# N897US: Fokker F.28 MK 0100, registration cancelled 2018-01-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 17, 2018 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Fokker F.28 MK 0100](https://openairdocs.org/model/fokker-f-28-mk-0100) (registry code 4990807) - Serial number: 11392 - Type of aircraft: Fixed wing multi engine - Certificate issued: October 31, 2006 - Last registry action: May 30, 2008 - Mode S code: AC6128 - Owner when cancelled: [Aircraft Finance Services Inc](https://openairdocs.org/faa-owner/AIRCRAFT%20FINANCE%20SERVICES%20INC) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Corporation - Owner's area on the map: 25.7655° N, 80.1843° W: Placed by OpenAirDocs at the center of ZIP code 33131, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N897US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=897US - Page: https://openairdocs.org/deregistered/N897US-2018-01-17 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 USAAF01061](https://openairdocs.org/sdr/USAAF01061), Jul 30, 2001: FIRE DETECTOR. MALFUNCTIONED. TRI - FLT 896 - EN ROUTE PIT-CLT, AT FL310, RECEIVED AN APU FIRE WARNING. THE FIRE EXTINGUISHING SYSTEM AUTOMATICALLY DISCHARGED. THE FLIGHT DIVERTED TO TRI AND - [SDR USAAF01051](https://openairdocs.org/sdr/USAAF01051), Jul 24, 2001: EXTINGUISHER. DISCHARGED. CLT-IND - FLT 476 - THE WATER FIRE EXTINGUISHER DISCHARGED INTO THE LAVATORY TRASH BIN IN FLIGHT. NO SMOKE OR FIRE WAS DETECTED. THE FLIGHT LANDED WITHOUT INCID - [SDR USAAF01048](https://openairdocs.org/sdr/USAAF01048), Jul 17, 2001: ODOR. DETECTED. STL-CLT - FLT 1249 - THE LAVATORY SMOKE ALARM BEGAN TO CHIME AND AN ODOR OF SMOKE WAS PRESENT IN THE AFT CABIN AREA DURING CLIMB. THE FLIGHT RETURNED TO FIELD I - [SDR USAAF01049](https://openairdocs.org/sdr/USAAF01049), Jul 17, 2001: TIMER. MALFUNCTIONED. STL-PIT - FLT 9281 - SLIGHT FUMES WERE NOTICED COMING FROM BOTH LAVATORIES, AND SMOKE DETECTORS ACTIVATED FOR A BRIEF TIME DURING CRUISE FLIGHT. FLIGHT LANDED I - [SDR USAAF00069](https://openairdocs.org/sdr/USAAF00069), Sep 15, 2000: STRUT. DISCHARGED. PIT-BNA - FLT 1532 - THE NOSE LANDING GEAR FAILED TO COME DOWN DURING APPROACH. RECEIVED A GEAR UNSAFE WARNING. THE FLIGHT PERFORMED A GO-AROUND AND CYCLED THE - [SDR USAAF00043](https://openairdocs.org/sdr/USAAF00043), Jun 4, 2000: BRAKE ASSY. MALFUNCTIONED. CMH-PHL - FLT 835 - ON LANDING ROLL, EXCESSIVE BRAKE PRESSURE REQUIRED TO STOP AIRCRAFT ON CAPTAINS SIDE. FIRST OFFICERS BRAKES SEEM NORMAL AT TAXI SPEED. MAINT - [SDR USAAF00040](https://openairdocs.org/sdr/USAAF00040), Jun 1, 2000: BRAKE. MALFUNCTIONED. BHM-CLT - FLT 1511 - DURING ROLL OUT, MUCH MORE THAN NORMAL BRAKE PEDAL FORCE SEEMED TO BE REQUIRED FOR NORMAL BRAKING EFFORT. MAINTENANCE BLED NR 3 AND NR 4 BR - [SDR USAAF00034](https://openairdocs.org/sdr/USAAF00034), May 3, 2000: SPRING. BROKEN. CLT - FOUND SERVICE DOOR GIRT BAR SLIDER HAS BROKEN SPRING. MAINTENANCE REPLACED THE SPRING IN SLIDER. CHECKS NORMAL. (M) - [SDR USAA991233](https://openairdocs.org/sdr/USAA991233), Nov 1, 1999: FITTING. CRACKED. PIT - DURING RON VISIT, FOUND 1.125 INCH CRACK IN T-FITTING (W/O JOGGLE) AT BOTTOM END OF T-FITTING AFT SIDE APBH BL 1027L. STOP DRILLED CRACK PER CD. REINSTALL - [SDR USAAF99048](https://openairdocs.org/sdr/USAAF99048), Sep 28, 1999: BATTERY PACK. DISCHARGED. GSO - EMERGENCY LIGHT STRIP NEAR CENTER EXIT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) - [SDR USAAF99044](https://openairdocs.org/sdr/USAAF99044), Sep 13, 1999: BATTERY PACK. DISCHARGED. IND - FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROW 12 THROUGH 17. MAINTENANCE REPLACED THE NR 7 BATTERY PACK. (M) - [SDR USAAF99012](https://openairdocs.org/sdr/USAAF99012), Mar 13, 1999: WINDOW. CRACKED. CLT - FLT 8076 - EN ROUTE TO CLT AT FL240, THE OUTER PANE OF THE LEFT COCKPIT SLIDING WINDOW CRACKED. FLIGHT WAS A NON-REVENUE FERRY FLIGHT. AIRCRAFT LANDED CLT - [SDR USAAF00003](https://openairdocs.org/sdr/USAAF00003), Jan 7, 1999: ANTI-SKID SYSTEM. MALFUNCTIONED. CLT-BHM - FLT 1252 - ON TAXI OUT FOR TAKEOFF, WHEN BRAKES WERE APPLIED (20 KNOTS), ANTI-SKID WOULD RELEASED BRAKES, MAKING IT HARD TO SLOW DOWN. MAINTENANCE ACT - [SDR USAAF98093](https://openairdocs.org/sdr/USAAF98093), Nov 30, 1998: BULB. FAILED. CRW - FLT 435 - ON APPROACH TO CRW WHEN LANDING GEAR WAS SELECTED DOWN, THERE WAS NO GEAR DOWN AND SAFE INDICATION. CREW RECYCLED LANDING GEAR BUT THERE WAS STI - [SDR USAAF98066](https://openairdocs.org/sdr/USAAF98066), Aug 2, 1998: BATTERY PACK. DISCHARGED. GSO - FORWARD EMERGENCY LIGHTS WEAK. MAINTENANCE REPLACED THE BATTERY PACK. (M) - [SDR USAAF96026](https://openairdocs.org/sdr/USAAF96026), Feb 25, 1996: BULB. FAILED. FLT 578 - CLT - RIGHT MAIN GEAR FAILED TO INDICATE DOWN AND GREEN. RECYCLED GEAR, CHANGED BULBS WITH NO CHANGE. LANDED NORMALLY, TAXIED WITH GEAR PINNED. PERFOR - [SDR USAA950451](https://openairdocs.org/sdr/USAA950451), May 6, 1995: LINES. UNINSTALLED. PIT - FLT 8554 - DURING TAKEOFF AT ROTATION, THE AC LOST ALL INSTRUMENTATION. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO PIT. MAINTENANCE REINSTALLED THE - [SDR USAA950580](https://openairdocs.org/sdr/USAA950580), May 5, 1995: STRINGER. CRACKED. PIT - DURING SCHEDULED INSPECTION OF USAIR CD 53F00762 HFEC INSPECTION OF STRINGERS NR 6, 7, 68 AFT OF FRAME STATION 3870, FOUND .5 INCH CRACK (RADICAL) AT STRI - [SDR USAA950579](https://openairdocs.org/sdr/USAA950579), May 5, 1995: STRINGER. CRACKED. PIT - DURING SCHEDULED INSPECTION USAIR PCI 289 CD 53F00762, FOUND A .5 INCH CRACK IN STRINGER 68 RT SIDE AFT OF FRAME 3870. INSTALLED SPLICE REPAIR TO STRINGER - [SDR USAA950232](https://openairdocs.org/sdr/USAA950232), Mar 13, 1995: PUMP. INOPERATIVE. PIT - FLT 0141 - THE R1 FUEL BOOST PUMP FAULT LIGHT ILLUMINATED IN-FLIGHT. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTEANCE REPLACED THE R1 AND R2 ## 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 19981221044019I](https://openairdocs.org/incident/19981221044019I), Dec 21, 1998: Fokker F28MK0100 (N897US), Greensboro, NC. (-5) Pilot reported left main gear problem. Pilot made a fly-by to okay gear down. Landed without incident. Maintenance replaced left landing gear light bulb… - [Incident 19930924043589I](https://openairdocs.org/incident/19930924043589I), Sep 24, 1993: Fokker F28MK0100 (N897US), Cleveland, OH, Minor damage. NR1 hydraulic light on during approach. Landed safely. Leaking at pressure output due to defective o ring. --- 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.