# Service difficulty reports: N804ME, cancelled May 7, 2013

A list on [N804ME, cancelled May 7, 2013](https://openairdocs.org/deregistered/N804ME-2013-05-07.md).

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

Page 1 of 3 · 119 reports

- [SDR MWEA080132](https://openairdocs.org/sdr/MWEA080132.md): Inverter · faulty · Nov 16, 2008 · N804ME · Doug DC981 · AC Inverter
  > BAS A/C EMERGENCY BUS COMES ON WHEN EMERGENCY POWER IS SELECTED ON. REPLACED EMERGENCY INVERTER. (K)
- [SDR MEW2008F00000](https://openairdocs.org/sdr/MEW2008F00000.md): Battery Pack · inoperative · Aug 6, 2008 · N804ME · Doug DC981 · Emergency Lighting
  > EMERGENCY LIGHTS ABOVE, ON COCKPIT CEILING ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. (K)
- [SDR MWE2008F00007](https://openairdocs.org/sdr/MWE2008F00007.md): Slide · unwanted deploy · Jul 7, 2008 · N804ME · Doug DC981 · Escape Slide
  > DURING CLIMB, THE PITCH AUTHORITY (ELEVATOR) FELT STIFF ALTHOUGH CONTROLLABLE, PRIMARY PITCH TRIM WORK OK, ALT LONG TRIM AND AUTO PILOT WORKED NORMAL INSP OF AFT ACCESSORY COMPARTMENT FOR ELEVATOR AUTHORITY ISSUE FOUND THE TAIL CONE SLIDE HAD DEPLOYED IN THE
- [SDR MWEA080044](https://openairdocs.org/sdr/MWEA080044.md): Pan · cracked · Mar 22, 2008 · N804ME · Doug DC981 · Cargo/Baggage Doors
  > CENTER CARGO DOOR OUTER PAN HAS A.75 INCH CRACK IN PAN RADIUS AT THE FORWARD END OF DOOR, INLINE WITH BEAM NR 1. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWE2008F00008](https://openairdocs.org/sdr/MWE2008F00008.md): Slide · inoperative · Dec 10, 2007 · N804ME · Doug DC981 · Escape Slide
  > TAILCONE SLIDE PRESSURE AT (0). REMOVED AND REPLACED TAILCONE SLIDE. (K)
- [SDR MWEA070116](https://openairdocs.org/sdr/MWEA070116.md): Bottle · low pressure · May 11, 2007 · N804ME · Doug DC981 · Escape Slide
  > TAIL CONE EVACUATION SLIDE BOTTLE PRESSURE GAUGE NOT IN THE GREEN BAND. REMOVED AND REPLACED TAIL CONE SLIDE ASSEMBLY.
- [SDR MWEA060285](https://openairdocs.org/sdr/MWEA060285.md): Battery · inoperative · Sep 15, 2006 · N804ME · Doug DC981 · Emergency Lighting
  > CEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY
- [SDR MWEA060217](https://openairdocs.org/sdr/MWEA060217.md): Wire · broken · Aug 22, 2006 · N804ME · Doug DC981 · Light System Wiring
  > EXIT ROW WON'T EXTINGUISH WHEN POWER IS REMOVED FROM AIRCRAFT. REPLACED BROKEN WIRE.
- [SDR MWEA060178](https://openairdocs.org/sdr/MWEA060178.md): Seat Track · corroded · Aug 22, 2006 · N804ME · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON INBOARD FLANGE OF SEAT TRACK AT FRAME STATION 1136 TO 1146, X +44. Z 0, AROUND BOARD FASTENER HOLES. FABRICATED AND INSTALLED SEAT TRACK.
- [SDR MWEA060177](https://openairdocs.org/sdr/MWEA060177.md): Floorbeam · corroded · Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Main, Floor Beam
  > SUPPORT ON FLOORBEAM UPPER FLANGE AT FRAME STATION 1169, X-29, Z 0. FABRICATED AND INSTALLED FLOORBEAM.
- [SDR MWEA060176](https://openairdocs.org/sdr/MWEA060176.md): Web · cracked · Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Miscellaneous Structure
  > FOUND WEB CRACKED AT FRAME STATION Y 1300 X+48. FABRICATED AND INSTALLED WEB.
- [SDR MWEA060174](https://openairdocs.org/sdr/MWEA060174.md): Fitting · corroded · Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Main, Attach Fittings
  > GALLEY 1 INBOARD FUSE MOUNTED FOOT, FRAME STATION 152 X-45 Z 0. FABRICATED AND INSTALLED FITTINGS.
- [SDR MWEA060173](https://openairdocs.org/sdr/MWEA060173.md): Fitting · corroded · Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Miscellaneous Structure
  > GALLEY 1 OUTBOARD FUSE MOUNTED FOOT FRAME STATION 152 X-51 Z0 IS CORRODED. FABRICATED AND INSTALLED FITTINGS.
- [SDR MWEA060172](https://openairdocs.org/sdr/MWEA060172.md): Strap · corroded · Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Miscellaneous Structure
  > FOUND SURFACE CORROSION ON THRESHOLD STRAP Z-46, X-18 AND FRAME STATION Y 636-693. FABRICATED AND INSTALLED STRAP.
- [SDR MWEA060171](https://openairdocs.org/sdr/MWEA060171.md): Strap · corroded · Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Miscellaneous Structure
  > FOUND SURFACE CORROSION ON THRESHOLD STRAP Z-46, X-18 AND FRAME STATION Y 1155 TO 1219. FABRICATED AND INSTALLED NEW STRAP.
- [SDR MWEA060170](https://openairdocs.org/sdr/MWEA060170.md): Seat Track · corroded · Aug 22, 2006 · N804ME · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND SEAT TRACK IS CORRODED AT NUTPLATE AS VIEWED FROM AFT CARGO BAY Y 1267 AND X +24, Z 0. FABRICATED AND INSTALLED SEAT TRACK.
- [SDR MWEA060175](https://openairdocs.org/sdr/MWEA060175.md): Panel · corroded · Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Miscellaneous Structure
  > FOUND FORWARD GALLEY SERVICE DOOR THRESHOLD FLOOR PANEL CORRODED. FABRICATED AND INSTALLED PANEL.
- [SDR MWEA060145](https://openairdocs.org/sdr/MWEA060145.md): Controller · inoperative · Jul 13, 2006 · N804ME · Doug DC981 · Cabin Pressure Controller
  > MASTER WARNING (CABIN ALERT) ILLUMINATED. REMOVED AND REPLACED CABIN PRESSURE CONTROL.
- [SDR MWEA060012](https://openairdocs.org/sdr/MWEA060012.md): Blades · bent · Feb 7, 2006 · N804ME · Doug DC981 · Turbine Engine Compressor Section
  > LEFT ENGINE COMPRESSOR STALL/SURGE. REMOVED BENT TIPS AS NECESSARY ON VARIOUS ENGINE BLADES AND BLENDED AS REQUIRED PER IAW BOEING MM 72-33-22.
- [SDR MWEA060011](https://openairdocs.org/sdr/MWEA060011.md): Tab · obstructed · Feb 3, 2006 · N804ME · Doug DC981 · Elevator Control System
  > NO CONTROL INPUT EVEN WHEN CONTROL COLUMN WAS MOVED AFT. REMOVED SCREW THAT WAS WEDGED BETWEEN ELEVATOR CONTROL TAB STOP AND INBOARD ATTACHED FITTING.
- [SDR MWEA060009](https://openairdocs.org/sdr/MWEA060009.md): Indicator · inoperative · Feb 1, 2006 · N804ME · Doug DC981 · Engine Oil Temperature
  > RIGHT ENGINE OIL TEMERATURE PEGGED OVER 165, ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED RIGHT ENGINE OIL TEMERATURE INDICATOR.
- [SDR MWEA050104](https://openairdocs.org/sdr/MWEA050104.md): Skin · corroded · Sep 7, 2005 · N804ME · Doug DC981 · Leading Edge Devices
  > LEADING EDGE AT STATION 375 HAS CORROSION. FABRICATED AND INSTALLED DOUBLER AND FILLER.
- [SDR MWEA050060](https://openairdocs.org/sdr/MWEA050060.md): Structure · vibration · Jun 27, 2005 · N804ME · Doug DC981 · Fuselage Main, Structure
  > DURING CRUISE PILOT REPORTED A LOUD HUMMING SOUND AND VIBRATION. VISUALLY INSPECTED ALL LANDING GEARS AND WHEEL WELLS, INSPECTED AIRCRAFT FUSELAGE, DOORS,WINGS AND PANELS. PERFORMED ENGINE VIBRATION TEST. NO DEFECTS FOUND.
- [SDR MWEA040194](https://openairdocs.org/sdr/MWEA040194.md): Slide · discharged · Oct 22, 2004 · N804ME · Doug DC981 · Escape Slide
  > AFT GALLEY SLIDE PRESSURE INDICATOR IS INDICATING IN THE RED (READS 2000 PSI). REMOVED AND REPLACED AFT GALLEY DOOR SLIDE.
- [SDR MWEA040154](https://openairdocs.org/sdr/MWEA040154.md): Seat Track · worn · Aug 25, 2004 · N804ME · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > CAPTAIN'S AFT INBOARD SEAT TRACK IS WORN. FABRICATED AND INSTALLED CHANNEL.
- [SDR MWEA040151](https://openairdocs.org/sdr/MWEA040151.md): Seat Track · worn · Aug 24, 2004 · N804ME · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > FIRST OFFICER'S AFT INBOARD SEAT TRACK IS WORN. FABRICATED AND INSTALLED SEAT TRACK TEE.
- [SDR MWEA040150](https://openairdocs.org/sdr/MWEA040150.md): Intercostal · corroded · Aug 24, 2004 · N804ME · Doug DC981 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT FRAME STATION 775 BETWEEN LONGERON 27 AND 28 LEFT. FABRICATED AND INSTALLED INTERCOSTAL.
- [SDR MWEA040149](https://openairdocs.org/sdr/MWEA040149.md): Seat Track · corroded · Aug 23, 2004 · N804ME · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > AFT BAGGAGE PIT, RIGHT SEAT TRACK BETWEEN STATION 1212 AND 1325 HAS SEVERAL AREAS OF CORROSION. FABRICATED AND INSTALLED TRACK.
- [SDR MWEA040148](https://openairdocs.org/sdr/MWEA040148.md): Fitting · corroded · Aug 23, 2004 · N804ME · Doug DC981 · Fuselage Main, Attach Fittings
  > FLOOR SUPPORT FITTINGS AT FRAME STATION 430 BETWEEN NUMBER 30 AND 29 RIGHT LONGERON HAS MODERATE CORROSION ON THE UPPER SURFACE, ALSO NUT PLATES ARE CORRODED. FABRICATED AND INSTALLED FITTING AND INSTALLED TWO EACH NUT PLATES.
- [SDR MWEA040110](https://openairdocs.org/sdr/MWEA040110.md): Generator · inoperative · Jun 24, 2004 · N804ME · Doug DC981 · AC Generation System
  > LEFT GENERATOR FAILED. REMOVED AND REPLACED LEFT GENERATOR.
- [SDR MWEA040097](https://openairdocs.org/sdr/MWEA040097.md): Generator · inoperative · Jun 13, 2004 · N804ME · Doug DC981 · AC Generation System
  > AIRCRAFT CROSSTIE LOCKOUT ILLUMINATED WITH LEFT GENERATOR OFF LIGHT. REMOVED AND REPLACED LEFT ENGINE GENERATOR.
- [SDR MWEA040086](https://openairdocs.org/sdr/MWEA040086.md): Window Frame · lightning strike · Jun 7, 2004 · N804ME · Doug DC981 · Fuselage Main, Structure
  > LIGHTNING STRIKE ON LEFT SIDE CABIN WINDOW FRAME NR 34 ON AFT UPPER SIDE. BLENDED OUT DAMAGE, ACCEPTABLE FOR STRENGTH AS IS.
- [SDR MWEA040085](https://openairdocs.org/sdr/MWEA040085.md): Window Frame · lightning strike · Jun 7, 2004 · N804ME · Doug DC981 · Fuselage Main, Structure
  > LIGHTNING STRIKE ON CABIN WINDOW FRAME 29 AFT LOWER SIDE. BLENDED OUT DAMAGE, ACCEPTABLE AS TEMPORARY REPAIR TO BE PERMANENTLY REPAIRED ON OR BEFORE 7,000 CYCLES.
- [SDR MWEA040084](https://openairdocs.org/sdr/MWEA040084.md): Window Frame · lightning strike · Jun 7, 2004 · N804ME · Doug DC981 · Fuselage Main, Structure
  > LIGHTNING STRIKE ON LEFT SIDE CABIN WINDOW NR 29 FRAME ON LOWER FORWARD CORNER. BLENDED OUT DAMAGE, ACCEPTABLE AS TEMPORARY REPAIR TO BE PERMANENTLY REPAIRED ON OR BEFORE 7,000 CYCLES.
- [SDR MWEA040075](https://openairdocs.org/sdr/MWEA040075.md): Separator · inoperative · May 12, 2004 · N804ME · Doug DC981 · Humidity Control System
  > STRONG FUMES IN CABIN. REMOVED AND REPLACED WATER SEPARATOR.
- [SDR MWEA040069](https://openairdocs.org/sdr/MWEA040069.md): Generator · inoperative · May 9, 2004 · N804ME · Doug DC981 · AC Generation System
  > LEFT GENERATOR LIGHT CAME ON, WAS ABLE TO RESET LEFT GENERATOR, THEN FOURTY-FIVE MINUTES LATER LEFT GENERATOR LIGHT CAME ON AGAIN, STARTED AUXILIARY POWER UNIT, BUT UNABLE TO POWER LEFT SIDE OF ELECTRICAL POWER SYSTEM. REMOVED AND REPLACED GENERATOR CONTROL
- [SDR MWEA040013](https://openairdocs.org/sdr/MWEA040013.md): Bolt · misinstalled · Jan 28, 2004 · N804ME · Doug DC981 · Fasteners
  > DURING GEAR RETRACTION A LOUD NOISE COMING FROM THE NOSE GEAR AREA. LT FORWARD NOSE GEAR DOOR RETRACT LINK NOT LATCHED COMPLETELY, FOUND RELEASE HANDLE BOLT INSTALLED IMPROPERLY. REPOSITIONED BOLT CLOSED AND LOCKED FORWARD NOSE GEAR DOOR.
- [SDR MWEA030475](https://openairdocs.org/sdr/MWEA030475.md): Pitot Line · leaking · Dec 6, 2003 · N804ME · Doug DC981 · Pitot/Static System
  > CAPTAIN'S MACH INDICATOR HAS.14 MACH SPLIT AND EIGHT KNOTS SPLIT BETWEEN FIRST OFFICER'S AIRSPEED. SELECTING CENTRAL AIR DATA COMPUTER TO BOTH ON ONE AND TWO CORRECTED THE SPLIT. FOUND MASSIVE LEAK IN PITOT ON NUMBER ONE PITOT SYSTEM, TIGHTENED FITTINGS, LE
- [SDR MWEA030394](https://openairdocs.org/sdr/MWEA030394.md): Skin · cracked · Sep 25, 2003 · N804ME · Doug DC981 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN IS CRACKED APPROXIMATELY 1.25 INCH AT STATION 1437 BETWEEN LONGERON 3 AND 4 RT. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA030389](https://openairdocs.org/sdr/MWEA030389.md): Seat Track · worn · Sep 22, 2003 · N804ME · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > FIRST OFFICERS SEAT TRACK (FORWARD INBOARD) HAS WORN AREAS. FABRICATED AND INSTALLED NEW SEAT TRACK.
- [SDR MWEA030376](https://openairdocs.org/sdr/MWEA030376.md): Spacer · corroded · Sep 16, 2003 · N804ME · Doug DC981 · Fuselage Main, Structure
  > AFT CARGO DOOR LOWER JAMB HAS LIGHT CORROSION ALONG THE ENTIRE LENGTH AROUND AND INSIDE SCREW HOLES. FABRICATED AND INSTALLED JAMB SPACER.
- [SDR MWEA030375](https://openairdocs.org/sdr/MWEA030375.md): Skin · cracked · Sep 16, 2003 · N804ME · Doug DC981 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN IS CRACKED APPROXIMATELY.25 INCH OUT OF RIVER HOLE AT STATION 1437 BETWEEN LONGERON 2 AND 3 LEFT. REMOVED CRACK IN SKIN, FABRICATED AND INSTALLED DOUBLER AND FILLER.
- [SDR MWEA030374](https://openairdocs.org/sdr/MWEA030374.md): Doubler · cracked · Sep 16, 2003 · N804ME · Doug DC981 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN IS CRACKED APPROXIMATELY 1 INCH AT STATION 1437 BETWEEN LONGERON 3 AND 4 LEFT. FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FILLER.
- [SDR MWEA030373](https://openairdocs.org/sdr/MWEA030373.md): Doubler · dented · Sep 16, 2003 · N804ME · Doug DC981 · Fuselage Main, Plate/Skin
  > DENT LOCATED BETWEEN LONGERON 26 LEFT AND 25 LEFT AT STATION 694. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA030372](https://openairdocs.org/sdr/MWEA030372.md): Doubler · dented · Sep 16, 2003 · N804ME · Doug DC981 · Fuselage Main, Plate/Skin
  > DENT LOCATED AT 1 INCH BELOW LONGERON 4 LEFT AND SEVERAL VERY SMALL DENTS LOCATED AROUND THIS DENT AT STATION 219. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA030243](https://openairdocs.org/sdr/MWEA030243.md): Contactor · inoperative · Jun 9, 2003 · N804ME · Doug DC981 · Stabilizer Control System
  > PRIMARY TRIM INOPERATIVE. REMOVED AND REPLACED NOSE DOWN PRIMARY LONGITUDINAL TRIM CONTACTOR.
- [SDR MWEA030241](https://openairdocs.org/sdr/MWEA030241.md): Retainer · corroded · Jun 3, 2003 · N804ME · Doug DC981 · Flight Compartment Windows
  > RIGHT UPPER COCKPIT WINDOW RETAINER IS CORRODED IN LOWER FORWARD CORNER. REMOVED DAMAGE AND INSTALLED FILLER AND EXTERNAL DOUBLER.
- [SDR MWEA030228](https://openairdocs.org/sdr/MWEA030228.md): Motor · defective · May 21, 2003 · N804ME · Doug DC981 · Stabilizer Control System
  > PRIMARY TRIM PROBLEM. REMOVED AND REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR AND FIRST OFFICERS YOKE TRIM SWITCH AND REPLACED CONNECTORS.
- [SDR MWEA030128](https://openairdocs.org/sdr/MWEA030128.md): Bolt · sheared · Feb 23, 2003 · N804ME · Doug DC981 · Tire
  > NR 1 MAIN WHEEL ASSY THROUGH BOLT SHEARED OFF. REPLACED NR 1 WHEEL AND TIRE ASSEMBLY.
- [SDR MWEA030036](https://openairdocs.org/sdr/MWEA030036.md): Line · disconnected · Jan 18, 2003 · N804ME · Doug DC981 · Engine Controls
  > ON LEFT THROTTLE, SPLIT INCREASED WITH ALTITUDE TO ABOUT 1 1/2 KNOBS. -- RECONNECTED PRESSURE TOTAL 2 LINE.

Next page: https://openairdocs.org/deregistered/N804ME-2013-05-07/reports.md?page=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 = 'N804ME' AND deregistration_id = 'N804ME-2013-05-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N804ME-2013-05-07/reports

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