# N856US: 1989 Fokker F.28 MK 0100, registration cancelled 2003-07-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 18, 2003 - Exported to: United Kingdom - 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: 11286 - Year built: 1989 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 7, 1990 - Certificate issued: June 9, 2003 - Last registry action: June 9, 2003 - Mode S code: ABBF75 - Owner when cancelled: [Aircraft Finance Services Inc](https://openairdocs.org/faa-owner/AIRCRAFT%20FINANCE%20SERVICES%20INC) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Corporation - Owner's area on the map: 25.7655° N, 80.1843° W: Placed by OpenAirDocs at the center of ZIP code 33131, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N856US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=856US - Page: https://openairdocs.org/deregistered/N856US-2003-07-18 From the FAA registry file of October 28, 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 (29) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAF00076](https://openairdocs.org/sdr/USAAF00076), Oct 26, 2000: SLIDE. INOPERATIVE. GSO - FOUND THE FORWARD GALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE HAD LOW PRESSURE. MAINTENANCE REPLACED THE FORWARD GALLEY SERVICE DOOR EMERGENCY EVACUATI - [SDR USAAF00058](https://openairdocs.org/sdr/USAAF00058), Aug 4, 2000: BATTERY PACK. DISCHARGED. PIT - FOUND THE EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BATTERY PACK. OK FOR SERVICE. (M) - [SDR USAAF00049](https://openairdocs.org/sdr/USAAF00049), Jun 28, 2000: CONTROL VALVE. OUT OF ADJ. ATL-PIT - FLT 545 - FULL BRAKE PEDAL APPLICATION REQUIRED TO RECEIVE MINIMAL BRAKING ACTION. MAINTENANCE BLED THE BRAKES AND ADJUSTED THE RIGHT NORMAL BRAKE CON - [SDR USAAF00045](https://openairdocs.org/sdr/USAAF00045), Jun 8, 2000: FIRE LOOP. FAILED. IND-DCA - FLT 1212 - ON CLIMB-OUT, NR 2 ENGINE FIRE WARNING ILLUMINATED AT FL 100. THE NR 2 ENGINE WAS SHUTDOWN AND BOTH FIRE EXTINGUISHING BOTTLES WERE FIRED. - [SDR USAAF00032](https://openairdocs.org/sdr/USAAF00032), Apr 24, 2000: SLIDE. DISCHARGED. PHL - FOUND SLIDE PACK ON DOOR 1L APPEARING TO BE LOW. MAINTENANCE REPLACED FORWARD LEFT ENTRY DOOR ESCAPE SLIDE. CHECKS GOOD. (M) - [SDR USAAF99046](https://openairdocs.org/sdr/USAAF99046), Sep 19, 1999: POWER SUPPLY. INOPERATIVE. IND - FOUND AFT SECTION OF LOW LEVEL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY. (M) - [SDR USAAF99021](https://openairdocs.org/sdr/USAAF99021), Apr 3, 1999: DOOR. CRACKED. CLT - FLT 2276 - AFTER TAKEOFF FROM CLT, THE LEFT AND RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAI - [SDR USAAF99019](https://openairdocs.org/sdr/USAAF99019), Apr 2, 1999: VALVE. FAILED. CLT - FLIGHT 861 - AFTER TAKEOFF FROM CLT, A BLEED NR 2 DUCT FAULT OCCURRED. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACE - [SDR 99ZZZM263](https://openairdocs.org/sdr/99ZZZM263), Apr 2, 1999: SEAL. FAILED. CLT - FLIGHT 861 - AFTER TAKEOFF FROM CLT, A BLEED NR 2 DUCT FAULT OCCURRED. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACE - [SDR USAAF98067](https://openairdocs.org/sdr/USAAF98067), Aug 11, 1998: BATTERY PACK. DISCHARGED. IND - FORWARD ENTRY DOOR EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) - [SDR USAAF97100](https://openairdocs.org/sdr/USAAF97100), Dec 8, 1997: FUEL PUMP. FAILED. FLT 1283 - PHL-MSP - TEN MINUTES AFTER DEPARTURE FROM PHL THE NR 1 CENTER FUEL TANK BOOST PUMP FAILED. THE CAPTAIN SWITCHED TO CENTER CROSSFEED BUT IT DID NOT O - [SDR USAAF97069](https://openairdocs.org/sdr/USAAF97069), Aug 11, 1997: IDG GENERATOR. FAILED. FLT 245 - CLT-DTW - WHILE EN ROUTE TO DTW, THE APU SHUT DOWN DUE TO A LOW OIL PRESSURE WARNING. THE NR 2 IDG WAS ON MEL. THE CREW ELECTED TO DIVERT TO PIT FOR M - [SDR USAAF97032](https://openairdocs.org/sdr/USAAF97032), Mar 24, 1997: BREAKER. TRIPPED. BUF - EMERGENCY EXIT SIGN LIGHTS DO NOT COME ON AFTER GEAR EXTENSION. MAINTENANCE RESET BREAKER FOR RELAY K2618A. OPERATIONAL CHECKED GOOD. (M) - [SDR USAAF96080](https://openairdocs.org/sdr/USAAF96080), Jul 21, 1996: INDICATOR MODULE. MALFUNCTIONED. FLT NR 503 - CLT-DAY - LEFT MAIN GEAR GREEN LIGHT REMAINS ON WITH GEAR RETRACTED. RETURNED TO FIELD. MAINTENANCE REPLACED THE LANDING GEAR INDICATOR MODULE. (M) - [SDR USAAF96014](https://openairdocs.org/sdr/USAAF96014), Jan 24, 1996: SEQUENCING VLV. FAILED. CHS - AFTER TAKEOFF, CREW WOULD NOT GET THE MAIN GEAR TO RETRACT. THE GEAR WAS CYCLED TWICE. FLIGHT RETURNED TO CHS AND LANDED WITH NO FURTHER INCIDENT. AIRCRAF - [SDR USAA960005](https://openairdocs.org/sdr/USAA960005), Jan 3, 1996: FLOOR BEAM. CORRODED. PIT - DURING Q-1 INSPECTION, FOUND CORROSION .005 INCH TO .053 INCH ON FLOOR BEAM AT STATION 1127R FWD OF FRAME 4850. REPLACED SECTION OF BEAM FROM STATION 4850 - [SDR USAA960003](https://openairdocs.org/sdr/USAA960003), Jan 3, 1996: SKIN. DELAMINATION. PIT - DURING Q-1 INSPECTION, FOUND SKIN DELAMINATION LEFT STUB WING TO FUSELAGE AT STATION 24011 TO 26011. INSTALLED DOUBLER REPAIR PER USAIR EA NR 29492B AND E - [SDR USAA960002](https://openairdocs.org/sdr/USAA960002), Jan 3, 1996: SKIN. LIGHTNING STRIKE. PIT - DURING Q-1 INSPECTION, FOUND LIGHTNING STRIKE DAMAGE ABOVE CO-PILOTS SLIDING WINDOW IN FUSELAGE SKIN PITTED. INSTALLED FLUSH REPAIR PER USIAR EA NR 31049. - [SDR USAA960001](https://openairdocs.org/sdr/USAA960001), Jan 3, 1996: FLOOR BEAM. CORRODED. PIT - DURING Q-1 INSPECTION, FOUND CORROSION ON FLOOR BEAM BLO AT STATION 3845 T-CAP. REMOVED SECTION OF CORRODED T-CAP FROM STATION 3845 TO 5315 AND SPLICED IN - [SDR USAA960000](https://openairdocs.org/sdr/USAA960000), Jan 3, 1996: SKIN. DELAMINATION. PIT - DURING Q-1 INSPECTION, FOUND SKIN DELAMINATION RIGHT STUB WING TO FUSELAGE AT STATION 24011-26011. INSTALLED DOUBLER REPAIR PER USAIR EA NR 29492B AND EA - [SDR USAA951355](https://openairdocs.org/sdr/USAA951355), Dec 27, 1995: STRINGER. CORROSION. PIT - Q1/C2 INSPECTION, FOUND CORROSION ON STRINGER NR 3 STATION 11257. SPLICED IN NEW SECTION OF STRINGER PER SRM 51-70-06 REPAIR NR 5. (M) - [SDR USAA951354](https://openairdocs.org/sdr/USAA951354), Dec 27, 1995: STRINGER. CORRODED. PIT - Q1/C2 INSPECTION, FOUND CORROSION ON STRINGER NR 3 AT STATION 12791 TO STATION 13851. SPLICED IN NEW SECTION OF STRINGER NR 3 PER SRM 51-70-06 REPAIR NR 5 - [SDR USAA950409](https://openairdocs.org/sdr/USAA950409), Apr 25, 1995: FUEL VENT VALVE. FAILED. DCA - FLT 200 - ON TAKEOFF, TOWER ADVISED FLIGHT THAT FUEL WAS BEING SIPHONED OUT OF WING. FLIGHT RETURNED TO DCA WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANC - [SDR USAA950201](https://openairdocs.org/sdr/USAA950201), Mar 1, 1995: PRSOV. MALFUNCTIONED. PHL - FLT 0244 - CABIN PRESSURE CONTINUED TO CLIMB AT FL 330. CREW DECLARED AN EMERGENCY TO GET LOWER PRESSURE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPL - [SDR 95ZZZZ155](https://openairdocs.org/sdr/95ZZZZ155), Mar 1, 1995: VALVE. INOPERATIVE. PHL - FLT 0244 - CABIN PRESSURE CONTINUED TO CLIMB AT FL 330. CREW DECLARED AN EMERGENCY TO GET LOWER PRESSURE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPL - [SDR USAA950211](https://openairdocs.org/sdr/USAA950211), Feb 26, 1995: VALVE. INOPERATIVE. TPA - FLT 8003 - THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. CREW TRIED TO RECYCLE GEAR. GEAR REMAINED EXTENDED AND CREW RETURNED TO TPA. MAINTENANCE REPLACED THE - [SDR USAA950218](https://openairdocs.org/sdr/USAA950218), Feb 23, 1995: SWITCH. INTERMITTENT. CLT - FLT 2188 - AIRCRAFT LOST PRESSURIZATION AT FL 330 AND CABIN ALTITUDE WAS INCREASING. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLA - [SDR 95ZZZZ154](https://openairdocs.org/sdr/95ZZZZ154), Feb 23, 1995: SEALS. LEAKING. CLT - FLT 2188 - AIRCRAFT LOST PRESSURIZATION AT FL 330 AND CABIN ALTITUDE WAS INCREASING. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLA - [SDR USAA950149](https://openairdocs.org/sdr/USAA950149), Feb 20, 1995: VALVE. STICKING. PIT - FLT 428 - AT FL 330 GOT EXCESSIVE CABIN ALTITUDE MESSAGE. CABIN WAS APPROACHING 11,000 FEET. CREW DID EMERGENCY DESCENT IAW PROCEDURES. ALSO, TRIED MANUAL ## 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 19910309010919I](https://openairdocs.org/incident/19910309010919I), Mar 9, 1991: Fokker F28MK0100 (N856US), Pittsburgh, PA. Left lavatory smoke detector went off. Declared emergency and returned. Left lavatory water heater overheated. - [Incident 19900528025829I](https://openairdocs.org/incident/19900528025829I), May 28, 1990: Fokker F28MK0100 (N856US), Pittsburgh, PA, Minor damage. Left outboard wheel departed aircraft while taxiing to gate. Advised of loss by other aircraft. --- 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.