N1444N

Cancelled 2004

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

Cancelled
May 26, 2004
Status when cancelled
Triennial form not returned
Serial number
11447
Year built
1993
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
March 25, 1993
Certificate issued
March 25, 1993
Last registry action
March 19, 2002
Mode S code
A0B47D
Owner when cancelled
American Airlines Inc
Physical address
Dallas/Ft Worth, TX
Owner type
Corporation

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.

Service difficulty reports · 12

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

SDR AALA20021892Coupling · defectiveDFW - FLT 1024 - EN ROUTE MEM-DFW, LOST SYSTEM 1 HYDRAULIC QUANTITY, SHUT OFF PUMPS. EMERGENCY EXTENDED LANDING GEAR. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED QUICK DISCONNECT COUPLING AND O-RING ON PRESSURE AND SUCTION PORTS ON LEFT ENGINE NR 1 SYSTEMDec 28, 2002 · N1444N · Fokker F28MK0100 · Hydraulic System, MainSDR AALA20021822Connector · looseDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 11 INOPERATIVE. RESECURED CONNECTOR TO EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Dec 17, 2002 · N1444N · Fokker F28MK0100 · Emergency LightingSDR AALA20011822Light · inoperativeDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Sep 26, 2001 · N1444N · Fokker F28MK0100 · Emergency LightingSDR AALA20011554Light · inoperativeORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT MID CABIN INOPERATIVE. REPLACED MID CABIN EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Aug 1, 2001 · N1444N · Fokker F28MK0100 · Emergency LightingSDR AALA20011544Light · inoperativeORD - FLT 31 - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD CABIN INOPERATIVE. REPLACED FORWARD CABIN EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Jul 31, 2001 · N1444N · Fokker F28MK0100 · Emergency LightingSDR AALA20001105Connector · defectiveDFW DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT ESCAPE PATH LIGHTS BETWEEN ROWS 8 AND 11 INOPERATIVE. REPLACED CONNECTOR AT ROW 8. SYSTEM GROUND CHECK NORMAL OPERATION.Jul 2, 2000 · N1444N · Fokker F28MK0100 · Emergency LightingSDR AALA20000397Sensor · defectiveSAT - FLT 1713 - ON DEPARTURE AFTER LANDING GEAR UP, RIGHT AND LEFT GEAR MESSAGE APPEARED. CYCLED GEAR MESSAGE REAPPEARED. REPLACED RIGHT GEAR DOOR SENSOR. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECK NORMAL OPERATION. (M)Mar 2, 2000 · N1444N · Fokker F28MK0100 · Landing Gear Position and WarningSDR AALA991418Wire · brokenDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE FROM ROW 13 TO 15. REPLACED WIRING TO EMERGENCY EXIT FLOOR PATH LIGHTING STRIPS FROM ROW 13 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Sep 20, 1999 · N1444N · Fokker F28MK0100 · Light System WiringSDR AALA991059Wire · shortedORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIPS MID CABIN INOPERATIVE. REPAIRED A SHORTED WIRE CONNECTED TO THE EMERGENCY EXIT FLOOR PATH LIGHT STRIPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Jul 20, 1999 · N1444N · Fokker F28MK0100 · Light System WiringSDR AALA990681Connector · looseDFW - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FORWARD CABIN INOPERATIVE. RESEATED LOOSE EMERGENCY EXIT FLOOR PATH LIGHT WIRE CONNECTOR IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)May 10, 1999 · N1444N · Fokker F28MK0100 · Emergency LightingSDR AALA970369Limiter Monitor · defectiveDFW - FLT T1420 - AFTER TAKEOFF DFW DURING CLIMB-OUT, RUDDER 2 FAIL AND YAW DAMPER 1 FAIL LIGHTS AND MESSAGES ILLUMINATED. AFER SELECTING NR 2 RUDDER OFF, RUDDER 1 AND 2 FAIL MESSAGES APPEARED FOLLOWED BY STAB TRIM 1 AND 2 FAIL AND YAW DAMPER 1 AND 2 FAIL. AFeb 20, 1997 · N1444N · Fokker F28MK0100 · Rudder Control SystemSDR AALA970301Stringer · crackedTUL - STR 68 CRACKED APPROXIMATELY STA 4000. INSTALLED DOUBLER PER SRM 51-70-06-R5. TST: 9,397.14 HOURS. CYCLES, 6,734. (X)Feb 6, 1997 · N1444N · Fokker F28MK0100 · Fuselage Main, Longeron/Stringer

Other aircraft with N1444N · 2

The FAA can assign a mark to another aircraft once a registration is cancelled. N1444N is registered now to the first aircraft listed.