# N204ME: 1975 Mcdonnell Douglas DC-9-32, registration cancelled 2005-02-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 24, 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 series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 47680 - Year built: 1975 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 10, 1994 - Certificate issued: November 18, 2004 - Last registry action: November 18, 2004 - Mode S code: A1A1F7 - 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/N204ME - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=204ME - Page: https://openairdocs.org/deregistered/N204ME-2005-02-24 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 (188, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR MWEA020732](https://openairdocs.org/sdr/MWEA020732), Dec 14, 2002: FIRE DETECTOR. FAULTY. CARGO FIRE DETECTOR LOOP LIGHT CAME ON. REMOVED AND REPLACED THE METERING VALVE, BOTTLE ASSEMBLY, SQUIB DIVERTER AND SQUIB. - [SDR MWEA020425](https://openairdocs.org/sdr/MWEA020425), Jun 20, 2002: CIRCUIT BREAKER. TRIPPED. ON CLIMBOUT ALL LEFT MAIN FUEL TANK PUMP CIRCUIT BREAKERS POPPED. VISUALLY INSPECTED THE EXTERNAL POWER, GENERATOR AND CROSS TIE RELAYS. CHECKED CIRCUIT BREAKER - [SDR MWEA020328](https://openairdocs.org/sdr/MWEA020328), May 15, 2002: SWITCH. FAULTY. UPON GEAR RETRACTION RIGHT GEAR UNSAFE LIGHT STAYED ON WITH GEAR HANDLE UP. FOUND RIGHT MAIN GEAR DOWN SWITCH AT FAULT. REMOVED AND REPLACED SWITCH PER MM 32-60 - [SDR MWEA020329](https://openairdocs.org/sdr/MWEA020329), May 15, 2002: PROXIMITY SENSOR. FAILED. UPON GEAR RETRACTION RIGHT GEAR UNSAFE LIGHT (RED) STAYED ON WITH GEAR HANDLE UP. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR UP LIMIT PROX SENSOR IAW MM 32-60 - [SDR MWEA020322](https://openairdocs.org/sdr/MWEA020322), May 8, 2002: FRAME. UNSERVICEABLE. CUT AND REMOVED FRAME STATION 775 AT LONGERONS 27 LEFT THROUGH 27 RIGHT TO FACILITATE OTHER MAINTENANCE. -- CUT SHEAR TIE, REMOVED FRAME TO INTERCOSTAL CLIPS TO - [SDR MWEA020318](https://openairdocs.org/sdr/MWEA020318), May 8, 2002: DOOR FRAME. DENTED. FORWARD PIT, LOWER DOOR JAM WEB HAS SEVERAL SMALL DENTS AT STATION 418 AND 430. FABRICATED AND INSTALLED SECTION OF WEB AND DOUBLER. - [SDR MWEA020317](https://openairdocs.org/sdr/MWEA020317), May 8, 2002: FRAME. CORRODED. FRAME AT STATION 180 LONGERON 30 HAS AREA OF CORROSION. CUT OUT DAMAGED AREA CHANNEL AND FILLER. FABRICATED AND INSTALLED SPLICES AND FILLER. - [SDR MWEA020316](https://openairdocs.org/sdr/MWEA020316), May 8, 2002: VANE. GOUGED. GOUGE ON LEADING EDGE OF MIDDLE FIXED VANE. FABRICATED AND INSTALLED FIXED VANE REPAIR. - [SDR MWEA020315](https://openairdocs.org/sdr/MWEA020315), May 8, 2002: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT STATION 352 LONGERON 28 RIGHT TO LONGERON 29 LEFT. FABRICATED AND INSTALLED SPLICE. - [SDR MWEA020314](https://openairdocs.org/sdr/MWEA020314), May 8, 2002: SPLICE. CORRODED. AFT PIT CORROSION ON LONGERON 29 LEFT SPLICE IN TWO LOCATIONS STATION 836 AND 844. REMOVED AND REPLACED SPLICE. - [SDR MWEA020313](https://openairdocs.org/sdr/MWEA020313), May 8, 2002: FRAME. CORRODED. CORROSION ON TOP OF STATION 965 ABOVE LONGERON 30. REMOVED AND REPLACED FRAME SEGMENT. FABRICATED AND INSTALLED SPLICES. - [SDR MWEA020312](https://openairdocs.org/sdr/MWEA020312), May 8, 2002: SPLICE. CORRODED. AFT PIT CORROSION ON LONGERON 28 LEFT SPLICE AT STATION 828. REMOVED AND REPLACED SPLICE. - [SDR MWEA020311](https://openairdocs.org/sdr/MWEA020311), May 8, 2002: FITTING. CORRODED. AFT PIT LONGERON 30 END FITTING AT STATION 756 HAS BARE METAL AND POSSIBLE LIGHT CORROSION PRESENT. REMOVED AND REPLACED LONGERON AND INSTALLED CORRECT LENGTH H - [SDR MWEA020267](https://openairdocs.org/sdr/MWEA020267), Apr 23, 2002: SKIN. TOOL DAMAGE. AFT PIT SKIN HAS TOOLING DAMAGE @ FS 948 ABOVE LONGERON 26 RIGHT. -- FABRICATED AND INSTALLED REPAIR DOUBLER. - [SDR MWEA020282](https://openairdocs.org/sdr/MWEA020282), Feb 26, 2002: FLOORBOARD. DAMAGED. CABIN FLOORBOARD B-8 HAS DAMAGE TO THE FORWARD EDGE. FABRICATED AND INSTALLED SKIN AND HAT CHANNELS. - [SDR MWEA011248](https://openairdocs.org/sdr/MWEA011248), Sep 6, 2001: ENGINE. OVERTEMP. ON TAKEOFF IN OMA AT A REDUCED POWER TAKEOFF OF 1.94 EPR THE RIGHT ENGINE EGT ROSE TO 600 DEGREES FOR 5 SECONDS BEFORE POWER COULD BE REDUCED. AIRCRAFT TO REMAI - [SDR MWEA011075](https://openairdocs.org/sdr/MWEA011075), Jul 24, 2001: FITTING. WORN. DURING CLIMB 17,000 FEET, GEAR DOOR LIGHT CAME ON, SO MAINTENANCE CONTROL DIVERTED AIRCRAFT TO MILWAUKEE MAINTENANCE BASE. REMOVED AND REPLACED LEFT AND RIGHT M - [SDR MWEA010714](https://openairdocs.org/sdr/MWEA010714), May 1, 2001: SENSOR. INOPERATIVE. AFTER TAKEOFF FROM MILWAUKEE WITH GEAR UP, GEAR DOWN OPEN LIGHT IS ON. RETURNED TO MILWAUKEE. NOTE: WITH GEARDOWN AND THREE GREEN, GEAR DOOR OPEN LIGHT WAS OFF, - [SDR MWEA010668](https://openairdocs.org/sdr/MWEA010668), May 1, 2001: SKIN. CORRODED. FUSELAGE SKIN UNDER AFT CARGO DOOR EXTERIOR SKUFF PLATE IS CORRODED. REMOVED CORROSION, FABRICATED, LOCATED, DRILL AND INSTALLED REPAIR DOUBLERS AND FILLER. - [SDR MWEA010655](https://openairdocs.org/sdr/MWEA010655), Apr 25, 2001: LONGERON. CORRODED. LIGHT CORROSION, LONGERON 30, STATION 917. REMOVED AND REPLACED LONGERON. - [SDR MWEA010654](https://openairdocs.org/sdr/MWEA010654), Apr 25, 2001: SKIN. CRACKED. RUDDER SKIN IS CRACKED AT RIB NR 3 LEFT SIDE. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER. - [SDR MWEA010653](https://openairdocs.org/sdr/MWEA010653), Apr 25, 2001: SPLICE. CORRODED. LONGERON NR 30 SPLICE AT STATION 955 IS CORRODED. REMOVED AND REPLACED LONGERON SPLICE. - [SDR MWEA010652](https://openairdocs.org/sdr/MWEA010652), Apr 25, 2001: DOUBLER. CRACKED. LONGERON NR 30 STATION 803-995. TWO DOUBLERS ARE CRACKED. FABRICATED AND INSTALLED DOUBLERS. - [SDR MWEA010651](https://openairdocs.org/sdr/MWEA010651), Apr 25, 2001: SKIN. CRACKED. AFT CARGO SKIN IS CRACKED AT STATION 803 BETWEEN LONGERON 29 RIGHT AND 30, FROM SKIN SPLICE FORWARD TO THE FASTENER. FABRICATED AND INSTALLED REPAIR DOUBLER, FI - [SDR MWEA010650](https://openairdocs.org/sdr/MWEA010650), Apr 25, 2001: STRAP. DAMAGED. BUTT SPLICE STRAP IS DAMAGED. STRAP IS LOCATED IN AFT BAG PIT STATION 823 LONGERON 26 LEFT THROUGH 26 RIGHT. FABRICATED AND INSTALLED BUTT SPLICE DOUBLER. - [SDR MWEA010649](https://openairdocs.org/sdr/MWEA010649), Apr 25, 2001: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT STATION 945, BETWEEN LONGERON 14 AND 15 LEFT. FABRICATED AND INSTALLED FORMER. - [SDR MWEA010648](https://openairdocs.org/sdr/MWEA010648), Apr 25, 2001: FRAME. CORRODED. FRAME CORRODED, STATION 852, LONGERON 30, AFT SIDE OF FRAME. FABRICATED AND INSTALLED FRAME REPAIR PARTS. - [SDR MWEA010647](https://openairdocs.org/sdr/MWEA010647), Apr 25, 2001: FRAME. CORRODED. FRAME CORRODED, STATION 833, LONGERON 30, AFT SIDE OF FRAME. FABRICATED AND INSTALLED FRAME REPAIR PARTS. - [SDR MWEA010646](https://openairdocs.org/sdr/MWEA010646), Apr 25, 2001: SPLICE. CORRODED. LONGERON 30, SPLICE CORRODED, STATION 795-814. BLENDED CORROSION ON LONGERON. BLEND IS WITHIN LIMITS. MAINTENANCE REMOVED AND REPLACED SPLICE. - [SDR MWEA010645](https://openairdocs.org/sdr/MWEA010645), Apr 25, 2001: SKIN. CRACKED. RIGHT MAIN LANDING GEAR DOOR CRACKED AT UPPER FORWARD INBOARD CORNER. FABRICATED AND INSTALLED REPAIR SHIM AND REPAIR DOUBLER. - [SDR MWEA010644](https://openairdocs.org/sdr/MWEA010644), Apr 25, 2001: PAN. CRACKED. FORWARD CARGO DOOR HAS A CRACK ON AFT SIDE OF OUTER PAN BETWEEN 2 LOWER STOP PADS. FABRICATED AND INSTALLED REPAIR DOUBLER. - [SDR MWEA010628](https://openairdocs.org/sdr/MWEA010628), Apr 20, 2001: SPAR CAP. DAMAGED. ELEVATOR S/N ESA5 REQUIRED A SPAR CAP REPLACEMENT TO CLEAR CARRY OVER 2401. REMOVED AND INSTALLED NEW SPAR. - [SDR MWEA010626](https://openairdocs.org/sdr/MWEA010626), Apr 19, 2001: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT STATION 965, BETWEEN LONGERON 13 AND 14 RIGHT. FABRICATED AND INSTALLED SHEAR TIE REPAIR. - [SDR MWEA010625](https://openairdocs.org/sdr/MWEA010625), Apr 19, 2001: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT STATION 980, BELOW LONGERON 14 RIGHT AND ABOVE 16 RIGHT. FABRICATED AND INSTALLED -45 DOUBLER, L-ANGLES, STRAPS, AND RADIUS FILLERS. - [SDR MWEA010624](https://openairdocs.org/sdr/MWEA010624), Apr 19, 2001: SHEAR TIE. CRACKED. REPAIR DOUBLER CRACKED ON SHEAR TIE REPAIR AT STATION 980 AND BELOW LONGERON 14 LEFT. REMOVED AND REPLACED SHEAR TIE. FABRICATED AND INSTALLED LONGERON TO FRAME - [SDR MWEA010623](https://openairdocs.org/sdr/MWEA010623), Apr 19, 2001: BULKHEAD. CHAFED. PYLON FORWARD BULKHEAD, AT STATION 965, WEB THAT CONNECTS RIGHT AND LEFT BULKHEADS TOGETHER IS CHAFED IN BOTH CORNERS. FABRICATED AND INSTALLED STACKED ANGLE RE - [SDR MWEA010622](https://openairdocs.org/sdr/MWEA010622), Apr 19, 2001: WEB. CRACKED. FOUND 2 CRACKED NUT PLATE HOLES IN SUBFLOOR BENEATH THE NR 4 SEAT TRACK BETWEEN STATION 200 - 218. FABRICATED AND INSTALLED REPAIR DOUBLER. - [SDR MWEA010621](https://openairdocs.org/sdr/MWEA010621), Apr 19, 2001: FRAME. CRACKED. FRAME CORRODED, STATION 917, LONGERON 30. FOUND CRACK JUST AFT OF OUTBOARD FASTENER HOLE. FABRICATED AND INSTALLED FRAME SPLICES AND DOUBLERS. - [SDR MWEA010620](https://openairdocs.org/sdr/MWEA010620), Apr 19, 2001: FRAME. DAMAGED. DAMAGE ON FRAME RADIUS STATION 207 AFT SIDE LONGERON 17 LEFT. FABRICATED AND INSTALLED REPAIR ANGLES. - [SDR MWEA010619](https://openairdocs.org/sdr/MWEA010619), Apr 19, 2001: DOUBLER. CRACKED. DOUBLER PLATE WAS CRACKED AT STATION 975 RIGHT LAVATORY AREA ABOVE LONGERON 17 RIGHT. REMOVED DOUBLER, FABRICATED, DRILLED, AND INSTALLED NEW DOUBLER. - [SDR MWEA010618](https://openairdocs.org/sdr/MWEA010618), Apr 19, 2001: LONGERON. CRACKED. LONGERON 13 RIGHT WAS CRACKED AT STATION 965. REMOVED DAMAGED SECTION, FABRICATED, DRILLED AND INSTALLED NEW SECTION. - [SDR MWEA010617](https://openairdocs.org/sdr/MWEA010617), Apr 19, 2001: LONGERON. CRACKED. LONGERON 17 RIGHT WAS CRACKED AT STATION 965. REMOVED DAMAGED SECTION, FABRICATED DRILLED, INSTALLED NEW SECTION. - [SDR MWEA010616](https://openairdocs.org/sdr/MWEA010616), Apr 19, 2001: LONGERON. CRACKED. LONGERON 17 LEFT WAS CRACKED AT STATION 980 UPPER AND LOWER ATTACH POINTS. REMOVED DAMAGED SECTION, FABRICATED, DRILLED AND INSTALLED NEW LONGERON. - [SDR MWEA010615](https://openairdocs.org/sdr/MWEA010615), Apr 19, 2001: WEB. DAMAGED. CABIN SUBFLOOR AT STATION 200 BETWEEN SEAT TRACKS 3 AND 4 HAD A DRILL STOP. FABRICATED, DRILLED, INSTALLED REPAIR DOUBLER. - [SDR MWEA010614](https://openairdocs.org/sdr/MWEA010614), Apr 19, 2001: WEB. CRACKED. SUBFLOOR WAS CRACKED AT STATION 218 OUTBOARD OF NR 4 SEAT TRACK NEAR PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR, STOP DRILLED CRACK, FABRICATED NEW REPAIR DOUBLER - [SDR MWEA010613](https://openairdocs.org/sdr/MWEA010613), Apr 19, 2001: FLOORBEAM. GOUGED. GOUGE ON BOTTOM OF FLOORBEAM AT STATION 408, 2 INCHES RIGHT OF CENTER INTERCOSTAL. BLENDED GOUGE, FABRICATED, LOCATED, DRILLED, AND INSTALLED REPAIR. - [SDR MWEA010612](https://openairdocs.org/sdr/MWEA010612), Apr 19, 2001: FRAME. CRACKED. AT RIGHT KEEL AREA, FUSELAGE FRAME STATION 617 WAS CRACKED AT OUTBOARD ATTACH. REMOVED, LOCATED, DRILLED, AND INSTALLED NEW FRAME. - [SDR MWEA010611](https://openairdocs.org/sdr/MWEA010611), Apr 19, 2001: WEB. CORRODED. SUBFLOOR AT STATION 218 BETWEEN CENTER LINE AND NR 3 SEAT TRACK HAD AREAS OF MODERATE CORROSION. BLENDED, REMOVED CORROSION, FABRICATED, LOCATED, DRILLED, AND I - [SDR MWEA010610](https://openairdocs.org/sdr/MWEA010610), Apr 19, 2001: SEAT TRACK. CORRODED. NR SEAT TRACK HAD SEVERAL AREAS OF MODERATE CORROSION AND BARE METAL AT STATION 200 - 229. REMOVED SEAT TRACK, CUT, FORMED, LOCATED, DRILLED AND INSTALLED NEW S - [SDR MWEA010609](https://openairdocs.org/sdr/MWEA010609), Apr 19, 2001: WEB. CORRODED. CABIN SUBFLOOR BETWEEN CENTERLINE AND RIGHT FLOOR SUPPORT FORWARD OF NR 4 SEAT TRACK HAD AREAS OF CHAFES AND LIGHT CORROSION. BLENDED, REMOVED CORROSION, FABRIC All 188: https://openairdocs.org/deregistered/N204ME-2005-02-24/reports.md ## FAA accident and incident reports (1) 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 19950621021179I](https://openairdocs.org/incident/19950621021179I), Jun 21, 1995: Doug DC931 (N204ME), Omaha, NE. Gear warning light at retraction. Returned. Left main gear proximity sensor at fault. Replaced. ## Other aircraft with N204ME - [Registered now](https://openairdocs.org/aircraft/N204ME): Socata TB20, S/N 909, built 1989 --- 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.