N868US

Cancelled 2003

Deregistered aircraft · 1990 Fokker F.28 MK 0100 · Rolls-Royce TAY-650-15

Cancelled
March 31, 2003
Exported to
Germany
Status when cancelled
Valid registration
Serial number
11313
Year built
1990
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
September 18, 1990
Certificate issued
February 20, 2003
Last registry action
February 20, 2003
Mode S code
ABEE62
Owner when cancelled
Wilmington Trust Co Trustee
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 · 14

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

SDR USAAF01064Battery Pack · inoperativeRIC - THE FIRST CLASS EMERGENCY EXIT FLOOR LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE GROUND/FLIGHT SWITCH. OPERATIONALLY CHECKED OK. (M)Aug 15, 2001 · N868US · Fokker F28MK0100 · Emergency LightingSDR USAA010811Skin · delaminatedPIT - FOUND SKIN DELAMINATED 10 INCHES BY 12 INCHES, LEFT AND RIGHT LAVATORIES, STATION 24011 AND 24611 STRINGER 51 AND 53. INSTALLED RIVETS IN LEFT AND RIGHT LAVATORIES PER EA. (M)Jun 7, 2001 · N868US · Fokker F28MK0100 · Fuselage Structure (General)SDR USAAF01019Battery Pack · dischargedIND - THE EMERGENCY LIGHTS AND EMERGENCY EXIT LIGHT IN THE FORWARD ENTRANCE AREA WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN THE POWER SUPPLY. OPS CHECKED OK. (M)May 5, 2001 · N868US · Fokker F28MK1000 · Emergency LightingSDR USAAF99045Battery Pack · dischargedIND - FOUND AFT LAVATORY AREA AND AISLE LIGHT 6 INOPERATIVE. MAINTENANCE REPLACED THE NR 8 BATTERY PACK. (M)Sep 11, 1999 · N868US · Fokker F28MK1000 · Emergency LightingSDR USAAF98041Upstop Damper · failedPIT - FLT 536 - AFTER TAKEOFF FROM PIT, LEFT MAIN GEAR DID NOT FULLY RETRACT. CREW RECYCLED GEAR TWO TIMES WITH SAME RESULT. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR UPSTOP DAMPER. (M)May 9, 1998 · N868US · Fokker F28MK1000 · Landing Gear Retraction/Extension SystemSDR USAAF98017Qty Transmitter · malfunctionedPIT - CAPTAIN ADVISED VIA ACARS THE THE NR 1 HYD QTY WAS LOW AND LOST NOSE WHEEL STEERING. AN EMERGENCY WAS DECLARED AND THE A/C LANDED WITHOUT FURTHER INCIDENT. THE A/C WAS CHECKED, NO LEAKS WERE NOTED. SERVICED HYD NR 1 AND NR 2 SYSTEM. FOUND NR 1 HYDRO Feb 17, 1998 · N868US · Fokker F28MK1000 · Hydraulic Quantity SensorSDR USAAF98003Battery Pack · dischargedIND - THE AFT RIGHT WING FAIRING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE CORRESPONDING POWER SUPPLY AND BATTERY PACK. (M)Jan 7, 1998 · N868US · Fokker F28MK1000 · Emergency LightingSDR 98ZZZM204Power Supply · inoperativeIND - THE AFT RIGHT WING FAIRING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE CORRESPONDING POWER SUPPLY AND BATTERY PACK. (M)Jan 7, 1998 · N868US · Fokker F28MK1000 · Emergency LightingSDR USAAF97040Engine · vibrationBHM/CLT - FLT 1480 - WHLE IN HOLDING PATTERN OVER CLT DUE TO WEATHER CONDITIONS, VIBRATION WAS EXPERIENCED ON RIGHT ENGINE. CREW WENT TO ALTERNATE PROCEDURES. INDICATION STILL EXCEEDED LIMITATIONS. THE RIGHT ENGINE WAS PUT TO IDLE. THE CREW DECLARED AN EMEApr 22, 1997 · N868US · Fokker F28MK1000 · Engine (Turbine/Turboprop)SDR USAA970136Bulkhead Angles · crackedPIT - DURING Q1 VISIT, FOUND 1 INCH CRACK LEFT SIDE, .50 INCH CRACK RIGHT SIDE AT FUSELAGE CTR PRESS BULKHEAD ANGLE CRACK, STR NR 11 AND STR NR 64. INSTALLED ANGLE REPAIRS PER US AIRWAYS EA NR 46607. (X)Apr 15, 1997 · N868US · Fokker F28MK1000 · Fuselage Main, BulkheadSDR USAAF96020Pseu Computer · failedPIT - FL 1193 - ON CLIMB-OUT FROM PHL, CREW RECEIVED TCAS FAULT AND GROUND/FLIGHT CONTROL FAULT. EN ROUTE TO MCI, CREW RECEIVED THE TAKEOFF CONFIGURATION STAB TRIM FAULT. FLIGHT DIVERTED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE PFeb 12, 1996 · N868US · Fokker F28MK1000 · Ground Proximity SystemSDR USAA951042Sensor · failedPIT - FLT NR 1025 - AFTER TAKEOFF WE RECEIVED A GND/FLT CONTROL MSG ON MFDU. ALL INDICATIONS INDICATED AIRCRAFT WAS STILL ON GND. RETURNED TO PIT AFTER CONSULTING WITH MAINTENANCE CONTROL. REPLACED NR 3 RT PROXIMITY SENSOR PER MM 32-63-03. ADJUSTED AND OPSSep 30, 1995 · N868US · Fokker F28MK1000 · Landing Gear Position and WarningSDR USAA951095Skin · gougedPIT - C-1 CHECK INSPECTION, FOUND GOUGE 5 INCH LENGTH AND .047 DEEP, MAXIMUM AT THE TOP IN VERTICAL STAB RIGHT SIDE NEAR RIB NR 5, UNDER ICE SCRAPPER. INSTALLED EXTERNAL DOUBLER REPAIR PER USAIR EA NR 31389. (M)Sep 29, 1995 · N868US · Fokker F28MK1000 · Vertical Stabilizer, Plate/SkinSDR USAA950021Downlock Act · malfunctionedPHL - FLT NR 183 - ON FINAL APPROACH, CREW COULD NOT GET 3 GREEN LIGHTS ON THE GEAR. THE LEFT MAIN GEAR LIGHT TESTED BUT WOULD NOT ILLUMINATE. CYCLED GEAR, THEN AN INTERMITTENT LEFT LANDING GEAR DOWNLOCK SWITCH LIGHT ON MULTIFUNCTION DISPLAY UNIT. AIRCRAFT Jan 16, 1995 · N868US · Fokker F28MK1000 · Landing Gear Retraction/Extension System

Other aircraft with N868US · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N868US is registered now to the first aircraft listed.