51-31-01.
- [SDR QXEA0102084](https://openairdocs.org/sdr/QXEA0102084.md): Frame · cracked · Dec 13, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - CASTELLATION ON AFT SIDE OF FRAME 13815A BETWEEN STRINGERS 72 AND 73 IS CRACKED ALONG RIVET LINE. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.
- [SDR QXEA0102083](https://openairdocs.org/sdr/QXEA0102083.md): Frame · cracked · Dec 13, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - CASTELLATION ON AFT SIDE OF FRAME 13815A BETWEEN STRINGERS 3 AND 2 HAS A CRACK IN THE RADIUS AND A CRACK FROM RIVET WITH WASHER. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.
- [SDR QXEA0102125](https://openairdocs.org/sdr/QXEA0102125.md): Frame · corroded · Dec 12, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - CORROSION ON FRAME BELOW NUT PLATES, FRAME 9305B AND STRINGER 74. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 51-10-4.
- [SDR QXEA0102122](https://openairdocs.org/sdr/QXEA0102122.md): Clip · corroded · Dec 12, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - CORROSION ON AFT CLIP FOR DATO PANEL ON LT FORWARD OVERWING EXIT LOWER APERTURE. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 6, PARAGRAPH 4B AND SRM 51-31-05.
- [SDR QXEA0102121](https://openairdocs.org/sdr/QXEA0102121.md): Clip · corroded · Dec 12, 2001 · N488US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - CORROSION ON FORWARD CLIP FOR DATO PANEL ON LT AFT OVERWING EXIT LOWER APERTURE. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 6, PARAGRAPH 4B AND SRM 51-31-05.
- [SDR QXEA0102117](https://openairdocs.org/sdr/QXEA0102117.md): Shear Tie · cracked · Dec 12, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Structure
  > PDX - FUSELAGE FRAME 16060 TIE-IN CLIP TO SKIN IS CRACKED THROUGH RIVET HOLE AT STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.
- [SDR QXEA0102116](https://openairdocs.org/sdr/QXEA0102116.md): Shear Tie · cracked · Dec 12, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Structure
  > PDX - FUSELAGE FRAME 16660 TIE-IN CLIP TO SKIN IS CRACKED THROUGH RIVET HOLE AT STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.
- [SDR QXEA0102115](https://openairdocs.org/sdr/QXEA0102115.md): Shear Tie · cracked · Dec 12, 2001 · N488US · Fokker F28MK4000 · Fuselage Main, Structure
  > PDX - FUSELAGE FRAME 16660 TIE-IN CLIP TO SKIN IS CRACKED THROUGH RIVET HOLE AT STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51/31/01.
- [SDR QXEA0102167](https://openairdocs.org/sdr/QXEA0102167.md): Skin · corroded · Dec 12, 2001 · N488US · Fokker F28MK4000 · Wing, Plate/Skin
  > PDX - RT WING FUEL PANEL 74B APERTURE HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-13-01 AND 57-01-01, PAGE 5.

Next page: https://openairdocs.org/deregistered/N488US-2002-05-17/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 = 'N488US' AND deregistration_id = 'N488US-2002-05-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N488US-2002-05-17/reports

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