# Service difficulty reports: N482US, cancelled Mar 1, 2002

A list on [N482US, cancelled Mar 1, 2002](https://openairdocs.org/deregistered/N482US-2002-03-01.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 9 · 433 reports

- [SDR QXEA0102018](https://openairdocs.org/sdr/QXEA0102018.md): Rivet · missing · Nov 29, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX - TWO RIVET HEADS MISSING ON FUSELAGE SKIN AT FRAME 16060 NEAR STRINGER 55. REPAIRED IAW FOKKER SRM 51-31-01.
- [SDR QXEA0102017](https://openairdocs.org/sdr/QXEA0102017.md): Angle · damaged · Nov 28, 2001 · N482US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - REMOVE DAMAGED LOWER THRESHOLD COAMING AND REPLACE WITH A34918-007. REPAIRED IAW HORIZON AIR EA 4-53-904A AND FOKKER MM 51-30-00, PAGE 701-706.
- [SDR QXEA0102015](https://openairdocs.org/sdr/QXEA0102015.md): Rivet · loose · Nov 28, 2001 · N482US · Fokker F28MK4000 · Vertical Stabilizer, Plate/Skin
  > PDX - VERTICAL STABILIZER SMOKING RIVETS LT SIDE JUST BELOW RIB 5 ON 50 PERCENT SPAR. REPAIRED IAW HORIZON AIR EA 4-55-299.
- [SDR QXEA0102014](https://openairdocs.org/sdr/QXEA0102014.md): Rivet · loose · Nov 28, 2001 · N482US · Fokker F28MK4000 · Vertical Stabilizer, Plate/Skin
  > PDX - VERTICAL STABILIZER SMOKING RIVET JUST BELOW RIB 5 ON 50 PERCENT SPAR RT SIDE. REPAIRED IAW HORIZON AIR EA 4-55-299.
- [SDR QXEA0102012](https://openairdocs.org/sdr/QXEA0102012.md): Shim · damaged · Nov 27, 2001 · N482US · Fokker F28MK4000 · Wing Miscellaneous Structure
  > PDX - LT WING FUEL ACCESS APERTURE 71A, SHIM HAS BEEN BLENDED COMPLETELY THROUGH AT SEVERAL SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-568.
- [SDR QXEA0102016](https://openairdocs.org/sdr/QXEA0102016.md): Floorbeam · cracked · Nov 24, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Floor Beam
  > PDX - FLOORBEAM CRACKED 9 INCHES AFT OF FRAME 3450 AND APPROXIMATELY 30 INCHES FROM SERVICE/EMERGENCY DOOR. REPAIRED IAW HORIZON AIR EA 4-53-1525 AND FOKKER SRM 53-02-14.
- [SDR QXEA0102006](https://openairdocs.org/sdr/QXEA0102006.md): Structure · chafed · Nov 20, 2001 · N482US · Fokker F28MK4000 · Wing Main, Frame Structure
  > PDX - STRUCTURE IS CHAFED AT LOWER ATTACH POINT FOR LT WING ROOT FAIRING 91J. REPAIRED IAW HORIZON AIR EA 4-57-569.
- [SDR QXEA0102005](https://openairdocs.org/sdr/QXEA0102005.md): Shear Tie · corroded · Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Structure
  > PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE IN TO BELLY SKIN BETWEEN STRINGER 1 AND 2 HAS CORROSION ON TOP SURFACE WITH POSSIBLE CRACK AT VERTICAL FLANGE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4 B AND C, PAGE 9.
- [SDR QXEA0101974](https://openairdocs.org/sdr/QXEA0101974.md): Shear Tie · corroded · Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Structure
  > PDX - ANGLED FRAME 15810 TIE IN CLIP TO FUSELAGE BELLY SKIN HAS CORROSION ON TOP SURFACE BETWEEN STRINGERS 73 AND 74. REPAIRED IAW FOKKER SRM 51-31-01.
- [SDR QXEA0101976](https://openairdocs.org/sdr/QXEA0101976.md): Shear Tie · corroded · Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Structure
  > PDX - FUSELAGE FRAME 15635 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND RIVETS BETWEEN STRINGER 73 AND 74. REPAIRED IAW FOKKER SRM 51-31-01.
- [SDR QXEA0101975](https://openairdocs.org/sdr/QXEA0101975.md): Skin · corroded · Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX - FUSELAGE INTERIOR BELLY SKIN HAS CORROSION AROUND (8) RIVETS BETWEEN FRAMES 15635 AND 15810, FROM STRINGER 73 AND 74. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9 AND SRM 51-31-01.
- [SDR QXEA0101973](https://openairdocs.org/sdr/QXEA0101973.md): Frame · corroded · Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - ANGLED FRAME 15810 HAS CORROSION ON FORWARD AND AFT SIDES AT CUTOUTS AROUND STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.
- [SDR QXEA0101972](https://openairdocs.org/sdr/QXEA0101972.md): Doubler · corroded · Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX - FUSELAGE INTERIOR BELLY SKIN DOUBLER HAS CORROSION AROUND (3) RIVETS AT AFT SIDE OF ANGLED FRAME 15810 BETWEEN STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 6.
- [SDR QXEA0101971](https://openairdocs.org/sdr/QXEA0101971.md): Shear Tie · corroded · Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Structure
  > PDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND (3) RIVETS BETWEEN STRINGERS 2 AND 3. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.
- [SDR QXEA0101970](https://openairdocs.org/sdr/QXEA0101970.md): Shear Tie · corroded · Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Structure
  > PDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND (3) RIVETS BETWEEN STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4.
- [SDR QXEA0101969](https://openairdocs.org/sdr/QXEA0101969.md): Skin · corroded · Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX - FUSELAGE INTERIOR BELLY SKIN AT AFT SIDE OF FRAME 16060 BETWEEN STRINGER 1 AND 2 HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.
- [SDR QXEA0101968](https://openairdocs.org/sdr/QXEA0101968.md): Stringer · corroded · Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Longeron/Stringer
  > PDX - FUSELAGE BELLY STRINGER 1 HAS CORROSION AT TIE IN CLIP AREA AFT SIDE OF FRAME 16060. REPAIRED IAW FOKKER SRM 51-10-01, 4B, C, PAGE 9.
- [SDR QXEA0101967](https://openairdocs.org/sdr/QXEA0101967.md): Shear Tie · corroded · Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Structure
  > PDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE ROUND RIVETS BETWEEN STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.
- [SDR QXEA0101966](https://openairdocs.org/sdr/QXEA0101966.md): Shear Tie · corroded · Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Structure
  > PDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND (3) RIVETS BETWEEN STRINGERS 73 AND 74. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4.
- [SDR QXEA0102008](https://openairdocs.org/sdr/QXEA0102008.md): Doubler · chafed · Nov 19, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - FRAME 11905 RT COLD SLEEVE REPAIR PLATE HAS 10/32 SCREW CHAFE DAMAGE AT.023 DEEP. REPAIRED IAW HORIZON AIR EA 4-53-1523.
- [SDR QXEA0101995](https://openairdocs.org/sdr/QXEA0101995.md): Frame · cracked · Nov 19, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - FRAME 22293 CRACKED APPROXIMATELY 1.5 INCH IN OUTBOARD RADIUS AT AFT END OF STRINGER 53A. REPAIRED IAW HORIZON AIR EA 4-53-1524.
- [SDR QXEA0101994](https://openairdocs.org/sdr/QXEA0101994.md): Frame · cracked · Nov 19, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - FRAME 22293 CRACKED APPROXIMATELY.5 INCH IN OUTBOARD RADIUS. REPAIRED IAW HORIZON AIR EA 4-53-1524.
- [SDR QXEA0102009](https://openairdocs.org/sdr/QXEA0102009.md): Clip · cracked · Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - CLIP CONNECTING LOWER WING TO FUSELAGE FAIRING SUPPORT AT FRAME 13815A AND CENTER RIB IS CRACKED. REPAIRED IAW FOKKER SRM 53-53-04, FIGURE 5, ITEM 190, SRM 51-30-01.
- [SDR QXEA0101993](https://openairdocs.org/sdr/QXEA0101993.md): Frame · cracked · Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - FRAME 22293 CRACKED APPROXIMATELY 1.25 INCH IN OUTBOARD RADIUS AT AFT END OF STRINGER 21A. REPAIRED IAW HORIZON AIR EA 4-53-1524.
- [SDR QXEA0101985](https://openairdocs.org/sdr/QXEA0101985.md): Seat Track · corroded · Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - RT INBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 306 - 327. REPAIRED IAW HORIZON AIR EA 4-53-1527.
- [SDR QXEA0101984](https://openairdocs.org/sdr/QXEA0101984.md): Seat Track · corroded · Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - RT INBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 340-404. REPAIRED IAW HORIZON AIR EA 4-53-1527.
- [SDR QXEA0101983](https://openairdocs.org/sdr/QXEA0101983.md): Seat Track · corroded · Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - RT INBOARD SEAT TRACK IS PITTED ON INBOARD FLANGE AT APPROXIMATELY STATION 676 - 685. REPAIRED IAW HORIZON AIR EA 4-53-1527.
- [SDR QXEA0101982](https://openairdocs.org/sdr/QXEA0101982.md): Seat Track · corroded · Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - RT OUTBOARD SEAT TRACK HAS THREE PITS ON OUTBOARD FLANGE AT APPROXIMATELY STATION 232 - 234. REPAIRED IAW HORIZON AIR EA 4-53-1528.
- [SDR QXEA0101981](https://openairdocs.org/sdr/QXEA0101981.md): Seat Track · corroded · Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON OUTBOARD FLANGE AT APPROXIMATELY STATION 325 - 327. REPAIRED IAW HORIZON AIR EA 4-53-1528.
- [SDR QXEA0101980](https://openairdocs.org/sdr/QXEA0101980.md): Seat Track · corroded · Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 349 - 357. REPAIRED IAW HORIZON AIR EA 4-53-1528.
- [SDR QXEA0101979](https://openairdocs.org/sdr/QXEA0101979.md): Floorbeam · corroded · Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Floor Beam
  > PDX - FLOORBEAM REPAIR BL 0 JUST FORWARD OF FRAME 4900 TOP TIE PLATE HAS LIGHT CORROSION. REPAIRED IAW HORIZON AIR EA 4-53-1526.
- [SDR QXEA0101917](https://openairdocs.org/sdr/QXEA0101917.md): Stringer · chafed · Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Longeron/Stringer
  > PDX - CLIP ON CASTELLATION, FRONT SIDE OF FRAME 50-2 IS CHAFING INTO STRINGER 27. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, PARAGRAPH 3E AND SRM 51-10-4.
- [SDR QXEA0101915](https://openairdocs.org/sdr/QXEA0101915.md): Seat Track · corroded · Nov 17, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - RT INBOARD SEAT TRACK HAS LIGHT CORROSION ON OUTBOARD FLANGE AT APPROXIMATELY STATION 180.5 TO 191. REPAIRED IAW FOKKER SRM 51-31-01, SRM 51-11-4, AND SRM 51-30-02.
- [SDR QXEA0101997](https://openairdocs.org/sdr/QXEA0101997.md): Support · bent · Nov 16, 2001 · N482US · Fokker F28MK4000 · Aerodynamic Fairings
  > PDX - BENT FAIRING SUPPORT STRUCTURE IS BENT. REPAIRED IAW FOKKER SRM 53-53-11, PAGE 35, ITEM 265, SRM 51-10-4, PARAGRAPH 4 B AND C.
- [SDR QXEA0102003](https://openairdocs.org/sdr/QXEA0102003.md): Structure · dented · Nov 15, 2001 · N482US · Fokker F28MK4000 · Cargo/Baggage Doors
  > PDX - DENT 1.8 INCH LONG, 1.2 INCH WIDE, APPROXIMATELY.10 INCH DEEP ON TOP EDGE OF CENTER CARGO DOOR, 15INCHES AFT OF LEADING EDGE OF DOOR. REPAIRED IAW MM 51-00-00, PAGE 1 AND MM 51-30-02.
- [SDR QXEA0101999](https://openairdocs.org/sdr/QXEA0101999.md): Rib · cracked · Nov 15, 2001 · N482US · Fokker F28MK4000 · Horizontal Stabilizer, Spar/Rib
  > PDX - HORIZONTAL STABILIZER LEADING EDGE 51B THIRD RIB FROM INBOARD END CRACK TOP FORWARD. REPAIRED IAW FOKKER SRM 51-10-4, SRM 51-31-01, PAGE 13, PARAGRAPH 7B.
- [SDR QXEA0101991](https://openairdocs.org/sdr/QXEA0101991.md): Frame · cracked · Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - CASTELLATION CRACKED AT LOWER RIVET ON FRAME 20075 ABOVE STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3, SRM 51-31-01 AND SRM 53-10-05.
- [SDR QXEA0101990](https://openairdocs.org/sdr/QXEA0101990.md): Strap · cracked · Nov 15, 2001 · N482US · Fokker F28MK4000 · Spoilers
  > PDX - SPEEDBRAKE ACCUMULATOR FORWARD MOUNT ASSEMBLY TOP FINGER STRAP CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.
- [SDR QXEA0101977](https://openairdocs.org/sdr/QXEA0101977.md): Clip · cracked · Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - FRAME 16660 CLIP CRACKED AT INBOARD END IN RADIUS. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4.
- [SDR QXEA0101952](https://openairdocs.org/sdr/QXEA0101952.md): Skin · corroded · Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX - CORROSION ON FUSELAGE SKIN CUTOUT NEXT TO RIVETS AND NUT PLATES WHERE AFT BLANKING PLATE ATTACHES FOR RADIO ALTIMETER ANTENNA. REPAIRED IAW HORIZON AIR EA 4-53-1521.
- [SDR QXEA0101947](https://openairdocs.org/sdr/QXEA0101947.md): Frame · cracked · Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 4 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
- [SDR QXEA0101946](https://openairdocs.org/sdr/QXEA0101946.md): Frame · cracked · Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 5 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
- [SDR QXEA0101945](https://openairdocs.org/sdr/QXEA0101945.md): Frame · cracked · Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 6 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
- [SDR QXEA0101944](https://openairdocs.org/sdr/QXEA0101944.md): Frame · cracked · Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - AFT CARGO BAY FRAME 14755 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 70 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
- [SDR QXEA0101940](https://openairdocs.org/sdr/QXEA0101940.md): Doubler · torn · Nov 15, 2001 · N482US · Fokker F28MK4000 · Cargo/Baggage Doors
  > PDX - BOTTOM TRAILING CORNER OF REPAIR DOUBLER TORN, CENTER CARGO DOOR INNER SKIN, 10 INCHES FORWARD OF TRAILING EDGE OF CENTER CARGO DOOR, ALONG BOTTOM OF DOOR. REPAIRED IAW HORIZON AIR EA 4-52-462 AND FOKKER MM 51-30-00 AND FOKKER SRM 51-31-01.
- [SDR QXEA0101939](https://openairdocs.org/sdr/QXEA0101939.md): Strap · damaged · Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX - THREE RIVETS PULLED THROUGH STRAP ON BELLY SKIN JUST AFT OF RT MAIN LANDING GEAR DOOR. REPAIRED IAW FOKKER SRM 51-31-05.
- [SDR QXEA0101938](https://openairdocs.org/sdr/QXEA0101938.md): Vane · chafed · Nov 15, 2001 · N482US · Fokker F28MK4000 · Trailing Edge Flaps
  > PDX - LT WING INBOARD, TRAILING EDGE FLAP, VANE, LEADING EDGE IS CHAFED AT OUTBOARD END. REPAIRED IAW FOKKER SRM 51-10-4, SRM 57-01-01, PAGE 3 AND FOKKER MM 51-30-00.
- [SDR QXEA0101922](https://openairdocs.org/sdr/QXEA0101922.md): Frame · cracked · Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - CASTELLATION AT TOP OF OBLIQUE FRAME 41-2 AT STRINGER 43 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 6, PAGE 8, SRM 51-10-4 AND 53-31-01.
- [SDR QXEA0102011](https://openairdocs.org/sdr/QXEA0102011.md): Frame · corroded · Nov 14, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - AFT CARGO BAY FRAME 14755 HAS CORROSION ON TOP SURFACE AND UNDER SIDE OF TOP FLANGE AT STRINGER 3. REPAIRED IAW FOKKER SRM 51-31-01.
- [SDR QXEA0102007](https://openairdocs.org/sdr/QXEA0102007.md): Frame · corroded · Nov 14, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
  > PDX - AFT CARGO BAY FRAME 14755 CORROSION TOP SURFACE AND UNDERSIDE OF TOP FLANGE AT STRINGER 72. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-04, PARAGRAPH 4 B AND C, PAGE 9.

Next page: https://openairdocs.org/deregistered/N482US-2002-03-01/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 = 'N482US' AND deregistration_id = 'N482US-2002-03-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N482US-2002-03-01/reports

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