# N484US: 1986 Fokker F.28 MK4000, registration cancelled 2002-08-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 14, 2002
- Exported to: Indonesia
- Status when cancelled: Valid registration
- Airframe: [Fokker F.28 MK4000](https://openairdocs.org/model/fokker-f-28-mk4000) (registry code 4990810)
- Engine: [Rolls-Royce SPEY-555-15](https://openairdocs.org/engine/rolls-royce-spey-555-15) (registry code 54521)
- Data sheets: [TCDS E2EU](https://openairdocs.org/tcds/E2EU) (OpenAirDocs)
- Serial number: 11234
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Special flight permit
- Airworthiness date: June 3, 2001
- Certificate issued: June 5, 2002
- Last registry action: June 5, 2002
- Mode S code: A5F948
- Owner when cancelled: [Southern Cross Aviation Inc](https://openairdocs.org/faa-owner/SOUTHERN%20CROSS%20AVIATION%20INC)
- Location: [Camarillo, CA](https://openairdocs.org/faa-place/CA/Camarillo)
- Owner type: Corporation
- Owner's area on the map: 34.2279° N, 119.0796° W: Placed by OpenAirDocs at the center of ZIP code 93010, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N484US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=484US
- Page: https://openairdocs.org/deregistered/N484US-2002-08-14

From the FAA registry file of November 12, 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 (317, newest 50)

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

- [SDR QXEA011301](https://openairdocs.org/sdr/QXEA011301), Aug 2, 2001: CIRCUIT BOARD. DEFECTIVE. 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), Jul 11, 2001: CIRCUIT BOARD. INOPERATIVE. 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), Jun 5, 2001: SIGN. INOPERATIVE. PDX- FORWARD FACING CABIN OVERHEAD EXIT SIGN HAS BULBS INOP. REMOVED AND REPLACED EXIT SIGN WITH SERVICEABLE SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO
- [SDR QXEA0100629](https://openairdocs.org/sdr/QXEA0100629), Apr 23, 2001: SIGN. INOPERATIVE. 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), Apr 23, 2001: SIGN. INOPERATIVE. 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), Apr 23, 2001: SIGN. INOPERATIVE. 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), Mar 13, 2001: BRACKET. BROKEN. 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), Mar 5, 2001: WINDOW POST. CRACKED. 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. OPERATIO
- [SDR QXEA0100004](https://openairdocs.org/sdr/QXEA0100004), Jan 4, 2001: SIGN. MALFUNCTIONED. 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 SER
- [SDR QXEA0100003](https://openairdocs.org/sdr/QXEA0100003), Jan 4, 2001: SIGN. MALFUNCTIONED. 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), Nov 21, 2000: LIGHT. INOPERATIVE. 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), Nov 17, 2000: HARNESS. DAMAGED. 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 SE
- [SDR QXEA0002885](https://openairdocs.org/sdr/QXEA0002885), Oct 18, 2000: CIRCUIT BOARD. INOPERATIVE. FAT - CENTER OVERHEAD AISLE EMERGENCY LIGHTS REPORTED INOPERATIVE. FERRIED AIRCRAFT TO PDX. REMOVED AND REPLACED CIRCUIT BOARDS. OPERATIONAL CHECKS GOOD. AIRCRA
- [SDR QXEA0002780](https://openairdocs.org/sdr/QXEA0002780), Oct 2, 2000: BRAKE. FAILED. BZN - DURING LANDING ROLL, LEFT BRAKE WAS INEFFECTIVE UNTILL FULL PEDAL DEFLECTION. PERFORMED SERVICE BLEED OF NR 2 BRAKE. OPERATIONAL CHECKS GOOD. AIRCRAFT RET
- [SDR QXEA0002274](https://openairdocs.org/sdr/QXEA0002274), Aug 13, 2000: BATTERY PACK. INOPERATIVE. 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), Aug 8, 2000: SKIN. CHAFED. 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 HORIZ
- [SDR QXEA0002266](https://openairdocs.org/sdr/QXEA0002266), Aug 8, 2000: SKIN. CHAFED. 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 HOR
- [SDR QXEA0002265](https://openairdocs.org/sdr/QXEA0002265), Aug 8, 2000: SKIN. CHAFED. 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 
- [SDR QXEA0002264](https://openairdocs.org/sdr/QXEA0002264), Aug 8, 2000: SKIN. CHAFED. 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), Aug 4, 2000: SHEAR TIE. CRACKED. 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 WA
- [SDR QXEA0002271](https://openairdocs.org/sdr/QXEA0002271), Aug 4, 2000: SKIN. CRACKED. 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), Aug 4, 2000: SKIN. CHAFED. 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, 5
- [SDR QXEA0002267](https://openairdocs.org/sdr/QXEA0002267), Aug 4, 2000: SKIN. CHAFED. 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), Aug 4, 2000: CLIP. CRACKED. 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), Aug 4, 2000: SHEAR TIE. CRACKED. 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), Aug 4, 2000: BRACKET. CRACKED. 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), Aug 4, 2000: BRACKET. CRACKED. 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), Aug 4, 2000: SKIN. DAMAGED. 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), Aug 3, 2000: STIFFENER. BENT. 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), Aug 3, 2000: STIFFENER. BENT. 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), Aug 3, 2000: STIFFENER. BENT. 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), Aug 3, 2000: STIFFENER. BENT. 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), Aug 3, 2000: STIFFENER. BENT. 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), Aug 3, 2000: STIFFENER. BENT. 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), Aug 3, 2000: STIFFENER. BENT. 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), Aug 3, 2000: ANGLE. CRACKED. 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), Aug 3, 2000: STIFFENER. BENT. 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), Aug 3, 2000: STIFFENER. BENT. 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), Aug 3, 2000: STIFFENER. BENT. 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), Aug 3, 2000: STIFFENER. BENT. 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), Aug 3, 2000: STIFFENER. BENT. 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), Aug 3, 2000: STIFFENER. BENT. 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), Aug 3, 2000: SKIN. CRACKED. 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), Aug 3, 2000: BEAM. CRACKED. 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), Aug 3, 2000: SKIN. SCRATCHED. 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), Aug 3, 2000: SKIN. SCRATCHED. 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), Aug 2, 2000: SKIN. DAMAGED. 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-
- [SDR QXEA0002231](https://openairdocs.org/sdr/QXEA0002231), Aug 2, 2000: CLIP. MISDRILLED. 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. R
- [SDR QXEA0002225](https://openairdocs.org/sdr/QXEA0002225), Aug 2, 2000: FASTENER. LOOSE. 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-
- [SDR QXEA0002220](https://openairdocs.org/sdr/QXEA0002220), Aug 2, 2000: FASTENER. LOOSE. 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

All 317: https://openairdocs.org/deregistered/N484US-2002-08-14/reports.md

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