# Service difficulty reports: N864US, cancelled Jul 15, 2003

A list on [N864US, cancelled Jul 15, 2003](https://openairdocs.org/deregistered/N864US-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 USAAF01073](https://openairdocs.org/sdr/USAAF01073.md): Actuator · failed · Sep 16, 2001 · N864US · Fokker F28MK0100 · Landing Gear Actuator
  > RDU - FLT 1286 - EN ROUTE - RDU-PHL, THE LEFT MLG WOULD NOT RETRACT AFTER TAKEOFF. THE LANDING GEAR WAS RECYCLED, BUT THE LEFT MLG STILL DID NOT RETRACT. THE FLIGHT RETURNED TO THE FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT MLG R
- [SDR USAAF01062](https://openairdocs.org/sdr/USAAF01062.md): Battery Pack · inoperative · Aug 2, 2001 · N864US · Fokker F28MK0100 · Emergency Lighting
  > PIT - THE FORWARD FLOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED A BATTERY PACK. OPERATIONALLY CHECKED OK. (M)
- [SDR USAAF98087](https://openairdocs.org/sdr/USAAF98087.md): Sensor · inoperative · Oct 27, 1998 · N864US · Fokker F28MK0100 · Fuel Indicating System
  > PHL - FLT 320 - AFTER TAKEOFF FROM PHL, THE TOWER REPORTED THAT FUEL WAS VENTING FROM THE RIGHT WING. AN 'AUTO FUEL FEED' FAULT ALSO ILLUMINATED. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CENTER FUEL TANK RIGHT FLO
- [SDR USAAF98077](https://openairdocs.org/sdr/USAAF98077.md): Controller · inoperative · Sep 17, 1998 · N864US · Fokker F28MK0100 · Cabin Pressure Controller
  > ILM - FLT 1690 - AFTER TAKEOFF FROM ILM, THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO ILM AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 AUTOMATIC PRESSURIZATION CONTROLLER. (M)
- [SDR USAAF98048](https://openairdocs.org/sdr/USAAF98048.md): Gasket · failed · Jun 10, 1998 · N864US · Fokker F28MK0100 · Hydraulic Pump, Auxiliary
  > CLT - FLT 1694 - AFTER TAKEOFF FROM CLT, SYSTEM NR 2 HYDRAULIC QUANTITY DROPPED TO 14 PERCENT. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE NR 2 HYDRAULIC PUMP DUE TO BLOWN GASKETS. (X)
- [SDR USAAF98018](https://openairdocs.org/sdr/USAAF98018.md): Dnlock Plunger · lack of lube · Feb 18, 1998 · N864US · Fokker F28MK0100 · Landing Gear Retraction/Extension System
  > FLT 1672 - PIT-MDT - AFTER TAKEOFF FROM PIT, NOSE GEAR ALERT ILLUMINATED ON MFDU. THE BLUE INTRANSIT LIGHT REMAINED LIT IN GEAR HANDLE. CREW RECYCLED GEAR WITH SAME RESULT. CAPTAIN DECLARED AND EMERGENCY AND FLIGHT RETURNED TO PIT. FLIGHT LANDED WITHOUT FU
- [SDR USAAF97093](https://openairdocs.org/sdr/USAAF97093.md): Downlock · overserviced · Nov 16, 1997 · N864US · Fokker F28MK0100 · Landing Gear Retraction/Extension System
  > FLT 275 - GSO-PHL - ON CLIMB-OUT FROM GSO, THE NOSE LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO GSO WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND AN EXCESSIVE AMOUNT OF GREASE IN AND AROUND THE NOSE GEAR DOWNLOCK PLUNGER. CLEANED AND EXCESSIVE AMOUNT O
- [SDR USAAF97084](https://openairdocs.org/sdr/USAAF97084.md): Press X-Mitter · failed · Oct 25, 1997 · N864US · Fokker F28MK0100 · Engine Oil Pressure
  > FLT 579 - CLT-PNS - ON FINAL APPROACH OVER THE OUTER MARKER, CREW RECEIVED 'OIL PRESS OIL LIMIT' MESSAGE FOLLOWED BY 'OIL PRESS LOW' MESSAGE ON THE MULTI FUNCTION DISPLAY. CAPTAIN SHUT DOWN THE ENGINE AND DECLARED AN EMERGENCY. FLIGHT LANDED PNS WITHOUT FURT
- [SDR USAAF97074](https://openairdocs.org/sdr/USAAF97074.md): Air Data Comp · failed · Sep 15, 1997 · N864US · Fokker F28MK0100 · Air Data Computer
  > FLT 998 - CLT-DTW - EN ROUTE TO DTW, THE NR 1 AIR DATA COMPUTER FAILED. CREW DECIDED TO DIVERT TO PIT FOR MAINTENANCE CONVENIENCE. FLIGHT LANDED PIT WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 AIR DATA COMPUTER. (M)
- [SDR USAAF97042](https://openairdocs.org/sdr/USAAF97042.md): Relay · failed · Apr 25, 1997 · N864US · Fokker F28MK0100 · Landing Gear Retraction/Extension System
  > DCA/BOS - FLT 1503 - ON APPROACH TO BOS, THE NOSE GEAR WOULD NOT EXTEND. THERE WAS NO NOSE GEAR GREEN LIGHT. AT 1,000 FEET 'GEAR UNSAFE' ILLUMINATED ON THE MULTIFUNCTION DISPLAY. CREW CYCLED THE GEAR. ALL INDICATIONS NORMAL. FLIGHT LANDED AT BOS WITHOUT F
- [SDR 97ZZZX2014](https://openairdocs.org/sdr/97ZZZX2014.md): Relay · failed · Apr 25, 1997 · N864US · Fokker F28MK0100 · Landing Gear Retraction/Extension System
  > DCA/BOS - FLT 1503 - ON APPROACH TO BOS, THE NOSE GEAR WOULD NOT EXTEND. THERE WAS NO NOSE GEAR GREEN LIGHT. AT 1,000 FEET 'GEAR UNSAFE' ILLUMINATED ON THE MULTIFUNCTION DISPLAY. CREW CYCLED THE GEAR. ALL INDICATIONS NORMAL. FLIGHT LANDED AT BOS WITHOUT F
- [SDR USAAF97041](https://openairdocs.org/sdr/USAAF97041.md): Proximity Sensor · broken · Apr 24, 1997 · N864US · Fokker F28MK0100 · Landing Gear Retraction/Extension System
  > BUF/PHL - FLT 871 - AFTER TAKEOFF, GEAR WOULD NOT RETRACT AND GEAR WARNING INDICATED. AT 400 FEET 'AIR/GND SENSOR' WARNING APPEARED ON MFDU. FLIGHT RETURNED TO BUF WITHOUT FURTHER INCIDENT. AIRCRAFT FERRIED GEAR DOWN TO PIT FOR MAINTENANCE. MAINTENANCE REP
- [SDR USAA970093](https://openairdocs.org/sdr/USAA970093.md): Skin · cracked · Mar 18, 1997 · N864US · Fokker F28MK0100 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-1 CHECK, FOUND 3 CRACKS AT FUSELAGE LOW PRESSURE CONNECTION PORT AT UP SLOT ATTACHMENT ON SKIN. INSTALLED DOUBLER REPAIR PER US AIRWAYS EA 29161. (M)
- [SDR USAA970092](https://openairdocs.org/sdr/USAA970092.md): Frame · cracked · Mar 18, 1997 · N864US · Fokker F28MK0100 · Fuselage Main, Frame
  > PIT - DURING Q1 CHECK, FOUND 2.5 INCH CRACK AT LEFT SIDE FRAME 14911 AT STRINGER NR 11. ROUTED OUT DAMAGED AREA. INSTALLED A SHIM AND TWO NEW REPAIR ANGLES PER EA NR 46396. (M)
- [SDR USAA970091](https://openairdocs.org/sdr/USAA970091.md): Frame · cracked · Mar 18, 1997 · N864US · Fokker F28MK0100 · Fuselage Main, Frame
  > PIT - DURING Q1 CHECK, FOUND 3 INCH CRACK AT RT SIDE, FRAME 14911, AT STRINGER NR 64. ROUTED OUT DAMAGED AREA. INSTALLED A SHIM AND TWO NEW REPAIR ANGLES PER EA 46396. (M)
- [SDR USAAF96101](https://openairdocs.org/sdr/USAAF96101.md): Fuel Pump · failed · Sep 21, 1996 · N864US · Fokker F28MK0100 · Fuel Boost Pump
  > PIT-DTW - FLT 1140Z - ON CLIMB-OUT, RECEIVED FAULT LIGHTS FOR NR 1 AND NR 2 RIGHT FUEL PUMPS. AIRCRAFT RETURNED TO PIT. NO FURTHER INCIDENTS DURING FLIGHT. MAINTENANCE REPLACED R1 AND R2 FUEL BOOST PUMPS. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA950411](https://openairdocs.org/sdr/USAA950411.md): Eel Relay · inoperative · Apr 26, 1995 · N864US · Fokker F28MK0100 · Emergency Lighting
  > PIT - FOUR OVERWING EXIT LIGHTS AND OVERHEAD EXIT LIGHTS DO NOT ILLUMINATE WITH GEAR DOWN. MAINTENANCE REPLACED RELAY K2618-A, CHECK NORMAL. (Z)
- [SDR USAA950022](https://openairdocs.org/sdr/USAA950022.md): Sensor · faulted · Jan 22, 1995 · N864US · Fokker F28MK0100 · Landing Gear Position and Warning
  > MCO - FLT 8004 - ON TAKEOFF, LIFT DUMPER FAULTED. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE L3 SENSOR ON LT GEAR MM 32-63-03 PG 401. RAN BITE TEST. NO FAULT ON LIFT DUMPERS, OPERATIONS CHECK NORMAL. (W)
- [SDR USAA950023](https://openairdocs.org/sdr/USAA950023.md): Seal · worn · Jan 17, 1995 · N864US · Fokker F28MK0100 · Passenger/Crew Doors
  > PIT - FLT 114 - RUSHNG AIR SOUND WAS HEARD COMING FROM THE MED BY F/A. CABIN BEGAN TO CLIMB. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MAIN ENTRANCE DOOR SEAL. PRESSURIZED AND OPERATIONS CHECK OK. (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 = 'N864US' AND deregistration_id = 'N864US-2003-07-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N864US-2003-07-15/reports

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