# N808ME: 1981 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2011-01-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 28, 2011 - 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: 48070 - Year built: 1981 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: January 8, 1999 - Certificate issued: November 3, 1999 - Last registry action: October 20, 2009 - Mode S code: AB00AD - Owner when cancelled: [US Bancorp Equipment Finance Inc](https://openairdocs.org/faa-owner/US%20BANCORP%20EQUIPMENT%20FINANCE%20INC) - Location: [Portland, OR](https://openairdocs.org/faa-place/OR/Portland) - Owner type: Corporation - Owner's area on the map: 45.5235° N, 122.6762° W: Placed by OpenAirDocs: center of Portland, OR, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N808ME - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=808ME - Page: https://openairdocs.org/deregistered/N808ME-2011-01-28 From the FAA registry file of October 28, 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 (140, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR MWEA080028](https://openairdocs.org/sdr/MWEA080028), Feb 13, 2008: LATCH. INCORRECT. 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 REPL - [SDR MWEA070099](https://openairdocs.org/sdr/MWEA070099), May 2, 2007: B-NUT. LOOSE. 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), Apr 22, 2007: B-NUT. LEAKING. 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), Apr 4, 2007: SKIN. DENTED. 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), Mar 1, 2007: SKIN. GOUGED. 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), Feb 16, 2007: GYRO. FAILED. CAPTAIN'S ATTITUDE INDICATOR FAILED. REMOVED AND REPLACED CAPTAINS FOG GYRO. - [SDR MWEA070002](https://openairdocs.org/sdr/MWEA070002), Jan 12, 2007: CHANNEL. PUNCTURED. STATION 218 BULKHEAD WALL ZEE CHANNEL STATION 0.007" ABOVE FLOOR IS PUNCTURED. INSTALLED ZEE CHANNEL. - [SDR MWEA070001](https://openairdocs.org/sdr/MWEA070001), Jan 12, 2007: BULKHEAD. PUNCTURED. 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), Dec 15, 2006: SKIN. CRACKED. 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, - [SDR MWEA060290](https://openairdocs.org/sdr/MWEA060290), Nov 7, 2006: WARNING MESSAGE. ILLUMINATED. 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), Oct 6, 2006: SKIN. LIGHTNING STRIKE. LIGHTNING STRIKE FROM FRAME STATION 337-356 LONGERON 28 TO 19 RIGHT. FABRICATED AND INSTALLED DOUBLER. - [SDR MWEA070023](https://openairdocs.org/sdr/MWEA070023), Aug 3, 2006: SCREW. MISSING. THE PIN FROM TOP OF AFT PRESSURE BULKHEAD FAILED TO ENGAGE THE ARM. INSTALLED MISSING SCREW. - [SDR MWEA060135](https://openairdocs.org/sdr/MWEA060135), Jun 24, 2006: BULB. INOPERATIVE. RIGHT LANDING GEAR LIGHT DID NOT ILLUMINATE -RED AND GREEN-. INSPECTED SENSORS & WIRING AT RIGHT MAIN LANDING GEAR, NO PROBLEMS. REMOVED MAIN LANDING GEAR INDIC - [SDR MWEA060046](https://openairdocs.org/sdr/MWEA060046), May 1, 2006: HYDRAULIC LINE. BROKEN. 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), Mar 24, 2006: SKIN. DAMAGED. FOUND RIGHT ELEVATOR TOP, OUTBOARD, TRAILING EDGE SKIN HAS DAMAGE APPROXIMATELY AT STATION XHR 210, APPROXIMATELY 1.125" BY .25". FABRICATED AND INSTALLED DOUBL - [SDR MWEA070014](https://openairdocs.org/sdr/MWEA070014), Mar 3, 2006: BATTERY PACK. DISCHARGED. BOTH LEFT & RIGHT EMERGENCY LIGHTS INOPERATIVE ON OVERWING OUTSIDE. REMOVED AND REPLACED OVERWING BATTERY PACK. - [SDR MWEA060016](https://openairdocs.org/sdr/MWEA060016), Feb 18, 2006: ENGINE. FROZEN. 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), Jan 30, 2006: VANE. GOUGED. LEFT WING INBOARD FIXED VANE HAS GOUGE ON LOWER SIDE, OUTBOARD EDGE. FABRICATED AND INSTALLED DOUBLER. - [SDR MWEA060005](https://openairdocs.org/sdr/MWEA060005), Jan 10, 2006: FRAME. CRACKED. 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), Jan 9, 2006: LONGERON. CRACKED. 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), Sep 1, 2005: BATTERY PACK. INOPERATIVE. FOUR CEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES IN BATTERY PACK. - [SDR MWEA050098](https://openairdocs.org/sdr/MWEA050098), Sep 1, 2005: FLOORBOARD. CORRODED. 8 FLOORBOARD ATTACH STRIP FIRST INBOARD OF PASSENGER DOOR HAS CORROSION. FABRICATED AND INSTALLED FLOORBOARD SUPPORT ANGLE. - [SDR MWEA050097](https://openairdocs.org/sdr/MWEA050097), Sep 1, 2005: FLOORBOARD. CORRODED. 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 AN - [SDR MWEA050096](https://openairdocs.org/sdr/MWEA050096), Sep 1, 2005: DOUBLER. CORRODED. 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), Sep 1, 2005: SEAT TRACK. DAMAGED. PIOLT SEAT INBOARD SEAT TRACK HOLES ARE ENLONGATED. FABRICATED AND INSTALLED SEAT TRACK. - [SDR MWEA050094](https://openairdocs.org/sdr/MWEA050094), Sep 1, 2005: SEAT TRACK. DAMAGED. CO-PILOT'S CREW SEAT INBOARD SEAT TRACK HOLES ARE ENLONGATED. FABRICATED AND INSTALLED NEW SEAT TRACK. - [SDR MWEA050089](https://openairdocs.org/sdr/MWEA050089), Aug 23, 2005: FLOOR SUPPORT. CORRODED. RT SIDE, MOST OB FLOORBOARD ATTACH STRIP HAS HOLE CORRODED, STATION 218. FABRICATED AND INSTALLED FLOOR SUPPORT. - [SDR MWEA050087](https://openairdocs.org/sdr/MWEA050087), Aug 23, 2005: DOUBLER. DENTED. DENT ON EMERGENCY EXIT DOOR. FABRICATED AND INSTALLED DOUBLER. - [SDR MWEA050093](https://openairdocs.org/sdr/MWEA050093), Aug 23, 2005: SKIN. DENTED. 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 - [SDR MWEA050092](https://openairdocs.org/sdr/MWEA050092), Aug 23, 2005: PANEL. CORRODED. 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), Aug 23, 2005: PANEL. CORRODED. 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), Aug 23, 2005: SUPPORT ANGLE. DAMAGED. 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), Aug 23, 2005: FLOOR SUPPORT. CORRODED. 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), Aug 18, 2005: SEAT TRACK. CORRODED. SEAT TRACK CORRODED AT STATION 207. FABRICATED AND INSTALLED SEAT TRACK. - [SDR MWEA050084](https://openairdocs.org/sdr/MWEA050084), Aug 18, 2005: SEAT TRACK. CORRODED. 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), Aug 18, 2005: SEAT TRACK. CORRODED. NR 2 SEAT TRACK CORRODED, FORWARD END. FABRICATED AND INSTALLED SEAT TRACK. - [SDR MWEA050083](https://openairdocs.org/sdr/MWEA050083), Aug 18, 2005: SEAT TRACK. DAMAGED. FIRST OFFICER'S, INBOARD SEAT TRACK HOLES ARE ENLONGATED. FABRICATED AND INSTALLED SEAT TRACK. - [SDR MWEA050056](https://openairdocs.org/sdr/MWEA050056), May 14, 2005: WIRE. INOPERATIVE. SECTION OF EMERGENCY TRACK LIGHTS ARE INOPERATIVE FROM SEAT 9 THROUGH 18. REPAIRED WIRE. - [SDR MWEA050030](https://openairdocs.org/sdr/MWEA050030), Apr 7, 2005: SKIN. CRACKED. 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), Mar 5, 2005: SEAL. LEAKING. FIRST OFFICER'S WINDOW WAS LEAKING AND WOULD GET LOUDER AS ALTITUDE WAS INCREASED. PRESSURIZED AIRCRAFT AND FOUND FIRST OFFICER'S WINDOW LEAKING, INSPECTED FIRS - [SDR MWEA040228](https://openairdocs.org/sdr/MWEA040228), Dec 27, 2004: REGULATOR. MALFUNCTIONED. AT LEVEL OF AT FL250, FLOW METER CAME ON. REMOVED AND REPLACED AIR CONDITIONING PRESSURE REGULATOR. - [SDR MWEA040180](https://openairdocs.org/sdr/MWEA040180), Oct 1, 2004: CUSP WEB. CRACKED. CUSP MEMBRANE IS CRACKED AT STATION 1245 LT SIDE. FABRICATED AND INSTALLED DOUBLER. - [SDR MWEA040178](https://openairdocs.org/sdr/MWEA040178), Sep 28, 2004: SKIN. CORRODED. 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), Sep 27, 2004: SKIN. DENTED. 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 - [SDR MWEA040191](https://openairdocs.org/sdr/MWEA040191), Sep 23, 2004: CUSP WEB. CRACKED. LEFT FUSELAGE CUSP MEMBRANE AT FRAME STATION 1305 HAS A CRACK. FABRICATED AND INSTALLED DOUBLER. - [SDR MWEA040174](https://openairdocs.org/sdr/MWEA040174), Sep 23, 2004: SKIN. DENTED. 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 - [SDR MWEA040173](https://openairdocs.org/sdr/MWEA040173), Sep 23, 2004: DOUBLER. DENTED. 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 - [SDR MWEA040172](https://openairdocs.org/sdr/MWEA040172), Sep 23, 2004: DOUBLER. DENTED. 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), Sep 21, 2004: PAN. CRACKED. FORWARD BAGGAGE PIT DOOR, FORWARD PAN FLANGE CRACKED. FABRICATED AND INSTALLED DOUBLER. - [SDR MWEA040170](https://openairdocs.org/sdr/MWEA040170), Sep 21, 2004: SHEAR TIE. CRACKED. SHEAR TIE AT STATION 294 ABOVE LONGERON 17 LEFT IS CRACKED AND DENTED. FABRICATED AND INSTALLED NEW FORMER. All 140: https://openairdocs.org/deregistered/N808ME-2011-01-28/reports.md ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20000508030419I](https://openairdocs.org/incident/20000508030419I), May 8, 2000: Doug DC982 (N808ME), Peoria, IL. (-23)IGL1920000019-midwest express airlines flight 83, MD-80, was enroute from laguardia to Kansas city when the pilot advised of a medical emergency at… - [Incident 19990711022679I](https://openairdocs.org/incident/19990711022679I), Jul 11, 1999: Doug DC982 (N808ME), Kansas City, MO. On July 11, 1999, midwest express, Mcdonnell Douglas CD-0-82, N808ME, departed Kansas City International Airport (mci), and returned to mci due to #1 engine… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.