# N861US: 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: 11297 - 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 17, 2003 - Last registry action: December 11, 2003 - Mode S code: ABD461 - 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/N861US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=861US - Page: https://openairdocs.org/deregistered/N861US-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 (29) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAF01071](https://openairdocs.org/sdr/USAAF01071), Sep 4, 2001: BATTERY. INOPERATIVE. RDU - THE FLOOR STRIP EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M) - [SDR USAAF01015](https://openairdocs.org/sdr/USAAF01015), Apr 19, 2001: BATTERY PACK. DISCHARGED. GSO - THE SECOND STRIP OF FLOOR ESCAPE LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPS CHECKED OK. (M) - [SDR USAAF00075](https://openairdocs.org/sdr/USAAF00075), Oct 22, 2000: BATTERY PACK. FAULTY. IND - FOUND THE LEFT LOWER BELLY FAIRING EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY. OPS CHECKED OK. (M) - [SDR USAAF00038](https://openairdocs.org/sdr/USAAF00038), May 14, 2000: BATTERY. DISCHARGED. PIT - FOUND AFT SECTION FLOOR LEVEL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY AND BATTERY. OPS CHECKED GOOD. (M) - [SDR USAAF00035](https://openairdocs.org/sdr/USAAF00035), May 7, 2000: BULB. FAILED. GSO-CLT - FLT 1476 - LEFT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE WHEN GEAR WAS LOWERED. THERE WAS NO ABNORMAL INDICATION ON THE MULTIFUNCTION DISPLAY UNIT. - [SDR USAA000646](https://openairdocs.org/sdr/USAA000646), Apr 18, 2000: PLATE. CRACKED. PIT - FOUND TWO CRACKS ON DOUBLER LEFT 1 INCH AND .625 INCH AND 3 CRACKS RIGHT SIDE, .125 INCH .125 INCH AND .375 INCH, WL PLUS 1359 AND OBLIQUE FRAME 67-2. ROU - [SDR USAAF00021](https://openairdocs.org/sdr/USAAF00021), Feb 26, 2000: LIGHT. INOPERATIVE. IND - THE AFT SECTION OF FIRST CLASS FLOOR FLEX EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES, OPS CHECKED GOOD. (M) - [SDR USAAF00016](https://openairdocs.org/sdr/USAAF00016), Feb 18, 2000: ENGINE. MALFUNCTIONED. CLE-CLT - FLT 2173, AT FL270, NEAR CLT, THE CREW GOT A HIGH VIBRATION MESSAGE FOR THE NR 2 ENGINE. THE POWER WAS REDUCED TO IDLE AND BROUGHT BACK UP TO SEE IF T - [SDR USAAF99040](https://openairdocs.org/sdr/USAAF99040), Aug 4, 1999: RELAY. INOPERATIVE. CLT - FLT 1160 - THE EMERGENCY EXIT ADVISORY LIGHTS DID NOT ILLUMINATED WHEN THE GEAR WAS LOWERED. MAINTENANCE REPLACED THE K2618A RELAY. (M) - [SDR USAA990250](https://openairdocs.org/sdr/USAA990250), Mar 16, 1999: DOUBLER. GOUGED. PIT - DURING C-1 CHECK, FOUND ICE SCRAPER SCREWS GOUGED DOUBLER IN 3 PLACES (.250 L BY .03125 D) (.9375 L BY .032 D) (1.750 L BY .015625 D) AT LEFT VERT STABILI - [SDR USAAF99008](https://openairdocs.org/sdr/USAAF99008), Jan 25, 1999: WINDOW. LOOSE. CLT - FLT 8076 - AFTER TAKEOFF FROM CLT, THE LEFT COCKPIT SLIDING WINDOW WAS MAKING A LARGE AIR LEAK NOISE. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHE - [SDR USAAF98069](https://openairdocs.org/sdr/USAAF98069), Aug 19, 1998: BATTERY PACK. DISCHARGED. RIC - FOUND REAR FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (X) - [SDR USAAF98051](https://openairdocs.org/sdr/USAAF98051), Jun 19, 1998: COMPUTER. FAILED. CLT - FLT 1635 - AT APPROXIMATELY 4000 FT IN CLIMB-OUT FROM CLT, CREW RECEIVED THE FOLLOWING MESSAGES ON THE MULTIFUNCTION DISPLAY, 'STAB TRIM 1 AND 2, YD 1 AND - [SDR USAAF97098](https://openairdocs.org/sdr/USAAF97098), Nov 26, 1997: POWER SUPPLY. INOPERATIVE. PIT - FL 1239 PILOT REPORTED THAT THE FIRST CLASS FLOOR LEVEL LIGHTING WAS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPS CEHCK GOOD. (M) - [SDR USAAF97095](https://openairdocs.org/sdr/USAAF97095), Nov 20, 1997: CONDUIT. FAILED. PHL/MSP - FLT 1283 - ON APPROACH TO MSP WHEN LANDING GEAR WAS EXTENDED, AN UNSAFE RT GEAR INDICATION OCCURRED. THE CREW RECYCLED THE GEAR, BUT THE UNSAFE RT GEA - [SDR USAAF97077](https://openairdocs.org/sdr/USAAF97077), Sep 28, 1997: RETRACT CABLE. LACK OF LUBE. FLT 593 - PIT-CRW - AFTER TAKEOFF FROM PIT, CREW WAS UNABLE TO RAISE GEAR HANDLE. OVERRIDE WAS NO HELP. NO EMERGENCY WAS DECLARED AND FIGHT RETURNED TO PIT WITH - [SDR USAAF97063](https://openairdocs.org/sdr/USAAF97063), Jul 21, 1997: BATTERY PACK. DISCHARGED. FIRST CLASS EMERGENCY LIGHTING FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 9 EMERGENCY LIGHT BATTERY CHARGER AND BATTERY PACK. (M) - [SDR 97ZZZM774](https://openairdocs.org/sdr/97ZZZM774), Jul 21, 1997: BATTERY PACK. FAILED. PIT - FIRST CLASS EMERGENCY LIGHTING FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 9 EMERGENCY LIGHT BATTERY CHARGER AND BATTERY PACK. (M) - [SDR USAAF97044](https://openairdocs.org/sdr/USAAF97044), May 8, 1997: LIGHT. SHORTED. RDU - EXIT LIGHTING CIRCUIT BREAKER (LOCATION 17G) TRIPPED AND WOULD NOT RESET. OVERWING EMERGENCY EXIT AND FLOOR LIGHTING WAS INOPERATIVE. MAINTENANCE FOUND LE - [SDR USAAF97029](https://openairdocs.org/sdr/USAAF97029), Mar 15, 1997: SEQUENCE VLV. FAILED. MSP - FL 1543 - ON GEAR EXTENSION, THE NOSE GEAR DID NOT LOWER. CREW BROKE OFF APPROACH AND BEGAN TOWER FLY-BY. THE NOSE GEAR DID DROP AND LOWER CONFIRMED GEAR - [SDR USAAF96117](https://openairdocs.org/sdr/USAAF96117), Nov 14, 1996: UNSAFE LIGHT. ILLLUMINATED. FLT 7900 - PIT - DLIGHT WAS A MAINTENANCE TEST FLIGHT. LEFT MAIN GEAR SHOWED AN UNSAFE CONDITION. RECYCLED GEAR AND ALL THREE INDICATIONS WERE NORMAL. CAPTAIN R - [SDR 96ZZZM1558](https://openairdocs.org/sdr/96ZZZM1558), Nov 14, 1996: DOOR ASSY. DAMAGED. FLT 7900 - PIT - FLIGHT WAS A MAINTENANCE TEST FLIGHT. LEFT MAIN GEAR SHOWED AN UNSAFE CONDITION. RECYCLED GEAR AND ALL THREE INDICATIONS WERE NORMAL. CAPTAIN R - [SDR 96ZZZM1557](https://openairdocs.org/sdr/96ZZZM1557), Nov 14, 1996: UPLOCK ASSY. MALFUNCTIONED. FLT 7900 - PIT - FLIGHT WAS A MAINTENANCE TEST FLIGHT. LEFT MAIN GEAR SHOWED AN UNSAFE CONDITION. RECYCLED GEAR AND ALL THREE INDICATIONS WERE NORMAL. CAPTAIN R - [SDR 96ZZZM1556](https://openairdocs.org/sdr/96ZZZM1556), Nov 14, 1996: UPLOCK ASSY. MALFUNCTIONED. FLT 7900 - PIT - FLIGHT WAS A MAINTENANCE TEST FLIGHT. LEFT MAIN GEAR SHOWED AN UNSAFE CONDITION. RECYCLED GEAR AND ALL THREE INDICATIONS WERE NORMAL. CAPTAIN R - [SDR USAA960739](https://openairdocs.org/sdr/USAA960739), Nov 13, 1996: SKIN. DELAMINATED. PIT - DURING Q-1 CHECK, FOUND SKIN DISBONDED/DELAMINATION AT STATION 24011, STRINGER RT 51. INSTALLED FASTENERS LEFT SIDE AND SKIN REPAIR RIGHT SIDE PER USAIR E - [SDR USAA960738](https://openairdocs.org/sdr/USAA960738), Nov 13, 1996: BULKHEAD ANGLE. CRACKED. PIT - DURNIG Q-1 CHECK, FOUND TWO 3 INCH CRACKS IN ADDITION TWO NESTED ANGLES CRACKED .75 AFT CENTER PRESSURE BULKHEAD, CRACKS FOUND SUBJECT ANGLE ONE AT STRING - [SDR USAAF96067](https://openairdocs.org/sdr/USAAF96067), Jun 27, 1996: UPLOCK STOP. FAILED. PHL - FLT 701 - AFTER TAKEOFF, CREW HAD RIGHT LANDING GEAR SELECTOR LIGHT ON THE MFDU. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE R - [SDR USAA950751](https://openairdocs.org/sdr/USAA950751), Jul 9, 1995: SWITCH. FAULTY. CLT - FLT 446 - ON TAKEOFF, CREW RECEIVED AN ALERT MESSAGE OF A NR 1 HYDRAULIC SYSTEM FAILURES. CAPTAIN DECLARED AN EMERGENCY AND LANDED IN CLT. MAINTENANCE FOU - [SDR USAA950202](https://openairdocs.org/sdr/USAA950202), Feb 28, 1995: CONNECTOR. NOT SEATED. PIT - FLT 1842 - UPON TURNING WING ANTI-ICE ON, CREW RECEIVED A WING ANTI-ICE FAULT. FLIGHT RETURNED TO PIT WITHOUT INCIDENT. MAINTENANCE SEATED PIN HH IN CONNE ## 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 20001229037789I](https://openairdocs.org/incident/20001229037789I), Dec 29, 2000: Fokker F28MK0100 (N861US), Middletown, PA. (-23) Pilot reported that "going through 1000 ft AGL, aircraft pitched up to approx. 25 degrees nose up. Airspeed started bleeding off. Disconnected autopilot.… - [Incident 19900912059089I](https://openairdocs.org/incident/19900912059089I), Sep 12, 1990: Fokker F28MK0100 (N861US), Syracuse, NY. Loss of hydraulic system quantity. Precautionary landing. Leak at quick disconnect fitting of right engine pump. --- 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.