# Service difficulty reports: N859US, cancelled Mar 25, 2003 A list on [N859US, cancelled Mar 25, 2003](https://openairdocs.org/deregistered/N859US-2003-03-25.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAF01080](https://openairdocs.org/sdr/USAAF01080.md): Battery · discharged · Nov 1, 2001 · N859US · Fokker F28MK0100 · Emergency Lighting > CLT - THE EMERGENCY FLOOR LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAF01058](https://openairdocs.org/sdr/USAAF01058.md): Battery Pack · inoperative · Jul 28, 2001 · N859US · Fokker F28MK0100 · Emergency Lighting > GSO - THE EMERGENCY MARKER LIGHTS IN THE ENTRY AREA WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NR 1 BATTERY PACK. OPERATIONALLY CHECKED OK. (M) - [SDR USAAF00072](https://openairdocs.org/sdr/USAAF00072.md): Downlock Switch · failed · Sep 30, 2000 · N859US · Fokker F28MK0100 · Landing Gear Position and Warning > STL-CLT - FLT 1276 - THE LEFT LANDING GEAR LIGHT STAYS GREN WITH GEAR UP. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT LANDING GEAR PRIMARY DOWN LOCK SWITCH. OPS CHECK NORMAL. (M) - [SDR USAAF00055](https://openairdocs.org/sdr/USAAF00055.md): Engine · malfunctioned · Jul 29, 2000 · N859US · Fokker F28MK0100 · Engine (Turbine/Turboprop) > LEX-PIT - FLT 280 - THE NR 2 ENGINE WAS SHUTDOWN, APPROX 66 MILES FROM PIT, DUE TO SEVERE VIBRATION. ENCOUNTERED MODERATE RAIN AND ENGINE ANTI-ICE WAS IN USE DURING THE VIBRATION EVENT. QRH PROCEDURES WERE ACCOMPLISHED, AN EMERGENCY DECLARED, AND AN UNEVENTF - [SDR USAAF99042](https://openairdocs.org/sdr/USAAF99042.md): Power Supply · inoperative · Aug 28, 1999 · N859US · Fokker F28MK0100 · Emergency Lighting > RDU - FOUND FORWARD FLOOR PROXIMITY LIGHTS AND NR 1 AISLE CEILING LIGHT INOPERATIVE DURING EMERGENCY LIGHT TEST. MAINTENANCE REPLACED THE BATTERY PACK AND SUPPLY UNIT. (M) - [SDR USAAF99029](https://openairdocs.org/sdr/USAAF99029.md): Battery Pack · discharged · May 28, 1999 · N859US · Fokker F28MK0100 · Emergency Lighting > IND - FOUND FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (X) - [SDR USAAF99018](https://openairdocs.org/sdr/USAAF99018.md): Air Dist · odor · Apr 1, 1999 · N859US · Fokker F28MK0100 · Air Distribution System > ALB - FLT 701 - WHILE CLIMBING THROUGH 2000 FEET, A FLIGHT ATTENDANT INFORMED THE FLIGHT CREW OF A BURNING ODOR IN THE CABIN AROUND LEFT ROW 17. THE CREW DECLRED AN EMERGENCY AND ELECTED TO DIVERT THE FLIGHT TO ALB. ON APPROACH TO ALB, THE DOOR DISSIPATED. - [SDR USAAF99005](https://openairdocs.org/sdr/USAAF99005.md): Switch · malfunctioned · Jan 17, 1999 · N859US · Fokker F28MK0100 · Engine Oil Pressure > PIT - FLT 1534 - AFTER TAKEOFF FROM PIT, THE AIRCRAFT SUSTAINED A LIGHTNING STRIKE. THE LEFT ENGINE OIL PRESSURE INDICATOR DROPPED TO ZERO AND THE FLIGHT CREW SHUT DOWN THE LEFT ENGINE. THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. SINGLE - [SDR 99ZZZM156](https://openairdocs.org/sdr/99ZZZM156.md): Transmitter · malfunctioned · Jan 17, 1999 · N859US · Fokker F28MK0100 · Engine Oil Pressure > PIT - FLT 1534 - AFTER TAKEOFF FROM PIT, THE AIRCRAFT SUSTAINED A LIGHTNING STRIKE. THE LEFT ENGINE OIL PRESSURE INDICATOR DROPPED TO ZERO AND THE FLIGHT CREW SHUT DOWN THE LEFT ENGINE. THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. SINGLE - [SDR USAAF97085](https://openairdocs.org/sdr/USAAF97085.md): Power Supply · inoperative · Oct 28, 1997 · N859US · Fokker F28MK0100 · Emergency Lighting > IND - DURING ROUTINE MAINTENANCE VISIT, THE EMERGENCY EXIT LIGHT LOCATED ABOVE THE MAIN ENTRY DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. (M) - [SDR USAAF97051](https://openairdocs.org/sdr/USAAF97051.md): Control Unit · failed · Jun 24, 1997 · N859US · Fokker F28MK0100 · Fire Detection > FLT 854 - CLT-PNS - ON SHORT FINAL APPROACH TO PNS, AT APPROXIMATELY 200 FT, UPON COMPLETION OF APU START, CREW RECEIVED RED 'APU FIRE' WARNING. APU AUTO SHUTDOWN, AND FIRE BOTTLE WAS FIRED. NO EMERGENCY WAS DECLARED. FLIGHT LANDED PNS WITHOUT FURTHER INCID - [SDR USAAF97025](https://openairdocs.org/sdr/USAAF97025.md): Radome · damaged · Mar 5, 1997 · N859US · Fokker F28MK0100 · Aerodynamic Fairings > MDT - FL 1861 - AFTER TAKEOFF FROM PHL, CREW NOTED BIRD STRIKE ON LEFT SIDE OF NOSE. NO ADVERSE EFFECTS WERE NOTED ON COCKPIT GAUGES. FLIGHT CONTINUED. AT APPROXIMATELY 17,500 FEET, CREW NOTED THAT THE LEFT SIDE OF THE RADOME BEGAN TO COLLAPSE AND THE AIRSP - [SDR USAA960612](https://openairdocs.org/sdr/USAA960612.md): Frame · cracked · Sep 17, 1996 · N859US · Fokker F28MK0100 · Fuselage Main, Frame > PIT - DURING Q-1 CHECK, FOUND 3 INCH CRACKS (2 EACH) AND.075 INCH CRACKS (2 EACH) AT FUSELAGE CENTER WING FRONT SPAR FRAME AND ANGLES AT STA 11 (LHS) AND STA 64 (RHS). ROUTED OUT CRACK AREAS IN FRAME AND INSTALLED NEW ANGLES PER EA NR 33430 AND EA NR 32077. - [SDR USAA960611](https://openairdocs.org/sdr/USAA960611.md): Skin · delaminated · Sep 17, 1996 · N859US · Fokker F28MK0100 · Elevator, Plate/Skin > PIT - DURING Q-1 CHECK, FOUND 4 INCH BY 4 INCH DENT/DELAMINATION LT ELEVATOR BETWEEN RIB 215 AND RIB 1265. REPLACED AND REPAIRED DAMAGED SKIN AND HONEYCOMB CORE AND INSTALLED A DOUBLER PER SRM 51-70-03. (X) - [SDR USAA960610](https://openairdocs.org/sdr/USAA960610.md): Skin · delaminated · Sep 17, 1996 · N859US · Fokker F28MK0100 · Elevator, Plate/Skin > PIT - DURING Q-1 CHECK, FOUND 3 INCH BY 3 INCH DENT/DELAMINATION AT RT ELEVATOR JUST INBOARD OF RIB 1265. REPAIRED AND REPLACED DAMAGED SKIN AND HONEYCOMB CORE AND INSTALLED A DOUBLER PER SRM 51-70-03. (X) - [SDR USAA951038](https://openairdocs.org/sdr/USAA951038.md): Fire Warning · activated · Sep 27, 1995 · N859US · Fokker F28MK0100 · Fire Detection > CLT - FL 1229, ON APPROACH, CREW RECEIVED APU FIRE WARNING LIGHT AND APU AUTO SHUTDOWN. THE APU FIRE BOTTLE DISCHARGED AUTOMATICALLY. THE APPROACH CONTINUED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. NO INDICATION OF FIRE WAS FOUND. MAINTENANCE CHECKE - [SDR USAA950450](https://openairdocs.org/sdr/USAA950450.md): Sensor · faulty · May 7, 1995 · N859US · Fokker F28MK0100 · Leading Edge Slat Control System > MCO - FLT 0244 - AFTER TAKEOFF, THE CAPTAIN RECEIVED A FLAP DISAGREEMENT LIGHT. THE FLAPS WERE RECYCLED BUT THE INDICATAION STILL REMAINED. MAINTENANCE REPLACED THE FLAP LEVER RVDT. ALL TEST CHECKED GOOD. (M) - [SDR USAA950408](https://openairdocs.org/sdr/USAA950408.md): Actuators · failed · Apr 23, 1995 · N859US · Fokker F28MK0100 · Landing Gear Actuator > SRQ-TPA - FLT 2030 - ON TAKEOFF CREW RECEIVED RIGHT LANDING ALERT AFTER GEAR UP SELECTION, GEAR INDICATIONS NORMAL. RECYCLED GEAR SEVERAL TIMES AND DIVERTED FLIGHT TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH MAIN LANDING GEAR - [SDR USAA950359](https://openairdocs.org/sdr/USAA950359.md): Control Rod · out of adjust · Apr 6, 1995 · N859US · Fokker F28MK0100 · Landing Gear Door Retract Section > MCO - FLT 1203 - FLIGHT RETURNED TO MCO DUE TO GEAR DOOR RETRACT PROBLEM. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE CONTROL ROD. OPERATIONS CHECKED GOOD. (W) ## 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 = 'N859US' AND deregistration_id = 'N859US-2003-03-25' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N859US-2003-03-25/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.