# Service difficulty reports: N857US, cancelled Feb 23, 2005

A list on [N857US, cancelled Feb 23, 2005](https://openairdocs.org/deregistered/N857US-2005-02-23.md).

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

- [SDR USAAF01087](https://openairdocs.org/sdr/USAAF01087.md): Odor · detected · Dec 23, 2001 · N857US · Fokker F28MK0100 · Air Distribution System
  > ILM-CLT - FLT 1546 - DURING CLIMB-OUT THERE WERE STRONG FUMES IN THE CABIN AND THE LAV SMOKE DETECTORS SOUNDED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU, AIR CONDITIONING PACKS, AND ENGINES. NO ABNORMAL I
- [SDR USAAF01054](https://openairdocs.org/sdr/USAAF01054.md): Door · unserviceable · Jul 26, 2001 · N857US · Fokker F28MK0100 · Emergency Exits
  > FLT 835 - EN ROUTE PIT-STL, DURING CLIMB-OUT, THE RIGHT OVERWING EMERGENCY EXIT DOORS BEGAN TO MAKE NOISE, THEN THE COVERS FOR THE EMERGENCY DOOR EMERGENCY RELEASE HANDLE FELL OFF. THE PASSENGERS IN THE EXIT ROWS WERE RESEATED AND THE FLIGHT CONTINUED TO STL.
- [SDR USAAF01055](https://openairdocs.org/sdr/USAAF01055.md): Door · unserviceable · Jul 26, 2001 · N857US · Fokker F28MK0100 · Emergency Exits
  > CLT - FLT 9281 - EN ROUTE STL-CLT - DURING THE FLIGHT, THE RIGHT OVER-WING EMERGENCY EXIT DOORS BECAME UNLATCHED. AFTER LANDING, THE EMERGENCY EXIT DOORS FELL OUT OF THE EMERGENCY EXIT OPENINGS ONTO THE EMERGENCY ROW SEATS. MAINTENANCE REPLACED THE RIGHT SID
- [SDR USAA010934](https://openairdocs.org/sdr/USAA010934.md): Frame · cracked · Jul 25, 2001 · N857US · Fokker F28MK0100 · Fuselage Structure (General)
  > PIT - FOUND FRAME CRACKED 4 INCHES, FS 21736 BETWEEN STRINGER 3 AND THROUGH UPPER C-CHANNEL. INSTALLED TWO REPAIR ANGLES PER EA 71597. (M)
- [SDR USAAF01053](https://openairdocs.org/sdr/USAAF01053.md): Door · unsecure · Jul 25, 2001 · N857US · Fokker F28MK0100 · Emergency Exits
  > PIT - FLT 1472 - EN ROUTE PIT-SDF, DURING CLIMB-OUT, THE COVER FOR THE EMERGENCY DOOR EMERGENCY RELEASE HANDLE AND SOME SAFETY WIRE FELL OFF. THE EMERGENCY DOOR EMERGENCY RELEASE HANDLE WAS FOUND TO BE IN THE INCORRECT POSITION. THE FLIGHT RETURNED TO FIELD
- [SDR USAA010802](https://openairdocs.org/sdr/USAA010802.md): Skin · Jul 1, 2001 · N857US · Fokker F28MK0100 · Fuselage Structure (General)
  > PIT - FOUND SKIN WITH HEAT DAMAGE 8 INCH BY 12 INCH AREA, STATION 27026-27526 STRINGER 46-50. REMOVED HEAT DAMAGE, INSTALLED REPLACEMENT SKIN/DOUBLER PER EA 54649 AND TYP REPAIR 53-40-01. (M)
- [SDR USAAF01029](https://openairdocs.org/sdr/USAAF01029.md): Tube · cracked · May 26, 2001 · N857US · Fokker F28MK0100 · Hydraulic Power System
  > PIT-CLT - FLT 347 - AFTER TAKEOFF, A VERY STRONG ODOR OF SKYDROL WAS NOTED IN THE CABIN. FLIGHT RETURNED TO THE FIELD IN PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A CRACKED FLAIR ON THE RIGHT HYDRAULIC LINE TO THE PRESSURE FILTER. REPLACED
- [SDR USAAF01028](https://openairdocs.org/sdr/USAAF01028.md): Coalescer Bag · dirty · May 25, 2001 · N857US · Fokker F28MK0100 · Humidity Control System
  > STL-PIT - FLT 288 - UPON APPLICATION ON TAKEOFF THRUST, A STRONG, ACRID, MUSTY ODOR DEVELOPED IN THE COCKPIT AND AFT CABIN AREAS. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT AND RIGHT COALESCER BAGS. LEAK CHECKED GOOD. RAN THE
- [SDR USAAF00048](https://openairdocs.org/sdr/USAAF00048.md): Controller · faulty · Jun 24, 2000 · N857US · Fokker F28MK0100 · Windshield/Door Rain/Ice Removal
  > CLT-IND - FLT 235 - DURING CLIMB, SMOKE ODOR WAS PRESENT IN THE COCKPIT. ODOR DISSIPATED WHEN THE WINDOW HEAT WAS TURNED OFF. THE FLIGHT RETURNED TO THE FIELD DUE TO THE DEACTIVATED SYSTEM AND THE WEATHER EN ROUTE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENAN
- [SDR USAAF00006](https://openairdocs.org/sdr/USAAF00006.md): Light · inoperative · Jan 25, 2000 · N857US · Fokker F28MK0100 · Emergency Lighting
  > IND - THE RIGHT AFT OVERWING EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE BEHIND THE SOCKET ASSEMBLY. (M)
- [SDR USAAF99028](https://openairdocs.org/sdr/USAAF99028.md): Wire · broken · May 23, 1999 · N857US · Fokker F28MK0100 · Light System Wiring
  > RDU - FOUND THE PASSENGER DOOR AND FORWARD SERVICE DOOR EMERGENCY EXIT MARKERS AND FLIGHT COMPARTMENT DOME LIGHT REMAIN ILLUMINATED AT ALL TIMES. AIRCRAFT FERRIED TO PIT WHERE MAINTEANCE REPAIRED A BROKEN WIRE AT THE FORWARD EMERGENCY EXIT LIGHT. (X)
- [SDR USAAF99013](https://openairdocs.org/sdr/USAAF99013.md): Tire · failed · Mar 12, 1999 · N857US · Fokker F28MK0100 · Tire
  > PIT - FLT 7881 - AFTER LANDING PIT DURING ROLLOUT, BOTH LEFT MAIN GEAR TIRES BLEW OUT WHEN MODERATE BRAKING WAS APPLIED. MAINTENANCE REPLACED BOTH LEFT MAIN GEAR TIRE ASSEMBLIES AND THE LEFT GEAR GROUND/FLIGHT SWITCH. THE ANTI-SKID SYSTEM AND THE NOSE GEAR S
- [SDR USAAF98055](https://openairdocs.org/sdr/USAAF98055.md): Light · malfunctioned · Jul 13, 1998 · N857US · Fokker F28MK0100 · Emergency Lighting
  > PIT - FLT 671 - AFTER TAKEOFF FROM PIT, THE EMERGENCY EXIT LIGHTS REMAINED ILLUMINATED AFTER LANDING GEAR WAS RETRACTED. MAINTENANCE RESEATED RELAY K2618A AND THE SYSTEM OPERATED NORMALLY. THEY PROGRAMMED THE RELAY FOR CHANGE AS A PRECAUTIONARY MAINTENANCE A
- [SDR USAAF98016](https://openairdocs.org/sdr/USAAF98016.md): Handle · loose · Feb 17, 1998 · N857US · Fokker F28MK0100 · Cargo/Baggage Doors
  > CLE - FLT 598 - ON CLIMB-OUT OF CLE, CAPTAIN RECEIVED A MID CABIN DOOR WARNING LIGHT. FLIGHT RETURNED TO CLE WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MID CARGO HANDLE OPEN. CLOSED HANDLE. WARNING LIGHTS OPS NORMAL. (M)
- [SDR USAAF97055](https://openairdocs.org/sdr/USAAF97055.md): Supply Unit · failed · Jul 5, 1997 · N857US · Fokker F28MK0100 · Landing Gear Position and Warning
  > RDU/PHL - FLT 1408 - ON APPROACH TO PHL WHEN LANDING GEAR WAS SELECTED DOWN, IN-TRANSIT LIGHT ILLUMINATED BUT NONE OF THE THREE GREEN 'DOWN AND LOCKED' INDICATIONS ILLUMINATED. CREW RECYCLED THE GEAR WITH THE SAME RESULT. ATC CONFIRMED THAT ALL GEARS WERE DO
- [SDR USAAF96078](https://openairdocs.org/sdr/USAAF96078.md): Flt Cntrl Comptr · failed · Jul 17, 1996 · N857US · Fokker F28MK0100 · Flight Controller
  > PIT - FL 1601 - AFTER TAKEOFF, CREW RECEIVED 'NO AUTOLAND'MESSAGE. NEITHER AUTOPILOT WOULD TURN ON. FLIGHT RETURNED TO PIT ANDLANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 FCC.(M)
- [SDR USAA950940](https://openairdocs.org/sdr/USAA950940.md): Skin · delaminated · Aug 16, 1995 · N857US · Fokker F28MK0100 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-1 INSPECTION, FOUND FUSELAGE SKIN DELAMINATED APPROXIMATELY 10 INCH BY 24 INCH AREA BETWEEN RIGHT STUB WING UPPER AND LOWER CONNECTION ANGLE FROM STATION 24011 TO STATION 24611. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER USAIR EA NR
- [SDR USAA950939](https://openairdocs.org/sdr/USAA950939.md): Skin · delaminated · Aug 16, 1995 · N857US · Fokker F28MK0100 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-1 INSPECTION, FOUND FUSELAGE SKIN DELAMINATED BETWEEN LEFT STUBWING UPPER AND LOWER CONNECTION ANGLES. AREA APPROXIMATELY 10 INCHES BY 24 INCHES AT STATION 24011 TO STATION 24611. CUT OUT DAMAGED AREA INSTALLED DOUBLER REPAIR PER USAIR EA NR 3
- [SDR USAA9509937](https://openairdocs.org/sdr/USAA9509937.md): Angle · corroded · Aug 11, 1995 · N857US · Fokker F28MK0100 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 INSPECTION, FOUND CORROSION AT ATTACH ANGLE NR 2 RADIO RACK FLOOR PANEL. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 53-12-10. (M)
- [SDR USAA950936](https://openairdocs.org/sdr/USAA950936.md): Stringer · cracked · Aug 2, 1995 · N857US · Fokker F28MK0100 · Fuselage Main, Longeron/Stringer
  > PIT - DURING Q-1 INSPECTION, FOUND.5 INCH CRACK IN STRINGER NR 68 RIGHT SIDE 4 INCHES AFT OF FRAME 3870. INSTALLED DOUBLER REPAIR PER SRM 51-70-06 FIG 202. (M)
- [SDR USAA950941](https://openairdocs.org/sdr/USAA950941.md): Fitting · cracked · Jul 31, 1995 · N857US · Fokker F28MK0100 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 INSPECTION, FOUND.5 INCH CRACK BETWEEN STATION 8305 AND STATION 8805 AT STRINGER NR 2 FITTING. INSTALLED DOUBLER ANGLE PER SRM 53-00-02. (M)
- [SDR USAA950520](https://openairdocs.org/sdr/USAA950520.md): Spinner · moisture · May 18, 1995 · N857US · Fokker F28MK0100 · Turbine Engine Air Inlet Section
  > MEM - FLT 0358 - THE CREW RECEIVED AN ENGINE VIBRATION READING FROM THE NR 2 ENGINE. THE CAPTAIN CUT THE ENGINE BACK TO IDLE AND DECLARED AND EMERGENCY. FLIGHT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED THE SPINNER DUE TO THE PRESENCE OF MOISTURE

## 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 = 'N857US' AND deregistration_id = 'N857US-2005-02-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N857US-2005-02-23/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.