N1451N

Cancelled 2003

Deregistered aircraft · 1993 Fokker F.28 MK 0100 · Rolls-Royce TAY-650-15

Cancelled
November 21, 2003
Exported to
Switzerland
Status when cancelled
Valid registration
Serial number
11460
Year built
1993
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
September 7, 1993
Certificate issued
September 10, 2003
Last registry action
September 10, 2003
Mode S code
A0B7CB
Owner type
Corporation

From the FAA registry file of November 5, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 9

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

SDR AALA20002121Apu · leakingORD - FLT 576 - EN ROUTE ORD-RST AT GATE, SHORTLY AFTER STARTING ENGINES, CABIN FILLED WITH SMOKE. SHUTDOWN ENGINES. REPLACED APU. SYSTEM UNDER INVESTIGATION. (M)Dec 19, 2000 · N1451N · Fokker F28MK0100 · Airborne Auxiliary Power Unit (APU) SystemSDR AALA20001833Heat Exchanger · defectiveORD - FLT 1214 - EN ROUTE ORD-YYZ, CABIN PRESSURE CONTROL MESSAGE ILLUMINATED IN CABIN. UNABLE TO CONTROL CABIN PRESSURE IN THE MANUAL MODE. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE PACK. REPLACED PRIMARY AND SECONDARY HEAT EXCHNov 1, 2000 · N1451N · Fokker F28MK0100 · Cabin Cooling SystemSDR AALA20001812Valve · leakingORD - FLT 430 - EN ROUTE ORD-DCA AT 16,000 FEET, PACK ONE ILLUMINATED ON MFDU. SHORTLY AFTER COCKPIT FILLED WITH SMOKE. TURNED PACK NR 1 OFF AND ACCOMPLISHED SMOKE/FIRE PROCEDURES CHECKLIST. RETURNED ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED FLOW COct 31, 2000 · N1451N · Fokker F28MK0100 · Air Conditioning SystemSDR AALA991851Wire · brokenDFW - DURING OVERNIGHT MAINTENANCE, MAIN CABIN EMERGENCY EXIT FLOOR PATH LIGHT STRIP INOPERATIVE. REPAIRED WIRE SPLICE ON FLOOR STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Dec 5, 1999 · N1451N · Fokker F28MK0100 · Light System WiringSDR AALA991067Manifold · defectiveORD - FLT 1734 - ON CLIMB-OUT FROM ORD/YUL, RECEIVED FAULT INDICATION FOR RUDDERS 1 AND 2, YAW DAMPERS 1 AND 2, AND STABILIZER TRIMS 1 AND 2. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED ACTIVE RUDDER MANIFOLD, REPLACED HIGH PRESSURE SWITCHJul 21, 1999 · N1451N · Fokker F28MK0100 · Rudder Control SystemSDR AALA990290O-Ring · leakingDFW - FLT 640 - DURING CRUISE, THE NR 1 HYDRAULIC SYSTEM LOW LIGHT ILLUMINATED ON THE MULTIFUNCTION DISPALY UNIT (MFDU). CREW ACCOMPLISHED CHECKLIST FOR HYDRAULIC SYSTEM LOW QUANTITY AND ALTERNATE FLAP EXTENSION AND GEAR EXTENSION AND GEAR EXTENSION WEAR USEDFeb 28, 1999 · N1451N · Fokker F28MK0100 · Hydraulic System, MainSDR AALA960726Instr Panel · defectiveORD - FLT 1140 - AFTER TAKEOFF AUS, ELECTRICAL ODOR/SMOKE NOTED AT WINDSHIELD. SHUT OFF BOTH AUTO-THROTTLES AND ODOR/SMOKE DISAPPEARED WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED FLIGHT MODE PANEL. SYMay 5, 1996 · N1451N · Fokker F28MK0100 · Instrument PanelSDR AALA952066Retract Mech · lack of lubeORD - FLT NR 81 - AFTER TAKEOFF, WHEN LANDING GEAR RETRACTED, RECEIVED MULTIPLE WARNING MESSAGES ON MFDU ASSOCIATED WITH GROUND/FLIGHT CONTROL AND PRESSURIZATION. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. PSEU BITE CHECK ACCOMPLISHED INDICATING RDec 10, 1995 · N1451N · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR AALA951575Adc · defectiveORD - FLT NR 2085 - AFTER TAKEOFF ORD DURING CLIMB-OUT, LOST LEFT EFIS AIRSPEED INDICATION FOLLOWED BY NR 1 FLIGHT AUGMENTATION PANEL FAULTS. UNABLE TO RESET AND AIRCRAFT RETURNED TO ORD, LANDING WITHOUT INCIDENT. REPLACED NR 1 AIR DATA COMPUTER. SYSTEM GROSep 3, 1995 · N1451N · Fokker F28MK0100 · Air Data Computer

Other aircraft with N1451N · 2

The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N1451N now.