# N884US: 1991 Fokker F.28 MK 0100, registration cancelled 2003-08-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 18, 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) - Serial number: 11338 - Year built: 1991 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: September 6, 1991 - Certificate issued: June 9, 2003 - Last registry action: June 9, 2003 - Mode S code: AC2E84 - 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/N884US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=884US - Page: https://openairdocs.org/deregistered/N884US-2003-08-18 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 (20) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAF01020](https://openairdocs.org/sdr/USAAF01020), May 7, 2001: BATTERY PACK. DISCHARGED. IND - THE AFT CENTER CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATERY PACK IN THE POWER SUPPLY. OPS CHECKED OK. (M) - [SDR USAAF00081](https://openairdocs.org/sdr/USAAF00081), Nov 21, 2000: LIGHT. INOPERATIVE. IND - THE EMERGENCY FLOOR TRACK LIGHT AT ROW NINE WAS FOUND INOPERATIVE. MAINTENANCE REPLACED A FLEXIBLE FLOOR LIGHT. OPERATIONALLY CHECKED GOOD. (M) - [SDR USAAF00059](https://openairdocs.org/sdr/USAAF00059), Jul 30, 2000: SELECTOR VALVE. FAILED. BHM-CLT - FLT 430 - NOSE GEAR FAILED TO RETRACT ON TAKEOFF. BARBER POLE FOR GEAR SPEED STILL IN VIEW. NO MFDU MESSAGE PRESENT. RECYCLED GEAR AND NOSE GEAR CAME - [SDR USAAF00052](https://openairdocs.org/sdr/USAAF00052), Jul 13, 2000: INDICATOR. MALFUNCTIONED. ILM-CLT - FLT 443 - AFTER LANDING GEAR WAS SELECTED UP, NOSE LANDING GEAR LIGHT REMAINED ON. NO TRANSIT LIGHTS IN GEAR HANDLE OR MFDU MESSAGES. RECYCLED LANDING - [SDR USAAF00033](https://openairdocs.org/sdr/USAAF00033), Apr 27, 2000: WINDSHIELD. CRACKED. CLT-BNA - FLT 1989 - FIRST OFFICERS OUTER WINDSHIELD CRACKED IN FLIGHT. AN EMERGENCY WAS DECLARED AND FLIGHT WAS DIVERTED TO GSP WHERE IT LANDED WITHOUT INCIDEN - [SDR USAA000647](https://openairdocs.org/sdr/USAA000647), Apr 10, 2000: SKIN. DAMAGED. PIT - FOUND HEAT DAMAGED SKIN, 34 INCH BY 35 INCH AREA, STATION 27250 TO 27526 STATION 48. REPLACED DAMAGED SKIN AND FRAME SECTION PER SRM 51-70-1-06 REP NR 4 A - [SDR USAA000549](https://openairdocs.org/sdr/USAA000549), Apr 10, 2000: SKIN. FATIGUED. PIT - FOUND 12 INCH BY 10 INCH AREA SKIN AND INNER DOUBLER METAL FATIGUED DUE TO EXCESSIVE HEAT, RT SIDE STATION 27.250 STRINGER 48. REMOVED FATIGUED METAL. INS - [SDR USAAF00026](https://openairdocs.org/sdr/USAAF00026), Mar 19, 2000: WARNING LIGHT. ILLUMINATED. PIT-CLT - FLT 209 - ON TAKEOFF, RECEIVED AN L MAIN GEAR MESSAGE ON THE MULTI-FUNCTION DISPLAY UNIT. LEFT MAIN GEAR DID NOT RETRACT. RECYCLED PER QRH, ALL GEAR R - [SDR USAAF00017](https://openairdocs.org/sdr/USAAF00017), Feb 18, 2000: ATTACH FITTING. LOOSE. PHL-GSO - FLT 989 - LEFT MAIN GEAR WOULD NOT RETRACT. CYCLED GEAR, BUT CONDITION STILL EXISTED. SELECTED GEAR DOWN AND GOT THREE GREEN INDICATION. FLIGHT RETURN - [SDR USAAF00013](https://openairdocs.org/sdr/USAAF00013), Feb 14, 2000: DOOR. CRACKED. GSO-CLT - FLT 8078 - AIRCRAFT LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE REVIEWED PROCEDURE TO SECURE LEFT MLG SEQUENCE VALVE IN THE OPEN POSITIO - [SDR USAAF99052](https://openairdocs.org/sdr/USAAF99052), Oct 22, 1999: LT PACK. LEAKING. CLT - FLT 945 - AFTER TAKEOFF, A BURNING ODOR WAS NOTICED IN THE COCKPIT AND CABIN. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OIL - [SDR USAAF99002](https://openairdocs.org/sdr/USAAF99002), Jan 12, 1999: WINDSHIELD. CRACKED. PIT - FLT 864 - WHILE CLIMBING OUT FROM PIT AT FL 210, THE LEFT FRONT WINDSCREEN CRACKED. THE FLIGHT CREW FOLLOWED SPECIAL PROCEDURES AND DECLARED AN EMERGENCY. - [SDR USAAF98039](https://openairdocs.org/sdr/USAAF98039), May 2, 1998: SELECTOR VALVE. FAILED. PNS - FLT 243 - ON APPROACH TO PNS WHEN LANDING GEAR WAS SELECTED DOWN, NOSE GEAR DID NOT INDICATE DOWN AND LOCKED (NO GREEN 'SAFE'). CREW RECYCLED GEAR AND ALL - [SDR USAAF98002](https://openairdocs.org/sdr/USAAF98002), Jan 8, 1998: SYNCHRONIZER. FAILED. PHL/IND - FLT 1799 - ON CLIMB-OUT FROM PHL AT 1,000 FEET WHEN FLAPS WERE RETRACTED, FLAP ASYMMETRY' ILLUMINATED AT 8 DEGREES OF FLAP. FLIGHT RETURNED TO PHL WIT - [SDR USAA970337](https://openairdocs.org/sdr/USAA970337), Nov 16, 1997: SKIN. DAMAGED. PIT - DURING Q-1 CHECK, FOUND 9 INCH BY 14 INCH AREA OF SKIN DELAMINATION/HEAT DAMAGE AT LEFT STUBWING BETWEEN FRAMES 24011 AND 24611 AND STRINGERS 22 AND 23 ON - [SDR USAAF97073](https://openairdocs.org/sdr/USAAF97073), Sep 11, 1997: FIRE WARNING. ACTIVATED. FLT 1024 - CLT-MYR - APU FIREBOTTLE DISCHARGED AFTER SPEEDBRAKES WERE DEPLOYED IN FLIGHT. MAINTENANCE INSPECTED APU ENCLOSURE AND SEALS. NO EVIDENCE OF FIRE OR - [SDR USAAF97072](https://openairdocs.org/sdr/USAAF97072), Sep 5, 1997: HANDLE STRUT. WEAK. PIT/DAY - FLT 677 - AFTER TAKEOFF, MID-CARGO DOOR WARNING ILLUMINATED. THE AIRCRAFT ALSO STARTED TO DEPRESSURIZE. FLIGHT RETURNED TO PIT WITHOUT FURTHER INCIDEN - [SDR USAAF97064](https://openairdocs.org/sdr/USAAF97064), Jul 23, 1997: DOOR VENT. OPEN. PHL/JAX - FLT 1495 - ON CLIMB-OUT FROM PHL AT APPROXIMATELY 500 FEET, THE MID-CARGO DOOR WARNING LIGHT ILLUMINATED. FLIGHT RETURNED TO PHL AND LANDED OVERWEIGHT - [SDR USAAF96105](https://openairdocs.org/sdr/USAAF96105), Oct 15, 1996: HANDLE. NOT LATCHED. FLT 915 - CLT-JAX - AFTER TAKEOFF, MID CARGO DOOR WARNING LIGHT ILLUMINATED. FLIGHT RETURNED TO CLT WITH NO FURTHER INCIDENT. MAINTENANCE FOUND DOOR UPPER HANDL - [SDR USAAF96091](https://openairdocs.org/sdr/USAAF96091), Aug 14, 1996: BEARING. LOOSE. CLT-ILM - FLT 909 - ON APPROACH TO ILM, FLAP DISAGREE ALERTED. CREW TRIED TO RAISE FLAPS BUT THEY WERE STUCK AT 3 DEGREES. FLIGHT RETURNED TO CLT WITH FLAPS AT ## 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 19921202051209I](https://openairdocs.org/incident/19921202051209I), Dec 2, 1992: Fokker F28MK0100 (N884US), Rochester, NY. Struck a deer on takeoff ground roll. Pilot committed to takeoff. Continued to destination. Landed safely. ## Other aircraft with N884US - [Registered now](https://openairdocs.org/aircraft/N884US): Diamond Aircraft Ind DA 40, S/N 40.884, 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.