N883US

Cancelled 2003

Deregistered aircraft · 1991 Fokker F.28 MK 0100

Cancelled
April 28, 2003
Exported to
Netherlands
Status when cancelled
Valid registration
Serial number
11337
Year built
1991
Type
Fixed wing multi engine
Airworthiness
Standard, transport
Airworthiness date
September 6, 1991
Certificate issued
February 26, 2003
Last registry action
February 26, 2003
Mode S code
AC2ACD
Owner when cancelled
Wilmington Trust Co Trustee
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 · 1

FAA accident and incident reports matched to this aircraft by N883US and the event date: up to this one’s cancellation.

Service difficulty reports · 15

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

SDR USAAF01089Apu · malfunctionedABE-PIT - FLT 1660 - AFTER TAKEOFF, THE APU FAULTED WITH THE RIGHT ENGINE GENERATOR ON MEL. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE IDG AND PLACED THE APU ON MEL. (M)Dec 23, 2001 · N883US · Fokker F28MK0100 · APU Core EngineSDR USAAF01088Idg · failedABE - PIT - FLT 1660 - DURING ROTATION THE RIGHT ENGINE GENERATOR FAULTED. RESET DID NOT FIX. THE APU FAULTED AFTER RUNNING NORMALLY. THE AIRCRAFT RETURNED TO ABE AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE RIGHT ENGINE GENERATOR ON MEL. THE APU SDec 23, 2001 · N883US · Fokker F28MK0100 · AC Generator-AlternatorSDR USAAF0066Valve · failedCLT-BHM - FLT 2358 - ON LANDING GEAR RETRACTION, AFTER TAKEOFF, THERE WAS A NOSE GERA FAULT AND A BLUE LIGHT IN THE GEAR HANDLE. THE LANDING GEAR WAS CYCLED WITH SAME RESULTS. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLAAug 29, 2000 · N883US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAA990315Structure · crackedPIT - DURING C-CHECK, FOUND TWO CRACKS IN FUSELAGE SKIN ( 1 INCH AND 2 INCH LONG CRACKS) AT APU EXHAUST OUTLET AREA FS 27250 STRINGERS 46-50. DOUBLER INSTALLED, STRINGERS REPAIRED AND REPLACED PER EA NR 51808 DATED 4/6/99. (M)Apr 7, 1999 · N883US · Fokker F28MK0100 · Fuselage Main, StructureSDR USAAF99007Synchronizer · inoperativePIT - FLT 864 - AFTER TAKEOFF FROM PIT, A 'FLAP ASYMMETRY' WARNING ILLUMINATED. CREW PERFORMED THE ABNORMAL PROCEDURE CHECKLIST. THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 3 RIGHT SIDE FLAP SYNCHRONIZER. (XJan 22, 1999 · N883US · Fokker F28MK0100 · Trailing Edge Flap Control SystemSDR USAAF98044Generator · failedPIT FLT 0540 - EN ROUTE TO MKE, RIGHT GENERATOR FAULTED. APU WAS STARTED AND APU GENERATOR WAS PUT ON LINE. TEN MINUTES LATER, THE APU SHUT DOWN. FLIGHT RETURNED TO PIT DUE TO ONE GENERATOR OPERATION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RMay 22, 1998 · N883US · Fokker F28MK0100 · AC Generator-AlternatorSDR 98ZZZX2342Gcu · failedPIT FLT 0540 - EN ROUTE TO MKE, RIGHT GENERATOR FAULTED. APU WAS STARTED AND APU GENERATOR WAS PUT ON LINE. TEN MINUTES LATER, THE APU SHUT DOWN. FLIGHT RETURNED TO PIT DUE TO ONE GENERATOR OPERATION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RMay 22, 1998 · N883US · Fokker F28MK0100 · AC RegulatorSDR USAAF98024Temp Cntrl Valve · failedFLT 1773 - CLT - SHORTLY AFTER TAKEOFF FROM CLT, THE AIR CONDITIONING CABIN SUPPLY TEMPERATURE REACHED 134 F. CREW CYCLED THE PACK ON AND OFF. HIGH CABIN SUPPLY TEMP STILL EXISTED. SINCE THE LEFT AIR CONDITIONING PACK WAS ON MEL, THE FLIGHT RETURNED TO CLT Feb 28, 1998 · N883US · Fokker F28MK0100 · Cabin Temperature Control SystemSDR USAAF98021Door · damagedFLT 275 - PHL-BTV - AFTER T/O, GEAR WOULD NOT RETRACT. ALT PROCEDURES PERFORMED. GEAR SUCCESSFULLY RAISED WITH MANUAL OVERRIDE. FLT PROCEEDED TO BTV. ON DESCENT TO BTV WHEN LANDING GEAR WAS LOWERED, 'R MLG UNSAFE' MESSAGE ILLUMINATED. GREEN RMLG DOWN AND LFeb 24, 1998 · N883US · Fokker F28MK0100 · Landing Gear DoorsSDR 98ZZZM340Rod · failedFLT 275 - PHL-BTV - AFTER T/O, GEAR WOULD NOT RETRACT. ALT PROCEDURES PERFORMED. GEAR SUCCESSFULLY RAISED WITH MANUAL OVERRIDE. FLT PROCEEDED TO BTV. ON DESCENT TO BTV WHEN LANDING GEAR WAS LOWERED, 'R MLG UNSAFE' MESSAGE ILLUMINATED. GREEN RMLG DOWN AND LFeb 24, 1998 · N883US · Fokker F28MK0100 · Landing Gear Door Retract SectionSDR USAA970355Frame · crackedPIT - DURING Q1 CHECK, FOUND 1.75 INCH CRACK AT 24-2 OBLIQUE FRAME STR 34. FOUND DURING VISUAL INSPECTION. CUT OUT CRACK AND INSTALLED DOUBLER REPAIR PER EA 39164A. (X)Dec 5, 1997 · N883US · Fokker F28MK0100 · Fuselage Main, FrameSDR USAAF97037Selector Panel · inoperativeFLT 698 - GSO-LGA - AFTER TAKEOFF FROM GSO WHEN LANDING GEAR WAS RETRACTED, THE FOLLOWING MESSAGES APPEARED ON THE MULTI-FUNCTION DISPLAY; NOSE LG UNSAFE, RT MAIN LG UNSAFE, LT MAIN LG UNSAFE. GEAR WAS RECYCLED THREE TIMES WITH SAME INDICATION EACH TIME. FLIApr 11, 1997 · N883US · Fokker F28MK0100 · Landing Gear SelectorSDR USAAF96100Lamp · failedCLT - EMERGENCY EXIT LIGHT, ROW 11F, INOP. MAINTENANCE RELAMPED LIGHT. (M)Sep 13, 1996 · N883US · Fokker F28MK0100 · Emergency LightingSDR USAA951005Eel Wiring · brokenPHL - FLT NR 823 - FOUND FIRST CLASS EMERGENCY LIGHT WIRING INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE IN THE FIRST CLASS CLOSET. (M)Sep 23, 1995 · N883US · Fokker F28MK0100 · Emergency LightingSDR USAA950048Slide · faultyIND - ACCOMPLISHMENT OF JOB CARD J525-60-10 CALLS FOR SLIDE DEPLOYMENT. UPON DEPLOYMENT, SLIDE MOUNTED LIGHTS DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR EVACUATION SLIDE. (W)Jan 23, 1995 · N883US · Fokker F28MK0100 · Escape Slide