# N863US: 1990 Fokker F.28 MK 0100, registration cancelled 2003-07-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 22, 2003 - Exported to: Netherlands - Status when cancelled: Valid registration - Airframe: [Fokker F.28 MK 0100](https://openairdocs.org/model/fokker-f-28-mk-0100) (registry code 4990807) - Engine: [Rolls-Royce TAY-650-15](https://openairdocs.org/engine/rolls-royce-tay-650-15) (registry code 54557) - Data sheets: [TCDS E25NE](https://openairdocs.org/tcds/E25NE) (OpenAirDocs) - Serial number: 11303 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 6, 1990 - Certificate issued: May 20, 2003 - Last registry action: May 20, 2003 - Mode S code: ABDBCF - Owner when cancelled: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N863US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=863US - Page: https://openairdocs.org/deregistered/N863US-2003-07-22 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 MK 0100: https://openairdocs.org/model/fokker-f-28-mk-0100.md ## Service difficulty reports (19) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAF00079](https://openairdocs.org/sdr/USAAF00079), Nov 20, 2000: WIRE. BROKEN. IND - THE LAST SECTION OF FIRST CLASS FLOOR LEVEL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONALLY CHECKED GOOD. (M) - [SDR USAAF00080](https://openairdocs.org/sdr/USAAF00080), Nov 20, 2000: BATTERY PACK. DISCHARGED. IND - THE LEFT OVERWING EMERGENCY EXIT LIGHTS, WERE FOUND INOPERATIVE BETWEEN THE EXITS. MAINTENANCE REPLACED A BATTERY AND POWER SUPPLY PACK. OPERATIONALLY CHE - [SDR USAAF00050](https://openairdocs.org/sdr/USAAF00050), Jul 10, 2000: BATTERY. DISCHARGED. CLT - FOUND THE FIRST CLASS FLOOR LEVEL EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FOR THE FIRST CLASS EMERGENCY EXIT LIGHTS. OPS - [SDR USAAF00044](https://openairdocs.org/sdr/USAAF00044), Jun 4, 2000: SLIDE. DETACHED. CLT - FOUND FORWARD SERVICE DOOR SLIDE FALLING OUT OF SLIDE PACK. MAINTENANCE REPLACED SLIDE ASSY. OK FOR SERVICE. (M) - [SDR USAAF98008](https://openairdocs.org/sdr/USAAF98008), Jan 19, 1998: SHUTOFF VALVE. INOPERATIVE. GSO - FLT 875 - FLT EN ROUTE RIC TO CLT, WHEN NR 2 ENGINE ANTI-ICE FAILURE OCCURRED. CREW RESET CIRCUIT BREAKER AND IT POPPED. DUE TO WEATHER CONDITIONS IN CLT, - [SDR USAAF98004](https://openairdocs.org/sdr/USAAF98004), Jan 13, 1998: INDICATOR MODULE. FAILED. CLT - FLT 220 - THE GREEN LEFT MLG LIGHT STAYED ON AFTER RETRACTION, NO OTHER ABNORMAL INDICATIONS WERE PRESENT. THE AIRCRAFT RETURNED TO CLT. THE AIRCRAFT LAND - [SDR USAAF97061](https://openairdocs.org/sdr/USAAF97061), Jul 17, 1997: SEAL. FAILED. CLT/TYS - FLT 589 - DURING DESCENT INTO CLT AFTER STARTING THE APU, CREW ACTIVATED THE SPEED BRAKE AND RECEIVED A MOMENTARY 'APU FIRE' WARNING. THE APU AUTO-SHU - [SDR 97ZZZX4222](https://openairdocs.org/sdr/97ZZZX4222), Jul 17, 1997: SEAL. FAILED. CLT/TYS - FLT 589 - DURING DESCENT INTO CLT AFTER STARTING THE APU, CREW ACTIVATED THE SPEED BRAKE AND RECEIVED A MOMENTARY 'APU FIRE' WARNING. THE APU AUTO-SHU - [SDR 97ZZZX4221](https://openairdocs.org/sdr/97ZZZX4221), Jul 17, 1997: SEAL. FAILED. CLT/TYS - FLT 589 - DURING DESCENT INTO CLT AFTER STARTING THE APU, CREW ACTIVATED THE SPEED BRAKE AND RECEIVED A MOMENTARY 'APU FIRE' WARNING. THE APU AUTO-SHU - [SDR USAAF97049](https://openairdocs.org/sdr/USAAF97049), Jun 18, 1997: CONTROL UNIT. FAILED. PIT/STL - FLT 1531 - EN ROUTE TO STL APPROXIMATELY 90NM EAST OF IND, ESSENTIAL AC POWER BUS FAILED. FLIGHT DIVERTED TO IND FOR MAINTENANCE PURPOSES. NO EMERGENC - [SDR USAAF97036](https://openairdocs.org/sdr/USAAF97036), Apr 8, 1997: OUTFLOW VALVE. STUCK OPEN. FLT 1227 - CLT-IAD - AFTER TAKEOFF FROM CLT, THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO CLT. MAINTENANCE REPLACED THE PRIMARY OUTFLOW VALVE. (M) - [SDR USAAF97027](https://openairdocs.org/sdr/USAAF97027), Mar 9, 1997: AIR DISTRIBUTION. ODOR. DURING THE LAST FORTY MINUTES OF FLIGHT, CREW NOTED ACRID ODOR IN THE COCKPIT. MAINTENANCE INSPECTED THE AREA AND FOUND NO PROBLEM. THE EQUIPMENT COOLING AIR FI - [SDR USAA970026](https://openairdocs.org/sdr/USAA970026), Jan 20, 1996: SKIN. DAMAGED. PIT - DURING Q-1 CHECK, FOUND 18 INCH BY 20 INCH AREA OF DISBONDED AND HEAT DAMAGED SKIN AT RT STUBWING FUSELAGE SKIN BETWEEN FRAMES 24011 AND 24611 AND BETWEEN - [SDR USAA970025](https://openairdocs.org/sdr/USAA970025), Jan 20, 1996: SKIN. DAMAGED. PIT - DURING Q-1 CHECK, FOUND 18 INCH BY 24 INCH AREA OF DISBONDED AND HEAT DAMAGED SKIN AT LT STUBWING FUSELAGE SKIN BETWEEN FRAMES 24011 AND 24611 AND BETWEEN - [SDR USAA970024](https://openairdocs.org/sdr/USAA970024), Jan 20, 1996: BULKHEAD. CRACKED. PIT - DURING Q-1 CHECK, FOUND TWO .5 INCH CRACK (LT SIDE) OF CENTER FUEL TANK PRESSURE BULKHEAD AT FRAME 14911 AND STATION 11. STOP DRILLED AND CUT OUT CRACKED - [SDR USAA970023](https://openairdocs.org/sdr/USAA970023), Jan 20, 1996: BULKHEAD. CRACKED. PIT - DURING Q-1 CHECK, FOUND 3 INCH CRACK (RT SIDE) OF CENTER FUEL TANK PRESSURE BULKHEAD AT FRAME 14911 AND STATION 64. STOP DRILLED AND CUT OUT CRACKED AREA. - [SDR USAA970022](https://openairdocs.org/sdr/USAA970022), Jan 20, 1996: BEAM. CORRODED. PIT - DURING Q-1 CHECK, FOUND 2 INCH BY 2 INCH AREA OF CORROSION (.068 INCH DEEP) IN MID CARGO DOOR LATCH BEAM TOP SURFACE BETWEEN STATION 11333-12791, STATION - [SDR USAA951248](https://openairdocs.org/sdr/USAA951248), Dec 6, 1995: FLOOR BEAM. CORRODED. PIT - DURING APU MODIFICATION TRACK, FOUND CORROSION ON FLOOR BEAM, BETWEEN STATION 4850 AND 5305 AND BL 0. CUT OUT CORRODED SECTION OF BEAM AND SPLICED IN NEW - [SDR USAA950752](https://openairdocs.org/sdr/USAA950752), Jul 11, 1995: VALVE. LEAKING. RDU - FLT 109 - THE CABIN PRESSURE WOULD NOT CLIMB WITH ALTITUDE. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO RDU. MAINTENANCE INSTALLED A NEW VALVE AT TH ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB NYC98LA075](https://openairdocs.org/ntsb/NYC98LA075), Mar 12, 1998: Fokker F-100 (N863US), Philadelphia, PA, substantial damage. Probable cause: The driver's failure to maintain clearance from the parked airplane. Related factors were night conditions and the driver's diverted attention. ## 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. - [Accident 19980311024789A](https://openairdocs.org/incident/19980311024789A), Mar 11, 1998: Fokker F28MK0100 (N863US), Philadelphia, PA, Substantial damage. (.4)After the airplane was pushed back from the gate at night, a fuel truck travelling eastbound on the outer service road struck the left wing tip of the… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.