# Service difficulty reports: N810ME, cancelled Mar 31, 2010

A list on [N810ME, cancelled Mar 31, 2010](https://openairdocs.org/deregistered/N810ME-2010-03-31.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 4 · 170 reports

- [SDR MWEA080071](https://openairdocs.org/sdr/MWEA080071.md): Control Valve · faulty · May 17, 2008 · N810ME · Doug DC982 · Cabin Pressure Control System
  > LEFT AIRCRAFT SYSTEM UNABLE TO HOLD CABIN PRESSURE AT 24,000 FEET, FLOW LIGHT WAS ON WITH OUTFLOW VALVE CLOSED. REMOVED AND REPLACED LEFT PACK FLOW CONTROL VALVE.
- [SDR MWEA080016](https://openairdocs.org/sdr/MWEA080016.md): Support · corroded · Jan 28, 2008 · N810ME · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION AROUND BOLT HOLE ALONG ENTIRE LENGTH OF AFT CARGO DOOR THRESHOLD PLATE SUPPORT STRUCTURE. FABRICATED AND INSTALLED SPACERS.
- [SDR MWEA080014](https://openairdocs.org/sdr/MWEA080014.md): Skin · corroded · Jan 23, 2008 · N810ME · Doug DC982 · Fuselage Main, Plate/Skin
  > AFT LAVATORY SERVICE PANEL, BOX AND FUSELAGE SKIN SEPARATED AND CORROSION LEVEL 1 FOUND IN BETWEEN AT FORWARD LOWER CORNER. CUT OUT DAMAGE AND FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA080011](https://openairdocs.org/sdr/MWEA080011.md): Cusp Web · corroded · Jan 18, 2008 · N810ME · Doug DC982 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT HAS CORROSION ON BOTTOM OF CUSP MEMBRANE AT DOME NUT JUST AFT OF FRAME STATION 1174L. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA070310](https://openairdocs.org/sdr/MWEA070310.md): Smoke Detector · false indication · Dec 26, 2007 · N810ME · Doug DC982 · Smoke Detection
  > WHILE EN ROUTE, LEFT AFT LAVATORY SMOKE ALARM ACTIVATED. FLIGHT ATTENDANT REPORTED, NO SIGN OF SMOKE, NO SMELL OF SMOKE AND NO SIGNS OF TAMPERING. REMOVED AND REPLACED SMOKE DETECTOR.
- [SDR MWEA070263](https://openairdocs.org/sdr/MWEA070263.md): Wire · broken · Oct 28, 2007 · N810ME · Doug DC982 · Light System Wiring
  > FLOOR TRACK EMERGENCY LIGHT INOPERATIVE FROM ROW 27 AFT. FOUND SPLICE BROKEN REPLACED SPLICE.
- [SDR MWEA070259](https://openairdocs.org/sdr/MWEA070259.md): Smoke Detector · faulty · Oct 17, 2007 · N810ME · Doug DC982 · Smoke Detection
  > LEFT REAR LAV SMOKE ALARM SOUNDED. REMOVED AND REPLACED AFT LEFT LAVATORY SMOKE DETECTOR.
- [SDR MWEA070095](https://openairdocs.org/sdr/MWEA070095.md): Lanyard · broken · Apr 13, 2007 · N810ME · Doug DC982 · Emergency Equipment
  > AFT GALLEY GIRT BAR CABLE BROKEN. REMOVED AND REPLACED AFT GALLEY GIRT LANYARD.
- [SDR MWEA070094](https://openairdocs.org/sdr/MWEA070094.md): Girt Bar · stuck · Apr 13, 2007 · N810ME · Doug DC982 · Emergency Equipment
  > FLIGHT ATTENDANT UNABLE TO DISARM GIRT BAR AT AFT GALLEY DOOR. DISARMED AFT GALLEY SLIDE.
- [SDR MWEA070078](https://openairdocs.org/sdr/MWEA070078.md): Shear Tie · damaged · Apr 5, 2007 · N810ME · Doug DC982 · Fuselage Internal Mounting Structure
  > SHEAR CLIP DAMAGE FROM DRILL MARK. FABRICATED AND INSTALLED SHEAR TIE.
- [SDR MWEA070077](https://openairdocs.org/sdr/MWEA070077.md): Skin · dented · Apr 4, 2007 · N810ME · Doug DC982 · Fuselage Main, Plate/Skin
  > EVIDENCE OF SKIN DENTED AT STATION 541 BETWEEN LONGERERON 26 AND LONGERON 27. FABRICATED AND INSTALLED FILLER.
- [SDR MWEA070076](https://openairdocs.org/sdr/MWEA070076.md): Skin · dented · Apr 4, 2007 · N810ME · Doug DC982 · Fuselage Main, Plate/Skin
  > LONGERON 27 AT STATION 636 EVIDENCE OF SKIN DENTED. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA070041](https://openairdocs.org/sdr/MWEA070041.md): Latch · broken · Mar 5, 2007 · N810ME · Doug DC982 · Aerodynamic Fairings
  > AFT TAIL CONE DOOR ARMING, DISARMING GUARD WILL NOT REMAIN DOWN AND LOCKED ON PLACE. REMOVED AND REPLACED LATCH.
- [SDR MWEA070026](https://openairdocs.org/sdr/MWEA070026.md): Slide · low pressure · Feb 2, 2007 · N810ME · Doug DC982 · Escape Slide
  > AFT EVACUATION SLIDE PRESSURE IS LOW AT 1500 PSI. REMOVED AND REPLACED AFT SLIDE.
- [SDR MWEA060295](https://openairdocs.org/sdr/MWEA060295.md): Skin · damaged · Nov 12, 2006 · N810ME · Doug DC982 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON 2 EACH RIVET HEADS, STATION 484, 3 INCH OB OF LONGERON 3 LT. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA060286](https://openairdocs.org/sdr/MWEA060286.md): Flashlight · inoperative · Sep 2, 2006 · N810ME · Doug DC982 · Emergency Equipment
  > EMERGENCY LIGHT BESIDE ENTRANCE DOOR INOPERATIVE. REMOVED AND REPLACED FLASH LIGHT.
- [SDR MWEA060141](https://openairdocs.org/sdr/MWEA060141.md): Seal · cracked · Jul 5, 2006 · N810ME · Doug DC982 · Cargo/Baggage Doors
  > CARGO DOOR SEAL DRESSER HAS APPROXIMATELY.250 INCH CRACK, LOCATED AT BOTTOM EDGE OF DOOR CUTOUT AT STATION 674. FABRICATED AND INSTALLED SEAL DEPRESSOR.
- [SDR MWEA060140](https://openairdocs.org/sdr/MWEA060140.md): Support · corroded · Jul 5, 2006 · N810ME · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CARGO DOOR THRESHOLD PLATE SUPPORT STRUCTURE, LOCATED AT FORWARD, LOWER CORNER OF DOOR CUTOUT. FABRICATED AND INSTALLED STRAP.
- [SDR MWEA060139](https://openairdocs.org/sdr/MWEA060139.md): Threshold · corroded · Jul 5, 2006 · N810ME · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION ALONG ENTIRE LENGTH OF AFT CARGO DOOR THRESHOLD, PLATE SUPPORT STRUCTURE. FABRICATED AND INSTALLED SHEAR FASTENER.
- [SDR MWEA060138](https://openairdocs.org/sdr/MWEA060138.md): Doubler · delaminated · Jul 5, 2006 · N810ME · Doug DC982 · Rudder, Spar/Rib
  > SIX RUDDER TRIM TAB TRAILING EDGE IS DELAMINATED, NEAR THE CENTER OF THE TAB. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA060052](https://openairdocs.org/sdr/MWEA060052.md): Crank Assy · defective · May 27, 2006 · N810ME · Doug DC982 · Aerodynamic Fairings
  > TAIL CONE FAILED THE PULL TEST AND THE TAIL CONE DID NOT DEPLOY WHEN USING THE VENTRAL STAIR DOOR. REMOVED AND REPLACED CRANK ASSEMBLY.
- [SDR MWEA060041](https://openairdocs.org/sdr/MWEA060041.md): Skin · damaged · Apr 11, 2006 · N810ME · Doug DC982 · Passenger/Crew Doors
  > FOUND FORWARD PASSENGER DOOR DAMAGED. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA060018](https://openairdocs.org/sdr/MWEA060018.md): Engine · frozen · Feb 18, 2006 · N810ME · Doug DC982 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE PRESSURE RATIO DID NOT ADVANCE PAST 1.02, ALL OTHER INDICATIONS NORMAL. DISCONNECTED PT7 LINES AT CROSSBRIDAL AND DETERMINTED THAT THE LINES WERE OBSTRUCTED WITH ICE BETWEEN BRIDAL AND PT7 TRAP, RAN ENGINES, OPERATIONS CHECKED GOOD.
- [SDR MWEA070015](https://openairdocs.org/sdr/MWEA070015.md): Splice · faulty · Feb 14, 2006 · N810ME · Doug DC982 · Light System Wiring
  > FORWARD SECTION CABIN FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. FOUND BAD SPLICE, REPLACED SPLICE.
- [SDR MWEA060007](https://openairdocs.org/sdr/MWEA060007.md): Seat Track · out of alignment · Jan 19, 2006 · N810ME · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > FIRST OFFICERS INBOARD AFT SEAT TRACK NOT IN ALIGNMENT WITH THE OTHER SEAT TRACK. FABRICATED AND INSTALLED TEE FITTING.
- [SDR MWEA060001](https://openairdocs.org/sdr/MWEA060001.md): O-Ring · leaking · Jan 4, 2006 · N810ME · Doug DC982 · Hydraulic System, Main
  > RT HYDRAULIC QUANTITY LOW ONE QUART ON FINAL APPROACH. REMOVED AND REPLACED RT PRESSURE REDUCER O-RING.
- [SDR MWEA050115](https://openairdocs.org/sdr/MWEA050115.md): Engine · malfunctioned · Oct 12, 2005 · N810ME · Doug DC982 · Engine (Turbine/Turboprop)
  > NUMBER TWO ENGINE PRESSURE RATIO DECREASED AT 0.2 AND ENGINE PRESSURE RATIO AND 10 PERCENT N1 BOTH PACKS ALSO SHUTDOWN. SERVICED FUEL CONTROL BELLOWS. INSPECTED PT2 MOISTURE TRAP AND PT7 MOISTURE TRAP, PS4 STRAINER, CHECKED PT2 AND PT7 LINE AND FITTING AND B
- [SDR MWEA050107](https://openairdocs.org/sdr/MWEA050107.md): Pump · inoperative · Sep 28, 2005 · N810ME · Doug DC982 · Hydraulic Pump (Electric/Engine), Main
  > RT ENGINE HYDRAULIC PUMP INOPERATIVE. REMOVED AND REPLACED RT ENGINE HYDRAULIC PUMP.
- [SDR MWEA050106](https://openairdocs.org/sdr/MWEA050106.md): Overheat Sensor · inoperative · Sep 16, 2005 · N810ME · Doug DC982 · Overheat Detection
  > TAIL COMPARTMENT HIGH TEMPERATURE LIGHT CAME ON. REMOVED AND REPLACED OVERHEAT SENSOR AND TIGHTENED RIGHT CLAMP.
- [SDR MWEA050100](https://openairdocs.org/sdr/MWEA050100.md): Apu · overtemp · Sep 2, 2005 · N810ME · Doug DC982 · Airborne Auxiliary Power Unit (APU) System
  > TAIL COMPARTMENT HIGH LIGHT CAME ON. FOUND AUXILIARY POWER UNIT CONTROL VALVE LEAKING AND HOIST ACCESS PANEL OFF AND HOT AIR BLOWING OUT. REINSTALLED HOIST PANEL, VERIFIED LEAK AT V BAND CLAMP ON LOAD CONTROL OUTLET DUCT. REMOVED AND INSPECTED CLAMP, NO DEF
- [SDR MWEA050074](https://openairdocs.org/sdr/MWEA050074.md): Odor · detected · Jul 30, 2005 · N810ME · Doug DC982 · Air Distribution System
  > PILOT SMELLED AN ODOR LIKE ELECTRICAL WIRING COMING FROM COCKPIT (NO SMOKE OR FUMES). INSPECTED THE ELETRICAL ELETRONICS COMPARTMENT AND FORWARD ACCESSORY COMPARTMENT, LOWERED CENTER OVERHEAD COCKPIT COMPARMENT PANELS AND INSPECTED WIRING, NO FAULTS NOTED. V
- [SDR MWEA050067](https://openairdocs.org/sdr/MWEA050067.md): Seat Track · worn · Jul 5, 2005 · N810ME · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > FIRST OFFICERS UPPER AND LOWER SEAT TRACK IS WORN AND ADJUSTMENT HOLES ELONGATED. REMOVED AND REPLACED SEAT TRACK.
- [SDR MWEA050066](https://openairdocs.org/sdr/MWEA050066.md): Seat Track · worn · Jul 5, 2005 · N810ME · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > CAPTAIN'S UPPER AND LOWER SEAT TRACK IS WORN AND ADJUSTMENT HOLES ELONGATED. FABRICATED AND INSTALLED UPPER AND LOWER SEAT TRACK.
- [SDR MWEA050065](https://openairdocs.org/sdr/MWEA050065.md): Door · inoperative · Jul 3, 2005 · N810ME · Doug DC982 · Emergency Exits
  > DURING INVESTIGATION OF LOOSE EXIT SIGN, COULD NOT REMOVE LEFT AFT OVERWING EXIT DOOR. REMOVED LEFT AFT DOOR BY DISPLACING FORWARD AND AFT ADJACENT SIDE WALL TRIM STRIPES, ADJUSTED SAME SIDE WALL PANELS AND REINSTALLED DOOR, OPERATIONAL CHECKED NORMAL.
- [SDR MWEA050064](https://openairdocs.org/sdr/MWEA050064.md): Wire · misrouted · Jun 30, 2005 · N810ME · Doug DC982 · Light System Wiring
  > FLOOR TRACK LIGHTING IN FORWARD CABIN G2 AISLE AREA, WIRES ARE MISROUTED AND IS MISSING PROTECTIVE TRACK PIECE FROM CENTER TO RIGHT WALL. SECURED EMERGENCY FLOOR TRACK LIGHTING WIRES AT FORWARD CABIN INTO THE NEW WIRE PROTECTION TRACKS, OPERATIONS CHECKED GOO
- [SDR MWEA050046](https://openairdocs.org/sdr/MWEA050046.md): Drain · obstructed · Jun 5, 2005 · N810ME · Doug DC982 · Buffet/Galleys
  > LOUD SQUEAL WAS AUDIBLE THROUGHOUT CABIN AND COCKPIT SEEMED TO BE IN FORWARD GALLEY. FOUND GALLEY DRAIN PLUGGED POSSIBLE CAUSE OF SQUEAL. CLEANED DRAIN, CLEANED GALLEY PASSENGER DOOR SEALS, PRESSURIZED CABIN TO 7.5 PSI, LEAK DOORS AND SEALS NO AUDIBLE SQEALS
- [SDR MWEA050028](https://openairdocs.org/sdr/MWEA050028.md): Wire · exposed · Feb 25, 2005 · N810ME · Doug DC982 · Light System Wiring
  > EMERGENCY TRACK LIGHTING WIRES EXPOSED. REPAIRED WIRES AND SECURED END CAP IAW 20-50-00 AND 33-50-00. OPERATION CHECK GOOD.
- [SDR MWEA040209](https://openairdocs.org/sdr/MWEA040209.md): Strap · damaged · Nov 17, 2004 · N810ME · Doug DC982 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD TEE HAS FOUR HOLES WITH TOO SHORT OF EDGE DISTANCE IN FORWARD UPPER FLANGE OF TEE BETWEEN LONGERON 18 RIGHT AND 17 RIGHT. SUBMITTED TO BOEING FOR DISPOSITION. FABRICATED AND INSTALLED NEW STRAPS AND FASTENERS.
- [SDR MWEA040207](https://openairdocs.org/sdr/MWEA040207.md): Longeron · damaged · Nov 16, 2004 · N810ME · Doug DC981 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO BAY FRAME STATION 309 LONGERON 28 RIGHT NEEDS TO BE CUT AND SPLICED. FABRICATED AND INSTALLED NEW SPLICE.
- [SDR MWEA040203](https://openairdocs.org/sdr/MWEA040203.md): Bulkhead · damaged · Nov 12, 2004 · N810ME · Doug DC982 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD REQUIRES REPLACEMENT DUE TO BLENDING BETWEEN LONGERONS 19 AND 20 RIGHT. FABRICATED AND INSTALLED NEW SECTION.
- [SDR MWEA040206](https://openairdocs.org/sdr/MWEA040206.md): Skin · dented · Nov 1, 2004 · N810ME · Doug DC982 · Fuselage Main, Plate/Skin
  > SKIN DENT AT STATION 294 LONGERON 24 RIGHT. FOUND TO BE OUT OF LIMITS. REMOVED DOUBLER, COLD WORK SKIN AND INSTALLED DOUBLER.
- [SDR MWEA040166](https://openairdocs.org/sdr/MWEA040166.md): Warning Light · false indication · Sep 15, 2004 · N810ME · Doug DC982 · Central Warning
  > TAIL CONE ANNUCIATOR ILLUMINATED. INSPECTED TAIL CONE LOCK/LATCH INSTALLATION, RESET CABLE LOCKBALL. OK FOR CONTINUED SERVICE.
- [SDR MWEA040115](https://openairdocs.org/sdr/MWEA040115.md): Structure · oversized · Jul 6, 2004 · N810ME · Doug DC982 · Aerodynamic Fairings
  > DURING TAILCONE DROP TEST, AFT CABIN DOOR ARMING PIN WOULD NOT ENGAGE DUE TO PIN HITTING COVER ABOVE DOOR. TRIMMED SLOT LONGER.
- [SDR MWEA040119](https://openairdocs.org/sdr/MWEA040119.md): Doubler · cracked · Jul 6, 2004 · N810ME · Doug DC982 · Fuselage Main, Structure
  > AT STATION 370 ON THE FORWARD CARGO DOOR WEB THERE IS A CRACK ON THE WEB UNDER THE FLOOR RAIL. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040118](https://openairdocs.org/sdr/MWEA040118.md): Frame · worn · Jul 6, 2004 · N810ME · Doug DC982 · Fuselage Main, Frame
  > FRAME STATION 579 FRAME FORMER FROM LONGERON 22 LEFT THROUGH 23 LEFT REQUIRES FLANGE REPAIR. FABRICATED AND INSTALLED REPAIR FORMER.
- [SDR MWEA040117](https://openairdocs.org/sdr/MWEA040117.md): Angle · out of tolerance · Jul 6, 2004 · N810ME · Doug DC982 · Fuselage Main, Frame
  > FORWARD CARGO DOOR JAMB PAN REPAIR AFT END HAS TWO FASTENERS WITH EDGE DISTANCE BELOW TOLERANCE AND GAP IS EXCESSIVE BETWEEN REPAIR PAN AND WHERE ORIGINAL PAN WAS CUT. FABRICATED AND INSTALLED 2 EACH REPAIR ANGLES.
- [SDR MWEA040113](https://openairdocs.org/sdr/MWEA040113.md): Finger Doubler · out of tolerance · Jul 6, 2004 · N810ME · Doug DC982 · Fuselage Main, Plate/Skin
  > RIGHT PRIMARY STATIC PORT AREA FUSELAGE SKIN HAS A CONTOUR CHANGE OUT OF TOLERANCE WHERE REPAIR IS INSTALLED, STATION 607 IN BETWEEN LONGERON 22 RIGHT AND 23 RIGHT. FABRICATED AND INSTALLED FINGER DOUBLER AND FILLER.
- [SDR MWEA040114](https://openairdocs.org/sdr/MWEA040114.md): Torque Tube · corroded · Jul 6, 2004 · N810ME · Doug DC982 · Cargo/Baggage Doors
  > CENTER CARGO DOOR AFT TORQUE TUBE IS CORRODED. REMOVED AND REPLACED AFT TORQUE TUBE.
- [SDR MWEA040116](https://openairdocs.org/sdr/MWEA040116.md): Longeron · out of tolerance · Jul 6, 2004 · N810ME · Doug DC982 · Fuselage Main, Plate/Skin
  > RIGHT PRIMARY STATIC PORT AREA FUSELAGE SKIN BUTT JOINT SKIN TO SKIN FLUSHNESS IS OUT OF TOLERANCE LOCATED AT STATION 589 LONGERON 26 RIGHT, UPPER SKINS ARE OUT AT.022, LOWER SKINS ARE OUT AT.015. FABRICATED AND INSTALLED LONGERON.
- [SDR MWEA040112](https://openairdocs.org/sdr/MWEA040112.md): Door Frame · corroded · Jul 2, 2004 · N810ME · Doug DC982 · Fuselage Main, Structure
  > FORWARD CARGO DOOR JAMB PAN, LOWER EDGE HAS AREAS OF SEVERE CORROSION. FABRICATED AND INSTALLED REPAIR PARTS.

Next page: https://openairdocs.org/deregistered/N810ME-2010-03-31/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 = 'N810ME' AND deregistration_id = 'N810ME-2010-03-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N810ME-2010-03-31/reports

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