# N866US: 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: 11310 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 14, 1990 - Certificate issued: May 20, 2003 - Last registry action: May 20, 2003 - Mode S code: ABE6F4 - 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/N866US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=866US - Page: https://openairdocs.org/deregistered/N866US-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 USAAF01021](https://openairdocs.org/sdr/USAAF01021), May 8, 2001: GIRT BAR. DISCONNECTED. PIT - DURING A SCHEDULED SLIDE CHANGE, FOUND THE SLIDE TO BE REMOVED DID NOT HAVE THE SLIDE GIRT ATTACHED TO THE GIRT BAR, ALTHOUGH THE FIRING CABLE WAS STILL A - [SDR USAAF01003](https://openairdocs.org/sdr/USAAF01003), Jan 21, 2001: SIGN. INOPERATIVE. PHL - FOUND THE EMERGENCY EXIT LIGHT OVER SEAT 12F TO BE INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN. (M) - [SDR USAAF00008](https://openairdocs.org/sdr/USAAF00008), Jan 27, 2000: LIGHT. INOPERATIVE. RIC - FOUND EMERGENCY FLOOR LEVEL LIGHTING INOPERATIVE FROM ROW 4 THROUGH 9. MAINTENANCE REPLACED THE FORWARD SECTION OF FLOOR LIGHTING. (M) - [SDR USAAF00007](https://openairdocs.org/sdr/USAAF00007), Jan 27, 2000: LIGHT. SHORTED. RIC - THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 4 THROUGH 9 WERE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP AT SEAT ROWS 4 THROUGH 9 AND THE INVERTER. - [SDR USAAF99054](https://openairdocs.org/sdr/USAAF99054), Nov 22, 1999: BATTERY. DISCHARGED. FOUND EMERGENCY LIGHTS ONLY COME ON FOR 5 SECONDS AND THEN GO OUT. MX REPLACED THE BATTERY PACK, OPS CHECK GOOD. (M) - [SDR USAAF99050](https://openairdocs.org/sdr/USAAF99050), Oct 3, 1999: POWER SUPPLY. INOPERATIVE. IND - FOUND EXIT SIGN BETWEEN RIGHT OVERWING EXITS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY. (M) - [SDR USAAF98089](https://openairdocs.org/sdr/USAAF98089), Nov 4, 1998: CABLE. FAILED. BYH - FLT 7899 - AFTER TAKEOFF FROM BYH, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE 'UP' POSITION IN EITHER THE NORMAL OR OVERRIDE MODULE. FLIGHT RETURNED TO - [SDR USAA980236](https://openairdocs.org/sdr/USAA980236), Jun 5, 1998: SKIN. CRACKED. PIT - DURING C-4 CHECK, FOUND .1875 INCH CRACK AND .25 INCH CRACK IN SKIN AT LT AND RT AFT CORNERS OF NOSE GEAR BAY. REMOVED DAMAGED AREAS AND REINSTALLED FASTE - [SDR USAAF98046](https://openairdocs.org/sdr/USAAF98046), May 25, 1998: SENSOR. FAILED. CLT - FLT 8076 - EN ROUTE TO MSP, THE FOLLOWING MESSAGES APPEARED ON THE PFD: HYD STAB 2, HYD STAB 1&2, STAB TRIM 1&2. FLIGHT DIVERTED TO PIT FOR MAINTENANCE. F - [SDR USAAF98036](https://openairdocs.org/sdr/USAAF98036), Apr 11, 1998: SELECTOR VALVE. FAILED. PIT - ON APPROACH, GREEN 'NOSE' GEAR INDICATION DID NOT ILLUMINATE. CREW DID A GO-AROUND PROCEDURE AND RECYCLED THE LANDING GEAR. ALL THREE GREEN GEAR INDICATOR - [SDR USAAF98026](https://openairdocs.org/sdr/USAAF98026), Mar 11, 1998: RETRACT MECH. LACK OF LUBE. PIT - 1221 - DURING APPROACH INTOP PIT CREW RECEIVED A NOSE GEAR UNSAFE INDICATION WHEN LOWERING THE LANDING GEAR. CREW ADVISED ATC, EXECUTED A GO-AROUND AND RE - [SDR USAAF98023](https://openairdocs.org/sdr/USAAF98023), Feb 28, 1998: SENSOR. OUT OF ADJUST. FLT 533 - GSO - AFTER TAKEOFF FROM GSO, CREW WAS UNABLE TO RETRACT THE LANDING GEAR. MANUAL OVERRIDE GEAR RETRACTION WAS SUCCESSFUL. AT APPROXIMATELY 8000 FT TH - [SDR USAAF97094](https://openairdocs.org/sdr/USAAF97094), Nov 19, 1997: DOOR STOP. OUT OF ADJUST. FLT 275 - GSO-PHL - AFTER TAKEOFF FROM GSO, WHEN LANDING GEAR WAS RETRACTED, 'LMLG' MESSAGE APPEARED ON THE MULTIFUNCTION DISPLAY AND THE INTRANSIT LIGHT REMAIN - [SDR USAA970218](https://openairdocs.org/sdr/USAA970218), Jun 10, 1997: ANGLE. CRACKED. PIT - CRACKS IN SKIN CONNECTION ANGLES IN RADIUS AT FRAME 14911, STRINGER NR 11 LEFT, STRINGER 64 RT. INSTALLED DOUBLER REPAIR PER USAIRWAYS EA 47081. (M) - [SDR USAA970217](https://openairdocs.org/sdr/USAA970217), Jun 5, 1997: SKIN. DELAMINATED. PIT - DURING Q-1 CHECK, FOUND FUSELAGE SKIN DELAMINATED, LT SIDE, RT SIDE SHOWED HEAT DAMAGE BETWEEN FRAME 24011-24611, AND BETWEEN UPPER AND LOWER STUB WING CO - [SDR USAAF96122](https://openairdocs.org/sdr/USAAF96122), Nov 24, 1996: WIRE. BROKEN. MAINTENANCE CHECK REVEALED MID CABIN CEILING EXIT SIGN LIGHTS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE ON LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) - [SDR USAAF96114](https://openairdocs.org/sdr/USAAF96114), Nov 3, 1996: WINDSHIELD. CRACKED. FLT 511 - PIT-GSO - AFTER TAKEOFF, AT APPROXIMATELY 6500 FEET, A BIRD HIT THE CAPTAINS WINDSHIELD AND IT CRACKED. THE FLIGHT RETURNED TO PIT WITHOUT INCIDENT. N - [SDR USAA950602](https://openairdocs.org/sdr/USAA950602), Jun 13, 1995: ACTUATOR. OUT OF ADJUST. PIT - FLT 0753 - UPON GEAR RETRACTION, CREW RECEIVED AN INDICATION THAT THE RIGHT MAIN GEAR WAS NOT RETRACTED. FLIGHT RETURNED TO PIT. MAINTENANCE ADJUSTED THE - [SDR USAA950600](https://openairdocs.org/sdr/USAA950600), Jun 11, 1995: SENSOR. INOPERATIVE. CAK - FLT 0237 - ON APPROACH, THE COMPUTER REPORTED ERRONEOUS GEAR NOT DOWN MESSAGES. A FLYBY WAS PERFORMED. THE CAPTAIN DECLARED AND EMERGENCY AND THE FLIGHT L ## Other aircraft with N866US - [Registered now](https://openairdocs.org/aircraft/N866US): Diamond Aircraft Ind DA 40, S/N 40.866, built 2007 --- 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.