# N886US: 1991 Fokker F.28 MK 0100, registration cancelled 2013-06-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 19, 2013 - Status when cancelled: Sale reported, pending cancellation - 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: 11346 - Year built: 1991 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 6, 1991 - Last registry action: April 14, 2008 - Mode S code: AC35F2 - Location: Saint Lunaire, France - Owner type: Individual - The mark today: https://openairdocs.org/aircraft/N886US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=886US - Page: https://openairdocs.org/deregistered/N886US-2013-06-19 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 USAAF01031](https://openairdocs.org/sdr/USAAF01031), May 31, 2001: BATTERY PACK. DISCHARGED. RDU - THE AFT CABIN AND LAVATORY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN THE AFT EMERGENCY LIGHTS BATTERY PACK. OPS C - [SDR USAAF01025](https://openairdocs.org/sdr/USAAF01025), May 15, 2001: BATTERY PACK. CORRODED. RDU - THE AFT LAVATORY AREA EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE CLEANED CORROSION FROM BATTERY PACK CONTACTS IN NR 8 EMERGENCY POWER SUPPLY. OP - [SDR USAAF01012](https://openairdocs.org/sdr/USAAF01012), Mar 26, 2001: WIRE. BROKEN. RDU - THE RIGHT SERVICE DOOR EXIT LIGHT WAS INOPERATIVE IN STANDBY AND EMEGENCY LIGHTING. MAINTENANCE REPAIRED TWO BROKEN WIRES ON THE BACK OF THE EXIT LIGHT AS - [SDR USAAF00036](https://openairdocs.org/sdr/USAAF00036), May 8, 2000: UNKNOWN. ODOR. TYS-CLT - FLT 1731 - BURNING SMELL NOTED BY F/O, FLIGHT ATTENDANTS AND CAPTAIN DURING CLIMB-OUT. SMELL DIMINISHED CLIMBIN THROUGH 10,000, BUT STILL NOTICEABLE I - [SDR USAAF99041](https://openairdocs.org/sdr/USAAF99041), Aug 23, 1999: BATTERY PACK. DISCHARGED. CLT - FOUND THE NR 8 EMERGENCY BATTERY PACK INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) - [SDR USAAF98071](https://openairdocs.org/sdr/USAAF98071), Aug 20, 1998: WARNING SYSTEM. ACTIVATED. PIT - FLT 274 - EN ROUTE LGA-SDF, CREW RECEIVED THREE CHIME WARNING FROM THE MFDU AND NOTED THAT THE CABIN ALTITUDE WAS CLIMBING THROUGH 10,000 FT. CREW PERFORM - [SDR USAAF98065](https://openairdocs.org/sdr/USAAF98065), Aug 4, 1998: DETECTOR. MALFUNCTIONED. TYS - FLT 1633 - ON APPROACH TO TYS DESCENDING THROUGH 4000 FEET, WHEN SPEEDBRAKES WERE DEPLOYED THE APU FIRE WARNING ANNUNCIATED. THE APU AUTOMATICALLY SHUT DO - [SDR 98ZZZM607](https://openairdocs.org/sdr/98ZZZM607), Aug 4, 1998: GCU. FAILED. TYS - FLT 1633 - ON APPROACH TO TYS DESCENDING THROUGH 4000 FEET, WHEN SPEEDBRAKES WERE DEPLOYED THE APU FIRE WARNING ANNUNCIATED. THE APU AUTOMATICALLY SHUT DO - [SDR 98ZZZM606](https://openairdocs.org/sdr/98ZZZM606), Aug 4, 1998: IDG. FAILED. TYS - FLT 1633 - ON APPROACH TO TYS DESCENDING THROUGH 4000 FEET, WHEN SPEEDBRAKES WERE DEPLOYED THE APU FIRE WARNING ANNUNCIATED. THE APU AUTOMATICALLY SHUT DO - [SDR USAAF98034](https://openairdocs.org/sdr/USAAF98034), Apr 1, 1998: CONTROLLER. MALFUNCTIONED. CLT - FLT 1079 - EN ROUTE FROM MDT TO CLT WHILE DESCENDING FROM 350 TO 310, AIRCRAFT EXPERIENCED A LOSS OF CABIN PRESSURE. A RAPID DESCENT TO 10,000 FEET WAS MA - [SDR USAAF96043](https://openairdocs.org/sdr/USAAF96043), May 13, 1996: FLAP SYNCHRO. FAILED. PIT - FL 8075 - DURING DESCENT INTO AVP, THE CREW COULD NOT GET THE FLAPS TO EXTEND. A DECISION WAS MADE TO DIVERT TO PIT WHERE MAINTENANCE IS AVAILABLE TO MAKE - [SDR USAAF96004A](https://openairdocs.org/sdr/USAAF96004A), Jan 5, 1996: HARNESS. FAULTY. CLT - AFTER TAKEOFF, CREW RECEIVED GND/FLT FAULT, LIFT DUMPER FAULT, TCAS FAULT AND PROX SW SYS INOP. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT - [SDR USAAF96004](https://openairdocs.org/sdr/USAAF96004), Jan 5, 1996: GROUND SENSE. MALFUNCTIONED. FLT NR 1007 - CLT - THE FLIGHT RETURNED TO FIELD DUE TO A GROUND SENSE PROBLEM. (M) - [SDR USAAF96003A](https://openairdocs.org/sdr/USAAF96003A), Jan 5, 1996: PROX SENSOR. OUT OF ADJUST. FLT NR 1488 - RIC - SHORTLY AFTER GEAR RETRACTION THE FOLLOWING ALERTS, 'LD FAULT', 'STAB TRIM CONFIG' AND 'TCAS'. WHEN GEAR EXTENDED, LOUD RELAY CLICKING FOLLO - [SDR USAAF95008](https://openairdocs.org/sdr/USAAF95008), Dec 28, 1995: PACK. FAILED. FLT NR 689 - PIT - WHILE AT FL 350 THE AIRCRAFT PRESSURIZATION STARTED TO CLIMB TO 10K FEET. THE CAPTAIN REQUESTED DESCENT TO FL 100 AND RECEIVED SAME FROM ATC. - [SDR USAA950024](https://openairdocs.org/sdr/USAA950024), Jan 19, 1995: NUT. LOOSE. PIT - FLT 1025 - AFTER TAKEOFF, THE CREW GOT A 'HYD SYS 2 LO QTY' ALERT. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PRESSURE LINE 'B' ## 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 19920430014959I](https://openairdocs.org/incident/19920430014959I), Apr 30, 1992: Fokker F28MK0100 (N886US), Rochester, NY. Hydraulic leak on climb. Returned. Found o ring on NR1 engine hydraulic pump pressure line blown. --- 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.