# N887US: 1991 Fokker F.28 MK 0100, registration cancelled 2004-08-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 2, 2004
- Exported to: Australia
- 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: 11349
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 6, 1991
- Certificate issued: July 2, 2004
- Last registry action: July 2, 2004
- Mode S code: AC39A9
- 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/N887US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=887US
- Page: https://openairdocs.org/deregistered/N887US-2004-08-02

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 (20)

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

- [SDR USAAF01033](https://openairdocs.org/sdr/USAAF01033), Jun 15, 2001: COALESCER BAG. CONTAMINATED. TRI-CLT - FLT 242 - THE AIRCONDITIONING PACKS PRODUCED AN ODOR DURING CRUISE AND WOULD NOT COOL THE CABIN. THE FLIGHT CONTINUED AND LANDED IN CLT WITHOUT FURTHE
- [SDR USAA010588](https://openairdocs.org/sdr/USAA010588), May 19, 2001: FRAME. CRACKED. PIT - FOUND FRAME CRACKED 1.25 INCH, LEFT SIDE TOP OF OBLIQUE FRAME 67.2. TEMPORARY REPAIR WITH STOP DRILL PER EA 71082 AND SRM 51-22-01. (M)
- [SDR USAAF01016](https://openairdocs.org/sdr/USAAF01016), Apr 25, 2001: WIRE. DAMAGED. IND- A SECTION OF FLOOR ESCAPE LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED WIRING TO LIGHT STRIP. OPS CHECKED OK. (M)
- [SDR USAAF01005](https://openairdocs.org/sdr/USAAF01005), Jan 31, 2001: ACTUATOR. BROKEN. PHL-SYR - FLT 768 - AFTER GEAR UP WAS SELECTED, A LOUD FLUTTERING NOISE WAS PRESENT WITH A NOSE LANDING GEAR INDICATION LIGHT. THE FLIGHT RETURNED TO PHL AND MA
- [SDR USAAF99059](https://openairdocs.org/sdr/USAAF99059), Dec 31, 1999: SWITCH. OUT OF POSITION. CLT-IAH - FLT 463 - DURNG CLIMB-OUT FROM CLT, CAPTAIN RECEIVED AUTO FUEL CROSSFEED FAIL ALERT. ALSO, CLT TOWER ADVISED THAT THERE WAS SUBSTANTIAL FUEL ESCAPING 
- [SDR USAAF99039](https://openairdocs.org/sdr/USAAF99039), Aug 3, 1999: BATTERY PACK. DISCHARGED. IND - FOUND FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)
- [SDR USAAF98097](https://openairdocs.org/sdr/USAAF98097), Dec 18, 1998: TRIM SYSTEM. MALFUNCTIONED. CLT - FLT 2208 - ON CLIMB-OUT FROM CLT, CREW RECEIVED A DOUBLER STAB TRIM FAULT INDICATION. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENA
- [SDR USAAF98062](https://openairdocs.org/sdr/USAAF98062), Jul 26, 1998: CONTROL BOX. FAILED. CLT - FLT 476 - AFTER TAKEOFF FROM CLT, WHEN LANDING GEAR WAS RETRACTED, 'ANTI-SKID' FAULT MESSAGE APPEARED. FLIGHT RETUREND TO CLT. MESSAGE REMAINED ON UNTIL L
- [SDR USAAF98032](https://openairdocs.org/sdr/USAAF98032), Mar 25, 1998: DOWNLOCK PIN. NOT ENGAGED. PWM - FLT 1824 - ON APPROACH, NOSE GEAR WAS SHOWING AN UNSAFE NOSE LIGHT. AIRCRAFT DID A GO-AROUND. CAPTAIN DECIDED TO FREE FALL THE NOSE GEAR AND GOT A GREEN L
- [SDR USAAF98025](https://openairdocs.org/sdr/USAAF98025), Mar 4, 1998: SWITCH. FAILED. CLT - FLT 1210 - ON CLIMB-OUT OF CLT AIRCRAFT HAD A WING ANTI-ICE FAULT TWICE BETWEEN 9000 FEET - 11,000 FEET. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT 
- [SDR USAA980051](https://openairdocs.org/sdr/USAA980051), Mar 1, 1998: SKIN. DELAMINATED. PIT - DURING Q-1 CHECK, FOUND RT SKIN DELAMINATION AND SIGNS OF DISCOLORATION BETWEEN FRAMES 23011 AND 24611 AT STRINGER 53. CUT OUT DAMAGED AREA AND INSTALLED 
- [SDR USAAF97097](https://openairdocs.org/sdr/USAAF97097), Nov 25, 1997: ENGINE. VIBRATION. IND - FLT 1057 - EN ROUTE, CREW EXPERIENCED HIGH VIBRATION ON THE LEFT ENGINE. CREW WAS ABLE TO CONTROL THE VIBRATION BY REDUCING THE ENGINE EPR. VIBRATION RETU
- [SDR USAAF97066](https://openairdocs.org/sdr/USAAF97066), Jul 27, 1997: THRUST PLATE. DIRTY. PHL/ROC - FLT 504 - ON APPROACH TO ROC WHEN THE LANDING GEAR WAS EXTENDED, A 'NOSE GEAR UNSAFE' WARNING ILLUMINATED ALONG WITH NO ILLUMINATION OF GREEN 'NOSE GE
- [SDR USAAF97046](https://openairdocs.org/sdr/USAAF97046), May 13, 1997: BULB. FAILED. FLT 2228 - DCA-CLT - ON APPROACH TO CLT, DID NOT RECEIVE A GREEN DOWN AND LOCKED INDICATION FOR THE RIGHT MAIN GEAR. CAPTAIN ELECTED TO PERFORM A GO AROUND PROC
- [SDR USAAF97031](https://openairdocs.org/sdr/USAAF97031), Mar 15, 1997: FIRE WARNING. ACTIVATED. ERI - FL 1202 - ON APPROACH, WITH APU RUNNING, CREW RECEIVED APU FIRE WARNING. APU PERFORMED AUTO SHUT DOWN, AND THE FIRE BOTTLE DISCHARGED. FLIGHT LANDED WITH 
- [SDR USAAF97015](https://openairdocs.org/sdr/USAAF97015), Jan 13, 1997: SEQUENCE VALVE. FAILED. FLT 1239 - PIT-DAY - ON APPROACH TO DAY THE NOSE GEAR DID NOT EXTEND ON THE FIRST TRY. PILOT RECYCLED TEH GEAR AND ALL INDICATIONS WERE NORMAL ON THE SECOND TRY
- [SDR USAAF97014](https://openairdocs.org/sdr/USAAF97014), Jan 10, 1997: RETRACT MECH. LACK OF LUBE. FLT 466 - GSP-PHL - ON APPROACH TO PHL, THE NOSE GEAR DID NOT EXTEND ON THE FIRST TRY. PILOT ACCOMPLISHED ABNORMAL CHECKLIST ITEMS AND RECYCLED GEAR. THE SECOND
- [SDR USAAF96130](https://openairdocs.org/sdr/USAAF96130), Dec 21, 1996: RETRACT MECH. LACK OF LUBE. FLT 1475 - PHL-DTW - ON DESCENT INTO DTW RECEIVED AN UNSAFE GEAR INDICATION WARNING AT FL 010. NOSE GEAR DID NOT COME DOWN. CREW DID A GO AROUND AND RECYCLED TH
- [SDR USAAF96107](https://openairdocs.org/sdr/USAAF96107), Sep 21, 1996: DIODE. OVERHEATED. FLT 1206 - RDU-PIT, AT 50S OF PIT, CRWE GOT 'EMERGENCY DC BUS FAILED' ON MFDU. COMMUNICATINOS WERE LOST WITH ZOB AND PIT APPROACH. AIRCRAFT SHED SOME ELECTRICAL
- [SDR USAAF96082](https://openairdocs.org/sdr/USAAF96082), Aug 1, 1996: FLEX DUCT. LEAKING. GRR - FL 862 - UPON DESCENT INTO GRR, CREW RECEIVED APU FIRE WARNING. APU WAS AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. FLIGHT CONTINUED TO GRR AN

## 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 19960921037869I](https://openairdocs.org/incident/19960921037869I), Sep 21, 1996: Fokker F28MK0100 (N887US), Pittsburgh, PA. Narrative: when descending into pit at approximately 50 NM southeast of the airport, the crew got an emergency DC bus failure message on the multi-function…
- [Incident 19921027052459I](https://openairdocs.org/incident/19921027052459I), Oct 27, 1992: Fokker F28MK0100 (N887US), Indianapolis, IN. Abnormal gear indication on climbout. Returned. Landed safely. Found main landing gear up stop dampers overserviced

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