# N855US: 1989 Fokker F.28 MK 0100, registration cancelled 2007-06-12 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 12, 2007 - 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: 11283 - Year built: 1989 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 7, 1990 - Certificate issued: February 25, 2005 - Last registry action: February 25, 2005 - Mode S code: ABBBBE - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N855US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=855US - Page: https://openairdocs.org/deregistered/N855US-2007-06-12 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 (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAF02003](https://openairdocs.org/sdr/USAAF02003), Feb 12, 2002: O-RING. BROKEN. ORF-PHL - FLT 982 - DURING DESCENT, THE SYSTEM 1 HYDRAULIC LOW QUANTITY INDICATION ALERTED, FOLLOWED BY LOSS OF SYSTEM 1 HYDRAULICS. THE LANDING GEAR WAS LOWERE - [SDR USAAF01082](https://openairdocs.org/sdr/USAAF01082), Nov 5, 2001: WIRE. BROKEN. CLT - THE EMERGENCY FLOOR LIGHT AT SEAT ROW 4 WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE LIGHT. (M) - [SDR USAA011248](https://openairdocs.org/sdr/USAA011248), Sep 13, 2001: SKIN. DENTED. PIT - FOUND SKIN DENTED 4 INCHES BY 2 INCHES BY .125 INCHES, STATION 930.5 AT STRINGER 72. FILLER AND DOUBLER INSTALLED PER SRM 53-00-02. (M) - [SDR USAAF01023](https://openairdocs.org/sdr/USAAF01023), May 13, 2001: CONTROL PANEL. OVERHEATED. MKE-PIT - FLT 1455 - DURING THE FLIGHT, A 'HOT PLASTIC' SMELL WAS NOTD IN THE COCKPIT. THE LEFT WINDSHIELD HEAT BUTTON WAS SELECTED OFF AND THE SMELL DIMINISHED - [SDR USAA001978](https://openairdocs.org/sdr/USAA001978), Nov 4, 2000: SKIN. CANNING. PIT - FOUND SKIN OIL CANNING 3 INCH BY 5 INCH AREA, 11 INCHES AFT OF LOWER RADOME OPENING 4.75 INCH LEFT AC CENTER. INSTALLED DOUBLER PER EA 54843A. (M) - [SDR USAA001955](https://openairdocs.org/sdr/USAA001955), Nov 4, 2000: SKIN. CANNING. PIT - FOUND SKIN OIL CANNING 3 INCH BY 5 INCH AREA, 11 INCHES AFT LOWER RADOME OPENING 4.75 INCH LT AC CENTER LINE. INSTALLED DOUBLER (7.5 BY 11.875 INCH) PER E - [SDR USAAF00077](https://openairdocs.org/sdr/USAAF00077), Oct 25, 2000: LIGHT. INOPERATIVE. IND - FOUND THE LAST SECTION OF FIRST CLASS FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED AN EMERGENCY FLOOR LIGHT AT ROW FOUR. OPS CHECKED OK. - [SDR USAAF0007](https://openairdocs.org/sdr/USAAF0007), Oct 25, 2000: LIGHT. INOPERATIVE. IND - FOUND THE LAST SECTION OF FIRST CLASS FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. (M) - [SDR USAAF00061](https://openairdocs.org/sdr/USAAF00061), Aug 16, 2000: BATTERY PACK. DISCHARGED. DCA - FOUND THE COCKPIT EMERGENCY LIGHT. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY NR 1 AND NR 2. OPS CHECKS GOOD. (M) - [SDR USAA001432](https://openairdocs.org/sdr/USAA001432), Aug 3, 2000: SKIN. CRACKED. PIT - FOUND DOUBLER SKIN PANEL CRACKED 2 INCHES, NOSE GEAR TOP BAY COVER STATION 2475 FAR RIGHT SIDE. INSTALLED DOUBLER PER EA 55826. (M) - [SDR USAAF00018](https://openairdocs.org/sdr/USAAF00018), Feb 23, 2000: ACTUATOR. MALFUNCTIONED. CLT-GSP - FLT 1093 - RIGHT MAIN GEAR DISPLAYED NOT DOWN AND LANDING GEAR UNSAFE ON THE MFDU, AND ALSO RECEIVED THE LANDING GEAR TRANSIT INDICATION AND NO GREEN - [SDR USAAF99032](https://openairdocs.org/sdr/USAAF99032), Jun 12, 1999: MANIFOLD. FAILED. PIT-TOL - FLT 1045 - AFTER TAKEOFF, THE MFDS MESSAGE 1 INDICATED STAB TRIM CANNEL FAULT NR 1, NR 2, NR 3, YAW DAMPER CHANNEL NR 1, NR 2, AND 3 RUDDER CHANNEL FA - [SDR USAAF99006](https://openairdocs.org/sdr/USAAF99006), Jan 18, 1999: ENGINE. LIGHTNING STRIKE. PIT - FLT 717 - DURING DESCENT INTO PIT, AT AN ALTITUDE OF 7,000 FEET, THE AIRCRAFT SUSTAINED A LIGHTNING STRIKE. NUMEROUS FAULT MESSAGES ILLUMINATED. THE RIGHT - [SDR USAAF98094](https://openairdocs.org/sdr/USAAF98094), Dec 13, 1998: LIGHT. INOPERATIVE. IND - MAINTENANCE FOUND THE CEILING EMERGENCY/STANDBY LIGHT INOPERATIVE AT ROW 15. REPLACED THE LIGHT ASSEMBLY. (M) - [SDR USAA970268](https://openairdocs.org/sdr/USAA970268), Aug 22, 1997: SKIN. DAMAGED. PIT - DURING C4 CHECK, FOUND HEAT DAMAGE TO SKIN AND STRINGER AT APU OUTLET AREA, STATION 27250 AND STR 46. INSTALLED EXTERNAL DOUBLER REPAIR 20 INCH BY 16 INCH - [SDR USAAF97035](https://openairdocs.org/sdr/USAAF97035), Apr 8, 1997: SELECTOR VALVE. FAILED. FLT 864 - PIT-DTW - ON FINAL APPROACH TO DTW, RECEIVED A NOSE GEAR NOT DOWN INDICATION. ATC VERIFIED THE GEAR WAS NOT DOWN. CREW PERFORMED ALTERNATE GEAR EXTENS - [SDR USAAF96032](https://openairdocs.org/sdr/USAAF96032), Apr 12, 1996: SYNCHRONIZER. FAILED. CLT - FLT 1138 - AFTER TAKEOFF FROM CLT, CREW NOTED A FLAP DISAGREEMENT. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR - [SDR USAAF96022](https://openairdocs.org/sdr/USAAF96022), Feb 13, 1996: STAB CONTRL UNIT. FAILED. PIT - FL 862 - CREW RECEIVED HYDRAULIC STAB CHANNEL 2 FAULT. AFTER PERFORMING APPLICABLE PROCEDURE, RECEIVED CHANNEL 1 FAULT ALSO. MAINTENANCE REPLACED THE HORI - [SDR USAA960244](https://openairdocs.org/sdr/USAA960244), Feb 12, 1996: SKIN. DELAMINATED. PIT - DURING Q-1 CHECK INSPECTION, FOUND FUSELAGE SKIN DELAMINATION LEFT SIDE STUB WING LAY AREA AT FRAME STATION 24011. INSTALLED DOUBLER REPAIR PER USAIR EA N - [SDR USAA960243](https://openairdocs.org/sdr/USAA960243), Feb 12, 1996: SKIN. DELAMINATED. PIT - DURING Q-1 CHECK INSPECTION, FOUND FUSELAGE SKIN DELAMINATION RIGHT SIDE STUB WING LAY AREA AT FRAME STATION 23011. INSTALLED DOUBLER REPAIR PER USAIR EA - [SDR USAA960242](https://openairdocs.org/sdr/USAA960242), Feb 12, 1996: FRAME. CRACKED. PIT - DURING Q-1 CHECK INSPECTION, FOUND 1 INCH CRACK, FRAME STATION 14911 BL 883 R (HFEC INSPECTION). STOP DRILLED CRACK AND INSTALLED DOUBLERS PER USAIR EA NR - [SDR USAA960241](https://openairdocs.org/sdr/USAA960241), Feb 12, 1996: FRAME. CRACKED. PIT - DURING Q-1 CHECK INSPECTION, FOUND 3 INCH CRACK FRAME STATION 1491 BL 883L HIGH FREQUENCY EDDY CURRENT INSPECTION. STOP DRILLED CRACK AND INSTALLED DOUBLE - [SDR USAA950854](https://openairdocs.org/sdr/USAA950854), Jul 12, 1995: STRINGER. CRACKED. PIT - DURING C-CHECK INSPECTION, FOUND 2 INCH CRACK AND STRINGER NR 68R APPROXIMATELY 4 INCHES AFT OF STATION 3870. INSTALLED SPLICE REPAIR PER SRM 51-70-06 REP ## FAA accident and incident reports (5) 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 20000726036039I](https://openairdocs.org/incident/20000726036039I), Jul 26, 2000: Fokker F28MK0100 (N855US), Syracuse, NY. (-23)On Wednesday, July 26, 2000, U.S. Airways flight 1802, an F-100, N855US, was enroute from pittsburg, pa (pit) to new york, NY (lga) when the crew noted a… - [Incident 19990713023619I](https://openairdocs.org/incident/19990713023619I), Jul 13, 1999: Fokker F28MK0100 (N855US), Buffalo, NY. (-23) On Tuesday, July 13, 1999, at 1842 local, a usairways F100, N855US, reported a flap asymmetry problem inbound to Buffalo niagara airport. The aircraft… - [Incident 19931128048449I](https://openairdocs.org/incident/19931128048449I), Nov 28, 1993: Fokker F28MK0100 (N855US), Albany, NY. Smoke in cabin en route. Diverted to Albany. Found left pack contaminated with oil. - [Incident 19920514018219I](https://openairdocs.org/incident/19920514018219I), May 14, 1992: Fokker F28MK0100 (N855US), Des Moines, IA. NR1 hydraulic system low quantity light on. Found a crack in left MLG down line and leak in NR1 engine reverser. - [Incident 19900126009999I](https://openairdocs.org/incident/19900126009999I), Jan 26, 1990: Fokker F28MK0100 (N855US), Boston, MA. Experienced loss of fuel flow to left engine. Engine flamed out. An unsuccessful relight was attempted. --- 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.