# N881US: 1991 Fokker F.28 MK 0100, registration cancelled 2003-06-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 3, 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: 11333 - Year built: 1991 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 14, 1991 - Certificate issued: May 8, 2003 - Last registry action: May 8, 2003 - Mode S code: AC235F - 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/N881US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=881US - Page: https://openairdocs.org/deregistered/N881US-2003-06-03 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 (18) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAF01076](https://openairdocs.org/sdr/USAAF01076), Oct 7, 2001: ACTUATOR. FAILED. PIT-RDU - FLT 280 - AFTER TAKEOFF, THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. WHEN TRYING TO EXTEND THE LANDING GEAR, THE NOSE GEAR EXTENDED BUT NOT THE MAIN - [SDR USAAF01034](https://openairdocs.org/sdr/USAAF01034), Jun 23, 2001: WINDSHIELD. CRACKED. CLT-MEM - FLT 865 - THE RIGHT FORWARD WINDSHIELD INNER PANE SHATTERED, AND HAD A LARGE BUBBLE ON THE OUTER PANE DURING FLIGHT. THE FLIGHT LANDED WITHOUT FURTHER - [SDR USAAF00084](https://openairdocs.org/sdr/USAAF00084), Nov 27, 2000: BATTERY PACK. DISCHARGED. RDU - THE CABIN EMERGENCY EXIT LIGHTING FLOOR STRIP WAS INOPERATIVE JUST FORWARD OF THE EMERGENCY EXIT ROW. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY - [SDR USAAF00023](https://openairdocs.org/sdr/USAAF00023), Mar 9, 2000: SEQUENCE VALVE. MALFUNCTIONED. CLT-CMH - FLT 912 - AFTER TAKEOFF, THE NOSE GEAR RETRACTED BUT THE MAIN LANDING GEAR DID NOT. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE - [SDR USAAF00022](https://openairdocs.org/sdr/USAAF00022), Mar 7, 2000: SELECTOR VALVE. MALFUNCTIONED. CLT-CHS - FLT 553 - ON FINAL APPROACH, SELECTED GEAR DOWN AND ONLY RECEIVED NOSE GEAR DOWN INDICATION. A FLYBY OF THE TOWER CONFIRMED THAT ONLY THE NOSE GEAR WA - [SDR USAAF00020](https://openairdocs.org/sdr/USAAF00020), Feb 28, 2000: LIGHT. INOPERATIVE. CLE - THE GALLEY SERVICE DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE GALLEY SERVICE DOOR EMERGENCY EXIT LIGHT. (M) - [SDR USAAF99060](https://openairdocs.org/sdr/USAAF99060), Dec 31, 1999: SELECTOR VALVE. FAILED. CLT/ROA - FLT 2122 - DURING CLIMB OUT FROM CLT, LANDING GEAR WOULD NOT RETRACT. ACCOMPLISHED CHECKLIST PROCEDURES. RETURNED TO FIELD FOR A NORMAL LANDING. MAINT - [SDR USAAF00001](https://openairdocs.org/sdr/USAAF00001), Jan 2, 1999: SELECTOR VALVE. FAILED. RDU/CLT - FLT 2327 - DURING CLIMB-OUT FROM CLT, LANDING GEAR WOULD NOT RETRACT. RECYCLED GEAR AFTER 2-3 MINUTES, GEAR RETRACTED. ON APPROACH, GEAR SELECTED DOWN - [SDR USAA980576](https://openairdocs.org/sdr/USAA980576), Nov 11, 1998: SKIN. CHAFED. PIT - DURING C-1 CHECK, FOUND TWO 1 INCH HOLES CHAFFED IN SKIN BETWEEN STATION 27526 AND OBLIQUE FRAME NR 16-2. INSTALLED DOUBLER PER EA 50951. (M) - [SDR USAA980575](https://openairdocs.org/sdr/USAA980575), Nov 11, 1998: LONGERON. CHAFED. PIT - DURING C-1 CHECK, FOUND LONGERON CHAFED THROUGH .125 INCH BY .25 INCH AT LONGERON NR 50 CHAFED THROUGH AT STATION 27526. LONGERON DAMAGE CUT OUT, NEW PIEC - [SDR USAAF98045](https://openairdocs.org/sdr/USAAF98045), May 24, 1998: RT UNIT. FAILED. PIT - FLT 0669 - AFTER TAKEOFF FROM PIT, RA FLAG ON PFD ILLUMINATED ALONG WITH THE FOLLOWING FAULT MESSAGES: GPWS, ALAND, STAB TRIM 1. THE NR 1 AUTOPILOT DISENG - [SDR USAAF98033](https://openairdocs.org/sdr/USAAF98033), Mar 17, 1998: LIGHTS. INOPERATIVE. PIT - DURING OVERNIGHT MAINTENANCE VISIT, FOUND LOW LEVEL LIGHTING IN AFT CABIN INOPERATIVE. MAINTENANCE REPAIRED WIRING IN AFT LOW LEVEL LIGHTING CIRCUIT. (M) - [SDR USAAF97019](https://openairdocs.org/sdr/USAAF97019), Feb 14, 1997: FLOW CONTL VALVE. FAILED. ILM/GRR - FLT 1612 - EN ROUTE TO GRR, BOTH AUTOMATIC PRESSURIZATION SYSTEMS WENT OFF LINE. MANUAL SYSTEM WORKED OK. FLIGHT DIVERTED TO PIT TO ACCOMMODATE MAINTE - [SDR USAAF96111](https://openairdocs.org/sdr/USAAF96111), Oct 26, 1996: BATTERY PACK. DISCHARGED. DURING OVERNIGHT MAINTENANCE CHECK, MECHANIC FOUND FIRST CLASS FLOOR LEVEL EMERGENCY LIGHTING INOP. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. ( - [SDR USAAF96055](https://openairdocs.org/sdr/USAAF96055), Jun 7, 1996: INVERTER. INOPERATIVE. FIRST CLASS FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED INVERTER. (M) - [SDR USAAF96038](https://openairdocs.org/sdr/USAAF96038), Apr 28, 1996: ADC. MALFUNCTIONED. STL - FL 2129 - AT FL 350, CREW NOTICED THE THRUST WAS BEING REDUCED BY THE AUTOPILOT, THE CAPT'S AIRSPEED WAS DEGRADING DOWNWARD WHILE THE F/O'S WAS GOING TO R - [SDR USAAF96031](https://openairdocs.org/sdr/USAAF96031), Mar 25, 1996: TUBE. CRACKED. CLT - FLT 242 - AFTER TAKEOFF, CREW RECEIVED A NR 2 BLEED FAULT MESSAGE AND THEN A NR 2 DUCT LEAK MESSAGE. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INC - [SDR USAA950008](https://openairdocs.org/sdr/USAA950008), Jan 6, 1995: SHUT OFF VALVE. FAILED. PIT - FLT 508 - 'THE WING ANTI-ICE CAPACITY' MESSAGE CAME ON WITH THE WING AN TAIL ANTI-ICE TURNED ON. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINT ## 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 19920427015729I](https://openairdocs.org/incident/19920427015729I), Apr 27, 1992: Fokker F28MK0100 (N881US), Newark, NJ, Minor damage. Pilot conducting a no flap landing made a hard landing. Maintenance talked the pilot out of logging a hard landing. --- 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.