# Service difficulty reports: N484US, cancelled Aug 14, 2002

A list on [N484US, cancelled Aug 14, 2002](https://openairdocs.org/deregistered/N484US-2002-08-14.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 7 · 317 reports

- [SDR QXEA011301](https://openairdocs.org/sdr/QXEA011301.md): Circuit Board · defective · Aug 2, 2001 · N484US · Fokker F28MK4000 · Emergency Lighting
  > SEA-TWO EACH EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED CIRCUIT BOARDS ON BOTH FORWARD EXIT SIGNS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0101176](https://openairdocs.org/sdr/QXEA0101176.md): Circuit Board · inoperative · Jul 11, 2001 · N484US · Fokker F28MK4000 · Emergency Lighting
  > GEG- EXIT SIGN AT ROW 8 INOP. MAINTENANCE REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100937](https://openairdocs.org/sdr/QXEA0100937.md): Sign · inoperative · Jun 5, 2001 · N484US · Fokker F28MK4000 · Emergency Lighting
  > PDX- FORWARD FACING CABIN OVERHEAD EXIT SIGN HAS BULBS INOP. REMOVED AND REPLACED EXIT SIGN WITH SERVICEABLE SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100629](https://openairdocs.org/sdr/QXEA0100629.md): Sign · inoperative · Apr 23, 2001 · N484US · Fokker F28MK4000 · Emergency Lighting
  > BOI-EMERGENCY EXIT SIGN IN AFT CABIN HAS BURNT OUT BULBS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100628](https://openairdocs.org/sdr/QXEA0100628.md): Sign · inoperative · Apr 23, 2001 · N484US · Fokker F28MK4000 · Emergency Lighting
  > BOI-EMERGENCY EXIT SIGN AT CABIN ENTRYWAY HAS BURNT OUT BULBS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100627](https://openairdocs.org/sdr/QXEA0100627.md): Sign · inoperative · Apr 23, 2001 · N484US · Fokker F28MK4000 · Emergency Lighting
  > BOI-EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR HAS BURNT OUT BULBS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100271](https://openairdocs.org/sdr/QXEA0100271.md): Bracket · broken · Mar 13, 2001 · N484US · Fokker F28MK4000 · Emergency Lighting
  > PDX - EMERGENCY LIGHT BRACKET AT ROW 8B WAS FOUND BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100263](https://openairdocs.org/sdr/QXEA0100263.md): Window Post · cracked · Mar 5, 2001 · N484US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX-TYPE 3 CRACK ON RIGHT HAND NR 2 WINDOW POST. PERFORMED STOP DRILL REPAIR. PERFORMED EDDIE CURRENT NDT. NO FURTHER DEFECTS NOTED. RII COMPLIED WITH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
- [SDR QXEA0100004](https://openairdocs.org/sdr/QXEA0100004.md): Sign · malfunctioned · Jan 4, 2001 · N484US · Fokker F28MK4000 · Emergency Lighting
  > SEA- EXIT LIGHT OVER ISLE MID CABIN FACING AFT IS DIM. REMOVED AND REPLACED MID CABIN AFT EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100003](https://openairdocs.org/sdr/QXEA0100003.md): Sign · malfunctioned · Jan 4, 2001 · N484US · Fokker F28MK4000 · Emergency Lighting
  > SEA- FORWARD EXIT LIGHT OVER COCKPIT DOOR IS DIM. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0003084](https://openairdocs.org/sdr/QXEA0003084.md): Light · inoperative · Nov 21, 2000 · N484US · Fokker F28MK4000 · Emergency Lighting
  > PDX- EXIT LIGHT NEAR FRONT OF CABIN INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT NEAR FRONT OF CABIN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0003051](https://openairdocs.org/sdr/QXEA0003051.md): Harness · damaged · Nov 17, 2000 · N484US · Fokker F28MK4000 · Emergency Lighting
  > PDX - EVACUATION PATH LIGHTING NEAR ROW 12, 13 AND 14 WAS FOUND INOPERATIVE. UPON INSPECTION, FOUND DAMAGED WIRING HARNESS ON SEAT 14AB. REMOVED AND REPLACED SEAT 14AB. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002885](https://openairdocs.org/sdr/QXEA0002885.md): Circuit Board · inoperative · Oct 18, 2000 · N484US · Fokker F28MK4000 · Emergency Lighting
  > FAT - CENTER OVERHEAD AISLE EMERGENCY LIGHTS REPORTED INOPERATIVE. FERRIED AIRCRAFT TO PDX. REMOVED AND REPLACED CIRCUIT BOARDS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002780](https://openairdocs.org/sdr/QXEA0002780.md): Brake · failed · Oct 2, 2000 · N484US · Fokker F28MK4000 · Landing Gear Brake System
  > BZN - DURING LANDING ROLL, LEFT BRAKE WAS INEFFECTIVE UNTILL FULL PEDAL DEFLECTION. PERFORMED SERVICE BLEED OF NR 2 BRAKE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002274](https://openairdocs.org/sdr/QXEA0002274.md): Battery Pack · inoperative · Aug 13, 2000 · N484US · Fokker F28MK4000 · Emergency Lighting
  > PDX - THE FLOOR PATH LIGHTING WAS FOUND INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002269](https://openairdocs.org/sdr/QXEA0002269.md): Skin · chafed · Aug 8, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX- LEFT HAND LOWER FUSELAGE SKIN IS CHAFED BY PANEL 91BD INBOARD EDGE BETWEEN FRAME 14775 AND 15205. REPAIRED IAW FOKKER SRM 53-01-01 PAGE3, 51-10-4 AND HORIZON AIR EA 4-53-1303.
- [SDR QXEA0002266](https://openairdocs.org/sdr/QXEA0002266.md): Skin · chafed · Aug 8, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX- RIGHT HAND LOWER FUSELAGE SKIN CHAFED BY INBOARD EDGE OF PANEL 92BD BETWEEN FRAME 14775 AND 15205. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 3, 51-10-4 AND HORIZON AIR EA 4-53-1305.
- [SDR QXEA0002265](https://openairdocs.org/sdr/QXEA0002265.md): Skin · chafed · Aug 8, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX- RIGHT HAND FUSELAGE SKIN CHAFED BY OUTBOARD EDGE OF PANEL 92BD BETWEEN FRAME 14775 AND 15205. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 3, 51-10-4 AND HORIZON AIR EA 4-53-1306.
- [SDR QXEA0002264](https://openairdocs.org/sdr/QXEA0002264.md): Skin · chafed · Aug 8, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX- PREVIOUS REPAIR ON RIGHT HAND LOWER FUSELAGE SKIN CHAFED BY PANEL 91BC. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 3, 51-10-4 AND HORIZON AIR EA 4-53-1304.
- [SDR QXEA0002272](https://openairdocs.org/sdr/QXEA0002272.md): Shear Tie · cracked · Aug 4, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Structure
  > PDX- OBLIQUE FRAME TO FUSELAGE SKIN ATTACH CLIP, AFT SIDE OF FRAME 24-2 AND STRINGER 33 HAS A CRACK IN RADIUS OF CLIP. RIVET INSTALLED IN CRACKED HOLE, NEEDS WASHER UNDER BUCK TAIL. REPAIRED IAW FOKKER SRM 51-31-01, 51-10-4 AND 53-02-13 PAGE 7.
- [SDR QXEA0002271](https://openairdocs.org/sdr/QXEA0002271.md): Skin · cracked · Aug 4, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX- AFT CARGO DOOR AFT TOP CORNER OF APERTURE SUSPECT CRACK GOING BEYOND STOP DRILL IN APERTURE. REPAIRED IAW FOKKER SRM 51-10-4 AND 53-01-01 PAGE 8.
- [SDR QXEA0002268](https://openairdocs.org/sdr/QXEA0002268.md): Skin · chafed · Aug 4, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX- LEFT HAND LOWER FUSELAGE SKIN REPAIR CHAFED BY PANEL 91BC LEFT OF CENTER BOTTOM FUSELAGE BETWEEN FRAME 14285 AND 14775. REPAIRED IAW FOKKER SRM 51-31-01, 51-10-4 AND 53-02-01.
- [SDR QXEA0002267](https://openairdocs.org/sdr/QXEA0002267.md): Skin · chafed · Aug 4, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX- PREVIOUS REPAIR ON BOTTOM CENTER OF FUSELAGE CHAFED BY PANEL 91BC FORWARD OF FRAME 14285. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-01.
- [SDR QXEA0002232](https://openairdocs.org/sdr/QXEA0002232.md): Clip · cracked · Aug 4, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- OBLIQUE FRAME TO FUSELAGE CLIP AFT OF FRAME 32-2 AT STRINGER 48 HAS A CRACK. REPAIRED IAW FOKKER SRM 53-10-05 PAGE 601 AND SRM 53-02-13, PAGE 5.
- [SDR QXEA0002229](https://openairdocs.org/sdr/QXEA0002229.md): Shear Tie · cracked · Aug 4, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Structure
  > PDX- OBLIQUE FRAME TO FUSELAGE SKIN ATTACH CLIP HAS A CRACK ON AFT SIDE OF FRAME 41-2, STRINGER 45. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601 AND SRM 51-31-01.
- [SDR QXEA0002198](https://openairdocs.org/sdr/QXEA0002198.md): Bracket · cracked · Aug 4, 2000 · N484US · Fokker F28MK4000 · Empennage Flight Control Surfaces, Attach Fittings
  > PDX- FUSELAGE BOTTOM PANEL 98F SUPPORTING BRACKET IS CRACKED AT STATION 16495. REPAIRED IAW FOKKER SRM 55-53-04, PAGE 9 AND SRM 51-31-01.
- [SDR QXEA0002197](https://openairdocs.org/sdr/QXEA0002197.md): Bracket · cracked · Aug 4, 2000 · N484US · Fokker F28MK4000 · Aerodynamic Fairings
  > PDX- FUSELAGE BOTTOM PANEL 98G SUPPORTING BRACKET IS CRACKED AT STATION 16495. REPAIRED IAW FOKKER SRM 53-53-04, PAGE 12 AND SRM 51-31-01.
- [SDR QXEA0002169](https://openairdocs.org/sdr/QXEA0002169.md): Skin · damaged · Aug 4, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX- STRAP PATCH ON BOTTOM OF FUSELAGE ON FRAME 14285 IS CHAFED LEFT AND RIGHT OF CENTER BY PANEL 91BC. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-01.
- [SDR QXEA0002244](https://openairdocs.org/sdr/QXEA0002244.md): Stiffener · bent · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 68 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.
- [SDR QXEA0002243](https://openairdocs.org/sdr/QXEA0002243.md): Stiffener · bent · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 64 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.
- [SDR QXEA0002242](https://openairdocs.org/sdr/QXEA0002242.md): Stiffener · bent · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 62 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.
- [SDR QXEA0002241](https://openairdocs.org/sdr/QXEA0002241.md): Stiffener · bent · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 60 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.
- [SDR QXEA0002240](https://openairdocs.org/sdr/QXEA0002240.md): Stiffener · bent · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 11 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.
- [SDR QXEA0002239](https://openairdocs.org/sdr/QXEA0002239.md): Stiffener · bent · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 18 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.
- [SDR QXEA0002238](https://openairdocs.org/sdr/QXEA0002238.md): Stiffener · bent · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 32-2 AT STRINGER 7 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.
- [SDR QXEA0002228](https://openairdocs.org/sdr/QXEA0002228.md): Angle · cracked · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- CONNECTION ANGLE FOR COMPOSITE ATTACHMENT TO FRAME 22293 UPPER RIGHT HAND CORNER IS CRACKED PAST STOP DRILL. REPAIRED IAW HORIZON AIR EA 4-53-1298.
- [SDR QXEA0002237](https://openairdocs.org/sdr/QXEA0002237.md): Stiffener · bent · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 16-2, BETWEN STRINGERS 70R AND 71 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.
- [SDR QXEA0002236](https://openairdocs.org/sdr/QXEA0002236.md): Stiffener · bent · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 16-2, BETWEEN STRINGERS 68 AND 69 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.
- [SDR QXEA0002235](https://openairdocs.org/sdr/QXEA0002235.md): Stiffener · bent · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 16-2, BETWEEN STRINGERS 66 AND 67 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.
- [SDR QXEA0002234](https://openairdocs.org/sdr/QXEA0002234.md): Stiffener · bent · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- STIFFENER ON FORWARD SIDE OF FRAME 16-2, BETWEEN STRINGERS 8 AND 9 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.
- [SDR QXEA0002233](https://openairdocs.org/sdr/QXEA0002233.md): Stiffener · bent · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 16-2, BETWEEN STRINGERS 6 AND 7 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.
- [SDR QXEA0002230](https://openairdocs.org/sdr/QXEA0002230.md): Stiffener · bent · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- STIFFENER ON FORWARD SIDE OF OBLIQUE FRAME 16-2 BETWEEN STRINGERS 4 AND 5 IS BENT. REPAIRED IAW HORIZON AIR EA 4-53-1297.
- [SDR QXEA0002223](https://openairdocs.org/sdr/QXEA0002223.md): Skin · cracked · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX- FUSELAGE SKIN CRACKED AT RIVET AT FRAME 50-2 BETWEEN STRINGERS 49 AND 50. REPAIRED IAW FOKKER SRM 53-02-02 AND HORIZON AIR EA 4-53-1294.
- [SDR QXEA0002177](https://openairdocs.org/sdr/QXEA0002177.md): Beam · cracked · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- CRACK UNDER 1ST CROSS TIE BEAM AT ENTRY WAY STRINGER 73. REPAIRED IAW FOKKER SRM 53-24-07, PAGE 8 AND SRM 51-31-01, AND SRM 51-31-05.
- [SDR QXEA0002168](https://openairdocs.org/sdr/QXEA0002168.md): Skin · scratched · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX- SCRATCH IN FUSELAGE SKIN BELOW BOTTOM AFT CORNER OF MAIN CABIN DOOR APERTURE. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 53-01-01, PAGE 3.
- [SDR QXEA0002164](https://openairdocs.org/sdr/QXEA0002164.md): Skin · scratched · Aug 3, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX- SCRATCH IN FUSELAGE SKIN BETWEEN FRAME 3820 AND 3450 BETWEEN STRINGER 18 AND 19. REPAIRED IAW FOKKER SRM 51-10-4 AND HORIZON AIR EA 4-53-1298.
- [SDR QXEA0002116](https://openairdocs.org/sdr/QXEA0002116.md): Skin · damaged · Aug 2, 2000 · N484US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX- MTX REQUEST INSTALLATION OF REINFORCMENT DOUBLERS ON FORWARD LOWER CORNER OF SERVICE EMERGENCY DOOR APERTURE. REPAIRED IAW FOKKER SRM 53-02-16 PAGE 12, 51-32-01 AND HORIZON AIR EA 4-53-1281.
- [SDR QXEA0002231](https://openairdocs.org/sdr/QXEA0002231.md): Clip · misdrilled · Aug 2, 2000 · N484US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX- OBLIQUE FRAME TO FUSELAGE SKIN ATTACH CLIP HAS A PREVIOUS STOP DRILL THAT IS DRILLED THRU STRINGER ANGLE AND INTO FUSELAGE SKIN AT FRAME 32-2 STRINGER 9. REPAIRED IAW FOKKER SRM 53-02-12 AND SRM 53-02-13.
- [SDR QXEA0002225](https://openairdocs.org/sdr/QXEA0002225.md): Fastener · loose · Aug 2, 2000 · N484US · Fokker F28MK4000 · Horizontal Stabilizer Structure
  > PDX- RIGHT VERTICAL CONNECTION ANGLE HAS LOOSE AND SMOKING HI-LOKS AND BUTTON HEAD RIVETS AT AFT SPAR. REPAIRED IAW FOKKER SRM 51-30-02 AND HORIZON AIR EA 4-55-247.
- [SDR QXEA0002220](https://openairdocs.org/sdr/QXEA0002220.md): Fastener · loose · Aug 2, 2000 · N484US · Fokker F28MK4000 · Horizontal Stabilizer Structure
  > PDX- LEFT VERTICAL CONNECTION ANGLE HAS LOOSE HI-LOKS AND BUTTON HEAD RIVETS AT AFT SPAR. REPAIRED IAW FOKKER SRM 51-30-02, SRM 51-31-01 AND HORIZON AIR EA 4-55-247.

Next page: https://openairdocs.org/deregistered/N484US-2002-08-14/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 = 'N484US' AND deregistration_id = 'N484US-2002-08-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N484US-2002-08-14/reports

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