# N481US: Fokker F.28 MK4000, registration cancelled 2002-02-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 27, 2002
- Exported to: Ecuador
- Status when cancelled: Valid registration
- Airframe: [Fokker F.28 MK4000](https://openairdocs.org/model/fokker-f-28-mk4000) (registry code 4990810)
- Serial number: 11230
- Type of aircraft: Fixed wing multi engine
- Certificate issued: February 14, 2002
- Last registry action: February 14, 2002
- Mode S code: A5EE23
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N481US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=481US
- Page: https://openairdocs.org/deregistered/N481US-2002-02-27

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 (258, newest 50)

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

- [SDR QXEA0101694](https://openairdocs.org/sdr/QXEA0101694), Oct 20, 2001: PRINTED CKT BOARD. DEFECTIVE. PDX - FORWARD EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR HAS BURNED OUT BULBS. REMOVED AND REPLACED FORWARD EMERGENCY EXIT SIGN LAMP CARD. OPERATIONAL CHECK IS GOOD
- [SDR QXEA0101379](https://openairdocs.org/sdr/QXEA0101379), Aug 27, 2001: SIGN. INOPERATIVE. BOI - EXIT SIGN AT CABIN ENTRANCE HAS BURNED OUT BULBS. REPLACED EXIT SIGN IAW F-28 MAINTENANCE MANUAL 33-50-00, PAGES 412-413. OPERATIONAL CHECK IS GOOD. AIRCR
- [SDR QXEA0100947](https://openairdocs.org/sdr/QXEA0100947), Jun 7, 2001: GUIDE. DAMAGED. YYC - LEFT-HAND STUBWING REAR GUIDE BLOCK IS WORN. REPLACED IAW HORIZON AIR EA 4-54-130, FOKKER FAX TS04.55321 AND FOKKER MM 54-10-02, PAGE 3.
- [SDR QXEA0100945](https://openairdocs.org/sdr/QXEA0100945), Jun 7, 2001: STRUCTURE. DAMAGED. YYC - RIGHT-HAND STUBWING TRAILING EDGE HAS PLAY. REPAIED IAW HORIZON AIR EA 4-54-130 AND FOKKER MM 54-10-02, PAGE 3.
- [SDR QXEA0101025](https://openairdocs.org/sdr/QXEA0101025), Jun 6, 2001: RIB. CRACKED. YYC - RIB 3.2 CRACKED ALONG AFT LEFT-HAND RADIUS. REPAIRED IAW HORIZON AIR EA 4-55-294.
- [SDR QXEA0100972](https://openairdocs.org/sdr/QXEA0100972), Jun 6, 2001: FRAME. CORRODED. YYC - CORROSION ON UNDERSIDE OF FRAME 13815B ABOVE STRINGER 74. REPAIRED IAW HORIZON AIR EA 4-53-1496.
- [SDR QXEA0101026](https://openairdocs.org/sdr/QXEA0101026), Jun 3, 2001: GUIDE. WORN. YYC - AILERON ANTI-UP FLOAT CABLE GUIDE A STATION 7306 WORN. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14.
- [SDR QXEA0101019](https://openairdocs.org/sdr/QXEA0101019), Jun 3, 2001: WEB. CANNING. YYC - FUSELAGE, TAIL SECTION, OBLIQUE FRAME 16-2 AT STRINGER 58-59 WEB OIL CANNING. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 11, FIGURE 9.
- [SDR QXEA0101009](https://openairdocs.org/sdr/QXEA0101009), Jun 3, 2001: FRAME. CRACKED. YYC - CRACK ON CASTELLATION PROGRESSING BEYOND STOP DRILL HOLE AT FRAME 50-2 BETWEEN STRINGER 48 AND 49. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM
- [SDR QXEA0100967](https://openairdocs.org/sdr/QXEA0100967), Jun 3, 2001: SKIN. CORRODED. YYC - FUSELAGE CORROSION UNDER FORWARD RADIO ALTIMETER BLANKING PLATE REBATES. REPAIRED IAW HORIZON AIR EA 4-53-1491 AND SRM 51-20-00, PARAGRAPH 3.
- [SDR QXEA0100965](https://openairdocs.org/sdr/QXEA0100965), Jun 3, 2001: SKIN. CORRODED. YYC - ANTENNA MOUNT CORROSION FOUND ON MOUNTING PLATE FUSELAGE REBATE FOR THIS FORWARD RADIO ALTIMETER ANTENNA. REPAIED IAW HORIZON AIR EA 4-53-1491 AND FOKKER 
- [SDR QXEA0100957](https://openairdocs.org/sdr/QXEA0100957), Jun 3, 2001: SKIN. CHAFED. YYC - FUSELAGE SKIN CHAFED BY TRAILING EDGE OF PANEL 91BC. REPAIRED AIW HORIZON AIR EA 4-53-1495.
- [SDR QXEA0101028](https://openairdocs.org/sdr/QXEA0101028), May 31, 2001: PANEL. DAMAGED. YYC - 16 FASTENERS PULLING THOURGH PANEL 91J. REPAIRED IAW HORIZON AIR EA 4-53-1493.
- [SDR QXEA0101024](https://openairdocs.org/sdr/QXEA0101024), May 31, 2001: STRUCTURE. DAMAGED. YYC - STRUCTURE CRACKED AT RIVET ON RIGHT HAND SIDE. REPAIRED IAW FOKKER SRM 55-02-07, FIGURE 2 AND CHAPTER 51.
- [SDR QXEA0101020](https://openairdocs.org/sdr/QXEA0101020), May 31, 2001: FITTING. GOUGED. YYC - HORIZONTAL STAB DRIVE FITTING LEFT-HAND ARM GOUGED. REPAIRED IAW HORIZON AIR EA 4-55-293.
- [SDR QXEA0101018](https://openairdocs.org/sdr/QXEA0101018), May 31, 2001: STRUCTURE. DAMAGED. YYC - FUSELAGE, TAIL SECTION, OBLIQUE FRAME 16-2 AT STRINGER 59-61, WEB, OIL CANNING. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 4, FIGURE 2, SRM 51-31-01, PARAGRAP
- [SDR QXEA0101005](https://openairdocs.org/sdr/QXEA0101005), May 31, 2001: HINGE. CORRODED. YYC - MAIN CABIN DOOR DIAPHRAGM INBOARD OF HINGE CORRODED. REPAIRED IAW FOKKER SRM 52-02-02 FIGURE 1, SHEET1, PAGES 2 AND 3.
- [SDR QXEA0100999](https://openairdocs.org/sdr/QXEA0100999), May 31, 2001: SEAT TRACK. CORRODED. YYC - SURFACE CORROSION FOUND ON SEAT TRACK BL1127R BETWEEN STATION 4175 AND 4900. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGE 13 AND 14.
- [SDR QXEA0100996](https://openairdocs.org/sdr/QXEA0100996), May 31, 2001: SEAT TRACK. CORRODED. YYC - SURFACE CORROSION FOUND ON SEAT TRACK BL600L BETWEEN STATIONS 3870 TO STATION 4900. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14.
- [SDR QXEA0100984](https://openairdocs.org/sdr/QXEA0100984), May 31, 2001: BULKHEAD. CANNING. YYC - REAR PRESSURE BULKHEAD FRONT SIDE AT BUTT LINE 1050L AND HORIZONTAL BEAM XI, SKIN IN OIL CANNED INWARDS. REPAIRED IAW HORIZON AIR EA 4-53-1492.
- [SDR QXEA0100983](https://openairdocs.org/sdr/QXEA0100983), May 31, 2001: HINGE. WORN. YYC - MAIN CABIN DOOR HINGE WORN. REPAIRED IAW MM 52-00-1, TABLE 803 ANDREPALCED IAW FOKKER SRM 52-02-02, FIGURE A.
- [SDR QXEA0100973](https://openairdocs.org/sdr/QXEA0100973), May 31, 2001: DOOR FRAME. CORRODED. YYC - LIGHT CORROSION AROUND MAIN CABIN DOOR HINGE FLANGE AREA ON AIRFRAME AROUND BOLT HOLES. REPAIED IAW FOKKER SRM 53-01-01, PARAGRAPH 4, AND SRM 51-10-4, PAR
- [SDR QXEA0101030](https://openairdocs.org/sdr/QXEA0101030), May 30, 2001: FLOORBEAM. CRACKED. YYC - CRACKED STIFFNER ON CENTER FLOORBEAM AT FRAME 12405 BELOW FLOOR PANEL 94AD. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14.
- [SDR QXEA0101016](https://openairdocs.org/sdr/QXEA0101016), May 30, 2001: FRAME. CRACKED. YYC - CRACKED CASTELLATION AT FRAME 16-2 AND STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31-02, PAGES 9 AND 10 AND SRM 51-31-01, PAR
- [SDR QXEA0101015](https://openairdocs.org/sdr/QXEA0101015), May 30, 2001: FRAME. CRACKED. YYC - CASTELLATION CRACK AT FRAME 17565 AND STRINGER 23. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31-02, PAGES 9 AND 10, SRM 51-31-01, PARAGRA
- [SDR QXEA0101013](https://openairdocs.org/sdr/QXEA0101013), May 30, 2001: FRAME. CRACKED. YYC - CRACKED CASTELLATION AT FRAME 16-2 AND STRINGER 25. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31-02, PAGE 9 AND 10, SRM 51-31-01, PARAGRA
- [SDR QXEA0101012](https://openairdocs.org/sdr/QXEA0101012), May 30, 2001: FRAME. CRACKED. YYC - CRACK PROGRESSING BEYOND STOP DRILL HOLE AT FRAME 50-2 AND STRINGER 53. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31-02, PAGE 9 AND 10, A
- [SDR QXEA0101011](https://openairdocs.org/sdr/QXEA0101011), May 30, 2001: FRAME. CRACKED. YYC - CRACK PROGRESSING BEYOND STOP DRILL HOLE AT FRAME 32-2 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31-02, PAGES 9 AND 10 A
- [SDR QXEA0101010](https://openairdocs.org/sdr/QXEA0101010), May 30, 2001: FRAME. CRACKED. YYC - CATEGORY B CRACK BEYOND LIMITS ON CASTELLATION AT FRAME 32-2 AND STRINGER 27. REPAIED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51-31-02, PAGES 9 AND
- [SDR QXEA0101008](https://openairdocs.org/sdr/QXEA0101008), May 30, 2001: FRAME. CRACKED. YYC - CASTELLATION ON OBLIQUE FRAME 50-2 HAS CRACK PROGRESSING BEYOND STOP DRILL HOLE AT STRINGER 25. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3, SRM 51
- [SDR QXEA0101007](https://openairdocs.org/sdr/QXEA0101007), May 30, 2001: FRAME. CRACKED. YYC - CRACK PROGRESSING BEYOND STOP DRILL HOLE ON CASTELLATION AT FRAME 32-2 AND STRINGER 48. REPAIRED IAW FOKKER SRM 51-31-02, PAGES 9 AND 10, SRM 53-02-13, PA
- [SDR QXEA0101003](https://openairdocs.org/sdr/QXEA0101003), May 30, 2001: SEAT TRACK. CRACKED. YYC - SEAT TRACK BL600L SUPPORT ANGLE CRACKED AT STATION 4610 OUTBOARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14.
- [SDR QXEA0100995](https://openairdocs.org/sdr/QXEA0100995), May 30, 2001: SEAT TRACK. CRACKED. YYC - SEAT TRACK BL600L SUPPORT ANGLE CRACKED AT STATION 4610 INBOARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14.
- [SDR QXEA0100993](https://openairdocs.org/sdr/QXEA0100993), May 30, 2001: SKIN. CORRODED. YYC - FUSELAGE CORROSION FOUND UNDER UPPER NAV/COMM ANTENNA BASE ON SKIN. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4, PAGE 9.
- [SDR QXEA0100992](https://openairdocs.org/sdr/QXEA0100992), May 30, 2001: SKIN. CORRODED. YYC - FUSELAGE CORROSION FOUND UNDER UPPER ATC ANTENNA ON SKIN. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-4, PARAGRAPH 4, PAGE 9.
- [SDR QXEA0100971](https://openairdocs.org/sdr/QXEA0100971), May 30, 2001: BULKHEAD. DAMAGED. YYC - BEAM II REAR PRESSURE BULKHEAD RBL425 UPPER AND LOWER CONSOLES DAMAGED AND BEAM II LBL425 LOWER CONSOLE CRACKED. REPAIRED IAW FOKKER SRM 53-24-04, FIGURE 
- [SDR QXEA0100969](https://openairdocs.org/sdr/QXEA0100969), May 30, 2001: SKIN. CORRODED. YYC - FUSELAGE UPPER TCAS ANTENNA CORROSION FOUND ON SKIN. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-4, PARAGRAPH 4, PAGE 9.
- [SDR QXEA0100956](https://openairdocs.org/sdr/QXEA0100956), May 30, 2001: FRAME. CRACKED. YYC - CRACKED CASTELLATION ON FRAME 16660 REAR CARGO PIT, BETWEEN STRINGER 2 AND 3. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.
- [SDR QXEA0100954](https://openairdocs.org/sdr/QXEA0100954), May 30, 2001: FRAME. CRACKED. YYC - CRACKED CASTELLATION ON FRAME 16660 REAR CARGO PIT BETWEEN STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.
- [SDR QXEA0100953](https://openairdocs.org/sdr/QXEA0100953), May 30, 2001: BULKHEAD. CRACKED. YYC - REAR PRESSURE BULKHEAD, FORWARD SIDE, BEAM III, CRACKED IN UPPER ATTACH FLANGE RADIUS, BETWEEN BL425L AND BL425R. REPAIRED.
- [SDR QXEA0101023](https://openairdocs.org/sdr/QXEA0101023), May 29, 2001: SKIN. CHAFED. YYC - CHAFE DAMAGE ON NOSE OF RUDDER 8 INCHES BELOW MID HINGE OPENING. REPAIRED IAW FOKKER SRM 55-02-07, FIGURE 1.
- [SDR QXEA0101021](https://openairdocs.org/sdr/QXEA0101021), May 29, 2001: FITTING. CORRODED. YYC - HORIZONTAL STAB DRIVE FITTING RIGHT-HAND AND LEFT-HAND LOWER LUGS HAVE MINOR CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-292 AND FOKKER SRM 51-10-04, PARA
- [SDR QXEA0101017](https://openairdocs.org/sdr/QXEA0101017), May 29, 2001: ANGLE. OUT OF POSITION. YYC - STIFFENING ANGLE, AFT SIDE REAR PRESSURE BULKHEAD AT BUTT LINE 1050L AND HORIZONTAL BEAM INCORRECTLY POSITION BETWEEN BEAM 11 AND 10. REPOSITIONING OF ANG
- [SDR QXEA0101004](https://openairdocs.org/sdr/QXEA0101004), May 29, 2001: ANGLE. CRACKED. YYC - SEAT TRACK BL600L SUPPORT ANGLE CRACKED AT STATION 4175, INBOARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14.
- [SDR QXEA0101002](https://openairdocs.org/sdr/QXEA0101002), May 29, 2001: FRAME. MISREPAIRED. YYC - NON STANDARD REPAIR ON CASTELLATION FRAME 6805 AND STRINGERS 16 AND 17. REPAIRED IAW HORIZON AIR EA 4-53-1490 AND FOKKER SRM 53-15-04, FIGURE 11, ITEM 6SM
- [SDR QXEA0101001](https://openairdocs.org/sdr/QXEA0101001), May 29, 2001: FRAME. CRACKED. YYC - LEFT-HAND FUSELAGE FRAME 5805 AND STRINGER 15 CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-15-04, FIGURE 07, ITEM 240.
- [SDR QXEA0101000](https://openairdocs.org/sdr/QXEA0101000), May 29, 2001: FRAME. CRACKED. YYC - LEFT-HAND FUSELAGE FRAME 6305 AND STRINGER 18 CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-16-04, FIGURE 04, ITEM 200N.
- [SDR QXEA0100994](https://openairdocs.org/sdr/QXEA0100994), May 29, 2001: SEAT TRACK. CRACKED. YYC - SEAT TRACK BL600L SUPPORT ANGLE CRACKED AT STATION 4175, OUTBOARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14.
- [SDR QXEA0100982](https://openairdocs.org/sdr/QXEA0100982), May 29, 2001: FRAME. CRACKED. YYC - FUSELAGE LEFT-HAND, FRAME 5805, STRINGER 16, FRAME CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-15-04, FIGURE 07, ITEM 240.
- [SDR QXEA0100981](https://openairdocs.org/sdr/QXEA0100981), May 29, 2001: FRAME. CRACKED. YYC - FUSELAGE LEFT-HAND FRAME 5805, STRINGER 18, FRAME CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-16-04, FIGURE 04, ITEM 16AN.

All 258: https://openairdocs.org/deregistered/N481US-2002-02-27/reports.md

## FAA accident and incident reports (1)

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 19990320018519I](https://openairdocs.org/incident/19990320018519I), Mar 20, 1999: Fokker F28MK4000 (N481US), Moses Lake, WA. (-5) #2 Engine shutdown due vibration and rising tgt due lp turbine blade failure.

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