# Service difficulty reports: N866US, cancelled Jul 15, 2003 A list on [N866US, cancelled Jul 15, 2003](https://openairdocs.org/deregistered/N866US-2003-07-15.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAF01021](https://openairdocs.org/sdr/USAAF01021.md): Girt Bar · disconnected · May 8, 2001 · N866US · Fokker F28MK0100 · Emergency Equipment > PIT - DURING A SCHEDULED SLIDE CHANGE, FOUND THE SLIDE TO BE REMOVED DID NOT HAVE THE SLIDE GIRT ATTACHED TO THE GIRT BAR, ALTHOUGH THE FIRING CABLE WAS STILL ATTACHED. MAINTENANCE COMPLETED THE SLIDE CHANGE. (M) - [SDR USAAF01003](https://openairdocs.org/sdr/USAAF01003.md): Sign · inoperative · Jan 21, 2001 · N866US · Fokker F28MK0100 · Emergency Lighting > PHL - FOUND THE EMERGENCY EXIT LIGHT OVER SEAT 12F TO BE INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN. (M) - [SDR USAAF00008](https://openairdocs.org/sdr/USAAF00008.md): Light · inoperative · Jan 27, 2000 · N866US · Fokker F28MK0100 · Emergency Lighting > RIC - FOUND EMERGENCY FLOOR LEVEL LIGHTING INOPERATIVE FROM ROW 4 THROUGH 9. MAINTENANCE REPLACED THE FORWARD SECTION OF FLOOR LIGHTING. (M) - [SDR USAAF00007](https://openairdocs.org/sdr/USAAF00007.md): Light · shorted · Jan 27, 2000 · N866US · Fokker F28MK0100 · Emergency Lighting > RIC - THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 4 THROUGH 9 WERE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP AT SEAT ROWS 4 THROUGH 9 AND THE INVERTER. (M) - [SDR USAAF99054](https://openairdocs.org/sdr/USAAF99054.md): Battery · discharged · Nov 22, 1999 · N866US · Fokker F28MK0100 · Emergency Lighting > FOUND EMERGENCY LIGHTS ONLY COME ON FOR 5 SECONDS AND THEN GO OUT. MX REPLACED THE BATTERY PACK, OPS CHECK GOOD. (M) - [SDR USAAF99050](https://openairdocs.org/sdr/USAAF99050.md): Power Supply · inoperative · Oct 3, 1999 · N866US · Fokker F28MK0100 · Emergency Lighting > IND - FOUND EXIT SIGN BETWEEN RIGHT OVERWING EXITS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY. (M) - [SDR USAAF98089](https://openairdocs.org/sdr/USAAF98089.md): Cable · failed · Nov 4, 1998 · N866US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > BYH - FLT 7899 - AFTER TAKEOFF FROM BYH, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE 'UP' POSITION IN EITHER THE NORMAL OR OVERRIDE MODULE. FLIGHT RETURNED TO BYH WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR HANDLE TELEFLEX CABLE. (M) - [SDR USAA980236](https://openairdocs.org/sdr/USAA980236.md): Skin · cracked · Jun 5, 1998 · N866US · Fokker F28MK0100 · Fuselage Main, Plate/Skin > PIT - DURING C-4 CHECK, FOUND.1875 INCH CRACK AND.25 INCH CRACK IN SKIN AT LT AND RT AFT CORNERS OF NOSE GEAR BAY. REMOVED DAMAGED AREAS AND REINSTALLED FASTENERS PER EA 49826. (X) - [SDR USAAF98046](https://openairdocs.org/sdr/USAAF98046.md): Sensor · failed · May 25, 1998 · N866US · Fokker F28MK0100 · Stabilizer Control System > CLT - FLT 8076 - EN ROUTE TO MSP, THE FOLLOWING MESSAGES APPEARED ON THE PFD: HYD STAB 2, HYD STAB 1&2, STAB TRIM 1&2. FLIGHT DIVERTED TO PIT FOR MAINTENANCE. FLIGHT LANDED PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 STABILIZER PROXIMITY SE - [SDR USAAF98036](https://openairdocs.org/sdr/USAAF98036.md): Selector Valve · failed · Apr 11, 1998 · N866US · Fokker F28MK0100 · Landing Gear Selector > PIT - ON APPROACH, GREEN 'NOSE' GEAR INDICATION DID NOT ILLUMINATE. CREW DID A GO-AROUND PROCEDURE AND RECYCLED THE LANDING GEAR. ALL THREE GREEN GEAR INDICATORS ILLUMINATED PROPERLY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING - [SDR USAAF98026](https://openairdocs.org/sdr/USAAF98026.md): Retract Mech · lack of lube · Mar 11, 1998 · N866US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > PIT - 1221 - DURING APPROACH INTOP PIT CREW RECEIVED A NOSE GEAR UNSAFE INDICATION WHEN LOWERING THE LANDING GEAR. CREW ADVISED ATC, EXECUTED A GO-AROUND AND RECYCLED THE GEAR. AFTER RECYCLING THE GEAR ALL INDICATIONS WERE NORMAL. FLIGHT LANDED WITHOUT FURT - [SDR USAAF98023](https://openairdocs.org/sdr/USAAF98023.md): Sensor · out of adjust · Feb 28, 1998 · N866US · Fokker F28MK0100 · Landing Gear Position and Warning > FLT 533 - GSO - AFTER TAKEOFF FROM GSO, CREW WAS UNABLE TO RETRACT THE LANDING GEAR. MANUAL OVERRIDE GEAR RETRACTION WAS SUCCESSFUL. AT APPROXIMATELY 8000 FT THE FOLLOWING MESSAGES APPEARED ON THE MULTI-FUNCTION DISPLAY 'GND/FLT CONTROL', 'L/D FAULT', AND 'T - [SDR USAAF97094](https://openairdocs.org/sdr/USAAF97094.md): Door Stop · out of adjust · Nov 19, 1997 · N866US · Fokker F28MK0100 · Landing Gear Door Retract Section > FLT 275 - GSO-PHL - AFTER TAKEOFF FROM GSO, WHEN LANDING GEAR WAS RETRACTED, 'LMLG' MESSAGE APPEARED ON THE MULTIFUNCTION DISPLAY AND THE INTRANSIT LIGHT REMAINED ON IN THE GEAR HANDLE SELECTOR. THE CREW RECYCLED THE GEAR PER ABNORMAL PROCEDURES BUT THE PROBL - [SDR USAA970218](https://openairdocs.org/sdr/USAA970218.md): Angle · cracked · Jun 10, 1997 · N866US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - CRACKS IN SKIN CONNECTION ANGLES IN RADIUS AT FRAME 14911, STRINGER NR 11 LEFT, STRINGER 64 RT. INSTALLED DOUBLER REPAIR PER USAIRWAYS EA 47081. (M) - [SDR USAA970217](https://openairdocs.org/sdr/USAA970217.md): Skin · delaminated · Jun 5, 1997 · N866US · Fokker F28MK0100 · Fuselage Main, Plate/Skin > PIT - DURING Q-1 CHECK, FOUND FUSELAGE SKIN DELAMINATED, LT SIDE, RT SIDE SHOWED HEAT DAMAGE BETWEEN FRAME 24011-24611, AND BETWEEN UPPER AND LOWER STUB WING CONNECTION ANGLES. INSTALLED DOUBLER REPAIR RT SIDE AND RIVETED LEFT SIDE PER EA NR 28780A. (M) - [SDR USAAF96122](https://openairdocs.org/sdr/USAAF96122.md): Wire · broken · Nov 24, 1996 · N866US · Fokker F28MK0100 · Light System Wiring > MAINTENANCE CHECK REVEALED MID CABIN CEILING EXIT SIGN LIGHTS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE ON LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) - [SDR USAAF96114](https://openairdocs.org/sdr/USAAF96114.md): Windshield · cracked · Nov 3, 1996 · N866US · Fokker F28MK0100 · Flight Compartment Windows > FLT 511 - PIT-GSO - AFTER TAKEOFF, AT APPROXIMATELY 6500 FEET, A BIRD HIT THE CAPTAINS WINDSHIELD AND IT CRACKED. THE FLIGHT RETURNED TO PIT WITHOUT INCIDENT. NO EMEGENCY DECLARED. MAINTENANCE REPLACED THE WINDSHIELD. (M) - [SDR USAA950602](https://openairdocs.org/sdr/USAA950602.md): Actuator · out of adjust · Jun 13, 1995 · N866US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > PIT - FLT 0753 - UPON GEAR RETRACTION, CREW RECEIVED AN INDICATION THAT THE RIGHT MAIN GEAR WAS NOT RETRACTED. FLIGHT RETURNED TO PIT. MAINTENANCE ADJUSTED THE DOWNLOCK ACTUATOR. (M) - [SDR USAA950600](https://openairdocs.org/sdr/USAA950600.md): Sensor · inoperative · Jun 11, 1995 · N866US · Fokker F28MK0100 · Landing Gear Position and Warning > CAK - FLT 0237 - ON APPROACH, THE COMPUTER REPORTED ERRONEOUS GEAR NOT DOWN MESSAGES. A FLYBY WAS PERFORMED. THE CAPTAIN DECLARED AND EMERGENCY AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE SENSOR. OPERATIONS CHECKED GOOD. (M) ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N866US' AND deregistration_id = 'N866US-2003-07-15' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N866US-2003-07-15/reports --- 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.