# N857US: 1989 Fokker F.28 MK 0100, registration cancelled 2005-02-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 23, 2005 - Exported to: France - 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: 11289 - Year built: 1989 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 7, 1990 - Certificate issued: July 3, 2003 - Last registry action: July 3, 2003 - Mode S code: ABC32C - Owner when cancelled: [Al Bouraq Aviation Inc Trustee](https://openairdocs.org/faa-owner/AL%20BOURAQ%20AVIATION%20INC%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N857US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=857US - Page: https://openairdocs.org/deregistered/N857US-2005-02-23 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 (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAF01087](https://openairdocs.org/sdr/USAAF01087), Dec 23, 2001: ODOR. DETECTED. ILM-CLT - FLT 1546 - DURING CLIMB-OUT THERE WERE STRONG FUMES IN THE CABIN AND THE LAV SMOKE DETECTORS SOUNDED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WI - [SDR USAAF01054](https://openairdocs.org/sdr/USAAF01054), Jul 26, 2001: DOOR. UNSERVICEABLE. FLT 835 - EN ROUTE PIT-STL, DURING CLIMB-OUT, THE RIGHT OVERWING EMERGENCY EXIT DOORS BEGAN TO MAKE NOISE, THEN THE COVERS FOR THE EMERGENCY DOOR EMERGENCY RELE - [SDR USAAF01055](https://openairdocs.org/sdr/USAAF01055), Jul 26, 2001: DOOR. UNSERVICEABLE. CLT - FLT 9281 - EN ROUTE STL-CLT - DURING THE FLIGHT, THE RIGHT OVER-WING EMERGENCY EXIT DOORS BECAME UNLATCHED. AFTER LANDING, THE EMERGENCY EXIT DOORS FELL O - [SDR USAA010934](https://openairdocs.org/sdr/USAA010934), Jul 25, 2001: FRAME. CRACKED. PIT - FOUND FRAME CRACKED 4 INCHES, FS 21736 BETWEEN STRINGER 3 AND THROUGH UPPER C-CHANNEL. INSTALLED TWO REPAIR ANGLES PER EA 71597. (M) - [SDR USAAF01053](https://openairdocs.org/sdr/USAAF01053), Jul 25, 2001: DOOR. UNSECURE. PIT - FLT 1472 - EN ROUTE PIT-SDF, DURING CLIMB-OUT, THE COVER FOR THE EMERGENCY DOOR EMERGENCY RELEASE HANDLE AND SOME SAFETY WIRE FELL OFF. THE EMERGENCY DOOR - [SDR USAA010802](https://openairdocs.org/sdr/USAA010802), Jul 1, 2001: SKIN. PIT - FOUND SKIN WITH HEAT DAMAGE 8 INCH BY 12 INCH AREA, STATION 27026-27526 STRINGER 46-50. REMOVED HEAT DAMAGE, INSTALLED REPLACEMENT SKIN/DOUBLER PER EA 546 - [SDR USAAF01029](https://openairdocs.org/sdr/USAAF01029), May 26, 2001: TUBE. CRACKED. PIT-CLT - FLT 347 - AFTER TAKEOFF, A VERY STRONG ODOR OF SKYDROL WAS NOTED IN THE CABIN. FLIGHT RETURNED TO THE FIELD IN PIT AND LANDED WITHOUT FURTHER INCIDENT - [SDR USAAF01028](https://openairdocs.org/sdr/USAAF01028), May 25, 2001: COALESCER BAG. DIRTY. STL-PIT - FLT 288 - UPON APPLICATION ON TAKEOFF THRUST, A STRONG, ACRID, MUSTY ODOR DEVELOPED IN THE COCKPIT AND AFT CABIN AREAS. FLIGHT LANDED IN PIT WITHOUT F - [SDR USAAF00048](https://openairdocs.org/sdr/USAAF00048), Jun 24, 2000: CONTROLLER. FAULTY. CLT-IND - FLT 235 - DURING CLIMB, SMOKE ODOR WAS PRESENT IN THE COCKPIT. ODOR DISSIPATED WHEN THE WINDOW HEAT WAS TURNED OFF. THE FLIGHT RETURNED TO THE FIELD D - [SDR USAAF00006](https://openairdocs.org/sdr/USAAF00006), Jan 25, 2000: LIGHT. INOPERATIVE. IND - THE RIGHT AFT OVERWING EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE BEHIND THE SOCKET ASSEMBLY. (M) - [SDR USAAF99028](https://openairdocs.org/sdr/USAAF99028), May 23, 1999: WIRE. BROKEN. RDU - FOUND THE PASSENGER DOOR AND FORWARD SERVICE DOOR EMERGENCY EXIT MARKERS AND FLIGHT COMPARTMENT DOME LIGHT REMAIN ILLUMINATED AT ALL TIMES. AIRCRAFT FERRI - [SDR USAAF99013](https://openairdocs.org/sdr/USAAF99013), Mar 12, 1999: TIRE. FAILED. PIT - FLT 7881 - AFTER LANDING PIT DURING ROLLOUT, BOTH LEFT MAIN GEAR TIRES BLEW OUT WHEN MODERATE BRAKING WAS APPLIED. MAINTENANCE REPLACED BOTH LEFT MAIN GEA - [SDR USAAF98055](https://openairdocs.org/sdr/USAAF98055), Jul 13, 1998: LIGHT. MALFUNCTIONED. PIT - FLT 671 - AFTER TAKEOFF FROM PIT, THE EMERGENCY EXIT LIGHTS REMAINED ILLUMINATED AFTER LANDING GEAR WAS RETRACTED. MAINTENANCE RESEATED RELAY K2618A AND T - [SDR USAAF98016](https://openairdocs.org/sdr/USAAF98016), Feb 17, 1998: HANDLE. LOOSE. CLE - FLT 598 - ON CLIMB-OUT OF CLE, CAPTAIN RECEIVED A MID CABIN DOOR WARNING LIGHT. FLIGHT RETURNED TO CLE WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTEN - [SDR USAAF97055](https://openairdocs.org/sdr/USAAF97055), Jul 5, 1997: SUPPLY UNIT. FAILED. RDU/PHL - FLT 1408 - ON APPROACH TO PHL WHEN LANDING GEAR WAS SELECTED DOWN, IN-TRANSIT LIGHT ILLUMINATED BUT NONE OF THE THREE GREEN 'DOWN AND LOCKED' INDICATI - [SDR USAAF96078](https://openairdocs.org/sdr/USAAF96078), Jul 17, 1996: FLT CNTRL COMPTR. FAILED. PIT - FL 1601 - AFTER TAKEOFF, CREW RECEIVED 'NO AUTOLAND'MESSAGE. NEITHER AUTOPILOT WOULD TURN ON. FLIGHT RETURNED TO PIT ANDLANDED WITH NO FURTHER INCIDENT. M - [SDR USAA950940](https://openairdocs.org/sdr/USAA950940), Aug 16, 1995: SKIN. DELAMINATED. PIT - DURING Q-1 INSPECTION, FOUND FUSELAGE SKIN DELAMINATED APPROXIMATELY 10 INCH BY 24 INCH AREA BETWEEN RIGHT STUB WING UPPER AND LOWER CONNECTION ANGLE FROM - [SDR USAA950939](https://openairdocs.org/sdr/USAA950939), Aug 16, 1995: SKIN. DELAMINATED. PIT - DURING Q-1 INSPECTION, FOUND FUSELAGE SKIN DELAMINATED BETWEEN LEFT STUBWING UPPER AND LOWER CONNECTION ANGLES. AREA APPROXIMATELY 10 INCHES BY 24 INCHES - [SDR USAA9509937](https://openairdocs.org/sdr/USAA9509937), Aug 11, 1995: ANGLE. CORRODED. PIT - DURING Q-1 INSPECTION, FOUND CORROSION AT ATTACH ANGLE NR 2 RADIO RACK FLOOR PANEL. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 53-12-10. (M) - [SDR USAA950936](https://openairdocs.org/sdr/USAA950936), Aug 2, 1995: STRINGER. CRACKED. PIT - DURING Q-1 INSPECTION, FOUND .5 INCH CRACK IN STRINGER NR 68 RIGHT SIDE 4 INCHES AFT OF FRAME 3870. INSTALLED DOUBLER REPAIR PER SRM 51-70-06 FIG 202. (M) - [SDR USAA950941](https://openairdocs.org/sdr/USAA950941), Jul 31, 1995: FITTING. CRACKED. PIT - DURING Q-1 INSPECTION, FOUND .5 INCH CRACK BETWEEN STATION 8305 AND STATION 8805 AT STRINGER NR 2 FITTING. INSTALLED DOUBLER ANGLE PER SRM 53-00-02. (M) - [SDR USAA950520](https://openairdocs.org/sdr/USAA950520), May 18, 1995: SPINNER. MOISTURE. MEM - FLT 0358 - THE CREW RECEIVED AN ENGINE VIBRATION READING FROM THE NR 2 ENGINE. THE CAPTAIN CUT THE ENGINE BACK TO IDLE AND DECLARED AND EMERGENCY. FLIGHT ## 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 19930426019309I](https://openairdocs.org/incident/19930426019309I), Apr 26, 1993: Fokker F28MK0100 (N857US), Allentown, PA. NR2 engine vibrtation. Had epr fluctuation diverted to Allentown. Landed safely. Found no problem. Suspect fan blade --- 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.