# N862US: 1990 Fokker F.28 MK 0100, registration cancelled 2003-04-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 22, 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: 11300 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 1, 1990 - Certificate issued: February 26, 2003 - Last registry action: February 26, 2003 - Mode S code: ABD818 - 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/N862US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=862US - Page: https://openairdocs.org/deregistered/N862US-2003-04-22 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 (26) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAF01063](https://openairdocs.org/sdr/USAAF01063), Aug 5, 2001: SWITCH. PIT - FLT 1851 - EN ROUTE PIT-ATL - AFTER TAKEOFF, THE LANDING GAER WOULD NOT RETRACT. THE FLIGHT RETURNED TO FIELD IN PIT AND LANDED WITHOUT INCIDENT. MAINTENA - [SDR USAAF00082](https://openairdocs.org/sdr/USAAF00082), Nov 26, 2000: WARNING LIGHT. ILLUMINATED. MKE-CLT - FLT 891 - AFTER GEAR RETRACTION, RECEIVED A - RT MLG- FAULT WITH CHECKLIST. THE GEAR WAS CYCLED AND THE OPERATION WAS NORMAL. THE FLIGHT LANDED IN CLT - [SDR USAAF00083](https://openairdocs.org/sdr/USAAF00083), Nov 26, 2000: SENSOR. OUT OF ADJ. RDU-CLT - FLT 455 - AFTER GEAR RETRACTION, RECEIVED A -RT MLG- FAULT MESSAGE WITH CHECKLIST. THE GEAR WAS CYCLED AND THE MESSAGE REAPPEARED. WITH OTHER SYSTEMS - [SDR USAAF00074](https://openairdocs.org/sdr/USAAF00074), Oct 21, 2000: DOOR. OPEN. PIT-LEX, FLT 363, AFTER TAKEOFF, RECEIVED A MID-CARGO DOOR OPEN INDICATION ON THE MFDU. THE FLIGHT RETURNED TO PIT AND LANED WITHOUT INCIDENT. MAINTENANCE FOUND - [SDR USAAF00070](https://openairdocs.org/sdr/USAAF00070), Sep 23, 2000: DOWNLOCK SWITCH. MALFUNCTIONED. CHA-CLT - FLT 1152 - WHEN THE LANDING GEAR WAS RAISED AFTER TAKEOFF, THE LANDING GEAR RETRACTED, BUT THE RIGHT MAIN GEAR LIGHT REMAINED ON AND GREEN. THE FLIGHT - [SDR USAAF0067](https://openairdocs.org/sdr/USAAF0067), Sep 9, 2000: WARNING LIGHT. ILLUMINATED. CLT-PIT - FLT 1540 - THE MID CARGO DOOR WARNING LIGHT ILLUMINATED DURING CLIMB-OUT. QRH PROCEDURES WERE PERFORMED, AND THEN THE FLIGHT RETURNED TO THE FIELD AND - [SDR USAAF00005](https://openairdocs.org/sdr/USAAF00005), Jan 17, 2000: CONTROLLER. FAILED. PHL/IND - FLT 510 - DURING CRUISE, THE CABIN ALTITUDE ALERT DISPLAYED AND THE PRESSURIZATION SYSTEM WAS UNCONTROLLABLE. THE AIRCRAFT DIVERTED TO PIT AND LANDED - [SDR USAAF99034](https://openairdocs.org/sdr/USAAF99034), Jun 26, 1999: WINDSHIELD. DELAMINATING. BUF - FL 1122 - EN ROUTE PIT/EWR - CREW NOTED SMOKE COMING FROM THE GLARE SHIELD. FLIGHT DIVERTED TO BUF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND - [SDR USAAF99033](https://openairdocs.org/sdr/USAAF99033), Jun 25, 1999: FAN. FAILED. PIT - FL 591 - ON CLIMB-OUT FROM PIT, CREW NOTED SMOKE COMING FROM BEHIND THE GLARESHIELD. FLIGHT RETURNED TO PIT AND LANDED WTIH NO FURTHER INCIDENT. MAINTENAN - [SDR USAA980390](https://openairdocs.org/sdr/USAA980390), Sep 5, 1998: FITTING. BENT. PIT - DURING UNSCHEDULED MAINTENANCE, FOUND SHEARED BOLTS IN ACTUATOR ATTACK BRACKET AND 2 INCH CRACKED BULKHEAD IN RT WHEEL WELL AT ACTUATOR ATTACH FITTING ON - [SDR USAA980389](https://openairdocs.org/sdr/USAA980389), Sep 4, 1998: BRACKET. CRACKED. PIT - DURING RON, RIGHT FORWARD MLG DOOR ACTUATOR LOOSE 2 INCH CRACK ACTUATOR BRACKET DOUBLER AT RT WHEEL WELL FWD INBOARD CORNER AT MLG ACTUATOR BRACKET. INSTA - [SDR USAAF98072](https://openairdocs.org/sdr/USAAF98072), Aug 30, 1998: DOOR. SEPARATED. HSV - FLT 721 - ON APPROACH TO HSV AFTER LANDING GEAR SELECTED DOWN, MLG DOOR UNSAFE' MESSAGE ILLUMINATED. CREW RECYCLED GEAR. 10 SECONDS LATER THE MESSAGE APPE - [SDR USAAF98035](https://openairdocs.org/sdr/USAAF98035), Apr 4, 1998: DIMMING UNIT. INOPERATIVE. PVD - FLT 396 - ON APPROACH TO PVD WHEN LANDING GEAR WAS SELECTED DOWN, NO GREEN GEAR SAFE LIGHTS ILLUMINATED. NO FAULT MESSAGES WERE ILLUMINATED. TOWER FLYBY I - [SDR USAAF97092](https://openairdocs.org/sdr/USAAF97092), Nov 14, 1997: BATTERY PACK. DISCHARGED. IND - MAINTENANCE FOUND THE LEFT EMERGENCY EXIT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND BATTERY PACKS. (M) - [SDR 97ZZZM1172](https://openairdocs.org/sdr/97ZZZM1172), Nov 14, 1997: LIGHT. INOPERATIVE. IND - MAINTENANCE FOUND THE LEFT EMERGENCY EXIT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND BATTERY PACKS. (M) - [SDR USAAF97065](https://openairdocs.org/sdr/USAAF97065), Jul 17, 1997: BATTERY PACK. DISCHARGED. IND - DURING ROUTINE OVERNIGHT MAINTENANCE CHECK, MAINTENANCE FOUND THE RIGHT SIDE OVERWING EMERGENCY LIGHTS INOPERATIVE. THEY REPLACED THE BATTERY PACK. (X) - [SDR USAAF97060](https://openairdocs.org/sdr/USAAF97060), Jul 17, 1997: BATTERY PACK. DISCHARGED. IND - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) - [SDR USAAF97048](https://openairdocs.org/sdr/USAAF97048), Jun 12, 1997: UNION. CRACKED. FLT 1262 - MSP-PIT - DURING CLIMB-OUT FROM MSP, SYSTEM NR 1 HYDRAULIC FAILED. FLIGHT RETURNED TO MSP WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TOWED FROM RUNWAY TO - [SDR USAAF97009](https://openairdocs.org/sdr/USAAF97009), Feb 24, 1997: SWITCH. OUT OF ADJUST. CLT - FLT 1604 - AFTER TAKEOFF, CREW GOT WARNING CHIME THAT AIRCRAFT WAS STILL ON THE GROUND. GND/FLT MESSAGE APPEARED ON MFDU. CREW ALSO WAS UNABLE TO GET ANY - [SDR USAA960792](https://openairdocs.org/sdr/USAA960792), Dec 23, 1996: SKIN. GOUGED. PIT - DURING Q-1 CHECK, FOUND 1.125 INCH LONG, .1875 INCH WIDE (AT TOP) .09375 INCH WIDE (AT BOTTOM) .029 INCH DEEP GOUGES AT LEFT SIDE OF THE VERTICAL STAB SKI - [SDR USAA960791](https://openairdocs.org/sdr/USAA960791), Dec 23, 1996: BULKHEAD. CRACKED. PIT - DURING Q-1 CHECK, FOUND TWO 3 INCH CRACKS AND 2 .75 INCH CRACKS (LT AND RT SIDES) CENTER PRESSURE BULKHEAD STATION 14911 AT STATION NR 11 (LHS) AND AT STA - [SDR USAA960790](https://openairdocs.org/sdr/USAA960790), Dec 23, 1996: SKIN. DISBONDED. PIT - DURING Q-1 CHECK, FOUND 20 INCH BY 20 INCH DISBONDED SKIN AND HEAT DAMAGE IN FUSELAGE SKIN RIGHT SIDE AND SEAM BETWEEN FRAME 23011 AND 24611. CUT OUT DAMA - [SDR USAA960789](https://openairdocs.org/sdr/USAA960789), Dec 23, 1996: FRAME. CORRODED. PIT - DURING Q-1 CHECK FOUND .5 INCH BY .5 INCH BY .042 INCH MAX DEPTH TWO AREAS CORRODED AT AFT FRAME OF THE FORWARD CARGO DOOR OPENING AT FRAME 8805 AND BL 30 - [SDR USAAF96054](https://openairdocs.org/sdr/USAAF96054), Jun 7, 1996: BATTERY PACK. DISCHARGED. BOTH LAVATORY EMERGENCY LIGHTS INOP. REPLACED NR 8 BATTERY PACK. (M) - [SDR USAAF96017](https://openairdocs.org/sdr/USAAF96017), Jan 30, 1996: GEAR WARNING. ACTIVATED. STL - FL 1254 - AFTER TAKEOFF FROM STL AND GEAR RETRACTION, CREW RECEIVED MFDU MESSAGE THAT THE LEFT LANDING GEAR WAS NOT UP. GEAR WAS CYCLED WITH THE SAME RESU - [SDR USAA950453](https://openairdocs.org/sdr/USAA950453), May 8, 1995: CONTROL PANEL. INOP. BTR - FLT NR 0431 - AT FL 310, CREW RECEIVED RED LIGHTS IN THE COCKPIT. THE CABIN PRESSURE BEGAN CLIMBING RAPIDLY. AIRCRAFT MADE AN EMERGENCY DESCENT TO 10,000 ## FAA accident and incident reports (2) 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 19990626023629I](https://openairdocs.org/incident/19990626023629I), Jun 26, 1999: Fokker F28MK0100 (N862US), Buffalo, NY. (-23) On Saturday, June 26, 1999, a usairways Fokker F100, N862US, diverted to Buffalo niagra international airport after reporting smoke puffs above the… - [Incident 19900621032659I](https://openairdocs.org/incident/19900621032659I), Jun 21, 1990: Fokker F28MK0100 (N862US), Syracuse, NY. Vibration near rear door. Completed flight. Left stubwing blow out door was loose. Adjusted the spring tension. --- 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.