N898US

Cancelled 2008

Deregistered aircraft · 1992 Fokker F.28 MK 0100 · Rolls-Royce TAY-650-15

Cancelled
June 17, 2008
Exported to
Australia
Status when cancelled
Valid registration
Serial number
11398
Year built
1992
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Special flight permit
Airworthiness date
December 11, 2002
Certificate issued
June 5, 2008
Last registry action
June 5, 2008
Mode S code
AC64DF
Owner when cancelled
Bayview Aviation Inc Trustee
Owner type
Corporation

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.

Service difficulty reports · 12

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR USAAF01084Warning System · malfunctionedCMH-PHL - FLT 1147 - AFTER TAKEOFF AND LANDING GEAR RETRACTION, THE CREW RECEIVED A LEFT MLG FAULT DISPLAY ON THE MFDU. THE LANDING GEAR WAS CYCLED BUT THE INTRANSIT LIGHT REMAINED ILLUMINATED AND THE 'MAX AIRSPEED 220 KTS' MESSAGE REMAINED ON THE MFDU. THE Nov 21, 2001 · N898US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF01072Door · wornSDF - FLT 457 - EN ROUTE PIT-SDF, DURING APPROACH, RECEIVED A LEFT MAIN GEAR DOOR MESSAGE. PERFORMED THE QRH PROCEDURE WHILE EXECUTING A MISSED APPROACH. ACCOMPLISHED A FLY BY TO VERIFY THAT THE GEAR WAS DOWN. THE FLIGHT THEN LANDED WITHOUT FURTHER INCIDENTSep 9, 2001 · N898US · Fokker F28MK0100 · Landing Gear SystemSDR USAAF01046Battery Pack · inoperativeCLT - THE AFT FLOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK FOR THE FLOOR EMERGENCY LIGHTS. OPERATIONALLY CHECKED OK. (M)Jul 13, 2001 · N898US · Fokker F28MK0100 · Airborne Auxiliary Power Unit (APU) SystemSDR USAAF01044Smoke Detector · malfunctionedATL-CLT - FLT 536 - AFTER TAKEOFF AND CLIMBING THROUGH FL090, FLIGHT ATTENDANTS REPORTED SMOKE ALARMS IN BOTH AFT LAVATORIES WERE RINGING. NO SMOKE WAS NOTICED. THE FLIGHT RETURNED TO FIELD AS A PRECAUTION, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED Jul 12, 2001 · N898US · Fokker F28MK0100 · Smoke DetectionSDR USAAF01045Smoke Detector · malfunctionedATL-CLT - FLT 1536 - AT FL100, THE SMOKE ALARMS BEGAN TO CHIME IN THE AFT LAVATORY. THE CHIME STOPPED A MINUTE LATER. NO SMOKE WAS OBSERVED. FLIGHT LANDED IN CLT WITHOUT INCIDENT. (M)Jul 12, 2001 · N898US · Fokker F28MK0100 · Smoke DetectionSDR USAAF01027Battery Pack · inoperativeIND - THE AFT CABIN LOW LEVEL AND THE LOWER WING TO BODY EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN A POWER SUPPLY AT ROW 16. OPS CHECKED OK. (M)May 22, 2001 · N898US · Fokker F28MK0100 · Emergency LightingSDR USAAF01008Coalescer Bag · contaminatedCLT-PIT FLT 1240 - AFTER TAKEOFF, BOTH LAVATORY SMOKE DETECTORS BEGAN ALERTING. A SMELL OF SMOKE WAS ALSO PRESENT IN THE REAR CABIN AREA. THE AIR CONDITIONING PACKS WERE SWITCHED TO MANUAL, FULL COLD, TO COOL THE CLIMBING PACK TEMPERATURES. TEMPERATURES WERMar 7, 2001 · N898US · Fokker F28MK0100 · Humidity Control SystemSDR USAAF00004Fitting · brokenPIT/GRR - FLT 1136 - DURING DESCENT, THE NR 1 HYDRAULIC QUANTITY DROPPED TO ZERO. THE AIRCRAFT LANDED AT ITS DESTINATION WITHOUT INCIDENT AND WAS TOWED TO THE TERMINAL. MAINTENANCE REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP.Jan 16, 2000 · N898US · Fokker F28MK0100 · Hydraulic Pump (Electric/Engine), MainSDR USAAF96085Armrest · brokenCLT - BROKEN ARMREST ON THE RIGHT OVERWING EMERGENCY EXIT. MAINTENANCE REPLACED THE ARMREST. (M)Aug 1, 1996 · N898US · Fokker F28MK0100 · Emergency ExitsSDR USAAF96001Prox Switch · failedPIT - FL 317 - AFTER TAKEOFF AND UPON GEAR RETRACTION, CREW RECEIVED 'GND/FLT' MESSAGE ON MFDU, FOLLOWED BY SEVERAL AURAL AND VISUAL WARNINGS. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCH ELECTRONICS UJan 1, 1996 · N898US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAA950762Governor · leakingSRQ - FLT NR 0139 - DURING A GO-AROUND PROCEDURE DUE TO THUNDERSTORMS, THE LEFT ENGINE WOULD NOT PRODUCE SELECTED THRUST. CAPTAIN DECIDED TO DIVERT TO SRQ WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE LP SHAFT GOVERNOR. LEAK CHECKED GOOD. (Jul 20, 1995 · N898US · Fokker F28MK0100 · Turbine GovernorSDR USAA950446Hyd System · malfunctionedMCI - FLT NR 1481 - EN ROUTE TO MCI, CAPTAIN RECEIVED A NR 1 SYSTEM LOW PRESSURE WARNING LIGHT. THE CAPTAIN CONTINUED TO MCI BUT DECLARED AN EMERGENCY. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. (M)May 4, 1995 · N898US · Fokker F28MK0100 · Hydraulic System, Main