# N212ME: 1976 Mcdonnell Douglas DC-9-32, registration cancelled 2003-12-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 17, 2003
- Exported to: Republic of the Congo
- 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: 47701
- Year built: 1976
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 24, 1998
- Certificate issued: April 24, 2003
- Last registry action: April 28, 2003
- Mode S code: A1C208
- Owner when cancelled: [Professional Maintenance Services](https://openairdocs.org/faa-owner/PROFESSIONAL%20MAINTENANCE%20SERVICES)
- Location: [Hazelton, PA](https://openairdocs.org/faa-place/PA/Hazelton)
- Owner type: Partnership
- Owner's area on the map: 40.9544° N, 76.0460° W: Placed by OpenAirDocs at the center of ZIP code 18202, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N212ME
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=212ME
- Page: https://openairdocs.org/deregistered/N212ME-2003-12-17

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-9-32: https://openairdocs.org/model/mcdonnell-douglas-dc-9-32.md

## Service difficulty reports (267, newest 50)

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

- [SDR MWEA020699](https://openairdocs.org/sdr/MWEA020699), Nov 15, 2002: CSD. MALFUNCTIONED. CREW NOTICED RIGHT CSD LOW OIL PRESSURE LIGHT CAME ON. REMOVED AND REPLACED RIGHT CONSTANT SPEED DRIVE UNIT.
- [SDR MWEA020463](https://openairdocs.org/sdr/MWEA020463), Jul 17, 2002: SKIN. DENTED. FUSELAGE SKIN DENTED AT STATION 999 AFT OF LONGERON 27 RIGHT. -- CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA020462](https://openairdocs.org/sdr/MWEA020462), Jul 17, 2002: FRAME. CRACKED. LOWER FRAME ASSY STATION 1000 IS CRACKED, INLINE WITH LONGERON 28 RIGHT. -- INSTALLED REPAIR ANGLE.
- [SDR MWEA020458](https://openairdocs.org/sdr/MWEA020458), Jul 16, 2002: TEE FITTING. DENTED. AFT PRESSURE BULKHEAD TEE WAS DENTED BETWEEN LONGERONS 29 RIGHT AND 28 RIGHT. REMOVED TEE SECTION FROM LONGERON AND INSTALLED NEW TEE SECTION AND REPAIR SPLICES
- [SDR MWEA020443](https://openairdocs.org/sdr/MWEA020443), Jul 6, 2002: CONTROLLER. OUT OF ADJUST. AT 31,000 FEET THE AIRCRAFT LOST PRESSURE AND COULD NOT CONTROL IN AUTO OR MANUAL. MASKS AUTOMATICALLY DEPLOYED. PERFORMED ADJUSTMENT / TEST CABIN PRESSURE CONT
- [SDR MWEA020031](https://openairdocs.org/sdr/MWEA020031), Jan 7, 2002: BRACKET. CRACKED. AFT CARGO DOOR BEAM #3 END FITTING CRACKED, AFT SIDE OF DOOR. -- REMOVED FITTING AND ANGLE SUPPORT BRACKET. LOCATED AND DEBURRED NEW FITTING AND ANGLE SUPPORT B
- [SDR MWEA020030](https://openairdocs.org/sdr/MWEA020030), Jan 7, 2002: PAN. CRACKED. AFT CARGO DOOR INNER PAN IS CRACKED UNDER NUMBER 2 AFT. WORKING CORROSION NRI 12570. -- FABRICATED REPAIR ANGLE AND INSTALLED REPAIR ANGLE AND FITTING.
- [SDR MWEA020029](https://openairdocs.org/sdr/MWEA020029), Jan 7, 2002: FITTING. CRACKED. AFT CARGO DOOR BEAM NR 4 END FITTING CRACKED, AFT SIDE OF DOOR. REMOVED AND REPLACED NEW FITTING.
- [SDR MWEA020028](https://openairdocs.org/sdr/MWEA020028), Jan 7, 2002: DOUBLER. CRACKED. RIGHT AFT PYLON WEB DOUBLER P/N 9912246 AT STATION 1038 HAS CRACKS EMINATING FROM THE UPPER STRAP ATTACHMENT HOLES. -- FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA020027](https://openairdocs.org/sdr/MWEA020027), Jan 7, 2002: WEB. THE AFT PYLON BULKHEAD HAS OVERSIZED HOLE WHERE THE UPPER PYLON STRAP ATTACHES TO IT. -- FABRICATED AND INSTALLED WEB AND DOUBLERS.
- [SDR MWEA020026](https://openairdocs.org/sdr/MWEA020026), Jan 7, 2002: WEB. OVERSIZED. RIGHT AFT PYLON SPAR WEB (P/N 9958154-21) UPPER HOLES ARE OVERSIZED. -- FABRICATED AND INSTALLED WEB.
- [SDR MWEA020025](https://openairdocs.org/sdr/MWEA020025), Jan 7, 2002: SPAR. DAMAGED. REMOVE PYLON SPAR WEB (P/N 9958154-29). THE WEB HAS OVERSIZED HOLES. REMOVED DOUBLER. FABRICATED NEW DOUBLER. INSTALLED WEB.
- [SDR MWEA020024](https://openairdocs.org/sdr/MWEA020024), Jan 7, 2002: CHANNEL. CORRODED. CORROSION AROUND AND ON NUT PLATES LOCATED AT STATION 351 ON U-CHANNEL THAT'S RIVETED TO FLOORBEAM APPROXIMATELY 28 INCHES AND 33 INCHES TO THE LEFT OF CENTER. 
- [SDR MWEA020023](https://openairdocs.org/sdr/MWEA020023), Jan 7, 2002: CHANNEL. CORRODED. CORROSION AROUND AND ON NUT PLATES LOCATED ON U-CHANNEL THAT'S ATTACHED TO FLOORBEAM 427 ABOVE FORWARD AT CARGO DOOR OPENING. FABRICATED AND INSTALLED U-CHANNEL
- [SDR MWEA020022](https://openairdocs.org/sdr/MWEA020022), Jan 7, 2002: FRAME. DAMAGED. STATION 1038 RIGHT FRAME CAP (P/N 9912246-103) HAS TWO OVERSIZED HOLES WHERE THE AFT UPPER ENGINE PYLON ATTACHES. REPAIRED PER TELEX MWX-ORD-01-00570H 19 DEC 20
- [SDR MWEA020021](https://openairdocs.org/sdr/MWEA020021), Jan 7, 2002: FRAME. DAMAGED. STATION 1038 RIGHT FRAME CAP (P/N 9912246-105) HAS TWO OVERSIZED HOLES WHERE THE AFT UPPER ENGINE PYLON STRAP ATTACHES. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA020020](https://openairdocs.org/sdr/MWEA020020), Jan 7, 2002: FRAME. CRACKED. KEEL AREA FRAME AT STATION 637 IS CRACKED AT OUTBOARD END ON LEFT SIDE. FABRICATED AND INSTALLED REPAIR ANGLE.
- [SDR MWEA020019](https://openairdocs.org/sdr/MWEA020019), Jan 7, 2002: WEB. CORRODED. WEB AT GALLEY SERVICE DOOR, FROM STATION 150 TO STATION 200, IS CORRODED AT FORWARD SIDE OF SERVICE DOOR OPENING AND AFT SIDE OF SERVICE DOOR OPENING. FABRICATE
- [SDR MWEA020018](https://openairdocs.org/sdr/MWEA020018), Jan 7, 2002: LONGERON. CHAFED. LONGERON 22 RIGHT HAS CHAFE DAMAGE ON UPPER LEG (VIEW THROUGH RIGHT THRUST REVERSER BY PASS DOOR). FABRICATED AND INSTALLED LONGERON SECTION, LONGERON SPLICE AN
- [SDR MWEA020017](https://openairdocs.org/sdr/MWEA020017), Jan 7, 2002: FRAME. CRACKED. FUSELAGE FORMER CRACKED BELOW LONGERON 15 RIGHT VIEW FROM FORWARD SIDE OF FUSELAGE FRAME 1038. REMOVED AND REPLACED FORMER.
- [SDR MWEA020014](https://openairdocs.org/sdr/MWEA020014), Jan 7, 2002: FLOOR SUPPORT. CORRODED. FLOORBOARD SUPPORT AT STATION 200 HAS CORROSION BEYOND LIMITS LOCATED BETWEEN NR 3 SEAT TRACK AND NR 4 SEAT TRACK. REMOVED AND REPLACED FLOOR SUPPORT.
- [SDR MWEA020013](https://openairdocs.org/sdr/MWEA020013), Jan 7, 2002: FLOOR SUPPORT. CORRODED. FLOORBOARD SUPPORT AT STATION 200 HAS CORROSION BEYOND LIMITS LOCATED BETWEEN CENTER FLOOR SUPPORT AND NR 3 SEAT TRACK. REMOVED AND REPLACED FLOOR SUPPORT.
- [SDR MWEA020012](https://openairdocs.org/sdr/MWEA020012), Jan 4, 2002: FLOOR SUPPORT. CORRODED. FLOORBOARD SUPPORT LOCATED JUST FORWARD OF NUMBER 4 SEAT TRACK FROM STATION 160 TO 200 HAS TWO AREAS OF CORROSION ON TOP SIDE AND SEVERAL AREAS OF CORROSION ON 
- [SDR MWEA020010](https://openairdocs.org/sdr/MWEA020010), Jan 4, 2002: FRAME. CHAFED. FUSELAGE FRAME 1059 HAS CHAFE DAMAGE ON UPPER LEG AT LONGERON 21 RIGHT. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED, FIT, DRILLED AND INSTALLED REPAIR.
- [SDR MWEA020009](https://openairdocs.org/sdr/MWEA020009), Jan 4, 2002: WEB. DAMAGED. SUBFLOOR HAS SEVERAL AREAS OF BARE METAL AND RIVET HEAD WEAR MARKS FROM STATION 200 TO 218 BETWEEN NUMBER 2 SEAT TRACK AND CENTER FLOOR SUPPORT. FABRICATED AND 
- [SDR MWEA020008](https://openairdocs.org/sdr/MWEA020008), Jan 4, 2002: SEAT TRACK. CORRODED. NUMBER 3 SET TRACK HAS HEAVY CORROSION FROM STATION 218 TO 248. CUT AND REMOVED SEAT TRACK. LOCATED, DRILLED AND INSTALLED SEAT TRACK.
- [SDR MWEA020007](https://openairdocs.org/sdr/MWEA020007), Jan 4, 2002: FLOOR SUPPORT. CORRODED. CENTER FLOOR SUPPORT HAS LIGHT CORROSION AROUND SEVERAL FASTENER HOLES FROM STATION 192 TO 200. REMOVED CENTER FLOOR SUPPORT. DRILLED, TRIMMED AND INSTALLED NEW
- [SDR MWEA020006](https://openairdocs.org/sdr/MWEA020006), Jan 4, 2002: SKIN. CRACKED. STATION 1010, RIGHT HAND SIDE FUSELAGE SKIN HAS A SMALL CRACK ORIGINATING FROM RIVET BETWEEN LONGERON 14 RIGHT AND 16 RIGHT. CUT OUT CRACK. FABRICATED AND INSTA
- [SDR MWEA020002](https://openairdocs.org/sdr/MWEA020002), Jan 4, 2002: PANEL. DELAMINATED. RIGHT WING OUTBOARD TRAILING EDGE PANEL HAS APPROXIMATELY 80 SQUARE INCHES OF DELAMINATION ON THE TOP AREA, INCLUDES MOST OF THE TRAILING EDGE. REMOVED, LOCATED
- [SDR MWEA011487](https://openairdocs.org/sdr/MWEA011487), Dec 17, 2001: LONGERON. CHAFED. KEEL AREA LONGERON 27 LEFT HAS A CHAFE AT STATION 655 AB5. REMOVED, DRILLED AND INSTALLED LONGERON.
- [SDR MWEA011490](https://openairdocs.org/sdr/MWEA011490), Dec 6, 2001: LONGERON. CRACKED. CABIN LONGERON 4 LEFT IS CRACKED AT FRAME STATION 200. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SECTION OF LONGERON.
- [SDR MWEA011489](https://openairdocs.org/sdr/MWEA011489), Dec 6, 2001: LONGERON. CRACKED. CABIN LONGERON 4 LEFT IS CRACKED AT FRAME STATION 160. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SECTION OF LONGERON.
- [SDR MWEA011352](https://openairdocs.org/sdr/MWEA011352), Sep 24, 2001: CONTROL BOX. FAULTY. IN CRUISE NOSE GEAR UNSAFE LIGHT CAME ON, RIGHT GEAR HANDLE UP, RED LIGHT ON IN CRUISE AND APPROACH, LOWERED GEARS, NOSE GEAR RED STAYED ON. QRH PERFORMED, CONF
- [SDR MWEA011272](https://openairdocs.org/sdr/MWEA011272), Sep 15, 2001: WEB. CHAFED. FOUND MINOR CHAFE ON WEB IN NOSE WELL. -- BLENDED CHAFE AND REPAIRED WITH DOUBLER REPAIR.
- [SDR MWEA011240](https://openairdocs.org/sdr/MWEA011240), Sep 1, 2001: LIGHT. DEPARTED. AFTER TAKEOFF, PAX REPORTED RIGHT LOGO LIGHT BULB AND LOVER ASSY DEPARTED AIRCRAFT. CREW VERIFIED STRAY WIRES VISIBLE FROM CABIN AT WING TIP. REPLACED LOGO LIGH
- [SDR MWEA011001](https://openairdocs.org/sdr/MWEA011001), Jun 26, 2001: PRESSURE SWITCH. FAILED. ON APPROACH TO MILWAUKEE, RIGHT ENGINE OIL PRESSURE LOW LIGHT CAME ON, OIL PRESSURE WAS 42 PSI, OIL TEMP 110 DEGREES CELCIUS. SHUT OFF ENGINE, ENGINE WINDMILLED
- [SDR MWEA010580](https://openairdocs.org/sdr/MWEA010580), Apr 13, 2001: SWITCH. INOPERATIVE. TAKE OFF WARNING HORN CAME ON AT 105 KNOTS DURING TAKE OFF ROLL. ABORTED TAKE OFF. MAINTENANCE FOUND PARKING BRAKE SWITCH INOPERATIVE AND REPLACED SWITCH.
- [SDR MWEA010512](https://openairdocs.org/sdr/MWEA010512), Apr 1, 2001: TRANSDUCER. INOPERATIVE. STALL INDICATOR FAILURE ANNUNCIATOR CAME ON AT CLIMBOUT WITH INTERMEDIATE WINDSHEAR INOP LIGHT. REPLACED LEFT ANGLE OF ATTACH VANE.
- [SDR MWEA010161](https://openairdocs.org/sdr/MWEA010161), Feb 19, 2001: CLIP. BROKEN. TAIL CONE AFT INTERIOR HANDLE HAS A BROKEN CLIP AND FAILS PULL CHECK (25 - 35 LBS). REMOVED AND REPLACED CLIP.
- [SDR MWEA010166](https://openairdocs.org/sdr/MWEA010166), Feb 19, 2001: SKIN. DENTED. RUDDER LEFT SKIN HAS .75 INCH BY .75 INCH DENT .010 INCH DEEP AT ZR 28.936. REMOVED AND REPLACED DOUBLER.
- [SDR MWEA010165](https://openairdocs.org/sdr/MWEA010165), Feb 19, 2001: SKIN. DAMAGED. AFT CARGO BAG FUSELAGE SKIN HAS MECHANICAL DAMAGE FROM STATION 876 - STATION 890 BETWEEN LONGERON 23 THRU LONGERON 22 LEFT. FABRICATED AND INSTALLED REPAIR DOUB
- [SDR MWEA010164](https://openairdocs.org/sdr/MWEA010164), Feb 19, 2001: BELT. CORRODED. NR 20 LEFT WINDOW FRAME CORRODED IN BOTH LOWER, INNER CORNERS. REMOVED AND REPLACED WINDOW BELT.
- [SDR MWEA010162](https://openairdocs.org/sdr/MWEA010162), Feb 19, 2001: PANEL. DENTED. LEFT WING UPPER TRAILING EDGE PANEL IS DENTED, STATION 419, 4 INCHES AFT OF REAR SPAR. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER.
- [SDR MWEA010160](https://openairdocs.org/sdr/MWEA010160), Feb 19, 2001: RING. CRACKED. LEFT WINDOW RING CRACKED, STATION 639 - 658. REMOVED AND REPLACED WINDOW RING.
- [SDR MWEA010159](https://openairdocs.org/sdr/MWEA010159), Feb 19, 2001: SKIN. DENTED. FUSELAGE SKIN DENTED STATION 980, 2 INCHES BELOW LONGERON 2 RIGHT. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA010154](https://openairdocs.org/sdr/MWEA010154), Feb 13, 2001: WEB. CRACKED. VERTICAL WEB CRACKED IN RIGHT PYLON OUTBOARD OF 13TH STRINGER. BLEED NUT ACCESSIBLE THROUGH PANEL 8204A. FABRICATED AND INSTALLED REPAIR DOUBLERS.
- [SDR MWEA010153](https://openairdocs.org/sdr/MWEA010153), Feb 13, 2001: LONGERON. CORRODED. CORROSION ON LONGERON 12 LEFT AT STATION 1104. FABRICATED AND INSTALLED LONGERON AND ANGLE.
- [SDR MWEA010152](https://openairdocs.org/sdr/MWEA010152), Feb 13, 2001: FLOOR PANEL. CRACKED. FLOOR PANEL E-6 IS CRACKED ON AFT OUTBOARD CORNER. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA010151](https://openairdocs.org/sdr/MWEA010151), Feb 13, 2001: ANGLE. CRACKED. CRACK AT STATION 1121 AT LONGERON 17 RIGHT. DRILLED AND INSTALLED REPAIR ANGLES.
- [SDR MWEA010148](https://openairdocs.org/sdr/MWEA010148), Feb 9, 2001: FITTING. CRACKED. FITTING CRACKED AT VERTICAL WEB AT LEFT ENGINE PYLON STRUCTURE, VIEWED THROUGH PANEL 8105A. REMOVED AND REPLACED FITTING.

All 267: https://openairdocs.org/deregistered/N212ME-2003-12-17/reports.md

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