N896US

Cancelled 2003

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

Cancelled
October 7, 2003
Exported to
Netherlands
Status when cancelled
Valid registration
Serial number
11391
Year built
1992
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
July 1, 1992
Certificate issued
September 5, 2003
Last registry action
September 5, 2003
Mode S code
AC5D71
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.

FAA incident reports · 2

FAA accident and incident reports matched to this aircraft by N896US and the event date: up to this one’s cancellation.

Service difficulty reports · 14

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

SDR USAAF01039Sign · unserviceableRDU - THE RIGHT OVERWING EXIT SIGN WAS FOUND IN POOR CONDITION. MAINTENANCE REPLACED THE EXIT SIGN. OPERATIONALLY CHECKED OK. (M)Jun 30, 2001 · N896US · Fokker F28MK0100 · Emergency LightingSDR USAAF00073Engine · failedIND - FLT 1193 - EN ROUTE PHL-MCI, THE NR 2 ENGINE SHUT DOWN IN CRUISE FLIGHT, AT FL 350 AND .72 MACH. THE ATTEMPT TO RESTART THE ENGINE WAS UNSUCCESSFUL. AN EMERGENCY WAS DECLARED, AND THE FLIGHT WAS DIVERTED TO IND, WHERE IT LANDED WITHOUT INCIDENT. TOTALOct 1, 2000 · N896US · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR USAAF00029Windshield · crackedCLT-CHS - FLT 583 - FLIGHT WAS IN CRUISE AT FL230, WHEN SMOKE BECAME PRESENT IN THE COCKPIT. OXYGEN MASKS WERE DONNED. WHILE DONNING THE OXYGEN MASKS, THE AIRCRAFT WINDSHIELD BEGAN TO CRACK. AN EMERGENCY WAS DECLARED AND THE FLIGHT WAS DIVERTED TO CAE WHEREApr 12, 2000 · N896US · Fokker F28MK0100 · Flight Compartment WindowsSDR USAAF99022Controller · inoperativeORD - FLT 1543 - EN ROUTE TO MSP FROM CLT AT FL310, THE CABIN PRESSURE ALTITUDE CLIMBED OVER 10,000 FEET. CREW PERFORMED AN EMERGENCY DESCENT. DURING DESCENT THE MANUAL PRESSURIZATION OPERATED INTERMITTENTLY. THE FLIGHT DIVERTED TO ORD AND LANDED WITHOUT FUApr 8, 1999 · N896US · Fokker F28MK0100 · Cabin Pressure ControllerSDR USAAF99014Retract Mech · iced upIND - FLT 569 - ON APPROACH TO IND WHEN THE LANDING GEAR WAS SELECTED DOWN, THE NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. CREW PERFORMED A GO AROUND PROCEDURE AND RECYCLED THE LANDING GEAR BUT THE GEAR STILL DID NOT INDICATE DOWN AND LOCKED. AN ALTERNATE GMar 15, 1999 · N896US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAAF98096Bulb · failedLGA - FLT 464 - ON APPROACH, CREW DID NOT RECEIVE THE GREEN LGIHT ON THE LEFT MAIN LANDING GEAR. CREW CYCLED THE GEAR WITH SAME RESULT. CREW COMPLETED HANDBOOK PROCEDURE AND CONSIDERED GEAR DOWN AND LOCKED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANDec 17, 1998 · N896US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAA980540Beam · corrodedPIT - DURING Q-1 CHECK, FOUND CORROSION AROUND SCREW HOLES 1 INCH AT T-CAP BL 11276 STATION 3845-3450. REPLACED T-CAP. (M)Oct 22, 1998 · N896US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980539Angle · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK WING ATTACH ANGLE LEFT SIDE AT STATION 14911 BETWEEN STRINGER 10 AND 12. LOCALLY FABRICATED ANGLE JOB CARD NR J5-90-0900-029. INSTALLED DOUBLER. (M)Oct 22, 1998 · N896US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980538Angle · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK WING ATTACH ANGLE RIGHT SIDE AT STATION 14911 BETWEEN STRINGER 66 AND 64. LOCALLY FABRICATED ANGLE JOB CARD NR J5-90-09-000-029. INSTALLED DOUBLER. (M)Oct 22, 1998 · N896US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980537Beam · corrodedPIT - DURING Q-1 CHECK, FOUND CORROSION 4 INCHES, 100 PERCENT CORRODED THROUGH ON BEAM AT STATION 4850 BL NR 0. REPLACED T-CAP. (M)Oct 22, 1998 · N896US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980536Beam · corrodedPIT - DURING Q-1 CHECK, FOUND HEAVY CORROSION 8 INCHES BY WIDTH OF T-CAP 4 INCHES APPROX AT BL 1127L STATION 3845-3450. REPLACED T-CAP. (M)Oct 22, 1998 · N896US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980535Skin · corrodedPIT - DURING Q-1 CHECK, FOUND CORROSION 1 INCH AROUND SCREW HOLES ON SKIN AT BL 600 STATION 4850. REPLACED BEAM. (M)Oct 22, 1998 · N896US · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR USAAF96060Gear Indicator · failedMCI - FLT 1193 - UPON GEAR EXTENSION, CREW RECEIVED NOSE GEAR GREEN LIGHT AND THEN THE LIGHT EXTINGUISHED. ALL OTHER GEAR INDICATION WERE EXTINGUISHED. CREW PERFORMED ALTERNATE GEAR EXTENSION PROCEDURE AND TWO TOWER FLY BYS. FLIGHT LANDED WITH NO FURTHER INJun 19, 1996 · N896US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAA950454Fire Bottle · firedPHL - FLT NR 0298 - ON APPROACH, CREW RECEIVED AND APU FIRE INDICATION. THE APU AUTOMATICALLY SHUTDOWN AND THE BOTTLE FIRED, P/N 33100007. THERE WERE NO OTHER INDICATIONS OF A FIRE. MAINTENANCE INSPECTED THE APU FIRE EXIT SYSTEM. THE FIRE EXTINGUISHER BOTTMay 9, 1995 · N896US · Fokker F28MK0100 · Fire Bottle, Fixed