# N482US: 1985 Fokker F.28 MK4000, registration cancelled 2002-03-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 1, 2002
- Exported to: South Africa
- Status when cancelled: Valid registration
- Airframe: [Fokker F.28 MK4000](https://openairdocs.org/model/fokker-f-28-mk4000) (registry code 4990810)
- Serial number: 11231
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Certificate issued: December 17, 1999
- Last registry action: December 17, 1999
- Mode S code: A5F1DA
- Owner when cancelled: [First Union National Bank Trustee](https://openairdocs.org/faa-owner/FIRST%20UNION%20NATIONAL%20BANK%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N482US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=482US
- Page: https://openairdocs.org/deregistered/N482US-2002-03-01

From the FAA registry file of October 28, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Fokker F.28 MK4000: https://openairdocs.org/model/fokker-f-28-mk4000.md

## Service difficulty reports (433, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR QXEA0102018](https://openairdocs.org/sdr/QXEA0102018), Nov 29, 2001: RIVET. MISSING. 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), Nov 28, 2001: ANGLE. DAMAGED. 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), Nov 28, 2001: RIVET. LOOSE. 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), Nov 28, 2001: RIVET. LOOSE. 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), Nov 27, 2001: SHIM. DAMAGED. 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), Nov 24, 2001: FLOORBEAM. CRACKED. 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
- [SDR QXEA0102006](https://openairdocs.org/sdr/QXEA0102006), Nov 20, 2001: STRUCTURE. CHAFED. 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), Nov 20, 2001: SHEAR TIE. CORRODED. 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. 
- [SDR QXEA0101974](https://openairdocs.org/sdr/QXEA0101974), Nov 20, 2001: SHEAR TIE. CORRODED. 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), Nov 20, 2001: SHEAR TIE. CORRODED. 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), Nov 20, 2001: SKIN. CORRODED. 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, PA
- [SDR QXEA0101973](https://openairdocs.org/sdr/QXEA0101973), Nov 20, 2001: FRAME. CORRODED. 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), Nov 20, 2001: DOUBLER. CORRODED. 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 
- [SDR QXEA0101971](https://openairdocs.org/sdr/QXEA0101971), Nov 20, 2001: SHEAR TIE. CORRODED. 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,
- [SDR QXEA0101970](https://openairdocs.org/sdr/QXEA0101970), Nov 20, 2001: SHEAR TIE. CORRODED. 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,
- [SDR QXEA0101969](https://openairdocs.org/sdr/QXEA0101969), Nov 20, 2001: SKIN. CORRODED. 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), Nov 20, 2001: STRINGER. CORRODED. 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), Nov 20, 2001: SHEAR TIE. CORRODED. 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, PAG
- [SDR QXEA0101966](https://openairdocs.org/sdr/QXEA0101966), Nov 20, 2001: SHEAR TIE. CORRODED. 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 53-02-1
- [SDR QXEA0102008](https://openairdocs.org/sdr/QXEA0102008), Nov 19, 2001: DOUBLER. CHAFED. 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), Nov 19, 2001: FRAME. CRACKED. 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), Nov 19, 2001: FRAME. CRACKED. 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), Nov 18, 2001: CLIP. CRACKED. 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, SR
- [SDR QXEA0101993](https://openairdocs.org/sdr/QXEA0101993), Nov 18, 2001: FRAME. CRACKED. 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), Nov 18, 2001: SEAT TRACK. CORRODED. 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), Nov 18, 2001: SEAT TRACK. CORRODED. 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), Nov 18, 2001: SEAT TRACK. CORRODED. 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), Nov 18, 2001: SEAT TRACK. CORRODED. 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), Nov 18, 2001: SEAT TRACK. CORRODED. 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), Nov 18, 2001: SEAT TRACK. CORRODED. 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), Nov 18, 2001: FLOORBEAM. CORRODED. 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), Nov 18, 2001: STRINGER. CHAFED. 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), Nov 17, 2001: SEAT TRACK. CORRODED. 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
- [SDR QXEA0101997](https://openairdocs.org/sdr/QXEA0101997), Nov 16, 2001: SUPPORT. BENT. 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), Nov 15, 2001: STRUCTURE. DENTED. 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-
- [SDR QXEA0101999](https://openairdocs.org/sdr/QXEA0101999), Nov 15, 2001: RIB. CRACKED. 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), Nov 15, 2001: FRAME. CRACKED. 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), Nov 15, 2001: STRAP. CRACKED. PDX - SPEEDBRAKE ACCUMULATOR FORWARD MOUNT ASSEMBLY TOP FINGER STRAP CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.
- [SDR QXEA0101977](https://openairdocs.org/sdr/QXEA0101977), Nov 15, 2001: CLIP. CRACKED. 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), Nov 15, 2001: SKIN. CORRODED. 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
- [SDR QXEA0101947](https://openairdocs.org/sdr/QXEA0101947), Nov 15, 2001: FRAME. CRACKED. 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), Nov 15, 2001: FRAME. CRACKED. 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), Nov 15, 2001: FRAME. CRACKED. 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), Nov 15, 2001: FRAME. CRACKED. 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), Nov 15, 2001: DOUBLER. TORN. 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
- [SDR QXEA0101939](https://openairdocs.org/sdr/QXEA0101939), Nov 15, 2001: STRAP. DAMAGED. 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), Nov 15, 2001: VANE. CHAFED. 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-
- [SDR QXEA0101922](https://openairdocs.org/sdr/QXEA0101922), Nov 15, 2001: FRAME. CRACKED. 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), Nov 14, 2001: FRAME. CORRODED. 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), Nov 14, 2001: FRAME. CORRODED. 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

All 433: https://openairdocs.org/deregistered/N482US-2002-03-01/reports.md

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19960712021189I](https://openairdocs.org/incident/19960712021189I), Jul 12, 1996: Fokker F28MK4000 (N482US), Pittsburgh, PA, Minor damage. Narrative: on July 12, 1996, at 10:30 am, a usair F28MK4000, aircraft N482US, operating as flight 1606, attempted take-off at Pittsburgh international airport.…
- [Incident 19901024058829I](https://openairdocs.org/incident/19901024058829I), Oct 24, 1990: Fokker F28MK4000 (N482US), Columbia, SC. Left gear showed unsafe condition landed without incident.

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