# N864US: 1990 Fokker F.28 MK 0100, registration cancelled 2003-07-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 15, 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: 11306 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 6, 1990 - Certificate issued: June 9, 2003 - Last registry action: June 20, 2003 - Mode S code: ABDF86 - Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%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/N864US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=864US - Page: https://openairdocs.org/deregistered/N864US-2003-07-15 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 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 USAAF01073](https://openairdocs.org/sdr/USAAF01073), Sep 16, 2001: ACTUATOR. FAILED. RDU - FLT 1286 - EN ROUTE - RDU-PHL, THE LEFT MLG WOULD NOT RETRACT AFTER TAKEOFF. THE LANDING GEAR WAS RECYCLED, BUT THE LEFT MLG STILL DID NOT RETRACT. THE FL - [SDR USAAF01062](https://openairdocs.org/sdr/USAAF01062), Aug 2, 2001: BATTERY PACK. INOPERATIVE. PIT - THE FORWARD FLOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED A BATTERY PACK. OPERATIONALLY CHECKED OK. (M) - [SDR USAAF98087](https://openairdocs.org/sdr/USAAF98087), Oct 27, 1998: SENSOR. INOPERATIVE. PHL - FLT 320 - AFTER TAKEOFF FROM PHL, THE TOWER REPORTED THAT FUEL WAS VENTING FROM THE RIGHT WING. AN 'AUTO FUEL FEED' FAULT ALSO ILLUMINATED. FLIGHT RETURNE - [SDR USAAF98077](https://openairdocs.org/sdr/USAAF98077), Sep 17, 1998: CONTROLLER. INOPERATIVE. ILM - FLT 1690 - AFTER TAKEOFF FROM ILM, THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO ILM AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE - [SDR USAAF98048](https://openairdocs.org/sdr/USAAF98048), Jun 10, 1998: GASKET. FAILED. CLT - FLT 1694 - AFTER TAKEOFF FROM CLT, SYSTEM NR 2 HYDRAULIC QUANTITY DROPPED TO 14 PERCENT. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINT - [SDR USAAF98018](https://openairdocs.org/sdr/USAAF98018), Feb 18, 1998: DNLOCK PLUNGER. LACK OF LUBE. FLT 1672 - PIT-MDT - AFTER TAKEOFF FROM PIT, NOSE GEAR ALERT ILLUMINATED ON MFDU. THE BLUE INTRANSIT LIGHT REMAINED LIT IN GEAR HANDLE. CREW RECYCLED GEAR WITH - [SDR USAAF97093](https://openairdocs.org/sdr/USAAF97093), Nov 16, 1997: DOWNLOCK. OVERSERVICED. FLT 275 - GSO-PHL - ON CLIMB-OUT FROM GSO, THE NOSE LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO GSO WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND AN EXCESS - [SDR USAAF97084](https://openairdocs.org/sdr/USAAF97084), Oct 25, 1997: PRESS X-MITTER. FAILED. FLT 579 - CLT-PNS - ON FINAL APPROACH OVER THE OUTER MARKER, CREW RECEIVED 'OIL PRESS OIL LIMIT' MESSAGE FOLLOWED BY 'OIL PRESS LOW' MESSAGE ON THE MULTI FUNCTI - [SDR USAAF97074](https://openairdocs.org/sdr/USAAF97074), Sep 15, 1997: AIR DATA COMP. FAILED. FLT 998 - CLT-DTW - EN ROUTE TO DTW, THE NR 1 AIR DATA COMPUTER FAILED. CREW DECIDED TO DIVERT TO PIT FOR MAINTENANCE CONVENIENCE. FLIGHT LANDED PIT WITHOUT INC - [SDR USAAF97042](https://openairdocs.org/sdr/USAAF97042), Apr 25, 1997: RELAY. FAILED. DCA/BOS - FLT 1503 - ON APPROACH TO BOS, THE NOSE GEAR WOULD NOT EXTEND. THERE WAS NO NOSE GEAR GREEN LIGHT. AT 1,000 FEET 'GEAR UNSAFE' ILLUMINATED ON THE MULT - [SDR 97ZZZX2014](https://openairdocs.org/sdr/97ZZZX2014), Apr 25, 1997: RELAY. FAILED. DCA/BOS - FLT 1503 - ON APPROACH TO BOS, THE NOSE GEAR WOULD NOT EXTEND. THERE WAS NO NOSE GEAR GREEN LIGHT. AT 1,000 FEET 'GEAR UNSAFE' ILLUMINATED ON THE MULT - [SDR USAAF97041](https://openairdocs.org/sdr/USAAF97041), Apr 24, 1997: PROXIMITY SENSOR. BROKEN. BUF/PHL - FLT 871 - AFTER TAKEOFF, GEAR WOULD NOT RETRACT AND GEAR WARNING INDICATED. AT 400 FEET 'AIR/GND SENSOR' WARNING APPEARED ON MFDU. FLIGHT RETURNED TO - [SDR USAA970093](https://openairdocs.org/sdr/USAA970093), Mar 18, 1997: SKIN. CRACKED. PIT - DURING Q-1 CHECK, FOUND 3 CRACKS AT FUSELAGE LOW PRESSURE CONNECTION PORT AT UP SLOT ATTACHMENT ON SKIN. INSTALLED DOUBLER REPAIR PER US AIRWAYS EA 29161. - [SDR USAA970092](https://openairdocs.org/sdr/USAA970092), Mar 18, 1997: FRAME. CRACKED. PIT - DURING Q1 CHECK, FOUND 2.5 INCH CRACK AT LEFT SIDE FRAME 14911 AT STRINGER NR 11. ROUTED OUT DAMAGED AREA. INSTALLED A SHIM AND TWO NEW REPAIR ANGLES PER - [SDR USAA970091](https://openairdocs.org/sdr/USAA970091), Mar 18, 1997: FRAME. CRACKED. PIT - DURING Q1 CHECK, FOUND 3 INCH CRACK AT RT SIDE, FRAME 14911, AT STRINGER NR 64. ROUTED OUT DAMAGED AREA. INSTALLED A SHIM AND TWO NEW REPAIR ANGLES PER EA - [SDR USAAF96101](https://openairdocs.org/sdr/USAAF96101), Sep 21, 1996: FUEL PUMP. FAILED. PIT-DTW - FLT 1140Z - ON CLIMB-OUT, RECEIVED FAULT LIGHTS FOR NR 1 AND NR 2 RIGHT FUEL PUMPS. AIRCRAFT RETURNED TO PIT. NO FURTHER INCIDENTS DURING FLIGHT. MAIN - [SDR USAA950411](https://openairdocs.org/sdr/USAA950411), Apr 26, 1995: EEL RELAY. INOPERATIVE. PIT - FOUR OVERWING EXIT LIGHTS AND OVERHEAD EXIT LIGHTS DO NOT ILLUMINATE WITH GEAR DOWN. MAINTENANCE REPLACED RELAY K2618-A, CHECK NORMAL. (Z) - [SDR USAA950022](https://openairdocs.org/sdr/USAA950022), Jan 22, 1995: SENSOR. FAULTED. MCO - FLT 8004 - ON TAKEOFF, LIFT DUMPER FAULTED. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE L3 SENSOR ON LT GEAR MM 32-63-03 - [SDR USAA950023](https://openairdocs.org/sdr/USAA950023), Jan 17, 1995: SEAL. WORN. PIT - FLT 114 - RUSHNG AIR SOUND WAS HEARD COMING FROM THE MED BY F/A. CABIN BEGAN TO CLIMB. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REP ## 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 19970423011509I](https://openairdocs.org/incident/19970423011509I), Apr 23, 1997: Fokker F28MK0100 (N864US), Buffalo, NY. Narrative: on April 23, 1997, at 1530 EST, a Fokker 28, N864US, flight 821, operated by us airways, during the takeoff phase from Buffalo international airport… --- 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.