N1427A

Cancelled 2006

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

Cancelled
May 4, 2006
Exported to
Brazil
Status when cancelled
Valid registration
Serial number
11412
Year built
1992
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
January 25, 1993
Certificate issued
November 9, 2005
Last registry action
November 9, 2005
Mode S code
A0AD6C
Owner when cancelled
Fokker Aircraft N1427a Trust
Owner type
Corporation

From the FAA registry file of November 3, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N1427A and the event date: after January 18, 1974, when the previous aircraft’s registration ended, through this one’s cancellation.

Service difficulty reports · 9

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

SDR AALA20040565Windshield · crackedORD - FIRST OFFICER WINDSHIELD CRACKED AND ARCING. REPLACED FIRST OFFICER WINDSHIELD IN ACCORDANCE WITH MM 56-11-00-4. SYSTEM GROUND CHECKED NORMAL OPERATION.May 16, 2004 · N1427A · Fokker F28MK0100 · Flight Compartment WindowsSDR AALA20030545Engine · vibrationDURING LEVEL FLT AT 31,000 FT, AIRSPEED 270 KNTS, ON SELECTING 250 KNTS, NR 1 ENG INDICATED HIGH VIB ON MFDU ACCOMPANIED BY AUDIBLE NOISE & VIBRATION FELT THROUGH A/C. ATTEMPTED ICE CLEARING PROCEDURES WITH NO SUCCESS. ADVANCING THROTTLE ABOVE 1.14 EPR CAUSEMay 8, 2003 · N1427A · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR AALA20021092Manifold · failedDFW - FLT 551 - AFTER TAKEOFF, BOTH STAB TRIM FAULTED, BOTH YAW DAMPER AND NR 2 RUDDER SYSTEM FAULTED. STAB TRIM AND YAW DAMPER WERE RESET. LANDED DFW WITHOUT INCIDENT. REPLACED RUDDER MANIFOLD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M0Jul 24, 2002 · N1427A · Fokker F28MK0100 · Rudder Control SystemSDR AALA20021079Rudder · faultyAFTER TAKEOFF BOTH STABILIZER TRIM FAULTED, BOTH YAW DAMPER AND NR 2 RUDDER SYSTEM FAULTED. STABILIZER TRIM AND YAW DAMPER WERE RESET. LANDED WITHOUT INCIDENT. REPLACED RUDDER LIMITER MONITOR. SYSTEM GROUND CHECKED NORMAL OPERATION.Jul 23, 2002 · N1427A · Fokker F28MK0100 · Stabilizer Control SystemSDR AALA20002034Controller · defectiveDFW - FLT 890 - EN ROUTE DFW-MEM, FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL AND SMOKE IN CABIN. DECLARED EMERGENCY, RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED CABIN SKIN SENSOR. REPLACED NR 1 SIDE AND NR 2 SIDE CABIN TEMPERATURE CONTROLLERSDec 6, 2000 · N1427A · Fokker F28MK0100 · Cabin Temperature ControllerSDR AALA20000154Fitting · leakingDFW - FLT 581 - ON APPROACH ORD, HYDRAULIC SYSTEM ONE QTY LOW. MANUALLY EXTEND GEAR AND LANDED ORD WITHOUT INCIDENT. REPLACED NR 2 ENGINE NR 1 QUICK DISCONNECT FITTING. SERVICED NR 1 HYDRAULIC SYSTEM. ACCOMPLISHED LEAK CHECK. GROUND CHECKED NORMAL OPERATIJan 31, 2000 · N1427A · Fokker F28MK0100 · Hydraulic System, MainSDR AALA970280Stringer · crackedTUL - FOUND STRINGER NR 68 CRACKED APPROXIMATELY STATION 4000. INSTALLED NEW STRINGER AND SPLICE PAGE SRM 51-70-0L. (M)Feb 4, 1997 · N1427A · Fokker F28MK0100 · Fuselage Main, Longeron/StringerSDR AALA960061Light Strip · defectiveDFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY HAD ONE BULB INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)Jan 16, 1996 · N1427A · Fokker F28MK0100 · Emergency LightingSDR AALA951922Psu · defectiveDFW - FLT 1738 - EN ROUTE DTW/DFW DURING CRUISE, ODOR SIMILAR TO HOT PLASTIC NOTED IN CABIN. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO DFW LANDING WITHOUT INCIDENT. REPLACED PASSENGER SERVICE UNIT PANEL AT SEAT 5DE DUE TO RELAY FOUND HOT AND MENov 9, 1995 · N1427A · Fokker F28MK0100 · Passenger Compartment Equipment

Other aircraft with N1427A · 2

The FAA can assign a mark to another aircraft once a registration is cancelled. N1427A is registered now to the first aircraft listed.