# N457US: Fokker F.28 MK 1000, registration cancelled 1997-08-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 14, 1997 - Exported to: Canada - Status when cancelled: Triennial form not returned - Airframe: [Fokker F.28 MK 1000](https://openairdocs.org/model/fokker-f-28-mk-1000) (registry code 4990808) - Serial number: 11036 - Type of aircraft: Fixed wing multi engine - Certificate issued: August 15, 1989 - Last registry action: April 29, 1997 - Mode S code: A58DF0 - Owner when cancelled: [US Airways Inc](https://openairdocs.org/faa-owner/US%20AIRWAYS%20INC) - Location: [Arlington, VA](https://openairdocs.org/faa-place/VA/Arlington) - Owner type: Corporation - Owner's area on the map: 38.8783° N, 77.1007° W: Placed by OpenAirDocs: center of Arlington, VA, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N457US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=457US - Page: https://openairdocs.org/deregistered/N457US-1997-08-14 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. ADs and bulletins for the Fokker F.28 MK 1000: https://openairdocs.org/model/fokker-f-28-mk-1000.md ## Service difficulty reports (41) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR QXEA9700152](https://openairdocs.org/sdr/QXEA9700152), Apr 26, 1997: CIRCUIT BOARD. INOPERATIVE. EMERGENCY LIGHT ON CABIN BULKHEAD INOP. REPLACED CIRCUIT BOARD, OPERATIONAL CHECKS GOOD. - [SDR QXEA9700151](https://openairdocs.org/sdr/QXEA9700151), Apr 26, 1997: CIRCUIT BOARD. INOPERATIVE. EMERGENCY LIGHT ON COCKPIT BULKHEAD INOP. REPLACED CIRCUIT BOARD, OPERATIONAL CHECKS GOOD. - [SDR QXEA9700150](https://openairdocs.org/sdr/QXEA9700150), Apr 26, 1997: CIRCUIT BOARD. INOPERATIVE. EMERGENCY EXIT SIGN AT ROW 8 INOP. REPLACED LIGHTED CIRCUIT BOARD, OPERATIONAL CHECKS GOOD. - [SDR QXEA9700141](https://openairdocs.org/sdr/QXEA9700141), Apr 21, 1997: LIGHT MODULE. DEFECTIVE. EXIT SIGN LIGHTS ON THE BACKSIDE OF OVERHEAD SIGN AT ROW NR 8 ARE INOP. REPLACED LIGHT MODULE, OPERATIONAL CHECK GOOD. - [SDR QXEA9700098](https://openairdocs.org/sdr/QXEA9700098), Mar 27, 1997: SIGNS. INOPERATIVE. PDX- SEVERAL BULBS ARE OUT IN OVERHEAD EMERGENCY EXIT SIGNS. FORWARD AND BOTH MIDDLE OVERHEAD EMERGENCY EXIT SIGNS WERE REPLACED. SIGNS OPS CHECKED GOOD. - [SDR QXEA9700021](https://openairdocs.org/sdr/QXEA9700021), Jan 29, 1997: BALLAST. SHORTED. MAIN INSTRUMENT PANEL LIGHTS LEFT SIDE CIRCUIT BREAKER POPPED. STRONG ELECTRICAL SMELL IN COCKPIT. CREW DID NOT ATTEMPT TO RESET BREAKER. BALLAST TRANSFORMER RE - [SDR QXEA9700017](https://openairdocs.org/sdr/QXEA9700017), Jan 21, 1997: BULBS. FAILED. AFT GALLEY EMERGENCY LIGHT IS INOP, EXIT SIGN ABOVE PASSENGER DOOR IS PARTIALLY INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. - [SDR QXEA9700012](https://openairdocs.org/sdr/QXEA9700012), Jan 14, 1997: POWER SUPPLY. INOPERATIVE. PDX - MAIN CABIN DOOR EMERGENCY LIGHT WEAK AND WING ROOT EMERGENCY LIGHT INOPERATIVE. POWER SUPPLY REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SE - [SDR QXEA9600501](https://openairdocs.org/sdr/QXEA9600501), Dec 29, 1996: APU. MALFUNCTIONED. CABIN FILLED WITH SMOKE AFTER DEPARTURE. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER PROBLEM. PROBLEM TRACED TO OIL IN THE CABIN PACK FROM THE APU. PA - [SDR QXEA9600406](https://openairdocs.org/sdr/QXEA9600406), Sep 23, 1996: BULB. FAILED. EMERGENCY LIGHT THIRD FROM THE FRONT IN THE CABIN IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. - [SDR QXEA9600273](https://openairdocs.org/sdr/QXEA9600273), Aug 2, 1996: BULB. FAILED. EMERGENCY LIGHT OVER LEFT WING EXIT INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. - [SDR QXEA9600229](https://openairdocs.org/sdr/QXEA9600229), Jun 30, 1996: ACTUATOR. LEAKING. HYDRAULIC SYSTEM UTILITY MASTER WARNING LIGHT ILLUMINATED AND UTILITY SYSTEM HYDRAULIC QUANITITY DROPPED TO ZERO. ALTERNATE GEAR EXTENSION PERFORMED AND AIRCRAF - [SDR QXEA9600206](https://openairdocs.org/sdr/QXEA9600206), Jun 16, 1996: BULBS. FAILED. EXIT LIGHT AT ROW 8 IS OUT. LIGHT PANEL REPLACED AND LIGHT OPS CHECKED GOOD. - [SDR QXEA9600205](https://openairdocs.org/sdr/QXEA9600205), Jun 16, 1996: SPLICE. LOOSE. FLOOR PROXIMITY LIGHTS ON AISLE SEATS 4, 5 AND 6 ARE INOP. SPLICE REPAIRED AT SEAT 5AB, LIGHTS OPS CHECKED GOOD. - [SDR QXEA9600176](https://openairdocs.org/sdr/QXEA9600176), May 17, 1996: BULB. FAILED. OVERHEAD EVACUATION LIGHT ROW 7 WON'T ILLUMINATE. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. - [SDR QXEA9600151](https://openairdocs.org/sdr/QXEA9600151), Apr 18, 1996: FUSE. FAILED. ENTRANCE WAY EXIT SIGN EVAC LIGHT BULBS ARE INOP. FUSE WAS REPLACED IN BATTERY PACK, LIGHTS OPS CHECKED GOOD. - [SDR QXEA9600129](https://openairdocs.org/sdr/QXEA9600129), Mar 22, 1996: CIRCUIT BOARD. FAILED. EXIT LIGHT ABOVE COCKPIT DOOR IS INOP. LIGHT CIRCUIT BOARD REPLACED AND LIGHT OPS CHECKED GOOD. - [SDR QXEA9600127](https://openairdocs.org/sdr/QXEA9600127), Mar 22, 1996: WINDOW POST. CRACKED. DURING HFEC INSPECTION OF LT NR 3 WINDOW POST REARWARD FLANGE TYPE-D, CRACK WAS NOTED AT BOLT HOLE NR 4 AND 6. CRACK LENGTH AT BOLT HOLE NR 4 IS .625 INCH, CRAC - [SDR QXEA9600126](https://openairdocs.org/sdr/QXEA9600126), Mar 22, 1996: SKIN. CRACKED. THREE SMALL CRACKS NOTED IN FUSELAGE SKIN BELOW NUMBER TWO WINDOW POST ON LEFT SIDE OF FUSELAGE. CRACKS NOTED DURING C-CHECK AND REPAIRED I/A/W SRM. - [SDR QXEA9600125](https://openairdocs.org/sdr/QXEA9600125), Mar 22, 1996: BLKHD WEB. CRACKED. REAR PRESSURE BULKHEAD 4 CRACKED BETWEEN BEAMS 425R AND 1050R AT HORIZONTIAL BEAM. CRACK RADIATES HORIZONTIALLY UNDER SUPPORT BRACKET BETWEEN HYDRAULIC LINES AN - [SDR QXEA9600124](https://openairdocs.org/sdr/QXEA9600124), Mar 22, 1996: RELEASE MECH. CORRODED. SERVICE/EMERGENCY DOOR EMERGENCY RELEASE MECHANISM WOULD NOT RELEASE DURING C-CHECK TASK CARD OPS CHECK. EMERGENCY RELEASE MECHANISM REMOVED, CLEANED, LUBED AND - [SDR QXEA9600123](https://openairdocs.org/sdr/QXEA9600123), Mar 22, 1996: BRACKET. CRACKED. FORWARD HOOK LATCH BRACKET FOR MAIN CABIN DOOR IS CRACKED THROUGH AFT LOWER RADIUS. CRACK NOTED DURING C-CHECK AND BRACKET REPLACED. - [SDR QXEA9600122](https://openairdocs.org/sdr/QXEA9600122), Mar 22, 1996: FITTING. CRACKED. AFT HOOK LATCH FITTING FOR MAIN CABIN DOOR IS CRACKED THROUGH THE FORWARD SUPPORT BRACKET IN THE DOOR STRUCTURE. CRACK NOTED DURING C-CHECK AND BRACKET REPLACED - [SDR QXEA9600121](https://openairdocs.org/sdr/QXEA9600121), Mar 22, 1996: BOX BEAM. CRACKED. LOGITUDINAL BOX BEAM AT RT SIDE OF PANEL 21A IS CRACKED AT FORWARD PRESS BULKHEAD. CRACK IS LOCATED ON TOP INBOARD CORNER. CRACK NOTED DURING C-CHECK. CRACK REP - [SDR QXEA9600120](https://openairdocs.org/sdr/QXEA9600120), Mar 22, 1996: BOX BEAM. CRACKED. LONGITUDINAL BOX BEAM LT SIDE OF PANEL 21A IS CRACKED AT FORWARD PRESS BULKHEAD. CRACK IS LOCATED ON TOP INBOARD CORNER. CRACK NOTED DURING C-CHECK AND REPAIRED - [SDR QXEA9600119](https://openairdocs.org/sdr/QXEA9600119), Mar 22, 1996: NLG BAY WEB. CRACKED. NOSE LANDING GEAR BAY TOP COVER IS CRACKED AT STA 2745, 4.5 TO 5 INCHES RIGHT ON CENTERLINE, CRACK LENGTH APPROX .5 INCH. SECOND CRACK NOTED AT RIVETS STA 2870, - [SDR QXEA9600118](https://openairdocs.org/sdr/QXEA9600118), Mar 22, 1996: SKIN. CRACKED. FUSELAGE OUTER SKIN IS CRACKED AT BULKHEAD FRAME STA 15205 AND STRINGER LT 15. ALSO, STRINGER CROSSOVER CASTALLATION REPAIR ON INTERIOR SIDE IS CRACKED. CRACK N - [SDR QXEA9600117](https://openairdocs.org/sdr/QXEA9600117), Mar 22, 1996: BLKHD ANGLE. CRACKED. FORWARD PRESSURE BULKHEAD CONNECTION ANGLE BETWEEN STRINGERS 2 AND 3 IS CRACKED 6 INCHES LEFT OF CENTER LINE BETWEEN 2ND AND 3RD HILOCK. CRACK LENGTH IS APPROX - [SDR QXEA9600116](https://openairdocs.org/sdr/QXEA9600116), Mar 22, 1996: BLKHD BEAM. CRACKED. A 4 TO 5 INCH CRACK ON FORWARD PRESSURE BULKHEAD AT BEAM NR 6 COPILOTS SIDE. CRACK NOTED DURING C-CHECK. CRACK REPAIRED I/A/W SRM. - [SDR QXEA9600115](https://openairdocs.org/sdr/QXEA9600115), Mar 22, 1996: BLKHD FRAME. CRACKED. CRACK NOTED ON FORWARD PRESSURE BULKHEAD FRAME 880/1550 LOWER CHORD LBL CRACK LENGH APPROX 2.5 INCH, LBL 3 TO 6. CRACK REPAIRED I/A/W EA 28-53-328. - [SDR QXEA9600114](https://openairdocs.org/sdr/QXEA9600114), Mar 22, 1996: BLKHD BEAM. CRACKED. AFT SURFACE OF FRONT PRESSURE BULKHEAD IS CRACKED AT RT HORIZONTAL BEAM NR 3, CRACK LENGTH IS APPROX 5 INCHES. CRACK NOTED DURING C-CHECK. CRACK REPAIRED I/A/W - [SDR QXEA9600113](https://openairdocs.org/sdr/QXEA9600113), Mar 22, 1996: BLKHD STIFFENER. CRACKED. A CRACK THROUGH RIVET ON VERTICAL STIFFENER BETWEEN NR 3 AND 4 HORIZONTAL BEAMS RT SIDE OF FRONT PRESSURE BULKHEAD FORWARD SIDE. CRACK NOTED DURING C-CHECK. CRA - [SDR QXEA9600060](https://openairdocs.org/sdr/QXEA9600060), Feb 13, 1996: WIRE. BROKEN. PDX - EVACUATION LIGHT AT ROW 3A INOP. BROKEN WIRE REPAIRED AT SEAT 2B. LIGHT OPS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9600034](https://openairdocs.org/sdr/QXEA9600034), Jan 29, 1996: BULB. FAILED. PDX - EXIT SIGN AT ROW 8 IS DIM ON BOTH SIDES. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9500442](https://openairdocs.org/sdr/QXEA9500442), Dec 13, 1995: BULB. FAILED. PDX - FORWARD CABIN AISLE EXIT SIGN HAS SEVERAL EMERGENCY LIGHT BULBS (28V) INOP. ALL SEVEN 28V BULBS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO - [SDR QXEA9500411](https://openairdocs.org/sdr/QXEA9500411), Nov 29, 1995: BULB. FAILED. PDX - EMERGENCY EXIT LIGHT BURNED OUT ON THE RIGHT SIDE. BULB WAS REPLACED AND LIGHT OPS CHECKED. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9500389](https://openairdocs.org/sdr/QXEA9500389), Nov 14, 1995: BULB. FAILED. PDX - LEFT OVERWING EXIT EMERGENCY LIGHT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9500364](https://openairdocs.org/sdr/QXEA9500364), Oct 30, 1995: BULB. FAILED. BOI - RIGHT SIDE EMERGENCY EXIT LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9500263](https://openairdocs.org/sdr/QXEA9500263), Aug 23, 1995: EEL BULB. FAILED. GEG - CENTER ISLE OVERHEAD EXIT SIGN IS INOP WITH EMERGENCY LIGHT ARMED. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9500114](https://openairdocs.org/sdr/QXEA9500114), Apr 15, 1995: UPLOCK SPRING. BROKEN. GEG - LEFT GEAR RED LIGHT REMAINS ILLUMINATED AFTER GEAR DOWN OR UP SELECTION. REPLACED BROKEN RETURN SPRING IN AFT GEAR DOOR UPLOCK ASSY. GEAR INDICATION OPS C - [SDR QXEA9500092](https://openairdocs.org/sdr/QXEA9500092), Mar 27, 1995: EEL BULB. FAILED. PDX - EMERGENCY EXIT LIGHT RIGHT SIDE INOP. REPLACED BULB AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ## Other aircraft with N457US - [Cancelled 2013-07-02](https://openairdocs.org/deregistered/N457US-2013-07-02): Boeing 737-59D, S/N 26421. Exported to Indonesia. Owner: [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE), Ditchingham Bungay --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.