# N860US: 1990 Fokker F.28 MK 0100, registration cancelled 2004-08-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 23, 2004
- Exported to: Nigeria
- 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: 11295
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 6, 1990
- Certificate issued: November 14, 2003
- Last registry action: December 11, 2003
- Mode S code: ABD0AA
- 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/N860US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=860US
- Page: https://openairdocs.org/deregistered/N860US-2004-08-23

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 (16)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR USAA010799](https://openairdocs.org/sdr/USAA010799), Jul 14, 2001: BEAM. PIT - FOUND APU INLET RIGHT BEAM WITH HOLE 2.5 INCHES BY 4 INCHES APU AIR INLET BEAM, FUSELAGE RIGHT STATION 22516-26026. MANUFACTURED REPAIR SPLICE AND CORNER 
- [SDR USAAF00064](https://openairdocs.org/sdr/USAAF00064), Aug 21, 2000: LIGHT. INOPERATIVE. PIT - FOUND THE FORWARD OVERHEAD CENTER AISLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPS CHECK GOOD. (M)
- [SDR USAAF00063](https://openairdocs.org/sdr/USAAF00063), Aug 17, 2000: LEVER. WORN. ORF - FLT 471 - EN ROUTE LGA-RIC, AT FL180, THE NR 1 ENGINE THRUST REVERSER DEPLOY LIGHT CAME ON WHILE ON DESCENT, FOLLOWED BY PRONOUNCED BUFFETING. THE NR 1 EN
- [SDR USAAF99056](https://openairdocs.org/sdr/USAAF99056), Dec 5, 1999: ENGINE. FAILED. MCO - FLT 7001 - ON CLIMB-OUT, EXPERIENCED ENGINE THRUST FLUCTUATION IN NR 1 ENGINE. ENGINE FAIL LIGHT CAME ON AND WENT OFF RIGHT AWAY. CAPTAIN THEN DECLARED AN
- [SDR USAAF99047](https://openairdocs.org/sdr/USAAF99047), Sep 24, 1999: LIGHT. INOPERATIVE. IND - FOUND FLOOR EMERGENCY LIGHTS IN THE FIRST CLASS SECTION INOPERATIVE. MAINTENANCE REPLACED BOTH LIGHT STRIPS. (M)
- [SDR USAAF98078](https://openairdocs.org/sdr/USAAF98078), Sep 15, 1998: BATTERY PACK. DISCHARGED. GSO - EMERGENCY EXIT SIGN AT ENTRY DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)
- [SDR USAAF98052](https://openairdocs.org/sdr/USAAF98052), Jun 30, 1998: POWER SUPPLY. INOPERATIVE. IND - EMERGENCY EXIT SIGN ABOVE GALLEY DOOR WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NR 9 POWER SUPPLY. (M)
- [SDR USAAF98054](https://openairdocs.org/sdr/USAAF98054), May 7, 1998: DAMPER. FAILED. PIT - FLT 434 - AFTER TAKEOFF FROM PIT, 'L MLG DOOR' MESSAGE APPEARED ON DISPLAY. CREW RECYCLED GEAR WITH SAME RESULT. FLT RETURNED TO PIT AND LANDED WITHOUT FU
- [SDR USAAF98038](https://openairdocs.org/sdr/USAAF98038), Apr 21, 1998: POWER SUPPLY. INOPERATIVE. RIC - MAINTENANCE FOUND THE FORWARD EMERGENCY FLOOR LIGHTING INOPERATIVE. THEY REPLACED THE POWER SUPPLY AND BATTERY PACK. REF: OPERATOR CONTROL NR 98ZZZX2057. 
- [SDR 98ZZZX2057](https://openairdocs.org/sdr/98ZZZX2057), Apr 21, 1998: BATTERY PACK. DISCHARGED. RIC - MAINTENANCE FOUND THE FORWARD EMERGENCY FLOOR LIGHTING INOPERATIVE. THEY REPLACED THE POWER SUPPLY AND BATTERY PACK. (REF: OPERATOR CONTROL NR USAAF98038.
- [SDR USAAF98015](https://openairdocs.org/sdr/USAAF98015), Feb 13, 1998: TRANSDUCER. FAILED. FLT 864 - PIT-DTW - AT ROTATION THE STICK SHAKER WARNING SYSTEM ACTIVATED ALONG WITH A STALL WARNING LIGHT. IT WAS TOO LATE FOR AN ABORTED TAKEOFF, SO CAPTAIN C
- [SDR USAAF97071](https://openairdocs.org/sdr/USAAF97071), Aug 31, 1997: BULB. FAILED. PIT/MSY - FLT 474 - AFTER TAKEOFF FROM PIT, CREW RECEIVED A FUEL SUCTION FEED MESSAGE AND THE FUEL FLOW BAR ENG 2 WAS NOT LIT. THE AIRCRAFT RETURNED TO PIT WITH
- [SDR USAAF96132](https://openairdocs.org/sdr/USAAF96132), Dec 29, 1996: CONNECTOR. LOOSE. FLT 946 - MEM-PIT - ON CLIMB-OUT, THE MID CARGO DORO UNSAFE LIGHT ILLUMINATED. THE FLIGHT RETURNED TO MEM WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE MID CA
- [SDR USAAF96127](https://openairdocs.org/sdr/USAAF96127), Dec 17, 1996: LOCK PLATE. BROKEN. PIT - FL 1193 - CREW RECIEVED BLUE LIGHT IN GEAR HANDLE AND MFDU MESSAGE 'R MLG' AFTER TAKEOFF. CREW CYCLED THE GEAR AND RECEIVED NORMAL INDICATIONS. CREW DECID
- [SDR USAAF96106](https://openairdocs.org/sdr/USAAF96106), Oct 16, 1996: SENSOR. OUT OF ADJUST. FLT 388 - RIC-PIT, AFTER TAKEOFF, LANDING GEAR WOULD NOT COME UP. GROUND/FLT ALERT MESSAGE ON MFDU. NO EMERGENCY DECLARED. FLIGHT RETURNED TO RIC WITHOUT FURTHE
- [SDR USAA950775](https://openairdocs.org/sdr/USAA950775), Jul 28, 1995: LOCK. BROKEN. MSP - FLT 0232 - THE LEFT LANDING GEAR DOOR DID NOT LOCK UPON GEAR RETRACTION. THE GEAR WAS CYCLED TWICE BUT THE LIGHT WOULD NOT EXTINGUISH. MAINTENANCE INSTALL

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB NYC00IA231](https://openairdocs.org/ntsb/NYC00IA231), Aug 17, 2000: Fokker F-100 (N860US), Norfolk, VA, incident, no damage. Probable cause: The failure of the airplane's ground/flight switch and a malfunction of the thrust reverser deploy switch, which resulted in an in-flight thrust reverser deployment.

## 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 20000817026129I](https://openairdocs.org/incident/20000817026129I), Aug 17, 2000: Fokker F28MK0100 (N860US), Norfolk, VA. (-23) On 8/17/2000 at 1522 EDT, a U.S. Airways flight 471 was enroute from lga to ric, when flight 471 diverted to orf and landed on runway 05 after the left…

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