# N899US: 1992 Fokker F.28 MK 0100, registration cancelled 2003-10-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 16, 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) - Serial number: 11399 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: July 1, 1992 - Certificate issued: September 5, 2003 - Last registry action: September 5, 2003 - Mode S code: AC6896 - 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/N899US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=899US - Page: https://openairdocs.org/deregistered/N899US-2003-10-16 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 (29) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAF01032](https://openairdocs.org/sdr/USAAF01032), Jun 6, 2001: BATTERY PACK. FAULTY. RIC - FOUND NR 6 CEILING AND LAVATORY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE NR 8 BATTERY PACK. OPERATIONALLY CHECKED OK. (M) - [SDR USAA010410](https://openairdocs.org/sdr/USAA010410), Mar 21, 2001: STRINGER. CRACKED. PIT - FOUND STRINGER CRACKED .75 INCH, STRINGER 69, STATION 3850. REPAIRED PER SRM 51-70-06 DOUBLER. (M) - [SDR USAAF00065](https://openairdocs.org/sdr/USAAF00065), Aug 22, 2000: SLIDE. MALFUNCTIONED. PIT - THE FORWARD ENTRY L1 DOOR WAS OPENED WITH THE SLIDE IN THE ARMED POSITION. THE SLIDE FELL FROM THE BUSTLE, BUT DID NOT DEPLOY. MAINTENANCE REPLACED THE L1 - [SDR USAAF00028](https://openairdocs.org/sdr/USAAF00028), Mar 28, 2000: SLIDE. INOPERATIVE. ALB - THE FORWARD SERVICE DOOR WAS INADVERTENTLY DEPLOYED, BUT THE SLIDE DID NOT INFLATE. MAINTENANCE REPLACED THE FORWARD SERVICE DOOR SLIDE. (M) - [SDR USAAF00019](https://openairdocs.org/sdr/USAAF00019), Feb 26, 2000: SENSOR. DAMAGED. CLT-ILM - FLT 704 - AFTER TAKEOFF, THE LANDING GEAR HANDLE WAS JAMMED. THE LANDING GEAR OVERRIDE WAS PRESSED AND THE GEAR BEGAN TO RETRACT. AT THAT THE TIME THE - [SDR USAAF00010](https://openairdocs.org/sdr/USAAF00010), Feb 2, 2000: BRACKET. BROKEN. RIC-CLT - FLT 1093 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT AND THE AIR GROUND FAULT DISPLAYED ON THE MFDU. MAINTENANCE REPLACED THE RIGHT MAIN LANDI - [SDR USAAF99001](https://openairdocs.org/sdr/USAAF99001), Jan 5, 1999: COFFEE MAKER. LEAKING. CLT - FLT 575 - AFTER DEPARTING CLT EN ROUTE TO TRI, THE FLIGHT ATTENDANT REPORTED A LARGE WATER LEAK IN THE FORWARD GALLEY AREA. THE FLIGHT ATTENDANT SHUT OFF - [SDR USAA980676](https://openairdocs.org/sdr/USAA980676), Dec 24, 1998: FITTING. CORRODED. PIT - DURING Q-1 CHECK, FOUND 2 INCHES BY 2 INCHES CORROSION AT PAX DOOR STATION 3820-4610 FITTING. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR 1156519. (M) - [SDR USAA980675](https://openairdocs.org/sdr/USAA980675), Dec 24, 1998: FITTING. CORRODED. PIT - DURING Q-1 CHECK, FOUND 2 INCH BY 2 INCH CORROSION AT FORWARD PAX DOOR GIRT BAR MOUNT FITTING. REPLACED BRACKET PER SRM 53-12-10, 51-22-01, 51-40-02. (M) - [SDR USAA980674](https://openairdocs.org/sdr/USAA980674), Dec 24, 1998: BEAM. CORRODED. PIT - DURING Q-1 CHECK, FOUND 1,000 MM BY 2 INCH CORROSION ON BEAM AT BL 600R STATION 5305, 6305. BLENDED OUT CORROSION PER EA 51234. (M) - [SDR USAA980673](https://openairdocs.org/sdr/USAA980673), Dec 24, 1998: BEAM. CORRODED. PIT - DURING Q-1 CHECK, FOUND CORROSION 2 INCHES BY 7 INCHES BL 0 T-CAP STATION 5305 BEAM. REPLACED T-CAP SECTION 1710037 2024T3 STOCK PER SRM 53-12-10, 51-40-0 - [SDR USAA980672](https://openairdocs.org/sdr/USAA980672), Dec 24, 1998: T-CAP. CORRODED. PIT - DURING Q-1 CHECK, FOUND 2 INCH SECTION OF UNDERSIDE OF T-CAP CORROSION AT FS NR 3845 ( 2 INCHES FORWARD) AT BL NR 0 T-CAP. REPLACED T-CAP STRIP SECTION WI - [SDR USAA980671](https://openairdocs.org/sdr/USAA980671), Dec 24, 1998: BEAM. CORRODED. PIT - DURING Q-1 CHECK, FOUND CORROSION 6 INCHES LONG 100 PERCENT CORRODED THROUGH AT FS 3845 AT BL NR 0 BEAM TOP SURFACE. REPLACED T-CAP SECTION USING 1710037 - [SDR USAA980670](https://openairdocs.org/sdr/USAA980670), Dec 24, 1998: BEAM. CORRODED. PIT - DURING Q-1 CHECK, FOUND 28 INCH APPROX SURFACE CORROSION ON BEAM BL 0 FS 5305-5805 T-CAP. REPLACED T-CAP SECTION USING 1710038 2024T3 STOCK PER SRM 53-12- - [SDR USAA980669](https://openairdocs.org/sdr/USAA980669), Dec 24, 1998: BEAM. CORRODED. PIT - DURING Q-1 CHECK, FOUND 2 INCH AREA TOP SURFACE CORRODED FS NR 3845 AT BL 914R BEAM. REPAIRED PER EA 51235. (M) - [SDR USAA980668](https://openairdocs.org/sdr/USAA980668), Dec 24, 1998: T-CAP. CORRODED. PIT - DURING Q-1 CHECK, FOUND CORROSION TOP SURFACE ENTIRE LENGTH 10 INCH T-CAP FS 3845-4850 AT BL 600R. REPLACED TOP CAP STRIP WITH LOCALLY FABRICATED PART OF - [SDR USAA980667](https://openairdocs.org/sdr/USAA980667), Dec 24, 1998: T-CAP. CORRODED. PIT - DURING Q-1 CHECK, FOUND CORROSION TOP SURFACE 100MM LONGERON FS 3845-4850 T-CAP ENTIRE LENGTH BL NR 1127R. REPLACED TOP CAP STRIP WITH PART OF LOCAL FABRI - [SDR USAA980666](https://openairdocs.org/sdr/USAA980666), Dec 24, 1998: BEAM. CORRODED. PIT - DURING Q-1 CHECK, FOUND 28 INCH APPROXIMATELY BY 2 INCH CORROSION ON BEAM AT BL 1127L STATION 3845-4850. TOP CAP STRIP REPLACED (LOCALLY FABRICATED) 2024- - [SDR USAA980665](https://openairdocs.org/sdr/USAA980665), Dec 24, 1998: BEAM. CORRODED. PIT - DURING Q-1 CHECK, FOUND 20 INCH APPROXIMATELY BY 2 INCH CORROSION ON BEAM AT BL 221R STATION 5805-6305. REPAIRED WITH MODIFIED 1155009 BEAM PER SRM 51-70- - [SDR USAA980664](https://openairdocs.org/sdr/USAA980664), Dec 24, 1998: T-CAP. CORRODED. PIT - DURING Q-1 CHECK, FOUND CORROSION AT SCREW HOLES TOP SURFACE FS NR 3845 AT 1127R T-CAP. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR 115-4834 PER SRM 53 - [SDR USAA980663](https://openairdocs.org/sdr/USAA980663), Dec 24, 1998: FITTING. CORRODED. PIT - DURING Q-1 CHECK, FOUND SURFACE CORROSION ENTIRE AREA FORWARD S/E DOOR GIRT BAR MOUNT FITTING 3845 OUTBOARD 1127R. DEFECTIVE PART REPLACED WITH IDENTICAL - [SDR USAA980662](https://openairdocs.org/sdr/USAA980662), Dec 24, 1998: FITTING. CORRODED. PIT - DURING Q-1 CHECK, FOUND CORROSION AT S/E DOOR SILL PLATE MOUNT FITTINGS 3845-4850 BL NR 1127R. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR 1154982 PER - [SDR USAAF98028](https://openairdocs.org/sdr/USAAF98028), Mar 12, 1998: SELECTOR VALVE. FAILED. FLT 743 - PWM - ON APPROACH TO PWM THE LANDING GEAR SELECTOR HANDLE WOULD NOT MOVE FROM THE 'UP' POSITION. CREW PERFORMED A GO AROUND AND LOWERED THE LANDING GE - [SDR USAAF97103](https://openairdocs.org/sdr/USAAF97103), Dec 23, 1997: FLOW REGULATOR. FAILED. CLT - FLT 668 - ON APPROACH TO CLT, AT 1000 FT AGL, CAPTAIN TRIED TO IDLE BACK ON THROTTLE FROM 80 PERCENT. NR 2 ENGINE WOULD NOT SET BACK AND HUNG AT 80 PERCEN - [SDR USAAF97091](https://openairdocs.org/sdr/USAAF97091), Nov 6, 1997: BATTERY PACK. DISCHARGED. IND - MAINTENANCE FOUND THE FORWARD ENTRY DOOR OVERHEAD EMERGENCY LIGHTS DIM. REPLACED THE BATTERY PACK. (M) - [SDR USAAF97030](https://openairdocs.org/sdr/USAAF97030), Mar 15, 1997: RELAY. FAILED. PHL - FL 723 - CABIN EMERGENCY LIGHTS DID NOT ILLUMINATED WHEN TESTED. MAINTENANCE REPLACED THE D-3982A RELAY. (M) - [SDR USAAF96042](https://openairdocs.org/sdr/USAAF96042), May 13, 1996: DNLOCK SENSOR. FAILED. PIT - FL 8076 - ON DESCENT INTO PIT, CREW LOWERED GEAR AND RECEIVED THREE GREEN LIGHTS WHILE BLUE LIGHTS IN GEAR HANDLE REMAINED ON AND A MFDU MESSAGE THAT READ - [SDR USAAF96041](https://openairdocs.org/sdr/USAAF96041), May 12, 1996: DOOR SENSOR. OUT OF ADJUST. DCA - FL 2286 - ON DESCENT INTO DCA, LEFT LANDING GEAR DOOR SWITCH CAME ON MFDU AFTER THE GEAR WAS LOWERED. CREW HAD THREE GREEN LIGHTS FOR GEAR BUT AS THEY DES - [SDR USAA950750](https://openairdocs.org/sdr/USAA950750), Jul 8, 1995: EEL PACK. FAILED. CLT - FLT 166 - AT APPROX FL 301, THE LT PACK WENT OUT MAKING A LOUD NOISE. CREW DECIDED TO DIVERTED TO CLT. MAINTENANCE REPLACED THE LT PACK ASSEMBLY, OPERATIO ## 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 19960209005399I](https://openairdocs.org/incident/19960209005399I), Feb 9, 1996: Fokker F28MK0100 (N899US), Ithaca, NY. Narrative: on feb. 9, 1996 at approx. 2345 EST a us air FK100 flight 1154 landed at ith airport without runway lights on/activated. Visual meteorological… - [Incident 19941020041399I](https://openairdocs.org/incident/19941020041399I), Oct 20, 1994: Fokker F28MK0100 (N899US), New York, NY. Speed brake extended at 500 mph. Caused pitch ups and downs prior disconnect. Post incident no anomalies found. --- 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.