# N206ME: 1979 Mcdonnell Douglas DC-9-32, registration cancelled 2005-01-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 21, 2005 - Exported to: Mexico - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-32](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32) (registry code 302206C) - Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47791 - Year built: 1979 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: February 10, 1999 - Certificate issued: September 10, 2004 - Last registry action: September 10, 2004 - Mode S code: A1A965 - Owner when cancelled: [Interglobal Inc](https://openairdocs.org/faa-owner/INTERGLOBAL%20INC) - Location: [Carson City, NV](https://openairdocs.org/faa-place/NV/Carson%20City) - Owner type: Corporation - Owner's area on the map: 39.2227° N, 119.7016° W: Placed by OpenAirDocs at the center of ZIP code 89706, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N206ME - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=206ME - Page: https://openairdocs.org/deregistered/N206ME-2005-01-21 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-9-32: https://openairdocs.org/model/mcdonnell-douglas-dc-9-32.md ## Service difficulty reports (187, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR MWEA030254](https://openairdocs.org/sdr/MWEA030254), Jun 24, 2003: RUDDER. INOPERATIVE. RUDDER FULL RIGHT APPLIED WITH NO APPARENT EFFECT. ADJUSTED CABLE RUN AND SENSING SECTOR, PERFORMED ADJUSTMENT TEST. NO DEFECTS NOTED. (AIRCRAFT PARKED SINCE 6- - [SDR MWEA030233](https://openairdocs.org/sdr/MWEA030233), May 25, 2003: SWITCH. DIRTY. RECEIVED TAKEOFF WARNING HORN WHILE ADVANCING THROTTLES. -- CLEANED STICKY SWITCH. - [SDR MWEA020618](https://openairdocs.org/sdr/MWEA020618), Oct 17, 2002: LINE. DISCONNECTED. RIGHT ENGINE PRESSURE RATIO GAUGE REMAINED AT 10. FOUND PT7 LINE DISCONNECTED AT LOWER AFT ATTACH FITTING. RECONNECTED PT7 LINE. - [SDR MWEA020319](https://openairdocs.org/sdr/MWEA020319), May 6, 2002: VALVE. CLOGGED. AILERON SERVO INDICATOR SHOWED FULL DEFLECTION. DISCONNECTED AUTO PILOT AND THE AIRCRAFT STARTED TO TURN TO THE LEFT. FOUND WATER DRAINING IN LEFT GEAR AREA AND - [SDR MWEA020296](https://openairdocs.org/sdr/MWEA020296), Apr 11, 2002: SUPPORT BRACKET. CORRODED. FORWARD PIT LEFT AUX TANK STRUT UPPER SUPPORT BRACKET HAS EXFOLIATION AROUND A FASTENER STATION 545 LONGERON 24 LEFT. REMOVED AND REPLACED FITTING. - [SDR MWEA020295](https://openairdocs.org/sdr/MWEA020295), Apr 11, 2002: SKIN. DAMAGED. REPLACE AFT CARGO PIT BELLY SKIN SECTION LONGERON 28 LEFT TO 28 RIGHT STATION 803 THROUGH 996 TO COMPLY WITH CARRY OVER NR 2201. REMOVED AND REPLACED SKIN. - [SDR MWEA020294](https://openairdocs.org/sdr/MWEA020294), Apr 11, 2002: LONGERON. CRACKED. FORWARD PIT LONGERON 29 RIGHT IS CRACKED AT STATION 570-578. -- REMOVED, MATCH DRILLED LONGERON AS REQUIRED PER DWG # 5910068, AND INSTALLED. - [SDR MWEA020222](https://openairdocs.org/sdr/MWEA020222), Apr 8, 2002: ANGLE. CRACKED. VERTICAL STABILIZER LEADING EDGE TAIL TO FUSELAGE DORSAL INTERNAL ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE BRACKET. - [SDR MWEA020223](https://openairdocs.org/sdr/MWEA020223), Apr 8, 2002: WEB. OUT OF TOLERANCE. REMOVAL AFT CARGO DOOR JAMB LOWER INNER WEB TO FACILITATE OTHER MAINTENANCE. -- OLD WEB FOUND OUT OF LIMITS. INSTALLED NEW WEB. - [SDR MWEA020221](https://openairdocs.org/sdr/MWEA020221), Apr 8, 2002: FORMER. CRACKED. FORMER AT STATION 237 LONGERON 18 LEFT TO 17 LEFT IS CRACKED. -- FABRICATED AND INSTALLED SHIM TO ACHIEVE EDGE DISTANCE. - [SDR MWEA020219](https://openairdocs.org/sdr/MWEA020219), Apr 8, 2002: WEB. MISDRILLED. FORWARD CARGO DOOR JAMB WEB AND FRAME AT 427 HAS A DOUBLE DRILLED HOLE BETWEEN LONGERON 29 RIGHT AND LONGERON 28 RIGHT. -- FABRICATED AND INSTALLED REPAIR STRAP - [SDR MWEA020217](https://openairdocs.org/sdr/MWEA020217), Apr 8, 2002: ANGLE. BROKEN. CORROSION ON LOWER LEG FORWARD SIDE OF ELECTRONIC POWER CENTER PANEL SUPPORT FROM COCKPIT DOOR JAMB TO BANANA PANEL. FOUND ANGLE CRACKED OFF. REMOVED AND REPLAC - [SDR MWEA020216](https://openairdocs.org/sdr/MWEA020216), Apr 8, 2002: SKIN. DAMAGED. FUSELAGE CLASS III DOUBLER NEEDS UPGRADE AT STATION 218 LONGERON 25 LEFT. REMOVED DOUBLER, VERIFIED AS NO CRACKS IN SKIN. INSTALLED DOUBLER. REPAIR PLACED ON WA - [SDR MWEA020215](https://openairdocs.org/sdr/MWEA020215), Apr 8, 2002: SKIN. CORRODED. RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AROUND SOME OF THE WRAP AROUND SCREWS (CENTER SECTION INBOARD AREA). THERE WAS PREVIOUS BLEND-OUT ALREADY - [SDR MWEA020214](https://openairdocs.org/sdr/MWEA020214), Apr 8, 2002: SKIN. CORRODED. LEFT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AROUND SOME OF THE WRAP AROUND SCREWS (CENTER SECTION INBOARD AREA). THERE WAS PREVIOUS BLEND OUT ALREADY - [SDR MWEA020213](https://openairdocs.org/sdr/MWEA020213), Apr 8, 2002: INTERCOSTAL. CRACKED. FORWARD CARGO DOOR, INTERCOSTAL CRACKED, LOWER AFT AREA OF DOOR. -- REMOVED AND REPLACED INTERCOSTAL. - [SDR MWEA020212](https://openairdocs.org/sdr/MWEA020212), Apr 8, 2002: DOUBLER. BLOWN. AFT CARGO COMPARTMENT DOUBLER AROUND THE SUGAR SCOOP IS BLOWN OUT ON THE BOTTOM AFT AREA AT STATION 965 ABOVE LONGERON 22 LEFT. -- REMOVED DOUBLER. DRILLED UP A - [SDR MWEA020211](https://openairdocs.org/sdr/MWEA020211), Apr 8, 2002: LONGERON. BLOWN. AFT CARGO COMPARTMENT HAS A LONGERON BLOWN OUT IN THE CENTER OF LONGERON 23 LEFT AT STATION 945. -- FABRICATED AND INSTALLED STRAP. - [SDR MWEA020210](https://openairdocs.org/sdr/MWEA020210), Apr 8, 2002: PANEL. DAMAGED. REMOVED CABIN FLOOR PANEL B-5 TO FACILITATE OTHER MAINTENANCE. -- FORWARD END OF PANEL IS DAMAGED. FABRICATED NEW SKIN AND REINSTALLED CABIN FLOOR PANEL. - [SDR MWEA020194](https://openairdocs.org/sdr/MWEA020194), Mar 27, 2002: PANEL. DAMAGED. DENT DAMAGE ON RUDDER LEADING EDGE STRUCTURE AT STATION ZR70 RIGHT SIDE. MEASURES APPROX 4 INCHES IN LENGTH. FABRICATED AND INSTALLED REPAIR. - [SDR MWEA020195](https://openairdocs.org/sdr/MWEA020195), Mar 27, 2002: GUSSET. CORRODED. GUSSET AT STATION 580 IS CORRODED ON INTERCOSTAL. -- FABRICATED AND INSTALLED GUSSET. - [SDR MWEA020193](https://openairdocs.org/sdr/MWEA020193), Mar 27, 2002: FITTING. MISDRILLED. FITTINGS MISDRILLED AT STATION 207 (INTERCOSTAL ATTACH CLIP). -- FABRICATED AND INSTALLED NEW FITTING. LOCATED AND PRIMED AND INSTALLED PARTS. - [SDR MWEA020192](https://openairdocs.org/sdr/MWEA020192), Mar 27, 2002: FITTING. DAMAGED. REMOVED FLOOR BEAM END FITTING AT CUSP, STATION 218 LEFT SIDE TO FACILITATE OTHER MAINTENANCE. -- FITTING DAMAGED UPON REMOVAL. INSTALLED NEW FITTING. - [SDR MWEA020191](https://openairdocs.org/sdr/MWEA020191), Mar 27, 2002: ANGLE. CORRODED. CORROSION ON CELING IN E&E BAY FROM STATION 200 TO 218 JUST BELOW THE CUSP LINE NEAR LONGERON 18 LEFT. REMOVED DAMAGED SECTION OF UPPER CUSP ANGLE. FABRICATED A - [SDR MWEA020190](https://openairdocs.org/sdr/MWEA020190), Mar 27, 2002: INTERCOSTAL. IMPROPER. FORWARD PIT INTERCOASTAL LOCATED BETWEEN LONGERON 28 RIGHT AND 27 RIGHT AND FRAMES 560-579 HAS SEVERAL DIVETS IMPROPERLY BACKED. -- FABRICATED AND INSTALLED AFT - [SDR MWEA020188](https://openairdocs.org/sdr/MWEA020188), Mar 27, 2002: BRACKET. CORRODED. CORROSION ON ANGLE BRACKET FOR FLOOR SUPPORT AT STATION 367 RIGHT SIDE. REMOVED AND REPLACED BRACKET. - [SDR MWEA020187](https://openairdocs.org/sdr/MWEA020187), Mar 22, 2002: SPLICE. CRACKED. LONGERON 28 LEFT SPLICE AT STATION 560 IS CRACKED OUT AFT HOLE. -- REMOVED LONGERON SPLICE FITTING. MATCH DRILLED FITTING. FABRICATED AND INSTALLED SHIMS TO SPL - [SDR MWEA020186](https://openairdocs.org/sdr/MWEA020186), Mar 22, 2002: PANEL. CORRODED. LEFT FLAP TRAILING EDGE PANEL NR 3 HAS MODERATE TO HEAVY CORROSION AROUND FINGER DOUBLERS IN SEVERAL BAYS. FINGER DOUBLERS LOOSE IN SEVERAL AREAS. FABRICATED AN - [SDR MWEA020185](https://openairdocs.org/sdr/MWEA020185), Mar 19, 2002: LONGERON. CORRODED. FORWARD PIT, CORROSION ON LONGERON AT STATION 570 LONGERON 30. REMOVED AND REPLACED LONGERON. FABRICATED AND INSTALLED RADIUS STRAP. - [SDR MWEA020184](https://openairdocs.org/sdr/MWEA020184), Mar 19, 2002: FRAME. CORRODED. STATION 980 FRAME UPPER -J- CHANNEL HAS AREAS OF LIGHT CORROSION BETWEEN LONGERON 29 LEFT THROUGH LONGERON 28 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLES, SPL - [SDR MWEA020183](https://openairdocs.org/sdr/MWEA020183), Mar 19, 2002: LONGERON. CRACKED. FORWARD PIT LONGERON 28 LEFT IS CRACKED UNDER SPLICE AT STATION 552 THROUGH 560. -- REMOVED LONGERON, POSITIONED AND DRILLED, REINSTALLED LONGERON. - [SDR MWEA020182](https://openairdocs.org/sdr/MWEA020182), Mar 19, 2002: CLIP. CORRODED. AFT CARGO COMPARTMENT UNDERSIDE OF SHOVEL CLIP CORRODED AT STATION 945 LONGERON 26 RIGHT. -- REMOVED AND REPLACED SHOVEL CLIP. - [SDR MWEA020181](https://openairdocs.org/sdr/MWEA020181), Mar 19, 2002: FRAME. CORRODED. STATION 832 FRAME AFT SIDE HAS CORROSION BETWEEN LONGERONS 29 RIGHT TO 28 RIGHT. FABRICATED AND INSTALLED FRAME REPAIR SECTIONS. - [SDR MWEA020180](https://openairdocs.org/sdr/MWEA020180), Mar 19, 2002: FRAME. CORRODED. STATION 917 FRAME FORWARD SIDE HAS CORROSION FROM LONGERON 28 LEFT TO 29 RIGHT UNDER THE FLOOR SUPPORT. FABRICATED AND INSTALLED FRAME SECTION, REPAIR DOUBLERS, - [SDR MWEA020179](https://openairdocs.org/sdr/MWEA020179), Mar 19, 2002: FRAME. CORRODED. STATION 965 FRAME HAS LIGHT CORROSION FROM LONGERON 25 LEFT TO 27 RIGHT AFT SIDE. REMOVED AND REPLACED SPLICE. - [SDR MWEA020177](https://openairdocs.org/sdr/MWEA020177), Mar 19, 2002: FRAME. CORRODED. FORMER AT STATION 980 HAS AREA OF LIGHT CORROSION BETWEEN LONGERON 25 THROUGH LONGERON 26 LEFT. FABRICATED AND INSTALLED FORMER AND SPLICES. - [SDR MWEA020178](https://openairdocs.org/sdr/MWEA020178), Mar 19, 2002: FITTING. CORRODED. CUSP SPLICE FITTING AT STATION 229 LEFT SIDE HAS CORROSION. REMOVED AND REPLACED FITTING. - [SDR MWEA020176](https://openairdocs.org/sdr/MWEA020176), Mar 19, 2002: SUPPORT. CRACKED. STATION 897 BETWEEN LONGERONS 27 LEFT AND 28 LEFT SUPPORT HAS CORROSION BY A FASTENER. WHILE REMOVING CORROSION, FOUND SUPPORT CRACK. REMOVED AND REPLACED SUPPO - [SDR MWEA020175](https://openairdocs.org/sdr/MWEA020175), Mar 19, 2002: FITTING. CORRODED. STATION 945 BETWEEN LONGERONS 28 LEFT AND 27 LEFT HAS A CORRODED SUPPORT FITTING. -- REMOVED AND REPLACED SUPPORT FITTING. - [SDR MWEA020174](https://openairdocs.org/sdr/MWEA020174), Mar 19, 2002: SUPPORT. CRACKED. STATION 980 BY LONGERON 27 RIGHT HAS A CRACKED SUPPORT. -- REMOVED AND REPLACED FLOOR SUPPORT. - [SDR MWEA020170](https://openairdocs.org/sdr/MWEA020170), Mar 15, 2002: FRAME. CORRODED. STATION 897 FRAME AT LONGERON 29 RIGHT TO 30 HAS CORROSION ON THE LOWER SURFACE. FABRICATED AND INSTALLED CLIP, REPAIR DOUBLERS, AND SHIMS. - [SDR MWEA020168](https://openairdocs.org/sdr/MWEA020168), Mar 15, 2002: LONGERON. DENTED. LONGERON 20 LEFT STATION 214 HAS DENT AND HAS CARRY OVER 5735. FABRICATED AND INSTALLED LONGERON SECTION. - [SDR MWEA020167](https://openairdocs.org/sdr/MWEA020167), Mar 15, 2002: LONGERON. CRACKED. LONGERON 2 RIGHT AT FUSELAGE STATION 1076 CRACKED AT END. -- REMOVED AND REPLACED WITH REPAIR, NEW LONGERON SPLICE. - [SDR MWEA020137](https://openairdocs.org/sdr/MWEA020137), Feb 22, 2002: FRAME. CRACKED. LEFT HAND LOWER RADOME GUIDE PIN HAS A 1.5 INCH CRACK EMANATING FROM ITS HOLE OUTWARD TO A RIVET. REPAIRED PER SRM 53-01-00 FIGURE 2 SHEET 3, DOUBLER ON AFT SID - [SDR MWEA010773](https://openairdocs.org/sdr/MWEA010773), May 17, 2001: FAN. FAILED. IN ROUTE TO DSM WEATHER RADAR FAILED. AIRCRAFT DIVERTED TO OMA. REMOVED AND REPLACED WEATHER RADAR RT AND RT FAN. - [SDR MWEA010669](https://openairdocs.org/sdr/MWEA010669), May 1, 2001: SKIN. CRACKED. AT STATION 980 RIGHT, THERE IS A SMALL CRACK EXTENDING FROM A FASTENER BETWEEN LONGERON 14 RIGHT AND 16 RIGHT. REMOVED DAMAGED AREA, FABRICATED FILLERS, DOUBLER - [SDR MWEA010664](https://openairdocs.org/sdr/MWEA010664), Apr 27, 2001: SEAT TRACK. DAMAGED. F/O''S AFT OUTBOARD SEAT TRACK LOCKING HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR STRAP. - [SDR MWEA010663](https://openairdocs.org/sdr/MWEA010663), Apr 27, 2001: SEAT TRACK. DAMAGED. CAPTAINS AFT SEAT TRACKS LOCKING HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR STRAP. - [SDR MWEA010662](https://openairdocs.org/sdr/MWEA010662), Apr 27, 2001: FRAME. CRACKED. STATION 980 RIGHT SIDE FRAME IS CRACKED ON LOWER LEG AT LONGERON 17 RIGHT. FABRICATED AND INSTALLED DOUBLERS. - [SDR MWEA010660](https://openairdocs.org/sdr/MWEA010660), Apr 27, 2001: SEAT TRACK. DAMAGED. CAPTAINS AFT, INBOARD SEAT TRACK LOCKING HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR STRAP. All 187: https://openairdocs.org/deregistered/N206ME-2005-01-21/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 20000619035799I](https://openairdocs.org/incident/20000619035799I), Jun 19, 2000: Doug DC932 (N206ME), Buffalo, NY. (-23)On July 19, 2000, at 1712 local, midwest express flight 6, a DC-9 N206ME, was enroute from laguardia airport, new york (lga) to milwaukee, WI (mke). The… - [Incident 19960326044729I](https://openairdocs.org/incident/19960326044729I), Mar 26, 1996: Doug DC932 (N206ME), Omaha, NE. Narrative: N206ME, a DC-9-32, being operated as midwest express airlines, inc., flight 58 enroute from milwaukee, WI, to Omaha, NE, shutdown the number 2… ## Other aircraft with N206ME - [Registered now](https://openairdocs.org/aircraft/N206ME): Textron T206H, S/N T20609816, built 2025 --- 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.