# N803PH: Fokker F.28 MK 1000, registration cancelled 2001-09-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 5, 2001
- Status when cancelled: Triennial form not returned
- Airframe: [Fokker F.28 MK 1000](https://openairdocs.org/model/fokker-f-28-mk-1000) (registry code 4990808)
- Serial number: 11031
- Type of aircraft: Fixed wing multi engine
- Certificate issued: December 26, 1990
- Last registry action: December 14, 1999
- Mode S code: AAEE4F
- Owner when cancelled: [General Electric Capital Corp](https://openairdocs.org/faa-owner/GENERAL%20ELECTRIC%20CAPITAL%20CORP)
- Location: [Danbury, CT](https://openairdocs.org/faa-place/CT/Danbury)
- Owner type: Corporation
- Owner's area on the map: 41.3778° N, 73.4575° W: Placed by OpenAirDocs at the center of ZIP code 06810, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N803PH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=803PH
- Page: https://openairdocs.org/deregistered/N803PH-2001-09-05

From the FAA registry file of October 29, 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 MK 1000: https://openairdocs.org/model/fokker-f-28-mk-1000.md

## Service difficulty reports (27)

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

- [SDR QXEA9700340](https://openairdocs.org/sdr/QXEA9700340), Jul 18, 1997: CIRCUIT BOARD. MALFUNCTION. CENTER CABIN, FORWARD AND AFT EVACUATION SIGNS HAVE SEVERAL LAMPS INOP. REPLACED AFT CIRCUIT BOARD AND RELAMPED FORWARD CIRCUIT BOARD, OPERATIONAL CHECK GOOD.
- [SDR QXEA9700301](https://openairdocs.org/sdr/QXEA9700301), Jun 20, 1997: BATTERY. DISCHARGED. FORWARD OVERHEAD EVACUATION LIGHT DIM. REMOVED AND REPLACED NR 2 BATTERY PACK, OPERATIONAL CHECKS GOOD.
- [SDR QXEA9700199](https://openairdocs.org/sdr/QXEA9700199), May 25, 1997: TRANSFORMER. MALFUNCTION. DURING DESCENT, NOTED FAINT ELECTRICAL SMELL IN COCKPIT. AFTER LANDING, SMELL BECAME STRONGER. REMOVED AND REPLACED TRANSFORMER BALLAST FOR CENTER RED FLOOD LIG
- [SDR QXEA9700127](https://openairdocs.org/sdr/QXEA9700127), Apr 12, 1997: CIRCUIT BOARD. DEFECTIVE. EXIT LIGHT IN CEILING CENTER POSITION BURNED OUT. REPLACED CIRCUIT BOARD FOR EXIT LIGHT AND PERFORMED OPERATIONAL CHECK, CHECKS GOOD.
- [SDR QXEA9700075](https://openairdocs.org/sdr/QXEA9700075), Mar 12, 1997: BULB. FAILED. SEVERAL CABIN EMERGENCY LIGHTS ARE INOP. BULBS WERE REPLACED AND EMERGENCY LIGHTS OPS CHECKED GOOD.
- [SDR QXEA9700049](https://openairdocs.org/sdr/QXEA9700049), Feb 11, 1997: BULB. FAILED. EMERGENCY LIGHT OVER EXIT IS INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD.
- [SDR QXEA9700015](https://openairdocs.org/sdr/QXEA9700015), Jan 17, 1997: BULB. FAILED. EMERGENCY LIGHT AT SEAT 8CDE IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD.
- [SDR QXEA9600459](https://openairdocs.org/sdr/QXEA9600459), Nov 10, 1996: LIGHT BALLAST. FAILED. BURNT ELECTRICAL SMELL IN COCKPIT, CREW FELT IT WAS LIGHTING BALLEST. SMELL TRACED TO BALLEST FOR WHITE FLOOD LIGHT. LIGHT PLACED ON MEL 33-1.
- [SDR QXEA9600407](https://openairdocs.org/sdr/QXEA9600407), Sep 23, 1996: BULB. FAILED. SEVERAL OVERHEAD EMERGENCY LIGHTS ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD.
- [SDR QXEA9600365](https://openairdocs.org/sdr/QXEA9600365), Sep 2, 1996: BULB. FAILED. LEFT OVERWING EMERGENCY LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD.
- [SDR QXEA9600357](https://openairdocs.org/sdr/QXEA9600357), Aug 30, 1996: BULB. FAILED. FORWARD EMERGENCY LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD.
- [SDR QXEA9600279](https://openairdocs.org/sdr/QXEA9600279), Aug 7, 1996: BULBS. FAILED. EXIT SIGN OVER COCKPIT DOOR INOP. SIGN REPLACED AND SIGN OPS CHECKED GOOD.
- [SDR QXEA9600230](https://openairdocs.org/sdr/QXEA9600230), Jun 30, 1996: HYD PUMP. LEAKING. UTILITY SYSTEM HYDRAULIC QUANITY DROPPED TO ZERO. ALTERNATE GEAR EXTENSION PERFORMED AND AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. NR 1 HYDRAULIC PUMP REPLACED 
- [SDR QXEA9600067](https://openairdocs.org/sdr/QXEA9600067), Feb 17, 1996: BULB. FAILED. GEG - LEFT HAND LIGHT FLICKERS. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA9600044](https://openairdocs.org/sdr/QXEA9600044), Feb 1, 1996: CIRCUIT BOARD. MALFUNCTIONED. PDX - EXIT SIGN LIGHT DIM IN PAX CABIN CEILING ROW 8. SIGN CIRCUIT BOARD REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA9600007](https://openairdocs.org/sdr/QXEA9600007), Jan 3, 1996: BULB. FAILED. GEG - TWO OVERHEAD EMERGENCY LIGHTS ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA9600001](https://openairdocs.org/sdr/QXEA9600001), Jan 1, 1996: BULB. FAILED. BOI - EMERGENCY EXIT LIGHT AT ROW 8 INOP RIGHTHAND SIDE. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA9500400](https://openairdocs.org/sdr/QXEA9500400), Nov 19, 1995: DIODE. SHORTED. PDX - LANDING GEAR HANDLE COULD NOT BE MOVED FROM THE DOWN POSITION AFTER TAKEOFF. CHECKLIST PERFORMED AND GEAR WAS RAISED USING OVERRIDE. DIODE REPLACED FOR GE
- [SDR QXEA9500399](https://openairdocs.org/sdr/QXEA9500399), Nov 19, 1995: BULB. FAILED. BOI - BOTH EMERGENCY LIGHTS ABOVE FORWARD FLIGHT ATTENDANT PANEL ARE INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA9500265](https://openairdocs.org/sdr/QXEA9500265), Aug 24, 1995: EEL WIRE. BROKEN. BOI - FORWARD THREE SEGMENTS OF FLOOR PROXIMITY LIGHTING ARE INOP. REPAIRED GROUND WIRE AT BATTERY PACK CANNON PLUG. FLOOR PROXIMITY LIGHTING OPS CHECKED GOOD. 
- [SDR QXEA9500134](https://openairdocs.org/sdr/QXEA9500134), May 4, 1995: EEL WIRE. BROKEN. GEG - CENTER SECTION FLOOR PROXIMITY LIGHTING INOP. REPAIRED BORKEN WIRE AT ROW 8 AND OPS CHECKED GOOD.
- [SDR QXEA9500118](https://openairdocs.org/sdr/QXEA9500118), Apr 16, 1995: SLIDE. LOW PRESS. PDX - EVACUATION SLIDE HAS LOW PRESSURE. REPLACED SLIDE ASSY AND AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA9500093](https://openairdocs.org/sdr/QXEA9500093), Mar 29, 1995: PIN. SHEARED OFF. SEA - AFTER GEAR RETRACTION, LEFT MLG DOOR LIGHT REMAINED ON. FLIGHT CONTINUED TO PDX WHERE LIGHT EXTINGUISHED WHEN GEAR COMPLETED EXTENSION CYCLE. FLIGHT LANDE
- [SDR QXEA9500062](https://openairdocs.org/sdr/QXEA9500062), Mar 2, 1995: PBE. DISCHARGED. BOI - DURING MAINTENANCE FOUND COCKPIT PBE WITH RED INDICATOR POPPED. REPLACED PBE. AIRCRAFT RELEASED FOR SERVICE.
- [SDR QXEA9500058](https://openairdocs.org/sdr/QXEA9500058), Feb 23, 1995: EEL LAMP. FAILED. GEG - RIGHT OVERWING EMERGENCY EXIT FOUND INOP DURING MAINTENANCE. RE-BULBED FIXTURE, OPERATIONALLY TESTED. AIRCRAFT RELEASED FOR SERVICE.
- [SDR QXEA9500033](https://openairdocs.org/sdr/QXEA9500033), Feb 4, 1995: APU. MALFUNCTIONED. SEA - OIL SMELL COMING FROM AIR VENTS. AIRCRAFT WAS ON DESCENT INTO SEA WITH ENGINES AT IDLE POWER FOR 10 MIN. CREW DETERMINED SMELL WAS FROM THE APU. REPLACED 
- [SDR QXEA9500008](https://openairdocs.org/sdr/QXEA9500008), Jan 10, 1995: EEL BULB. BURNED OUT. PDX - FORWARD EMERGENCY LIGHTS IN CABIN INOP. REPLACED BULBS AND LIGHTS. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

## Other aircraft with N803PH

- [Registered now](https://openairdocs.org/aircraft/N803PH): Dassault FALCON 2000EX, S/N 255, built 2012

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