# Service difficulty reports: N8944E, cancelled Aug 27, 2013

A list on [N8944E, cancelled Aug 27, 2013](https://openairdocs.org/deregistered/N8944E-2013-08-27.md).

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

- [SDR DALA100059988](https://openairdocs.org/sdr/DALA100059988.md): Wire · loose · Jan 2, 2010 · N8944E · Doug DC931 · Light System Wiring
  > DURING LINE CHECK FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 7-10 OF THE CABIN WERE INOPERATIVE. MX FOUND A LOOSE WIRE IN THE CONNECTOR, REPAIRED THE CONNECTOR PIN AND THE SYS RETURNED TO NORMAL OPERATION.
- [SDR NWAA093829988](https://openairdocs.org/sdr/NWAA093829988.md): Fuse · blown · Nov 4, 2009 · N8944E · Doug DC931 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 18-21 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE FUSE IN THE APPROPRIATE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD.
- [SDR NWAA081679988](https://openairdocs.org/sdr/NWAA081679988.md): Battery Pack · inoperative · Apr 18, 2008 · N8944E · Doug DC931 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE BATTERY PACK B5-28. OPERATIONAL CHECK WAS GOOD.
- [SDR NWAA071779988](https://openairdocs.org/sdr/NWAA071779988.md): Spar Cap · cracked · May 10, 2007 · N8944E · Doug DC931 · Wing Spar
  > DURING H-CHECK FOUND CRACK IN RIGHT WING AFT UPPER SPAR CAP AT STA XCWS 58.5. REPAIRED PER EA 99-208494.
- [SDR 0601109988](https://openairdocs.org/sdr/0601109988.md): Fitting · leaking · May 30, 2006 · N8944E · Doug DC931 · Hydraulic System, Main
  > FLIGHT CREW NOTICED THE RIGHT HYDRAULIC SYSTEM QUANTITY INDICATOR WAS SHOWING ZERO FLUID IN THE SYSTEM. COM PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY WAS DECLARED FOR LANDING AT MSN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AND WAS TOWED TO THE GATE
- [SDR 0400449988](https://openairdocs.org/sdr/0400449988.md): Clip · cracked · Jan 9, 2004 · N8944E · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING H-CHECK, FOUND CRACK IN FRAME SHEAR CLIP AT BS 1038 L14R. REPAIRED PER EA 99-197375.
- [SDR 0105159988](https://openairdocs.org/sdr/0105159988.md): Compressor · stalled · Dec 30, 2001 · N8944E · Doug DC931 · Turbine Engine Compressor Section
  > DURING CLIMBOUT, THE RIGHT ENGINE EXPERIENCED A STALL WITH ASSOCIATED VIBRATION AND POWER LOSS. CREW SHUT DOWN THE RIGHT ENGINE AND RETURNED TO DTW. MAINTENANCE REPLACED THE RIGHT ENGINE AND TWO PASSENGER WINDOWS ON THE FIGHT SIDE OF THE AIRCRAFT. ENGINE OP
- [SDR 0104809988](https://openairdocs.org/sdr/0104809988.md): Engine · stalled · Dec 30, 2001 · N8944E · Doug DC931 · Engine (Turbine/Turboprop)
  > DURING CLIMBOUT THE RIGHT ENGINE EXPERIENCED A STALL WITH ASSOCIATED VIBRATION AND POWER LOSS. CREW SHUTDOWN THE RIGHT ENGINE AND RETURNED TO DTW. ENGINE OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE.
- [SDR 0103249988](https://openairdocs.org/sdr/0103249988.md): Circuit Breaker · faulty · Sep 7, 2001 · N8944E · Doug DC931 · AC Power Distribution System
  > ELECTRIC SMOKE IN COCKPIT DURING CLIMB. CAPTAIN TURNED OFF "ENG GEN" AND TURNED ON EMERGENCY POWER. STILL SMELLED SMOKE WITH EMERGENCY POWER ON. PERFORMED COM PROCEDURES, DECLARED AN EMERGENCY, AND RETURNED TO STL AND LANDED WITHOUT INCIDENT. FOUND AUTO GROUND
- [SDR 0102209988](https://openairdocs.org/sdr/0102209988.md): Slide · unserviceable · Jun 26, 2001 · N8944E · Doug DC931 · Escape Slide
  > DURING LINE CHECK, DISCOVERED TAIL EVACUATION SLIDE PRESSURE AT ZERO PSI. REPLACED SLIDE AND RETURNED REMOVED SLIDE TO SHOP FOR REPAIR.
- [SDR 0103359988](https://openairdocs.org/sdr/0103359988.md): Skin · cracked · May 8, 2001 · N8944E · Doug DC931 · Fuselage Main, Plate/Skin
  > During H-check found a 1" crack on the fuselage skin panel. Repaired per EA. 99-181165.
- [SDR 0002739988](https://openairdocs.org/sdr/0002739988.md): Brake Assy · seized · Jul 30, 2000 · N8944E · Doug DC931 · Landing Gear Brake System
  > AFTER TAKEOFF, A STRONG BURNING SMELL WAS REPORTED IN CABIN. THERE WAS NO VISIBLE SMOKE PRESENT. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. EMERGENCY EQUIPMENT WAS CALLED OUT AS A PRECAUTION. MAINTENANCE FOUND NR 4 BRAKE DRAGGING AND NR 2 MAIN
- [SDR 9805929988](https://openairdocs.org/sdr/9805929988.md): Slide Bottle · low pressure · Apr 4, 1998 · N8944E · Doug DC931 · Escape Slide
  > DURING LINE MAINTENANCE INSPECTION, FOUND AFT EVACUATION SLIDE BOTTLE LOW ON PRESSURE. REPLACED SLIDE.
- [SDR 9801289988](https://openairdocs.org/sdr/9801289988.md): Fuse · blown · Jan 21, 1998 · N8944E · Doug DC931 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS BETWEEN ROWS 14 THROUGH 17 INOPERATIVE. REPLACED BLOWN FUSE. OPERATIONAL CHECK NORMAL.
- [SDR 9800669988](https://openairdocs.org/sdr/9800669988.md): Fuse · failed · Jan 11, 1998 · N8944E · Doug DC931 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE, OPERATIONAL CHECK NORMAL.
- [SDR 9800299988](https://openairdocs.org/sdr/9800299988.md): Fuse · inoperative · Jan 5, 1998 · N8944E · Doug DC931 · Emergency Lighting
  > DURING LINE CHECK, FOUND EMERGENCY PATHWAY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 14 THRU 17. MAINTENANCE REPLACED BLOWN FUSE AT SEAT ROW 12 RIGHT, OPERATIONAL CHECK OK.
- [SDR 9721409988](https://openairdocs.org/sdr/9721409988.md): Computer · inoperative · Nov 14, 1997 · N8944E · Doug DC931 · Air Data Computer
  > DURING CRUISE FLIGHT, THE AIR DATA COMPUTER BECAME INOPERATIVE. THE AIRCRAFT DIVERTED TO DTW AND THE FLIGHT CREW DISCUSSED THE SITUATION WITH MSP MAINTENANCE CONTROL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AIR DATA COMPUTER AND COMPLETED ALL AP
- [SDR 9720859988](https://openairdocs.org/sdr/9720859988.md): Battery Packs · discharged · Nov 4, 1997 · N8944E · Doug DC931 · Emergency Lighting
  > DURING PERIODIC CHECK, EMERGENCY LIGHT CHARGING AND CONTROL CIRCUIT BREAKERS POPPED. RESET WITH NO HELP. REPLACED BATTERY PACKS. OPERATIONAL CHECK NORMAL.
- [SDR 9719199988](https://openairdocs.org/sdr/9719199988.md): Hyd Pump · failed · Oct 10, 1997 · N8944E · Doug DC931 · Hydraulic Pump (Electric/Engine), Main
  > LEFT ENGINE HYDRAULIC PUMP FAILED AFTER TAKEOFF. FLIGHT. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED PUMP, OPERATIONAL CHECK NORMAL.
- [SDR 9711509988](https://openairdocs.org/sdr/9711509988.md): Transceiver · failed · May 28, 1997 · N8944E · Doug DC931 · Weather Radar System
  > WEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RADAR TRANSCEIVER, OPERATIONAL CHECK NORMAL.
- [SDR 9701889988](https://openairdocs.org/sdr/9701889988.md): Escape Line · binding · Jan 29, 1997 · N8944E · Doug DC931 · Emergency Equipment
  > DURING PERIODIC CHECK, FOUND LEFT AFT OVERWING EMERGENCY EXIT ESCAPE LINE WINDING IN HOUSING. MAINTENANCE LUBED REEL. OPERATIONAL CHECK NORMAL.
- [SDR 9602649988](https://openairdocs.org/sdr/9602649988.md): Epr Indicator · erratic · Jan 27, 1996 · N8944E · Doug DC931 · Engine Pressure Ratio (EPR)
  > THE NR 1 ENGINE EPR INDICATION WAS ERRATIC ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE INDICATOR WITH A SERVICEABLE UNIT.
- [SDR 6302649988](https://openairdocs.org/sdr/6302649988.md): Epr Indicator · failed · Jan 27, 1996 · N8944E · Doug DC931 · Engine Pressure Ratio (EPR)
  > THE NR 1 ENGINE EPR INDICATION WAS ERRATIC ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE INDICATOR WITH A SERVICEABLE UNIT.
- [SDR 9511879989](https://openairdocs.org/sdr/9511879989.md): Blkhd Web · corroded · Jun 19, 1995 · N8944E · Doug DC931 · Fuselage Main, Bulkhead
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LOWER WEB OF THE AFT PRESSURE BULKHEAD AT THE T-CHORD FS 996, APPROXIMATELY 8 OUTBOARD OF RADIALS 22L AND 22R. REPAIRED WEB (P/N 5910130-65) PER EA 99-94812.
- [SDR 9508899988](https://openairdocs.org/sdr/9508899988.md): Switch · out of adjust · Jun 1, 1995 · N8944E · Doug DC931 · Door Warning System
  > AFTER TAKEOFF MSP-DFW AT APPROXIMATELY 6000 FEET MSL, THE FORWARD STAIRWAY DOOR WARNING LIGHT ILLUMINATED. RETURNED TO MSP WITHOUT FURTHER INCIDENT. ADJUSTED THE SWITCH PER MM 52-62-0 PG 501, OPERATIONAL CHECK OK.
- [SDR 9508809989](https://openairdocs.org/sdr/9508809989.md): Longeron · corroded · May 29, 1995 · N8944E · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 30, FS 937 TO 945. REPAIRED LONGERON PER EA 99-094824.
- [SDR 9508049989](https://openairdocs.org/sdr/9508049989.md): Fitting · cracked · May 15, 1995 · N8944E · Doug DC931 · Cargo/Baggage Doors
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE AFT CARGO DOOR LOWER HORIZONTAL BEAM FORWARD END FITTING. REPLACED FITTING PER SRM 51-01, 51-10-1, AND 51-30-1. MFG PART NUMBER 3914025-2B.
- [SDR 9508279989](https://openairdocs.org/sdr/9508279989.md): Frame · corroded · May 12, 1995 · N8944E · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE AFT CARGO DOOR JAMB INTERNAL DOUBLER. REPAIRED PER EA 99-094819, MFG PART NUMBER 5910158-25.
- [SDR 9507639989](https://openairdocs.org/sdr/9507639989.md): Bulkhead · corroded · May 2, 1995 · N8944E · Doug DC931 · Fuselage Main, Bulkhead
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION BETWEEN THE APB T-FITTING AND BULKHEAD SKIN FS 996, LBL 38 TO BL 0 AND RBL 18. REPAIRED PER EA 99-094812. MFG PART NUMBER 5910130-65.
- [SDR 9507299989](https://openairdocs.org/sdr/9507299989.md): Trapezoid · corroded · May 2, 1995 · N8944E · Doug DC931 · Wing Miscellaneous Structure
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LEFT TRAPEZOIDAL PANEL AT THE FIXED STRUT ATTACH POINT. REPLACED PANEL.
- [SDR 9506899988](https://openairdocs.org/sdr/9506899988.md): Rib · cracked · Apr 22, 1995 · N8944E · Doug DC931 · Wing, Rib/Bulkhead
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN THE RIGHT WING LEADING EDGE NOSE RIBS LOWER ENDS, 3RD, 4TH, AND 6TH RIBS OUTBOARD OF THE NR 10 SLAT TRACK. REPAIRED RIBS PER XEA X9-57-19.
- [SDR 9506109988](https://openairdocs.org/sdr/9506109988.md): Longeron · corroded · Apr 12, 1995 · N8944E · Doug DC931 · Wing, Longeron/Stringer
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FORWARD SIDE OF THE LEFT WING STRINGER 17 AT THE ROOT. REPAIRED STRINGER PER XEA X9-57-14.
- [SDR 9506059988](https://openairdocs.org/sdr/9506059988.md): Frame · cracked · Apr 11, 1995 · N8944E · Doug DC931 · Fuselage Main, Bulkhead
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK AND CORROSION ON THE FS 69 FRAME, LOWER END FLANGE. REPAIRED PER XEA X9-53-87.
- [SDR 9505519989](https://openairdocs.org/sdr/9505519989.md): Fitting · corroded · Apr 5, 1995 · N8944E · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 29R TIE FITTING AT FS 996. REPLACED FITTING PER SRM 51 TO 42.
- [SDR 9505279988](https://openairdocs.org/sdr/9505279988.md): Frame · cracked · Mar 30, 1995 · N8944E · Doug DC931 · Fuselage Main, Frame
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN MAIN FRAME FS 658 ABOVE LONGERON 19L. REPAIRED PER EA X9-53-75.
- [SDR 9502559988](https://openairdocs.org/sdr/9502559988.md): Hinge · corroded · Feb 12, 1995 · N8944E · Doug DC931 · Trailing Edge Flaps
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORRROSION IN RIGHT WING NR 2 FLAP HINGE FASTENER BORES. REPAIRED PER XEA X9-27-17.
- [SDR 9502549988](https://openairdocs.org/sdr/9502549988.md): Hinge · corroded · Feb 12, 1995 · N8944E · Doug DC931 · Trailing Edge Flaps
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LEFT WING NR 2 FLAP HINGE FASTENER BORES. REPAIRED PER XEA X9-27-14.
- [SDR 9502539988](https://openairdocs.org/sdr/9502539988.md): Stringer · corroded · Feb 12, 1995 · N8944E · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, CORROSION ON LONGERON 30 SPLICE FITTING AT FS 925. REPLACED FITTING PER SRM 53-02.
- [SDR 9502179988](https://openairdocs.org/sdr/9502179988.md): Longeron · corroded · Feb 6, 1995 · N8944E · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 18L LOWER SPLICE FITTING AT FS 229. REPLACED FITTING PER SRM 51-30-5.
- [SDR 9502169988](https://openairdocs.org/sdr/9502169988.md): Skin · corroded · Feb 5, 1995 · N8944E · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON INNER FUSELAGE SKIN FS 897 - 917 BETWEEN LONGERONS 22L - 23L. REPAIRED PER XEA X9-53-57.
- [SDR 9505259988](https://openairdocs.org/sdr/9505259988.md): Fitting · corroded · Feb 1, 1995 · N8944E · Doug DC931 · Wing, Control Surface Attach Fittings
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON RIGHT WING NR 3 FLAP HINGE FASTENER BORES. REPLACED HINGE FITTING PER MM 57-40-1.
- [SDR 9501599988](https://openairdocs.org/sdr/9501599988.md): Fitting · cracked · Jan 29, 1995 · N8944E · Doug DC931 · Cargo/Baggage Doors
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND ONE INCH CRACK IN THE FORWARD CARGO DOOR NR 4 BEAM AFT END FITTING. REPLACED FITTING PER SRM 51-30-5.
- [SDR 9501489988](https://openairdocs.org/sdr/9501489988.md): Longeron · corroded · Jan 22, 1995 · N8944E · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LONGERON 27R END FITTING FS 996. REPLACED PER SRM 51-30-5.
- [SDR 9501479988](https://openairdocs.org/sdr/9501479988.md): Longeron · corroded · Jan 22, 1995 · N8944E · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LONGERON 23R END FITTING AT FS 950. REPLACED PER SRM 51-30-2.

## 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 = 'N8944E' AND deregistration_id = 'N8944E-2013-08-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8944E-2013-08-27/reports

---
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