# N868US: 1990 Fokker F.28 MK 0100, registration cancelled 2003-03-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 31, 2003 - Exported to: Germany - 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: 11313 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 18, 1990 - Certificate issued: February 20, 2003 - Last registry action: February 20, 2003 - Mode S code: ABEE62 - 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/N868US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=868US - Page: https://openairdocs.org/deregistered/N868US-2003-03-31 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 (14) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAF01064](https://openairdocs.org/sdr/USAAF01064), Aug 15, 2001: BATTERY PACK. INOPERATIVE. RIC - THE FIRST CLASS EMERGENCY EXIT FLOOR LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE GROUND/FLIGHT SWITCH. OPERATIONALLY CHECKED OK. (M) - [SDR USAA010811](https://openairdocs.org/sdr/USAA010811), Jun 7, 2001: SKIN. DELAMINATED. PIT - FOUND SKIN DELAMINATED 10 INCHES BY 12 INCHES, LEFT AND RIGHT LAVATORIES, STATION 24011 AND 24611 STRINGER 51 AND 53. INSTALLED RIVETS IN LEFT AND RIGHT L - [SDR USAAF01019](https://openairdocs.org/sdr/USAAF01019), May 5, 2001: BATTERY PACK. DISCHARGED. IND - THE EMERGENCY LIGHTS AND EMERGENCY EXIT LIGHT IN THE FORWARD ENTRANCE AREA WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN THE POWER SUPP - [SDR USAAF99045](https://openairdocs.org/sdr/USAAF99045), Sep 11, 1999: BATTERY PACK. DISCHARGED. IND - FOUND AFT LAVATORY AREA AND AISLE LIGHT 6 INOPERATIVE. MAINTENANCE REPLACED THE NR 8 BATTERY PACK. (M) - [SDR USAAF98041](https://openairdocs.org/sdr/USAAF98041), May 9, 1998: UPSTOP DAMPER. FAILED. PIT - FLT 536 - AFTER TAKEOFF FROM PIT, LEFT MAIN GEAR DID NOT FULLY RETRACT. CREW RECYCLED GEAR TWO TIMES WITH SAME RESULT. FLIGHT RETURNED TO PIT AND LANDED W - [SDR USAAF98017](https://openairdocs.org/sdr/USAAF98017), Feb 17, 1998: QTY TRANSMITTER. MALFUNCTIONED. PIT - CAPTAIN ADVISED VIA ACARS THE THE NR 1 HYD QTY WAS LOW AND LOST NOSE WHEEL STEERING. AN EMERGENCY WAS DECLARED AND THE A/C LANDED WITHOUT FURTHER INCIDENT - [SDR USAAF98003](https://openairdocs.org/sdr/USAAF98003), Jan 7, 1998: BATTERY PACK. DISCHARGED. IND - THE AFT RIGHT WING FAIRING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE CORRESPONDING POWER SUPPLY AND BATTERY PACK. (M) - [SDR 98ZZZM204](https://openairdocs.org/sdr/98ZZZM204), Jan 7, 1998: POWER SUPPLY. INOPERATIVE. IND - THE AFT RIGHT WING FAIRING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE CORRESPONDING POWER SUPPLY AND BATTERY PACK. (M) - [SDR USAAF97040](https://openairdocs.org/sdr/USAAF97040), Apr 22, 1997: ENGINE. VIBRATION. BHM/CLT - FLT 1480 - WHLE IN HOLDING PATTERN OVER CLT DUE TO WEATHER CONDITIONS, VIBRATION WAS EXPERIENCED ON RIGHT ENGINE. CREW WENT TO ALTERNATE PROCEDURES. I - [SDR USAA970136](https://openairdocs.org/sdr/USAA970136), Apr 15, 1997: BULKHEAD ANGLES. CRACKED. PIT - DURING Q1 VISIT, FOUND 1 INCH CRACK LEFT SIDE, .50 INCH CRACK RIGHT SIDE AT FUSELAGE CTR PRESS BULKHEAD ANGLE CRACK, STR NR 11 AND STR NR 64. INSTALLED AN - [SDR USAAF96020](https://openairdocs.org/sdr/USAAF96020), Feb 12, 1996: PSEU COMPUTER. FAILED. PIT - FL 1193 - ON CLIMB-OUT FROM PHL, CREW RECEIVED TCAS FAULT AND GROUND/FLIGHT CONTROL FAULT. EN ROUTE TO MCI, CREW RECEIVED THE TAKEOFF CONFIGURATION STAB T - [SDR USAA951042](https://openairdocs.org/sdr/USAA951042), Sep 30, 1995: SENSOR. FAILED. PIT - FLT NR 1025 - AFTER TAKEOFF WE RECEIVED A GND/FLT CONTROL MSG ON MFDU. ALL INDICATIONS INDICATED AIRCRAFT WAS STILL ON GND. RETURNED TO PIT AFTER CONSULTI - [SDR USAA951095](https://openairdocs.org/sdr/USAA951095), Sep 29, 1995: SKIN. GOUGED. PIT - C-1 CHECK INSPECTION, FOUND GOUGE 5 INCH LENGTH AND .047 DEEP, MAXIMUM AT THE TOP IN VERTICAL STAB RIGHT SIDE NEAR RIB NR 5, UNDER ICE SCRAPPER. INSTALLED - [SDR USAA950021](https://openairdocs.org/sdr/USAA950021), Jan 16, 1995: DOWNLOCK ACT. MALFUNCTIONED. PHL - FLT NR 183 - ON FINAL APPROACH, CREW COULD NOT GET 3 GREEN LIGHTS ON THE GEAR. THE LEFT MAIN GEAR LIGHT TESTED BUT WOULD NOT ILLUMINATE. CYCLED GEAR, THEN ## Other aircraft with N868US - [Registered now](https://openairdocs.org/aircraft/N868US): Diamond Aircraft Ind DA 40, S/N 40.868, 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.