# N207ME: 1979 Mcdonnell Douglas DC-9-32, registration cancelled 2005-04-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 18, 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: 47794
- Year built: 1979
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, normal
- Airworthiness date: February 10, 1999
- Certificate issued: October 22, 2004
- Last registry action: October 22, 2004
- Mode S code: A1AD1C
- 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/N207ME
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=207ME
- Page: https://openairdocs.org/deregistered/N207ME-2005-04-18

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 (199, newest 50)

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

- [SDR MWEA030422](https://openairdocs.org/sdr/MWEA030422), Oct 12, 2003: SMOKE DETECTOR. INOPERATIVE. DURING FLIGHT THE MASTER WARNING CAME ON WITH NO OTHER ANNUNCIATIONS FOUND, NO POWER TO CARGO DETECTION PANEL. REMOVED AND REPLACED CARGO SMOKE DETECTORS, OHMED
- [SDR MWEA030420](https://openairdocs.org/sdr/MWEA030420), Oct 10, 2003: CONTROL PANEL. INOPERATIVE. MASTER WARNING CAME ON WITH NO OTHER ANNUNCIATIONS. SMOKE DETECTOR PANEL CIRCUIT BREAKER POPPED. INSPECTED OVERHEAD PANEL WIRING AND CARGO FIRE SUPPRESSION CONT
- [SDR MWEA030316](https://openairdocs.org/sdr/MWEA030316), Aug 18, 2003: RELAY. FAILED. AFTER ROTATION STICK SHAKERS AND STALL INDICATION LIGHT CAME ON. REMOVED AND REPLACED RIGHT RELAY.
- [SDR MWEA030311](https://openairdocs.org/sdr/MWEA030311), Aug 17, 2003: RELAY. FAILED. SLAT EXTEND LIGHT INOPERATIVE. REMOVED AND REPLACED RELAY.
- [SDR MWEA030310](https://openairdocs.org/sdr/MWEA030310), Aug 15, 2003: CONNECTOR. DEFECTIVE. STALL INDICATION FAILURE LIGHT CAME ON. REMOVED AND REPLACED FIRST OFFICER'S STICK SHAKER CONNECTOR.
- [SDR MWEA030309](https://openairdocs.org/sdr/MWEA030309), Aug 14, 2003: TRANSMITTER. FAULTY. STALL INDICATION FAILURE LIGHT CAME. REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER. PERFORMED ADJUSTMENT TEST OF STALL SYSTEM CHECKED GOOD.
- [SDR MWEA030303](https://openairdocs.org/sdr/MWEA030303), Aug 1, 2003: COMPUTER. MALFUNCTIONED. STALL INDICATION FAILURE ANNUCIATOR COMES OFF AND ON. REMOVED AND REPLACED STALL WARNING COMPUTER.
- [SDR MWEA030273](https://openairdocs.org/sdr/MWEA030273), Jul 10, 2003: FLEX LINE. CRACKED. AT 35,000 FEET RED MASTER WARNING LIGHT ILLUMINATED ALONG WITH THE RED CABIN ANNUCIATOR, MASK DROPPED -- REPLACED COALESER BAG AND CLEANED BOTH WATER OUTLET SCE
- [SDR MWEA030133](https://openairdocs.org/sdr/MWEA030133), Mar 17, 2003: WINDSHIELD. FAILED. FIRST OFFICER'S WINDSHIELD SHATTERED AT ALTITUDE (OUTER PANE). REMOVED AND REPLACED FIRST OFFICER'S WINDSHIELD.
- [SDR MWEA030122](https://openairdocs.org/sdr/MWEA030122), Feb 27, 2003: COMPUTER. MALFUNCTIONED. DURING TAXI, STALL INDICATION FAILURE LIGHT CAME ON. SWAPPED AOA SYSTEM, CHECKS GOOD. MARKED FAULTLY TRANSDUCER ON NR 1 SIDE, NOW IN NR 1 POSITION, RESET NR 2 C
- [SDR MWEA030052](https://openairdocs.org/sdr/MWEA030052), Feb 3, 2003: BULKHEAD. CRACKED. STATION 965 RIGHT, FORWARD PYLON, BULKHEAD WEB HAS TWO SMALL CRACKS EMANATING FROM SNAPS AT OUTBOARD SIDE NEXT TO LONGERON 11 AND LONGERON 10. CUT OUT DAMAGE, F
- [SDR MWEA030054](https://openairdocs.org/sdr/MWEA030054), Feb 3, 2003: BULKHEAD. CRACKED. AT APPROXIMATELY STATION 965 RIGHT FORWARD BULKHEAD WALL HAS A CRACK APPROXIMATELY SIX INCHES INBOARD OF OUTSIDE BULKHEAD ATTACH ANGLE, CRACK IS EMITTING FROM B
- [SDR MWEA030053](https://openairdocs.org/sdr/MWEA030053), Feb 3, 2003: BULKHEAD. CRACKED. STATION 965 RIGHT FORWARD PYLON BULKHEAD HAS A CRACK GOING INBOARD OF LIGHTENING HOLE AT Z = 50.0. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA030051](https://openairdocs.org/sdr/MWEA030051), Feb 3, 2003: RIB. CRACKED. LEFT NR 5 SLAT OUTBOARD RIB IS CRACKED AT LOWER AFT CORNER. REMOVED CRACKED RIB AND INSTALLED NEW RIB.
- [SDR MWEA030050](https://openairdocs.org/sdr/MWEA030050), Feb 3, 2003: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT FRAME STATION 180 SHEAR TIE BETWEEN LONGERON 1&2 RIGHT. FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED DOUBLER.
- [SDR MWEA020609](https://openairdocs.org/sdr/MWEA020609), Oct 8, 2002: INDICATOR. OUT OF ADJUST. BOTH CAPTAINS AND FIRST OFFICERS HORIZONTAL DIRECTION GYRO INDICATORS 30 DEGREES OFF CORRECT HEADING. RESLAVED BOTH RADIO MAGNETIC INDICATORS IAW MM 34-21-00. O
- [SDR MWEA020418](https://openairdocs.org/sdr/MWEA020418), Jun 4, 2002: TRANSCEIVER. MALFUNCTIONED. JUST AFTER DEPARTURE FROM MILWAUKEE RADAR INDICATOR BLANKED OUT. RECYCLED UNIT OFF AND ON DISPLAY CAME YELLOW ONLY AND FLICKERED DISPLAY WAS SAME ALL THE WAY TO
- [SDR MWEA020331](https://openairdocs.org/sdr/MWEA020331), May 12, 2002: SKIN. MISDRILLED. STATION 794 THROUGH 813, 16 HOLES WERE MISDRILLED IN BOTTOM 2 ROWS OF REPAIR ABOVE LONGERON 15 LEFT. -- FABRICATED AND INSTALLED REPAIR BUSHINGS AND PLUGS.
- [SDR MWEA020330](https://openairdocs.org/sdr/MWEA020330), May 12, 2002: SKIN. MISDRILLED. STATION 756 LEFT SIDE 9 HOLES ARE TOO CLOSE TO WINDOW BELT SPLICE. -- FABRICATED AND INSTALLED REPAIR BUSHINGS.
- [SDR MWEA020325](https://openairdocs.org/sdr/MWEA020325), May 12, 2002: LONGERON. TOOL DAMAGE. DRILL START ON BOTTOM OF LONGERON 30 STATION 269. -- FABRICATED AND INSTALLED LONGERON SPLICE.
- [SDR MWEA020061](https://openairdocs.org/sdr/MWEA020061), Jan 24, 2002: SKIN. DAMAGED. FUSELAGE SKIN DAMAGED AT APPROXIMATLEY STATION 237 LONGERON 30. -- REMOVED DAMAGE INSTALL FLUSH INTERNAL REPAIR PER SRM 53-04 FIGURE 38 SHEET 31 TELEX MWX.MKE-0
- [SDR MWEA011432](https://openairdocs.org/sdr/MWEA011432), Nov 15, 2001: WEB. CORRODED. CORROSION OF AFT PIT DOOR WEB AT STATION 937 JUST FORWARD OF LONGERONS 24 RIGHT TO 26 RIGHT AFT PIT. REMOVED CORROSION, FABRICATED AND INSTALLED WEB.
- [SDR MWEA011431](https://openairdocs.org/sdr/MWEA011431), Nov 14, 2001: ANGLE. CRACKED. ANGLE CRACKED AT FUSELAGE STATION 83.5 AT INBOARD END, 1.0625 INCHES IN LENGTH. STOPPED DRILL, FABRICATED AND INSTALLED REPAIR ANGLE.
- [SDR MWEA011430](https://openairdocs.org/sdr/MWEA011430), Nov 14, 2001: ANGLE. CRACKED. ANGLE AT FUSELAGE STATION 83.5 HAS A 1 INCH CRACK AT INBOARD END. FABRICATED, DRILLED AND INSTALLED REPAIR ANGLE.
- [SDR MWEA011429](https://openairdocs.org/sdr/MWEA011429), Nov 14, 2001: FRAME. CRACKED. FRAME IS CRACKED AT FUSELAGE STATION 83.5 AT 10 RIGHT 1 INCH IN LENGTH. REMOVED, STOPPED DRILL, FABRICATED AND INSTALLED REPAIR ANGLE.
- [SDR MWEA011428](https://openairdocs.org/sdr/MWEA011428), Nov 14, 2001: FRAME. CRACKED. FRAME AT FUSELAGE STATION 83.5 BY 10 LEFT IS CRACKED. LENGTH OF CRACK IS 1.00 INCH. STOPPED DRILL, FABRICATED AND INSTALLED REPAIR ANGLE.
- [SDR MWEA011427](https://openairdocs.org/sdr/MWEA011427), Nov 14, 2001: ANGLE. CORRODED. GOUGES AND CORROSION ON INNER SKIN AND ANGLE BRACKETS OF LOWER BACK SIDE OF DOOR JAMB AFT PIT STATION 945-889. BLENDED CORROSION AND GOUGES. FABRICATED AND INST
- [SDR MWEA011426](https://openairdocs.org/sdr/MWEA011426), Nov 14, 2001: FRAME. CORRODED. CORROSION ON J-CHANNEL FUSELAGE STATION 503 BETWEEN LONGERON 29 LEFT AND RIGHT. REMOVED CORROSION, CUT OUT DAMAGE IN FRAME. INSTALLED REPAIR SPLICE.
- [SDR MWEA011420](https://openairdocs.org/sdr/MWEA011420), Nov 6, 2001: SKIN. DENTED. LEFT HAND ELEVATOR CONTROL TAB UPPER SURFACE HAS A DENT BETWEEN THE NR 3 AND NR 4 HINGE POINTS, .75 BY .5 INCH. FABRICATED CORE, FILLER AND DOUBLER. HOT BONDED 
- [SDR MWEA011421](https://openairdocs.org/sdr/MWEA011421), Nov 6, 2001: SKIN. CORRODED. CORROSION ON INNER FUSELAGE SKIN ST STATION 889 AND 897 ON RIGHT HAND SIDE OF INTERCOSTAL AFT PIT. REMOVED, FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA011416](https://openairdocs.org/sdr/MWEA011416), Nov 1, 2001: STRAP. CORRODED. CORROSION ON STRAP IN LONGERON 23 LEFT AT STATION 945 AFT PIT. BLENDED, FABRICATED AND INSTALLED LONGERON.
- [SDR MWEA011415](https://openairdocs.org/sdr/MWEA011415), Nov 1, 2001: LONGERON. CORRODED. CORROSION ON LONGERON 21 LEFT AT STATION 990 AFT PIT. BLENDED, DRILLED, LOCATED AND INSTALLED NEW LONGERON.
- [SDR MWEA011414](https://openairdocs.org/sdr/MWEA011414), Oct 30, 2001: LONGERON. CRACKED. STATION 1087 LONGERON 7 RIGHT IS CRACKED. FABRICATED AND INSTALLED NEW LONGERON AND LONGERON SPLICE.
- [SDR MWEA011413](https://openairdocs.org/sdr/MWEA011413), Oct 30, 2001: LONGERON. CRACKED. STATION 1087 LONGERON 7 LEFT IS CRACKED. REMOVED, FABRICATED AND INSTALLED LONGERON.
- [SDR MWEA011411](https://openairdocs.org/sdr/MWEA011411), Oct 30, 2001: DOUBLER. CRACKED. TWO AREAS OF CRACKS AROUND FASTENERS ON WINDOW INNER DOUBLER AT STATION 654 LOWER RIGHT CORNER AND AT STATION 643 UPPER LEFT CORNER OF DOUBLER. FABRICATED AND I
- [SDR MWEA011130](https://openairdocs.org/sdr/MWEA011130), Aug 19, 2001: GYRO. FAILED. ON CLIMB OUT WX RADAR ATT FAILURE DISPLAYED INTERMITTENTLY (MOSTLY ON) IN ALL RANGES. VERIFIED BAD NR 1 VG REMOVED AND REPLACED SAME, RETURNED ANTENNA CONNECTOR
- [SDR MWEA011090](https://openairdocs.org/sdr/MWEA011090), Jul 18, 2001: RIB. GOUGED. GOUGE ON INBOARD SLAT SUPPORT TRACK STATION 480.871. REMOVED AND REPLACED RIB.
- [SDR MWEA011089](https://openairdocs.org/sdr/MWEA011089), Jul 18, 2001: SKIN. CRACKED. RIGHT WING SLAT DOOR CUT OUT BETWEEN NR 4 AND NR 5 SLAT SKIN IS CRACKED. TRIMMED OUT CRACK, INSTALLED FILLER AND DOUBLER.
- [SDR MWEA011087](https://openairdocs.org/sdr/MWEA011087), Jul 18, 2001: LONGERON. DAMAGED. LONGERON 6 RIGHT DAMAGED BETWEEN STATION 503 AND 522. BLENDED DAMAGED AND ATTACHED SPLICE PLATE OVER DAMAGE.
- [SDR MWEA010482](https://openairdocs.org/sdr/MWEA010482), Mar 28, 2001: PLATE. OUT OF ADJ. ON TAKE OFF ROLL, FORWARD STAIRWAY DOOR ANNUNCIATOR CAME ON. -- ADJUSTED SWITCH STRIKER PLATE, PRESSURIZED AIRCRAFT TO 7 PSI, LIGHT REMAINED OFF.
- [SDR MWEA010391](https://openairdocs.org/sdr/MWEA010391), Mar 25, 2001: PUMP. INOPERATIVE. LEFT HYDRAULIC QUANTITY DROPPED TO 1 1/2 QUARTS IN FLIGHT, LEFT ENGINE DRIVER HYDRAULIC PUMP LEAKING. REPLACE LEFT ENGINE DRIVEN HYDRAULIC PUMP.
- [SDR MWEA010364](https://openairdocs.org/sdr/MWEA010364), Mar 21, 2001: RECEIVER. INOPERATIVE. NR 2 NAV CIRCUIT BREAKER TRIPPED WHEN NR 2 ENGINE STARTED AND APU POWER SWITCHED TO ENGINE ELECTRICAL. REPLACED NR 2 NAV RECEIVER.
- [SDR MWEA010143](https://openairdocs.org/sdr/MWEA010143), Jan 31, 2001: FUEL CONTROL. INOPERATIVE. LEFT ENGINE WS SLOW TO SPOOL UP. REPLACED FUEL CONTROL UNIT ON LEFT ENGINE.
- [SDR MWEA010126](https://openairdocs.org/sdr/MWEA010126), Jan 29, 2001: STRINGER. DAMAGED. STRINGER 22 RIGHT DAMAGED IN RADIUS BEYOND LIMITS/BETWEEN XCW 20 RIGHT AND XCW 42 RIGHT. REMOVED AND REPLACED STRINGER REPAIR ANGLE.
- [SDR MWEA010130](https://openairdocs.org/sdr/MWEA010130), Jan 29, 2001: RIB. CORRODED. RIGHT WING RIB STATION 69 WEB AND LOWER T-EXTRUSION HAS AREAS OF MODERATE CORROSION FROM AFT SPAR TO STRINGER 17. REMOVED AND REPLACED T-CORD.
- [SDR MWEA010129](https://openairdocs.org/sdr/MWEA010129), Jan 29, 2001: BULKHEAD. CRACKED. LEFT FORWARD WEB ON BULKHEAD AT STATION 965 CRACKED NEAR SUBFLOOR, OUTBOARD OF NR 1 SEAT TRACK. FABRICATED AND INSTALLED WEB.
- [SDR MWEA010128](https://openairdocs.org/sdr/MWEA010128), Jan 29, 2001: FLOORBOARD. DAMAGED. HOLE IN SUBFLOOR, RIGHT SIDE JUST AFT OF STATION 945, OUTBOARD OF NR 4 SEAT TRACK. FABRICATED AND INSTALLED DOUBLERS.
- [SDR MWEA010127](https://openairdocs.org/sdr/MWEA010127), Jan 29, 2001: LONGERON. CRACKED. LONGERON 17 LEFT IS CRACKED AT STATION 965. FABRICATED AND INSTALLED LONGERON AND SPLICES.
- [SDR MWEA010125](https://openairdocs.org/sdr/MWEA010125), Jan 29, 2001: PANEL. CORRODED. WINDOW NR 19 LEFT BELT PANEL HAS CORROSION IN ZONE 1 (INTERNAL) ON RIGHT SIDE. REMOVED AND REPLACED WINDOW BELT.
- [SDR MWEA010124](https://openairdocs.org/sdr/MWEA010124), Jan 29, 2001: SKIN. CORRODED. RIGHT AILERON UPPER OUTBOARD SKIN JUST FORWARD OF STATIC WICK HAS A SPOT OF CORROSION. FABRICATED AND INSTALLED DOUBLER.

All 199: https://openairdocs.org/deregistered/N207ME-2005-04-18/reports.md

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