# N854US: 1989 Fokker F.28 MK 0100, registration cancelled 2007-04-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 26, 2007 - Exported to: Myanmar - 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: 11282 - Year built: 1989 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 7, 1990 - Certificate issued: December 20, 2006 - Last registry action: December 20, 2006 - Mode S code: ABB807 - Owner when cancelled: [Aircraft Finance Services Inc Trustee](https://openairdocs.org/faa-owner/AIRCRAFT%20FINANCE%20SERVICES%20INC%20TRUSTEE) - 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/N854US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=854US - Page: https://openairdocs.org/deregistered/N854US-2007-04-26 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 (19) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAF01052](https://openairdocs.org/sdr/USAAF01052), Jul 25, 2001: SLIDE. PIT - DURING THE A-CHECK, THE FORWARD RIGHT EXIT DOOR SLIDE GIRT BAR WAS FOUND UNATTACHED TO THE SLIDE GIRT. MAINTENANCE ATTACHED THE SLIDE GIRT BAR. OK FOR SER - [SDR USAAF01004](https://openairdocs.org/sdr/USAAF01004), Jan 25, 2001: DAMPER. MALFUNCTIONED. PIT-ERI - FLT 257 - AFTER TAKEOFF, THE LANDING GEAR DID NOT RETRACT WHEN SELECTED UP. THE LANDING GEAR WAS RECYCLED, BUT STILL DID NOT RETRACT. THE FLIGHT THEN - [SDR USAAF99049](https://openairdocs.org/sdr/USAAF99049), Oct 2, 1999: POWER SUPPLY. INOPERATIVE. IND - FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 10 AND 15 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY. (M) - [SDR USAA990054](https://openairdocs.org/sdr/USAA990054), Jan 14, 1999: BEAM. CORRODED. PIT - DURING CORROSION TRACK VISIT FOUND .75 INCH BY .25 INCH CORROSION AND .75 INCH BY .25 INCH CORROSION. BOTH AREAS CORRODED AT CENTER CARGO BEAM AT STRINGER - [SDR USAA990051](https://openairdocs.org/sdr/USAA990051), Jan 14, 1999: FLOORBEAM. CORRODED. PIT - DURING UNSCHEDULED MAINTENANCE, FOUND CORROSION ON FLOORBEAM AT 1127R FROM STATION 4610 TO SPLICE AFT OF 5805. DOUBLERS WERE INSTALLED UNDER FLOORBEAM TO - [SDR USAAF98047](https://openairdocs.org/sdr/USAAF98047), Jun 2, 1998: DAMPER. FAILED. PIT - FLT 1696 - AFTER DEPARTURE FROM PIT, 'RT MLG' MESSAGE APPEARED ON MULTIFUNCTION DISPLAY AND BLUE INTRANSIT LIGHTS REMAINED ON IN GEAR HANDLE. CREW RECYCLE - [SDR USAAF98060](https://openairdocs.org/sdr/USAAF98060), Jun 1, 1998: SLIDE. RUPTURED. PIT - DURING AN ANNUAL ESCAPE SLIDE OPERATION CHECK SAMPLING PROGRAM, THE FORWARD ENTRY DOOR SLIDE FAILED TO HOLD INFLATION PRESSURE DUE TO TWO HOLES IN THE SLI - [SDR USAAF98020](https://openairdocs.org/sdr/USAAF98020), Feb 21, 1998: INVERTER. INOPERATIVE. PIT - FORWARD FLOOR PROXIMITY LIGHTS FOUND INOPERATIVE. MAINTENANCE REPLACED THE FLOOR PROXIMITY INVERTER. (M) - [SDR USAAF98013](https://openairdocs.org/sdr/USAAF98013), Feb 7, 1998: SELECTOR VALVE. FAILED. FLT 775 - PIT-MCI - DURING FINAL APPROACH TO MCI WHEN LANDING GEAR SELECTED DOWN, CREW DID NOT RECEIVE A GREEN 'NOSE GEAR DOWN AND LOCKED' INDICATION. CREW RECY - [SDR USAAF98012](https://openairdocs.org/sdr/USAAF98012), Feb 6, 1998: BULB. FAILED. FLT 1158 - RIC-PHL - ON FINAL APPROACH TO PHL, NOSE GEAR DOWN AND LOCKED GREEN INDICATOR DID NOT ILLUMINATE. CREW RECYCLED GEAR AND ALL INDICATORS ILLUMINATED N - [SDR USAAF98010](https://openairdocs.org/sdr/USAAF98010), Jan 30, 1998: SWITCH. FAILED. FLT 1275 - PIT-MSP - ON CLIMB-OUT FROM PIT WITH CLIMB POWER SET, 'WING ANTI-ICE LOW CAPACITY' MESSAGE ANNUNCIATED ON MULTI FUNCTION DISPLAY. DUE TO WEATHER COND - [SDR USAAF97018](https://openairdocs.org/sdr/USAAF97018), Feb 12, 1997: SWITCH. FAILED. CLT/SDF - FLT 2321 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RLG DOWNLOCK SWITCH WARNING DISPLAYED ON MULTIFUNCTION DISPLAY UNIT. CAPTAIN RECYCLED THE LA - [SDR USAAF96083](https://openairdocs.org/sdr/USAAF96083), Jul 29, 1996: BATT SUPPLY UNIT. DISCHARGED. MCI - EMERGENCY FLOOR LIGHTING SYSTEM INOPERATIVE WITH SWITCH IN ON POSITION. AIRCRAFT FERRIED TO CLT. MAINTENANCE REPLACED FOUR BATTERY SUPPLY UNITS. (M) - [SDR USAAF96046](https://openairdocs.org/sdr/USAAF96046), May 17, 1996: RETRACT MECH. MALFUNCTIONED. CLT - FL 494 - AFTER TAKEOFF FROM CLT, CAPTAIN COULD NOT RETRACT LANDING GEAR. MANUAL OVERRIDE WAS ATTEMPTED AND UNSUCCESSFUL. NO EMERGENCY WAS DECLARED AND THE - [SDR USAAF96021](https://openairdocs.org/sdr/USAAF96021), Feb 11, 1996: RELAY. FAILED. LGA- FLT 301 - UPON GEAR EXTENSION, THE CABIN STANDBY LIGHTS AND EXIT IDENTIFIERS DID NOT ILLUMINATE. MAINTENANCE REPLACED THE K2618A RELAY. (M) - [SDR USAA950914](https://openairdocs.org/sdr/USAA950914), Aug 23, 1995: CURRENT SENSOR. FAILED. PIT - FLT 967 - DURING CLIMB-OUT FROM PIT, CREW RECEIVED A STALL WARNING FAULT MESSAGE. CREW WAS ADVISED TO RETURN TO FIELD FOR REPAIRS. NON EMERGENCY AND NO OT - [SDR USAA950811](https://openairdocs.org/sdr/USAA950811), Jul 13, 1995: SKIN. DELAMINATION. PIT - DURING Q-1 CHECK INSPECTION, FOUND 14 INCH BY 24 INCH AREA OF DELAMINATION AT STATION 24011 AND 24611 RIGHT SIDE FUSELAGE SKIN. INSTALLED TITANIUM DOUBLER - [SDR USAA950810](https://openairdocs.org/sdr/USAA950810), Jul 13, 1995: SKIN. DELAMINATED. PIT - DURING Q-1 CHECK INSPECTION, FOUND 14 INCH BY 24 INCH AREA OF DELAMINATION AT STATION 24011 LEFT FUSELAGE SKIN. INSTALLED TITANIUM DOUBLER REPAIR PER USAI - [SDR USAA950812](https://openairdocs.org/sdr/USAA950812), Jun 29, 1995: SKIN. DENTED. PIT - DURING Q-1 CHECK INSPECTION, FOUND A DENT .085 INCH DEEP LEFT SIDE FUSELAGE STATION 5805. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-02 PG 201 AND 51-70-06 ## 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 19930916038919I](https://openairdocs.org/incident/19930916038919I), Sep 16, 1993: Fokker F28MK0100 (N854US), Kansas City, MO. Losing hydraulic quantity. Turned off until on approach. Landed safely. Pin hole in high pressure line. - [Incident 19910105002369I](https://openairdocs.org/incident/19910105002369I), Jan 5, 1991: Fokker F28MK0100 (N854US), Pittsburgh, PA. Experienced a NR1 DC bus failure on climbout. Returned. NR1 tru transformer rectifier had failed. --- 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.