# Service difficulty reports: N808ME, cancelled Jan 28, 2011

A list on [N808ME, cancelled Jan 28, 2011](https://openairdocs.org/deregistered/N808ME-2011-01-28.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 · 140 reports

- [SDR MWEA080028](https://openairdocs.org/sdr/MWEA080028.md): Latch · incorrect · Feb 13, 2008 · N808ME · Doug DC982 · Emergency Equipment
  > FLIGHT ATTENDANT ADVISED THAT THE GIRT BAR WAS THE INCORRECT SIZE & WOULD NOT FIT INTO FLOOR FITTINGS. REMOVED SEALANT FROM AFT GIRT BAR LATCH. REMOVED AND REPLACED FORWARD GALLEY GIRT BAR LATCH.
- [SDR MWEA070099](https://openairdocs.org/sdr/MWEA070099.md): B-Nut · loose · May 2, 2007 · N808ME · Doug DC982 · APU Bleed Air System
  > WITH BOTH ENGINES OFF APU ON, WITH AIR SELECTED ON WITH RIGHT PACK, CABIN GOT A OIL SMELL & HAZE. TIGHTENED B-NUT ON PRESSURE LINE, LEAK CHECKED GOOD.
- [SDR MWEA070096](https://openairdocs.org/sdr/MWEA070096.md): B-Nut · leaking · Apr 22, 2007 · N808ME · Doug DC982 · Hydraulic System, Main
  > ONE OR BOTH AIR CONDITIONING PACKS PUT OUT A FAINT HOT OIL SMELL, WHEN OPERATED BY THE APU. FOUND HYDRAULIC LEAK IN FRONT OF APU AIR INLET, TIGHTENED B NUT.
- [SDR MWEA070075](https://openairdocs.org/sdr/MWEA070075.md): Skin · dented · Apr 4, 2007 · N808ME · Doug DC982 · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE SKIN AT FRAME STATION 214 JUST ABOVE LONGERON 15 RIGHT. [SUP 4/13/07] FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA070039](https://openairdocs.org/sdr/MWEA070039.md): Skin · gouged · Mar 1, 2007 · N808ME · Doug DC982 · Fuselage Main, Plate/Skin
  > GOUGE/DENT IN FUSELAGE SKIN AT FRAME STATION 237 LEFT BETWEEN LONGERON 18 LEFT & LONGERON 17 LEFT. FABRICATED AND INSTALLED FILLER.
- [SDR MWEA070035](https://openairdocs.org/sdr/MWEA070035.md): Gyro · failed · Feb 16, 2007 · N808ME · Doug DC982 · Attitude Gyro and Indicating System
  > CAPTAIN'S ATTITUDE INDICATOR FAILED. REMOVED AND REPLACED CAPTAINS FOG GYRO.
- [SDR MWEA070002](https://openairdocs.org/sdr/MWEA070002.md): Channel · punctured · Jan 12, 2007 · N808ME · Doug DC982 · Fuselage Main, Bulkhead
  > STATION 218 BULKHEAD WALL ZEE CHANNEL STATION 0.007" ABOVE FLOOR IS PUNCTURED. INSTALLED ZEE CHANNEL.
- [SDR MWEA070001](https://openairdocs.org/sdr/MWEA070001.md): Bulkhead · punctured · Jan 12, 2007 · N808ME · Doug DC982 · Fuselage Main, Bulkhead
  > FOUND STATION 218 BULKHEAD WEB AT STATION 0.007" ABOVE FLOOR HAS PUNCTURE APPROXIMATELY 1/2" DIAGRAM. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA060303](https://openairdocs.org/sdr/MWEA060303.md): Skin · cracked · Dec 15, 2006 · N808ME · Doug DC982 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACK ON RIGHT SIDE OF NOSE, APPROXIMATELY STATION 58 AND 6 INCHES DOWN FROM CUSP LINE. ABOUT 18 INCHES FORWARD AND 4 INCHES DOWN ANGLE OF ATTACK, APPROXIMATELY 1.5 INCH LONG. CUT OUT DAMAGE, FLUSH REPAIR.
- [SDR MWEA060290](https://openairdocs.org/sdr/MWEA060290.md): Warning Message · illuminated · Nov 7, 2006 · N808ME · Doug DC982 · Cabin Pressure Control System
  > THE CABIN FLOW ANNUNCIATOR ILLUMINATED & REMAINED ON UNTIL A DESCENT TO 11,000. REMOVED AND REPLACED LEFT AND RIGHT WATER SEPARATOR SOCKS.
- [SDR MWEA060224](https://openairdocs.org/sdr/MWEA060224.md): Skin · lightning strike · Oct 6, 2006 · N808ME · Doug DC982 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE FROM FRAME STATION 337-356 LONGERON 28 TO 19 RIGHT. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA070023](https://openairdocs.org/sdr/MWEA070023.md): Screw · missing · Aug 3, 2006 · N808ME · Doug DC982 · Fuselage Main, Bulkhead
  > THE PIN FROM TOP OF AFT PRESSURE BULKHEAD FAILED TO ENGAGE THE ARM. INSTALLED MISSING SCREW.
- [SDR MWEA060135](https://openairdocs.org/sdr/MWEA060135.md): Bulb · inoperative · Jun 24, 2006 · N808ME · Doug DC982 · Landing Gear Position and Warning
  > RIGHT LANDING GEAR LIGHT DID NOT ILLUMINATE -RED AND GREEN-. INSPECTED SENSORS & WIRING AT RIGHT MAIN LANDING GEAR, NO PROBLEMS. REMOVED MAIN LANDING GEAR INDICATOR LIGHT, CLEANED SOCKET & REPLACED BULBS, OPERATION CHECKED GOOD.
- [SDR MWEA060046](https://openairdocs.org/sdr/MWEA060046.md): Hydraulic Line · broken · May 1, 2006 · N808ME · Doug DC982 · Hydraulic System, Main
  > RIGHT HYDRAULIC PRESSURE LOW ANNUCIATOR ILLUMINATED AND RIGHT HYDRAULIC QUANTITY STARTED DROPPING DOWN TO ONE QUART. REMOVED AND REPLACED HYDRAULIC LINE.
- [SDR MWEA060037](https://openairdocs.org/sdr/MWEA060037.md): Skin · damaged · Mar 24, 2006 · N808ME · Doug DC982 · Elevator, Plate/Skin
  > FOUND RIGHT ELEVATOR TOP, OUTBOARD, TRAILING EDGE SKIN HAS DAMAGE APPROXIMATELY AT STATION XHR 210, APPROXIMATELY 1.125" BY.25". FABRICATED AND INSTALLED DOUBLERS AND FILLER.
- [SDR MWEA070014](https://openairdocs.org/sdr/MWEA070014.md): Battery Pack · discharged · Mar 3, 2006 · N808ME · Doug DC982 · Emergency Lighting
  > BOTH LEFT & RIGHT EMERGENCY LIGHTS INOPERATIVE ON OVERWING OUTSIDE. REMOVED AND REPLACED OVERWING BATTERY PACK.
- [SDR MWEA060016](https://openairdocs.org/sdr/MWEA060016.md): Engine · frozen · Feb 18, 2006 · N808ME · Doug DC982 · Engine (Turbine/Turboprop)
  > CREW NOTICED NO ENGINE PRESSURE RATIO INDICATION ON RIGHT ENGINE. THAWED OUT RIGHT ENGINE PT7 SYSTEM, REMOVED AND REPLACED PT7 MOISTURE TRAP.
- [SDR MWEA060010](https://openairdocs.org/sdr/MWEA060010.md): Vane · gouged · Jan 30, 2006 · N808ME · Doug DC982 · Wing Main, Frame Structure
  > LEFT WING INBOARD FIXED VANE HAS GOUGE ON LOWER SIDE, OUTBOARD EDGE. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA060005](https://openairdocs.org/sdr/MWEA060005.md): Frame · cracked · Jan 10, 2006 · N808ME · Doug DC982 · Fuselage Main, Frame
  > CRACK FOUND ON FRAME AT STATION 389 WHERE IT ATTACHES TO LONGERON 17 RIGHT. FABRICATED AND INSTALLED DOUBLER AND FILLER.
- [SDR MWEA060003](https://openairdocs.org/sdr/MWEA060003.md): Longeron · cracked · Jan 9, 2006 · N808ME · Doug DC982 · Fuselage Main, Longeron/Stringer
  > LONGERON 17 RIGHT IS CRACKED AT STATION 408 WHERE IT ATTACHES TO THE FRAME AT THE LOWER POSITION. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA050099](https://openairdocs.org/sdr/MWEA050099.md): Battery Pack · inoperative · Sep 1, 2005 · N808ME · Doug DC982 · Emergency Lighting
  > FOUR CEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES IN BATTERY PACK.
- [SDR MWEA050098](https://openairdocs.org/sdr/MWEA050098.md): Floorboard · corroded · Sep 1, 2005 · N808ME · Doug DC982 · Fuselage Floor Panel
  > 8 FLOORBOARD ATTACH STRIP FIRST INBOARD OF PASSENGER DOOR HAS CORROSION. FABRICATED AND INSTALLED FLOORBOARD SUPPORT ANGLE.
- [SDR MWEA050097](https://openairdocs.org/sdr/MWEA050097.md): Floorboard · corroded · Sep 1, 2005 · N808ME · Doug DC982 · Fuselage Floor Panel
  > RIGHT SIDE OF STATION 160-200 FORWARD CABIN FLOORBOARD ATTACH ANGLE GOING FORWARD AND AFT FIRST INBOARD FROM SERVICE DOOR MANY AREAS OF CORROSION. FABRICATED AND INSTALLED FLOORBOARD SUPPORT ANGLE.
- [SDR MWEA050096](https://openairdocs.org/sdr/MWEA050096.md): Doubler · corroded · Sep 1, 2005 · N808ME · Doug DC982 · Landing Gear Doors
  > RIGHT GEAR DOOR EDGES AND AROUND 3 RIVETS HAVE SURFACE CORROSION AND A LARGE AMOUNT OF BARE METAL IS SHOWING. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA050095](https://openairdocs.org/sdr/MWEA050095.md): Seat Track · damaged · Sep 1, 2005 · N808ME · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > PIOLT SEAT INBOARD SEAT TRACK HOLES ARE ENLONGATED. FABRICATED AND INSTALLED SEAT TRACK.
- [SDR MWEA050094](https://openairdocs.org/sdr/MWEA050094.md): Seat Track · damaged · Sep 1, 2005 · N808ME · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > CO-PILOT'S CREW SEAT INBOARD SEAT TRACK HOLES ARE ENLONGATED. FABRICATED AND INSTALLED NEW SEAT TRACK.
- [SDR MWEA050089](https://openairdocs.org/sdr/MWEA050089.md): Floor Support · corroded · Aug 23, 2005 · N808ME · Doug DC982 · Fuselage Miscellaneous Structure
  > RT SIDE, MOST OB FLOORBOARD ATTACH STRIP HAS HOLE CORRODED, STATION 218. FABRICATED AND INSTALLED FLOOR SUPPORT.
- [SDR MWEA050087](https://openairdocs.org/sdr/MWEA050087.md): Doubler · dented · Aug 23, 2005 · N808ME · Doug DC982 · Electrical/Electronic Compartment Doors
  > DENT ON EMERGENCY EXIT DOOR. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA050093](https://openairdocs.org/sdr/MWEA050093.md): Skin · dented · Aug 23, 2005 · N808ME · Doug DC982 · Fuselage Main, Plate/Skin
  > DENT IN LEFT SIDE OF FUSELAGE 16 INCHES FROM THE LOWER FORWARD CORNER OF THE POTABLE WATER SERVICE PANEL, STATION 484 BETWEEN LONGERON 22 AND 23. FABRCATED AND INSTALLED DOUBLER.
- [SDR MWEA050092](https://openairdocs.org/sdr/MWEA050092.md): Panel · corroded · Aug 23, 2005 · N808ME · Doug DC982 · Fuselage Miscellaneous Structure
  > VENTRAL STAIR LEFT SIDE JUST FORWARD OF NR 3 ALIGNMENT PIN HAS CORROSION. FABRICATED AND INSTALLED NEW PANEL.
- [SDR MWEA050091](https://openairdocs.org/sdr/MWEA050091.md): Panel · corroded · Aug 23, 2005 · N808ME · Doug DC982 · Fuselage Miscellaneous Structure
  > VENTRAL STAIRWAY LEFT SIDE JUST FORWARD OF NR 1 ALIGNMENT PIN HAS CORROSION. FABRICATED AND INSTALLED NEW PANEL.
- [SDR MWEA050090](https://openairdocs.org/sdr/MWEA050090.md): Support Angle · damaged · Aug 23, 2005 · N808ME · Doug DC982 · Fuselage, Door Hinge
  > NOSE LANDING GEAR AFT LEFT DOOR HINGE POINT SUPPORT BOLT HOLES ENLONGATED. FABRICATED AND INSTALLED FRONT SUPPORT ANGLE.
- [SDR MWEA050088](https://openairdocs.org/sdr/MWEA050088.md): Floor Support · corroded · Aug 23, 2005 · N808ME · Doug DC982 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF FLOOR SUPPORT FOUND CORROSION ON WEB BELOW THE SUPPORT, STATION 218 RT SIDE. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA050085](https://openairdocs.org/sdr/MWEA050085.md): Seat Track · corroded · Aug 18, 2005 · N808ME · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT STATION 207. FABRICATED AND INSTALLED SEAT TRACK.
- [SDR MWEA050084](https://openairdocs.org/sdr/MWEA050084.md): Seat Track · corroded · Aug 18, 2005 · N808ME · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, TWO SCREWS MISSING AT STATION 1270 AND CORROSION AROUND THE HOLE. FABRICATED AND INSTALLED SEAT TRACK.
- [SDR MWEA050086](https://openairdocs.org/sdr/MWEA050086.md): Seat Track · corroded · Aug 18, 2005 · N808ME · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > NR 2 SEAT TRACK CORRODED, FORWARD END. FABRICATED AND INSTALLED SEAT TRACK.
- [SDR MWEA050083](https://openairdocs.org/sdr/MWEA050083.md): Seat Track · damaged · Aug 18, 2005 · N808ME · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > FIRST OFFICER'S, INBOARD SEAT TRACK HOLES ARE ENLONGATED. FABRICATED AND INSTALLED SEAT TRACK.
- [SDR MWEA050056](https://openairdocs.org/sdr/MWEA050056.md): Wire · inoperative · May 14, 2005 · N808ME · Doug DC982 · Light System Wiring
  > SECTION OF EMERGENCY TRACK LIGHTS ARE INOPERATIVE FROM SEAT 9 THROUGH 18. REPAIRED WIRE.
- [SDR MWEA050030](https://openairdocs.org/sdr/MWEA050030.md): Skin · cracked · Apr 7, 2005 · N808ME · Doug DC982 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE SKIN CRACKED AT STATION X15 = 136.421 AT SLAT TRACK. INSTALLED DOUBLER AND TRIPLER.
- [SDR MWEA050025](https://openairdocs.org/sdr/MWEA050025.md): Seal · leaking · Mar 5, 2005 · N808ME · Doug DC982 · Flight Compartment Windows
  > FIRST OFFICER'S WINDOW WAS LEAKING AND WOULD GET LOUDER AS ALTITUDE WAS INCREASED. PRESSURIZED AIRCRAFT AND FOUND FIRST OFFICER'S WINDOW LEAKING, INSPECTED FIRST OFFICER'S CLEARVIEW SEAL AND FOUND VOID IN UPPER FORWARD CORNER. RESEALED VOIDS, PRESSURIZED AIR
- [SDR MWEA040228](https://openairdocs.org/sdr/MWEA040228.md): Regulator · malfunctioned · Dec 27, 2004 · N808ME · Doug DC982 · Cabin Pressure Control System
  > AT LEVEL OF AT FL250, FLOW METER CAME ON. REMOVED AND REPLACED AIR CONDITIONING PRESSURE REGULATOR.
- [SDR MWEA040180](https://openairdocs.org/sdr/MWEA040180.md): Cusp Web · cracked · Oct 1, 2004 · N808ME · Doug DC982 · Fuselage Miscellaneous Structure
  > CUSP MEMBRANE IS CRACKED AT STATION 1245 LT SIDE. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040178](https://openairdocs.org/sdr/MWEA040178.md): Skin · corroded · Sep 28, 2004 · N808ME · Doug DC982 · Rudder, Tab Structure
  > RUDDER TAB HAS A SMALL AREA OF CORROSION/DELAMINATION ON LEFT BOTTOM FORWARD SIDE. CUT OUT DAMAGED AREA AND INSTALLED LEADING EDGE.
- [SDR MWEA040177](https://openairdocs.org/sdr/MWEA040177.md): Skin · dented · Sep 27, 2004 · N808ME · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING EVALUATION OF WATCH ITEM 7130 THE DENT NO LONGER MEETS THE REQUIRMENTS OF CONDITION, DUE TO THE DENT BEING WITHIN 1 INCH OF LONGERON 20 RIGHT. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040191](https://openairdocs.org/sdr/MWEA040191.md): Cusp Web · cracked · Sep 23, 2004 · N808ME · Doug DC982 · Fuselage Miscellaneous Structure
  > LEFT FUSELAGE CUSP MEMBRANE AT FRAME STATION 1305 HAS A CRACK. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040174](https://openairdocs.org/sdr/MWEA040174.md): Skin · dented · Sep 23, 2004 · N808ME · Doug DC982 · Fuselage Main, Plate/Skin
  > A DENT ON FUSELAGE SKIN IS 1.2500 INCH LONG BY 1 INCH WIDE LOCATED 1INCH BELOW 4 LT AND 1.6250 INCH AFT OF FRAME STATION 218 MAXIMUM DEPTH.007. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040173](https://openairdocs.org/sdr/MWEA040173.md): Doubler · dented · Sep 23, 2004 · N808ME · Doug DC982 · Fuselage Main, Plate/Skin
  > A DENT ON FUSELAGE SKIN IS 1.7500 INCH LONG BY 1.3750 INCH WIDE LOCATED.3750 INCH BELOW LONGERON 4 LT AND AT FRAME STA 218, MAXIMUM DEPTH.021. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040172](https://openairdocs.org/sdr/MWEA040172.md): Doubler · dented · Sep 23, 2004 · N808ME · Doug DC982 · Wing, Plate/Skin
  > LT WING FIXED VANE HAS MANY SMALL DENTS ON LOWER SURFACE IN A 6 IN X 6 IN AREA. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040169](https://openairdocs.org/sdr/MWEA040169.md): Pan · cracked · Sep 21, 2004 · N808ME · Doug DC982 · Cargo/Baggage Doors
  > FORWARD BAGGAGE PIT DOOR, FORWARD PAN FLANGE CRACKED. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040170](https://openairdocs.org/sdr/MWEA040170.md): Shear Tie · cracked · Sep 21, 2004 · N808ME · Doug DC982 · Fuselage Main, Structure
  > SHEAR TIE AT STATION 294 ABOVE LONGERON 17 LEFT IS CRACKED AND DENTED. FABRICATED AND INSTALLED NEW FORMER.

Next page: https://openairdocs.org/deregistered/N808ME-2011-01-28/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 = 'N808ME' AND deregistration_id = 'N808ME-2011-01-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N808ME-2011-01-28/reports

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