# N882US: 1991 Fokker F.28 MK 0100, registration cancelled 2003-10-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 7, 2003
- Exported to: Netherlands
- 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: 11334
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 14, 1991
- Certificate issued: June 9, 2003
- Last registry action: June 9, 2003
- Mode S code: AC2716
- Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N882US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=882US
- Page: https://openairdocs.org/deregistered/N882US-2003-10-07

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 (22)

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

- [SDR USAAF01090](https://openairdocs.org/sdr/USAAF01090), Dec 28, 2001: LIGHT. INOPERATIVE. PIT - THE RIGHT FAIRING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M)
- [SDR USAAF01075](https://openairdocs.org/sdr/USAAF01075), Oct 6, 2001: ACTUATOR. FAILED. RIC-CLT - FLT 1008 - AFTER TAKEOFF, THE NOSE LANDING GEAR FAILED TO RETRACT. THE GEAR WAS CYCLED WITH NO CHANGE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED W
- [SDR USAAF01024](https://openairdocs.org/sdr/USAAF01024), May 15, 2001: LIGHT. INOPERATIVE. IND - THE EMERGENCY EXIT LIGHT ON THE MAIN ENTRY DOOR HINGE WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. FUNCTIONALLY CHECKED OK. (M)
- [SDR USAAF99055](https://openairdocs.org/sdr/USAAF99055), Dec 1, 1999: UNKNOWN. ODOR. ORD - FLT 1999 - STRONG OIL BURNING ODOR DETECTED DURING TAKEOFF AND CLIMB-OUT. ODOR WENT AWAY ONCE THE NR 2 PACK WAS TURNED OFF. MAINTENANCE OPS CHECKED NR 2 P
- [SDR USAAF99027](https://openairdocs.org/sdr/USAAF99027), May 21, 1999: PUMP. FAILED. SBN - FLT 1240 EN ROUTE PIT-SBN, CREW EXPERIENCED TOTAL HYDRAULIC FAILURE. FLIGHT PROCEEDED TO SBN. UPON LANDING, THE NR 3 TIRE BLEW, CAUSING LOSS OF DIRECTIONA
- [SDR USAAF98063](https://openairdocs.org/sdr/USAAF98063), Jul 30, 1998: HYDRAULIC SYSTEM. FAILED. CLT - FLT 281 - ON CLIMB-OUT FROM CLT, SYSTEM 1 HORIZONTAL STABILIZER HYDRAULICS FAILED. SEVERAL MINUTES LATER, SYSTEM 2 HORIZONTAL STABILIZER HYDRAULICS FAILED
- [SDR USAAF98057](https://openairdocs.org/sdr/USAAF98057), Jul 18, 1998: MLG. FAILED. PIT - FLT 671 - ON APPROACH TO CRW WHEN THE LANDING GEAR WAS SELECTED DOWN, THE MAIN LANDING GEAR DID NOT EXTEND. CREW RECYCLED THE GEAR HANDLE WITH THE SAME RE
- [SDR 98ZZZX2863](https://openairdocs.org/sdr/98ZZZX2863), Jul 18, 1998: DOOR. DAMAGED. PIT - FLT 671 - ON APPROACH TO CRW WHEN THE LANDING GEAR WAS SELECTED DOWN, THE MAIN LANDING GEAR DID NOT EXTEND. CREW RECYCLED THE GEAR HANDLE WITH THE SAME RE
- [SDR USAAF98053](https://openairdocs.org/sdr/USAAF98053), Jun 17, 1998: PSEU. FAILED. CLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EVERY 2-3 MINUTES. FLIGHT RETURNED TO CLT 
- [SDR 98ZZZX2831](https://openairdocs.org/sdr/98ZZZX2831), Jun 17, 1998: SENSOR. FAILED. CLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EVERY 2-3 MINUTES. FLIGHT RETURNED TO CLT 
- [SDR 98ZZZX2830](https://openairdocs.org/sdr/98ZZZX2830), Jun 17, 1998: SENSOR. FAILED. CLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EVERY 2-3 MINUTES. FLIGHT RETURNED TO CLT 
- [SDR 98ZZZX2829](https://openairdocs.org/sdr/98ZZZX2829), Jun 17, 1998: HARNESS. FAILED. CLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EVERY 2-3 MINUTES. FLIGHT RETURNED TO CLT 
- [SDR USAAF97075](https://openairdocs.org/sdr/USAAF97075), Sep 22, 1997: BATTERY PACK. DISCHARGED. DURING ROUTINE OVERNIGHT MAINTENANCE INSPECTION, MAIN ENTRY DOOR EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK. (X)
- [SDR USAAF97057](https://openairdocs.org/sdr/USAAF97057), Jul 9, 1997: AUX POWER UNIT. FAILED. PIT/ERI - FLT 502 - ON DESCENT INTO ERI, THE APU SHUT DOWN AUTOMATICALLY WHEN THE SPEED BRAKE WAS DEPLOYED. A 'LOW AGENT' FOR THE APU FIRE SYSTEM ALSO ILLUMINAT
- [SDR USAAF97052](https://openairdocs.org/sdr/USAAF97052), Jun 26, 1997: SWIVEL JOINT. LEAKING. RDU/CLT - FLT 1614 - ON APPROACH TO CLT, APPROXIMATELY 15 MILES FROM AIRPORT, APU FIRE WARNING ILLUMINATED, ALONG WITH AUTOMATIC APU SHUT DOWN AND FIRE BOTTLE D
- [SDR 97ZZZX3180](https://openairdocs.org/sdr/97ZZZX3180), Jun 26, 1997: FIRE CONTL UNIT. MALFUNCTIONED. RDU/CLT - FLT 1614 - ON APPROACH TO CLT, APPROXIMATELY 15 MILES FROM AIRPORT, APU FIRE WARNING ILLUMINATED, ALONG WITH AUTOMATIC APU SHUT DOWN AND FIRE BOTTLE D
- [SDR USAAF97033](https://openairdocs.org/sdr/USAAF97033), Mar 22, 1997: BATTERY PACK. DISCHARGED. IND - FORWARD OVERHEAD EXIT SIGN AND AREA EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE BATTERY PACK. (M)
- [SDR USAAF97026](https://openairdocs.org/sdr/USAAF97026), Mar 8, 1997: WINDSHIELD. FAILED. PIT - FL 8565 - EN ROUTE MCO-PIT - CREW NOTED STRONG ELECTRICAL SMELL IN COCKPIT. CREW DONNED OXYGEN MASKS. FLIGHT LANDED AT PIT WITH NO FURTHER INCIDENT. MAINT
- [SDR USAAF96115](https://openairdocs.org/sdr/USAAF96115), Nov 5, 1996: BULB. FAILED. EMERGENCY EXIT LIGHT AT 12A IS OUT OF SERVICE. MAINTENANCE RELAMPED EXIT LIGHT. (M)
- [SDR USAAF96097](https://openairdocs.org/sdr/USAAF96097), Sep 8, 1996: BYPASS VLV. FAILED. RDU-PIT - FLT 1423 - ON CLIMB GOING THROUGH FL 100, PACK CABIN SUPPLY TEMP WENT TO 100F EVEN WITH TEMP SELECT FULL COLD. ONE PACK WAS ON MEL AS WELL AS APU BLEE
- [SDR USAAF96025](https://openairdocs.org/sdr/USAAF96025), Feb 24, 1996: WINDSHIELD. CRACKED. FLT NR 275 - RDU - OUTER PANE OF CAPTIANS WINDSHIELD SHATTERED IN FLIGHT AT 29,000 FEET PRECAUTIONARY LANDING MADE AT RDU. REPLACED L1 WINDOW. (M)
- [SDR USAAF96008](https://openairdocs.org/sdr/USAAF96008), Jan 12, 1996: SHUTOFF VALVE. INOPERATIVE. CLT - FL 1295 - EN ROUTE PIT - LGA, CREW RECEIVED TAIL ANTI-ICING FAULT SHORTLY AFTER SELECTING TAIL ANTI-ICE. FLIGHT DIVERTED TO CLT AND LANDED WITH NO FURTHER

## 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 19990521021819I](https://openairdocs.org/incident/19990521021819I), May 21, 1999: Fokker F28MK0100 (N882US), South Bend, IN, Minor damage. (From .19 this incident was investigated by NTSB) on may 21, 1999, at 1207 eastern standard time, a Fokker F-100, N882US, operated by us airways, incorporated,…
- [Incident 19911221059819I](https://openairdocs.org/incident/19911221059819I), Dec 21, 1991: Fokker F28MK0100 (N882US), Buffalo, NY. Unsafe left main gear light on final. Made go-around. Landed safely. Replaced left gear down lock proximity switch.

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