# N894US: 1992 Fokker F.28 MK 0100, registration cancelled 2007-08-10 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 10, 2007 - Exported to: Australia - 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: 11379 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 13, 1992 - Certificate issued: May 16, 2007 - Last registry action: May 16, 2007 - Mode S code: AC5603 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N894US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=894US - Page: https://openairdocs.org/deregistered/N894US-2007-08-10 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 (27) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAF01079](https://openairdocs.org/sdr/USAAF01079), Oct 16, 2001: LIGHT. INOPERATIVE. PIT - A FIRST CLASS SECTION OF THE FLOOR PROXIMITY EMERGENCY LIGHTS WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT SECTION. (M) - [SDR USAAF00047](https://openairdocs.org/sdr/USAAF00047), Jun 17, 2000: WARNING LIGHT. FALSE INDICATION. CLT-SAV - FLT 2395 - THE APU FIRE WARNING ILLUMINATED, WITH SUBSEQUENT FIRE BOTTLE DISCHARGE, AFTER THE SPEEDBRAKE WAS DEPLOYED DURING DESCENT. THE FLIGHT LANDE - [SDR USAAF99015](https://openairdocs.org/sdr/USAAF99015), Mar 17, 1999: ROLLER. OUT OF POSITION. PIT - FLT 864 - AFTER DEPARTURE FROM PIT, THERE WAS AN EXCESSIVE AMOUNT OF AIR NOISE FROM THE LEFT SLIDING WINDOW EVEN THOUGH THE WINDOW WAS CLOSED AND LOCKED. - [SDR USAA980493](https://openairdocs.org/sdr/USAA980493), Sep 29, 1998: MOUNT. CORRODED. PIT - DURING Q1 CHECK, FOUND CORROSION AT GIRT BAR MOUNT BEYOND LIMITS, 1 INCH BY .50 INCH AT STA 4850 AFT SIDE MED. REPAIRED PER SRM CHAPTER 51. (X) - [SDR USAA980492](https://openairdocs.org/sdr/USAA980492), Sep 29, 1998: FLOOR BEAM. CORRODED. PIT - DURING Q1 CHECK, FOUND .50 INCH BY 2 INCH FLOOR BEAM CORRODED AT STA 3870 - STA 4610, AT BL 600R. FABRICATED NEW PARTS FROM 2024-T-3, .032 INCH ANGLES AND - [SDR USAA980491](https://openairdocs.org/sdr/USAA980491), Sep 29, 1998: MOUNT. CORRODED. PIT - DURING Q1 CHECK, FOUND GALLEY 2 INBOARD MOUNT EXCESSIVLEY CORRODED, .50 INCH BY .25 INCH AREA AT STA 4850 - STA 5305. REPAIRED PER SRM 51-70-00. (X) - [SDR USAA980490](https://openairdocs.org/sdr/USAA980490), Sep 29, 1998: RAIL. CORRODED. PIT - DURING Q1 CHECK, FOUND LIGHT CORROSION (.50 INCH BY 12 INCH AREA) FORWARD SECTION OF CARGO RT TIE DOWN RAIL AFT. SECTION NEEDS REPLACED AT STA 18921 TO ST - [SDR USAA980489](https://openairdocs.org/sdr/USAA980489), Sep 29, 1998: BEAM. CORRODED. PIT - DURING Q1 CHECK, FOUND BL ZERO CORRODED THROUGH AT STA 3870, 1 INCH BY .50 INCH AREA, T-CAP (BEAM). REPAIRED PER SRMS 51-70-06. (X) - [SDR USAA980488](https://openairdocs.org/sdr/USAA980488), Sep 29, 1998: BEAM. CORRODED. PIT - DURING Q1 CHECK, FOUND BEAM CORRODED THROUGH AT STA 3820 (1 INCH BY 1 INCH AREA) AT BL 1127R. REPAIRED PER SRM CHAPTER 51. (X) - [SDR USAA980487](https://openairdocs.org/sdr/USAA980487), Sep 29, 1998: BEAM. CORRODED. PIT - DURING Q1 CHECK, FOUND CORROSION BEYOND LIMITS AFTER REMOVAL ON BEAM (3 INCHES BY .50 INCH AREA), AT BL 600R AT STA 3870 - STA 4610. REPAIRED PER SRM 53-1 - [SDR USAA980479](https://openairdocs.org/sdr/USAA980479), Sep 29, 1998: DOOR PAN. CRACKED. PIT - DURING Q1 CHECK, FOUND .5 INCH CRACK AFT CARGO DOOR PAN AT PAN AFT EDGE BELOW LATCH CAM ARM. INSTALLED DOUBLER PER SRM 52-05 FIG 35A. (M) - [SDR USAA980478](https://openairdocs.org/sdr/USAA980478), Sep 29, 1998: BEAM. CORRODED. PIT - DURING Q-1 CHECK, FOUND 29.125 INCH LONG 740MM CORRODED T-CAP BEYOND LIMITS AT T-CAP AT BL 1127R STATION 3870-4610. REPLACED T-CAP PER SRM CHAPTER 51. (M) - [SDR USAA980477](https://openairdocs.org/sdr/USAA980477), Sep 29, 1998: BEAM. CORRODED. PIT - DURING Q-1 CHECK, FOUND 38.625 INCH 980 MM CORRODED BEAM CORRODED BEYOND LIMITS MED FLOOR THRESHOLD SUPPORT AT STATION 3870-4850. REPLACED SUPPORT PER SRM - [SDR USAA980476](https://openairdocs.org/sdr/USAA980476), Sep 29, 1998: BEAM. CORRODED. PIT - DURING Q-1 CHECK, FOUND HEAVY CORROSION ON BEAM 24 INCHES LONG AT VALET AREA BL 475 AT STATION 5600-6600. REMOVED AND REPLACED PER SRM 51-70-06. (M) - [SDR USAA980475](https://openairdocs.org/sdr/USAA980475), Sep 29, 1998: BEAM. CORRODED. PIT - DURING Q-1 CHECK, FOUND CORRODED MATERIAL 29.125 INCH 740MM AT BL 1127L STATION 3870-4610 T-CAP CORRODED BEYOND LIMIT. REPLACED T-CAP PER SRM CHAPTER 51. - [SDR USAA980474](https://openairdocs.org/sdr/USAA980474), Sep 29, 1998: SKIN. DISBONDED. PIT - DURING Q-1 CHECK, FOUND DISBONDING 1.5 INCH BY 1.5 INCH AT SEAT AND 16 INCH BY 4.5 INCH STRINGER AT STATION 24011 AND 24611 WITHIN STRINGERS 21A AND 23 ON - [SDR USAA980428](https://openairdocs.org/sdr/USAA980428), Sep 29, 1998: BEAM. CRACKED. PIT - DURING Q1 CHECK, FOUND CORROSION FROM STA 4610 - STA 6030 BEAM BL 1127R, 1 INCH BY 3 INCH AREA. CORROSION ENTIRE LENGTH, DEEP AREA AT END OF SPLICE HAS .0 - [SDR USAAF98040](https://openairdocs.org/sdr/USAAF98040), May 9, 1998: BATTERY PACK. DISCHARGED. GSO - CENTER SECTION OF FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (X) - [SDR USAAF98014](https://openairdocs.org/sdr/USAAF98014), Feb 9, 1998: UPSTOP. FAILED. PIT - FLT 0864 - AFTER TAKEOFF FROM PIT, THE RT MLG WOULD NOT RETRACT. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MLG - [SDR USAAF97087](https://openairdocs.org/sdr/USAAF97087), Nov 6, 1997: SENSOR. LOOSE. FLT 1546 AND FLT 527 - ORF - BOTH FLIGHTS RETURNED TO ORF DUE TO LANDING GEAR PROBLEMS. ON BOTH OCCASIONS AFTER TAKEOFF FROM ORF, WHEN THE LANDING GEAR WAS RETR - [SDR USAAF97083](https://openairdocs.org/sdr/USAAF97083), Oct 19, 1997: VALVE. FAILED. PIT/BOS - FLT 1696 - AT FL 330, RECEIVED 3 CHIME ALARM INDICATING THE CABIN ALTITUDE WAS CLIMBING. CAPTAIN PERFORMED EMERGENCY DESCENT TO 10,000 FEET. THE MAXIM - [SDR USAAF97081](https://openairdocs.org/sdr/USAAF97081), Oct 14, 1997: SWITCH. FAILED. FLT 8077 - IND-MSP - ON CLIMB-OUT FROM IND, RUD2 FAULT ANNUNCIATED ON MFDU. FLIGHT RETURNED TO IND WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 ACTUATOR STICKING - [SDR USAAF97082](https://openairdocs.org/sdr/USAAF97082), Oct 13, 1997: MANIFOLD. FAILED. FLT 8078 - IND-PHL - EN ROUTE TO PHL, RUD2 FAULT ANNUNCIATED ON MFDU. FLIGHT DIVERTED TO RIC FOR MAINTEANCE CONVENIENCE. FLIGHT LANDED RIC WITHOUT FURTHER INCID - [SDR USAAF96069](https://openairdocs.org/sdr/USAAF96069), Jun 29, 1996: BATTERY PACK. DISCHARGED. PIT - FOUND EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT CIRCUIT BREAKERS AND REPLACED THE MAIN ENTRANCE DOOR EXIT SIGN BATTERY PACK. (M) - [SDR USAA951040](https://openairdocs.org/sdr/USAA951040), Sep 29, 1995: PROX SENSOR. MISALIGNED. GSO - FLIGHT NR 1794 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. GROUND FLIGHT FAULT ON MULTI FUNCTION DISPLAY UNIT. RETURNED TO GSO FOR LANDING. FOUND PRO - [SDR USAA950651](https://openairdocs.org/sdr/USAA950651), Jun 27, 1995: FIRE WIRE. CHAFED. PIT - FLT 348 - AFTER TAKEOFF, THE APU FIRE LIGHT ILLUMINATED. THE CAPTAIN DISCHARGED THE BOTTLES AND THE LIGHT EXTINGUISHED. FLIGHT RETURNED TO PIT. MAINTENANC - [SDR USAA950088](https://openairdocs.org/sdr/USAA950088), Feb 5, 1995: EEL BATT PACK. DISCHARGED. PIT - FLT 883 - DURING PREFLIGHT, FOUND FLT DECK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATION CHECKS NORMAL. (W) ## 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 19940915036679I](https://openairdocs.org/incident/19940915036679I), Sep 15, 1994: Fokker F28MK0100 (N894US), Huntsville, AL. Flap assemetry problem on approach, unable correct. No flap landing normal. Taxied to gate. Reset unit checked ok. --- 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.