# Service difficulty reports: N295US, cancelled Jun 1, 2004

A list on [N295US, cancelled Jun 1, 2004](https://openairdocs.org/deregistered/N295US-2004-06-01.md).

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

- [SDR 0004522295](https://openairdocs.org/sdr/0004522295.md): Doubler · corroded · Nov 7, 2000 · N295US · Boeing 727251 · Fuselage Main, Bulkhead
  > During "L" check found corrosion on bulkhead skin support doubler at BS 740. Repaired per EA 22-178765.
- [SDR 9902522295](https://openairdocs.org/sdr/9902522295.md): Stringer · cracked · May 18, 1999 · N295US · Boeing 727251 · Wing, Longeron/Stringer
  > DURING M CHECK, FOUND CRACK ON UPPER FORWARD STRINGER AT INBOARD SIDE OF RIGHT WING STATION 357. REPAIRED PER EA 22-166648.
- [SDR 9902502295](https://openairdocs.org/sdr/9902502295.md): Floorbeam · corroded · Apr 29, 1999 · N295US · Boeing 727251 · Fuselage Main, Floor Beam
  > DURING M CHECK, FOUND CORROSION ON NUT PLATE LOCATION ON 1175 FLOORBEAM. REPAIRED PER EA 22-166634.
- [SDR 9708352295](https://openairdocs.org/sdr/9708352295.md): Hyd Line · failed · Apr 27, 1997 · N295US · Boeing 727251 · Hydraulic System, Main
  > DURING TAKEOFF, LOST A-SYSTEM HYDRAULICS. AIRCRAFT DIVERTED TO TPA, DUMPED FUEL, AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT GEAR DOOR DOWN HYDRAULIC LINE. SERVICED A-HYDRAULIC SYSTEM AND CHECKED FOR LEAKS, LEAK AND OPERATIONAL CHECK OK.
- [SDR 9617072295](https://openairdocs.org/sdr/9617072295.md): Transceiver · failed · Aug 6, 1996 · N295US · Boeing 727251 · Weather Radar System
  > DURING FLIGHT RADAR FAILED, NO TEST PATTERN OBSERVED. NO GROUND RETURN IN NORMAL OR CONT/MSP. REPLACED WEATHER RADAR TRANSCEIVER, OPERATIONAL CHECK NORMAL.
- [SDR 9611622295](https://openairdocs.org/sdr/9611622295.md): Floor Beam · corroded · May 15, 1996 · N295US · Boeing 727251 · Fuselage Main, Floor Beam
  > DURING H-CHECK, FOUND CORROSION ON THE BS 1110 FLOOR BEAM CHORD FROM LBL 70 - RBL 19. REPAIRED CHORD (P/N 65-20837-24) PER EA 22-105312.
- [SDR 9611602295](https://openairdocs.org/sdr/9611602295.md): Floor Beam · cracked · May 13, 1996 · N295US · Boeing 727251 · Fuselage Main, Floor Beam
  > DURING H-CHECK, FOUND TWO CRACKS IN THE BS 760 FLOOR BEAM WEB AT RBL 60 AND RBL 70. REPAIRED WEB (P/N 65-16325) PER EA 22-102151.
- [SDR 9611532295](https://openairdocs.org/sdr/9611532295.md): Web · cracked · May 6, 1996 · N295US · Boeing 727251 · Wing Miscellaneous Structure
  > DURING H-CHECK, FOUND A 3 INCH CRACK AND BUCKLING OF THE RIGHT WING AUXILIARY SPAR NR 5 SPOILER SUPPORT WEB. REPAIRED WEB (P/N 65-16216-150) PER EA 22-105281.
- [SDR 9610962295](https://openairdocs.org/sdr/9610962295.md): Actuator Fitting · cracked · Apr 30, 1996 · N295US · Boeing 727251 · Leading Edge Slat Actuator
  > DURING H-CHECK, FOUND A CRACK AND CORROSION IN THE RIGHT WING NR 4 LEADING EDGE FLAP ACTUATOR FITTING. REPLACED FLAP (P/N 65-16225-6A) PER MM 27-81-01.
- [SDR 9600492295](https://openairdocs.org/sdr/9600492295.md): Compressor · stalled · Jan 3, 1996 · N295US · Boeing 727251 · Turbine Engine Compressor Section
  > NR 2 ENGINE COMPRESSOR STALLED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE AND NO DISCREPANCIES WERE NOTED. AIRCRAFT CONTINUED IN SERVICE.
- [SDR 9518052295](https://openairdocs.org/sdr/9518052295.md): Hyd Pump · failed · Nov 15, 1995 · N295US · Boeing 727251 · Hydraulic Pump (Electric/Engine), Main
  > DURING CLIMB AFTER GEAR RETRACTION, 'A' SYSTEM HYDRAULICS DROPPED BELOW TWO GALLONS WITH 'B' SYSTEM HYDRAULIC QUANTITY DROPPING TO ZERO. AIRCRAFT RETURNED TO MSP, DUMPED 10,000 LBS OF FUEL AND LANDED WITHOUT INCIDENT. FOUND QUICK DISCONNECT IN HYDRAULIC SYST
- [SDR 9516562295](https://openairdocs.org/sdr/9516562295.md): Safety Lock · missing · Oct 24, 1995 · N295US · Boeing 727251 · Leading Edge Slat Control System
  > NR 4 LEADING EDGE FLAP WOULD NOT RETRACT ON FLAP RETRACTION, AFTER TAKEOFF. FLAP POSITION AMBER LIGHT REMAINS ILLUMINATED WHEN FLAPS AT ZERO. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SAFETY LOCK MISSING ON SWITCH. ADJUSTED BO
- [SDR 9514532295](https://openairdocs.org/sdr/9514532295.md): Tube · broken · Sep 25, 1995 · N295US · Boeing 727251 · Turbine Engine Oil System
  > EN ROUTE TO DTW, THE NR 1 ENGINE OIL QUANTITY DECREASING AND LOW OIL PRESSURE INDICATION ILLUMINATED. SHUT DOWN NR 1 ENGINE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BROKEN OIL TUBE FROM NR 6 SCAVENGE PUMP. REPLACED TUBE. LEAK CHECK WAS N
- [SDR 9514512295](https://openairdocs.org/sdr/9514512295.md): Scavenge Line · broken · Sep 25, 1995 · N295US · Boeing 727251 · Turbine Engine Oil System
  > NR 1 ENGINE WAS SHUTDOWN AFTER THE OIL SUPPLY HAD BEEN DEPLETED, DUE TO A LEAK AT THE NR 6 BEARING SCAVENGE LINE. THE FLIGHT CONTINUED TO ITS PLANNED DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BROKEN SCAVENGE LINE AND INSPECTED THE ENG
- [SDR 9512102295](https://openairdocs.org/sdr/9512102295.md): Oil Press Sw · malfunctioned · Aug 6, 1995 · N295US · Boeing 727251 · Engine Oil Pressure
  > THE NR 1 ENGINE LOW OIL PRESSURE WARNING ILLUMINATED ON TAKEOFF. TAKEOFF WAS ABORTED, THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE LOW OIL PRESSURE AND DIFFERENTIAL PRESSURE SWITCHES. THE MAIN OIL FILTER WAS INSPECTED FOR CONTAMINANTS, NONE F
- [SDR 9511492295](https://openairdocs.org/sdr/9511492295.md): Fuel Qty Ind Sys · malfunctioned · Jul 28, 1995 · N295US · Boeing 727251 · Fuel Indicating System
  > DURING CLIMBOUT, THE NR 2 FUEL QUANTITY INDICATION DECREASED TO 3,500 LBS FROM 9,000 LBS. DURING RETURN TO BOI, INDICATION RETURNED TO PROPER READING. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DEFERRED NR 2 FQIS PER MEL 28-11A.
- [SDR 9508112295](https://openairdocs.org/sdr/9508112295.md): Warning Switch · sounded · May 19, 1995 · N295US · Boeing 727251 · Central Warning
  > WHEN TAKEOFF POWER WAS APPLIED, THE TAKEOFF WARNING HORN SOUNDED. FLAPS AND LEADING EDGE DEVICES INDICATED NORMAL. AIRCRAFT RETURNED TO THE GATE. REPLACED THE UPPER TRIM WARNING SWITCH. OPERATIONAL CHECK WAS NORMAL.
- [SDR 9504002295](https://openairdocs.org/sdr/9504002295.md): Hyd Pump · failed · Mar 14, 1995 · N295US · Boeing 727251 · Hydraulic Pump, Auxiliary
  > DURING FLIGHT, 'B' SYSTEM HYDRAULIC PUMP NR 2 PRESSURE INDICATION FLICKERING FOLLOWED BY DECREASE IN 'B' SYSTEM QUANTITY. CREW DECLARED AN EMERGENCY AND PERFORMED HYDRAULIC FLUID/SYSTEM LOSS CHECKLIST. JETTISONED 6900 POUNDS OF FUEL AND RETURNED TO MSP WITHO

## 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 = 'N295US' AND deregistration_id = 'N295US-2004-06-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N295US-2004-06-01/reports

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