# N810ME: 1981 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2010-03-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 31, 2010
- Status when cancelled: Triennial form not returned
- Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 48072
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: January 25, 1999
- Certificate issued: April 24, 1998
- Last registry action: August 18, 2009
- Mode S code: AB0A74
- Owner when cancelled: [Aviation Asset Trading LLC](https://openairdocs.org/faa-owner/AVIATION%20ASSET%20TRADING%20LLC)
- Location: [Elgin, IL](https://openairdocs.org/faa-place/IL/Elgin)
- Owner type: Corporation
- Owner's area on the map: 42.0321° N, 88.2397° W: Placed by OpenAirDocs at the center of ZIP code 60120, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N810ME
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=810ME
- Page: https://openairdocs.org/deregistered/N810ME-2010-03-31

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Mcdonnell Douglas DC-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md

## Service difficulty reports (170, newest 50)

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

- [SDR MWEA080071](https://openairdocs.org/sdr/MWEA080071), May 17, 2008: CONTROL VALVE. FAULTY. 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 VALV
- [SDR MWEA080016](https://openairdocs.org/sdr/MWEA080016), Jan 28, 2008: SUPPORT. CORRODED. 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), Jan 23, 2008: SKIN. CORRODED. 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 IN
- [SDR MWEA080011](https://openairdocs.org/sdr/MWEA080011), Jan 18, 2008: CUSP WEB. CORRODED. 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), Dec 26, 2007: SMOKE DETECTOR. FALSE INDICATION. 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 R
- [SDR MWEA070263](https://openairdocs.org/sdr/MWEA070263), Oct 28, 2007: WIRE. BROKEN. FLOOR TRACK EMERGENCY LIGHT INOPERATIVE FROM ROW 27 AFT. FOUND SPLICE BROKEN REPLACED SPLICE.
- [SDR MWEA070259](https://openairdocs.org/sdr/MWEA070259), Oct 17, 2007: SMOKE DETECTOR. FAULTY. LEFT REAR LAV SMOKE ALARM SOUNDED. REMOVED AND REPLACED AFT LEFT LAVATORY SMOKE DETECTOR.
- [SDR MWEA070095](https://openairdocs.org/sdr/MWEA070095), Apr 13, 2007: LANYARD. BROKEN. AFT GALLEY GIRT BAR CABLE BROKEN. REMOVED AND REPLACED AFT GALLEY GIRT LANYARD.
- [SDR MWEA070094](https://openairdocs.org/sdr/MWEA070094), Apr 13, 2007: GIRT BAR. STUCK. FLIGHT ATTENDANT UNABLE TO DISARM GIRT BAR AT AFT GALLEY DOOR. DISARMED AFT GALLEY SLIDE.
- [SDR MWEA070078](https://openairdocs.org/sdr/MWEA070078), Apr 5, 2007: SHEAR TIE. DAMAGED. SHEAR CLIP DAMAGE FROM DRILL MARK. FABRICATED AND INSTALLED SHEAR TIE.
- [SDR MWEA070077](https://openairdocs.org/sdr/MWEA070077), Apr 4, 2007: SKIN. DENTED. EVIDENCE OF SKIN DENTED AT STATION 541 BETWEEN LONGERERON 26 AND LONGERON 27. FABRICATED AND INSTALLED FILLER.
- [SDR MWEA070076](https://openairdocs.org/sdr/MWEA070076), Apr 4, 2007: SKIN. DENTED. LONGERON 27 AT STATION 636 EVIDENCE OF SKIN DENTED. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA070041](https://openairdocs.org/sdr/MWEA070041), Mar 5, 2007: LATCH. BROKEN. 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), Feb 2, 2007: SLIDE. LOW PRESSURE. AFT EVACUATION SLIDE PRESSURE IS LOW AT 1500 PSI. REMOVED AND REPLACED AFT SLIDE.
- [SDR MWEA060295](https://openairdocs.org/sdr/MWEA060295), Nov 12, 2006: SKIN. DAMAGED. 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), Sep 2, 2006: FLASHLIGHT. INOPERATIVE. EMERGENCY LIGHT BESIDE ENTRANCE DOOR INOPERATIVE. REMOVED AND REPLACED FLASH LIGHT.
- [SDR MWEA060141](https://openairdocs.org/sdr/MWEA060141), Jul 5, 2006: SEAL. CRACKED. 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), Jul 5, 2006: SUPPORT. CORRODED. 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), Jul 5, 2006: THRESHOLD. CORRODED. CORROSION ALONG ENTIRE LENGTH OF AFT CARGO DOOR THRESHOLD, PLATE SUPPORT STRUCTURE. FABRICATED AND INSTALLED SHEAR FASTENER.
- [SDR MWEA060138](https://openairdocs.org/sdr/MWEA060138), Jul 5, 2006: DOUBLER. DELAMINATED. 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), May 27, 2006: CRANK ASSY. DEFECTIVE. 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), Apr 11, 2006: SKIN. DAMAGED. FOUND FORWARD PASSENGER DOOR DAMAGED. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA060018](https://openairdocs.org/sdr/MWEA060018), Feb 18, 2006: ENGINE. FROZEN. 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 O
- [SDR MWEA070015](https://openairdocs.org/sdr/MWEA070015), Feb 14, 2006: SPLICE. FAULTY. FORWARD SECTION CABIN FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. FOUND BAD SPLICE, REPLACED SPLICE.
- [SDR MWEA060007](https://openairdocs.org/sdr/MWEA060007), Jan 19, 2006: SEAT TRACK. OUT OF ALIGNMENT. 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), Jan 4, 2006: O-RING. LEAKING. RT HYDRAULIC QUANTITY LOW ONE QUART ON FINAL APPROACH. REMOVED AND REPLACED RT PRESSURE REDUCER O-RING.
- [SDR MWEA050115](https://openairdocs.org/sdr/MWEA050115), Oct 12, 2005: ENGINE. MALFUNCTIONED. 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
- [SDR MWEA050107](https://openairdocs.org/sdr/MWEA050107), Sep 28, 2005: PUMP. INOPERATIVE. RT ENGINE HYDRAULIC PUMP INOPERATIVE. REMOVED AND REPLACED RT ENGINE HYDRAULIC PUMP.
- [SDR MWEA050106](https://openairdocs.org/sdr/MWEA050106), Sep 16, 2005: OVERHEAT SENSOR. INOPERATIVE. TAIL COMPARTMENT HIGH TEMPERATURE LIGHT CAME ON. REMOVED AND REPLACED OVERHEAT SENSOR AND TIGHTENED RIGHT CLAMP.
- [SDR MWEA050100](https://openairdocs.org/sdr/MWEA050100), Sep 2, 2005: APU. OVERTEMP. 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 PANE
- [SDR MWEA050074](https://openairdocs.org/sdr/MWEA050074), Jul 30, 2005: ODOR. DETECTED. PILOT SMELLED AN ODOR LIKE ELECTRICAL WIRING COMING FROM COCKPIT (NO SMOKE OR FUMES). INSPECTED THE ELETRICAL ELETRONICS COMPARTMENT AND FORWARD ACCESSORY COMPA
- [SDR MWEA050067](https://openairdocs.org/sdr/MWEA050067), Jul 5, 2005: SEAT TRACK. WORN. 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), Jul 5, 2005: SEAT TRACK. WORN. 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), Jul 3, 2005: DOOR. INOPERATIVE. 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 TR
- [SDR MWEA050064](https://openairdocs.org/sdr/MWEA050064), Jun 30, 2005: WIRE. MISROUTED. 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 FLOO
- [SDR MWEA050046](https://openairdocs.org/sdr/MWEA050046), Jun 5, 2005: DRAIN. OBSTRUCTED. 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
- [SDR MWEA050028](https://openairdocs.org/sdr/MWEA050028), Feb 25, 2005: WIRE. EXPOSED. 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), Nov 17, 2004: STRAP. DAMAGED. 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 BOE
- [SDR MWEA040207](https://openairdocs.org/sdr/MWEA040207), Nov 16, 2004: LONGERON. DAMAGED. 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), Nov 12, 2004: BULKHEAD. DAMAGED. 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), Nov 1, 2004: SKIN. DENTED. 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), Sep 15, 2004: WARNING LIGHT. FALSE INDICATION. TAIL CONE ANNUCIATOR ILLUMINATED. INSPECTED TAIL CONE LOCK/LATCH INSTALLATION, RESET CABLE LOCKBALL. OK FOR CONTINUED SERVICE.
- [SDR MWEA040115](https://openairdocs.org/sdr/MWEA040115), Jul 6, 2004: STRUCTURE. OVERSIZED. 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), Jul 6, 2004: DOUBLER. CRACKED. 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), Jul 6, 2004: FRAME. WORN. 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), Jul 6, 2004: ANGLE. OUT OF TOLERANCE. 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 W
- [SDR MWEA040113](https://openairdocs.org/sdr/MWEA040113), Jul 6, 2004: FINGER DOUBLER. OUT OF TOLERANCE. 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 RI
- [SDR MWEA040114](https://openairdocs.org/sdr/MWEA040114), Jul 6, 2004: TORQUE TUBE. CORRODED. CENTER CARGO DOOR AFT TORQUE TUBE IS CORRODED. REMOVED AND REPLACED AFT TORQUE TUBE.
- [SDR MWEA040116](https://openairdocs.org/sdr/MWEA040116), Jul 6, 2004: LONGERON. OUT OF TOLERANCE. 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
- [SDR MWEA040112](https://openairdocs.org/sdr/MWEA040112), Jul 2, 2004: DOOR FRAME. CORRODED. FORWARD CARGO DOOR JAMB PAN, LOWER EDGE HAS AREAS OF SEVERE CORROSION. FABRICATED AND INSTALLED REPAIR PARTS.

All 170: https://openairdocs.org/deregistered/N810ME-2010-03-31/reports.md

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