# N12064: Mcdonnell-Douglas DC-10-30, registration cancelled 2002-06-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 5, 2002 - Status when cancelled: Valid registration - Airframe: [Mcdonnell-Douglas DC-10-30](https://openairdocs.org/model/mcdonnell-douglas-dc-10-30) (registry code 3023501) - Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) (OpenAirDocs) - Serial number: 47862 - Type of aircraft: Fixed wing multi engine - Certificate issued: March 25, 2002 - Last registry action: March 25, 2002 - Mode S code: A056F9 - Owner when cancelled: [Memphis Group Inc](https://openairdocs.org/faa-owner/MEMPHIS%20GROUP%20INC) - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Corporation - Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N12064 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12064 - Page: https://openairdocs.org/deregistered/N12064-2002-06-05 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-10-30: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30.md ## Service difficulty reports (31) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0100926](https://openairdocs.org/sdr/CALA0100926), Sep 29, 2001: WARNING SYSTEM. MALFUNCTIONED. A FORWARD CARGO FIRE WARNING WAS INDICATED AT 10,000 FEET ON APPROACH TO HNL. BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT LANDED AT HNL WITHOUT INCIDENT. - [SDR CALA0100806](https://openairdocs.org/sdr/CALA0100806), Aug 26, 2001: FUSE. BLOWN. INSPECTION FOUND L-4 AND R-4 DOOR LOWER EXIT LIGHT INOPERATIVE. THE FUSE IN EMERGENCY LIGHT BATTERY PACK U1-165 WAS REMOVED AND REPLACED IAW WDM 33-52-04 AND OP - [SDR CALA0001635](https://openairdocs.org/sdr/CALA0001635), Oct 23, 2000: AIR BOX. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN LOWER CENTER PYLON AIR BOX WHERE THE PRECOOLER AIR DUCT ATTACHES (I/B SIDE). THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS IN - [SDR CALA9901718](https://openairdocs.org/sdr/CALA9901718), Dec 21, 1999: FLASHLIGHT. INOPERATIVE. INSPECTION FOUND TWO EACH EMERGENCY PORTABLE FLASHLIGHTS INOPERATIVE. THE FLASHLIGHTS WERE REPLACED AND TESTED IAW MM 25-60-00. - [SDR CALA9901600](https://openairdocs.org/sdr/CALA9901600), Dec 15, 1999: SPAR. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN LEFT HORIZONTAL STABILIZER PANEL SIDE UPPER CHORD. THE CHORD WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-33-01. - [SDR CALA9901599](https://openairdocs.org/sdr/CALA9901599), Dec 15, 1999: SUPPORT. CORRODED. INSPECTION FOUND LAV SUPPORT CORRODED AT STA 1860-1889, BL 0. THE LAV SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01. - [SDR CALA9901598](https://openairdocs.org/sdr/CALA9901598), Dec 15, 1999: CHANNEL. CORRODED. INSPECTION FOUND CENTER CARGO COMPARTMENT LEFT CHANNEL CORRODED UNDER OMNI ROLLERS. A NEW CHANNEL WAS INSTALLED IAW SRM 53-42-01. - [SDR CALA9901563](https://openairdocs.org/sdr/CALA9901563), Dec 6, 1999: SUPPORT. CORRODED. INSPECTION FOUND LAV SUPPORTS CORRODED AT STA 1860-1887, RBL 47 AND AT STA 1850-1890, LBL 47. THE SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM - [SDR CALA9901553](https://openairdocs.org/sdr/CALA9901553), Dec 5, 1999: SUPPORT. CORRODED. INSPECTION FOUND GALLEY FLOOR SUPPORT CORRODED BETWEEN STA 785 AND 789, RBL 47. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-7 - [SDR CALA9901552](https://openairdocs.org/sdr/CALA9901552), Dec 5, 1999: SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOORBEAM SUPPORT CORRODED BETWEEN STA 460 AND 515, LBL 33. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-0 - [SDR CALA9901551](https://openairdocs.org/sdr/CALA9901551), Dec 5, 1999: FRAME. CORRODED. INSPECTION FOUND CENTER CARGO COMPARTMENT LOWER FRAME CORRODED AT STA 1780 BETWEEN LONGERON 50L - 50R AND AT STA 1841, L49R - 50L. THE CORRODED AREAS WERE TRIMM - [SDR CALA9901550](https://openairdocs.org/sdr/CALA9901550), Dec 5, 1999: FRAME. CORRODED. INSPECTION FOUND CENTER CARGO COMPARTMENT LOWER FRAME CORRODED FROM STA 1660-1680, LONGERON 51L - 51R. THE CORRODED AREA WAS TRIMMED OUT AND REINFORCED WITH SHE - [SDR CALA9901543](https://openairdocs.org/sdr/CALA9901543), Nov 30, 1999: SUPPORT. CRACKED. INSPECTION FOUND FLOOR SUPPORT CRACKED AT UPPER LOBE CABIN FLOOR STA 495-615, RBL 14. THE CRACKED AREA OF FLOOR SUPPORT WAS TRIMMED OUT. A NEW SECTION WAS INSTA - [SDR CALA9901542](https://openairdocs.org/sdr/CALA9901542), Nov 30, 1999: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT UPPER LOBE CABIN FLOOR AT STA 395-457, RBL 28-33 AND STA 420-475, LBL 27. THE FLOOR SUPPORTS WERE REMOVED AND NEW SUP - [SDR CALA9900196](https://openairdocs.org/sdr/CALA9900196), Feb 27, 1999: FRAME. CRACKED. THE NR 3 ENGINE A AND B FIRELOOP LIGHTS ILLUMINATED AND THE FIRE HANDLE FLASHED AFTER TAKEOFF FROM HNL. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT - [SDR CALA9802049](https://openairdocs.org/sdr/CALA9802049), Nov 6, 1998: SKIN. DENTED. INSPECTION FOUND THE LT OUTBOARD TRAILING EDGE FLAP INBOARD SKIN DENTED AT LOWER FLAP 29 INCHES FROM INBOARD END. THE DENTED AREA WAS TRIMMED OUT AND REINFORCED - [SDR CALA9802048](https://openairdocs.org/sdr/CALA9802048), Nov 6, 1998: CHANNEL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL CHANNEL OF OUTBOARD AFT FAIRING AT RT MLG WHEEL WELL. THE CRACKED TEE WAS REMOVED AND A NEW TEE WAS INSTALLED IAW - [SDR CALA9802047](https://openairdocs.org/sdr/CALA9802047), Nov 5, 1998: LIGHT. INOP. INSPECTION FOUND THE EMERGENCY EXIT LIGHT AT SEATS 21B, 34K, AND 36B INOPERATIVE. THE EMERGENCY LIGHT IN SEATS 21B, 34K, AND 36B WERE REPLACED IAW MM 33-50-00. - [SDR CALA9802046](https://openairdocs.org/sdr/CALA9802046), Nov 5, 1998: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT STA 1289, RBL 107. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-70-00, FIGU - [SDR CALA9802045](https://openairdocs.org/sdr/CALA9802045), Nov 5, 1998: SKIN. DENTED. INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 1942, STRINGERS 51-52. THE DENTED AREA WAS TRIMMED OUT AND REINFORCED WITH INNER AND OUTER DOUBLERS IAW SRM 53-2 - [SDR CALA9802042](https://openairdocs.org/sdr/CALA9802042), Nov 5, 1998: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 515 TO 535, S28L. THE DENTED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER AND FINGER DOUBLER IAW SRM 53-20-00, - [SDR CALA9802041](https://openairdocs.org/sdr/CALA9802041), Nov 5, 1998: DOUBLER. CRACKED. INSPECTION FOUND A 2.7 INCH CRACK AND DELAMINATION ON RT WING MLG SUPPORT DOUBLER. THE CRACKED AND DELAMINATED AREAS WERE TRIMMED OUT AND REINFORCED WITH DOUBLE - [SDR CALA9802009](https://openairdocs.org/sdr/CALA9802009), Nov 2, 1998: DOOR. CRACKED. INSPECTION FOUND A 1.75 INCH CRACK AT AFT LOWER CORNER OF RT MLG WHEEL WELL DOOR. THE AREA WAS REINFORCED WITH A DOUBLER IAW SRM 51-21-01 AND 51-35-02. - [SDR CALA9802008](https://openairdocs.org/sdr/CALA9802008), Nov 1, 1998: BATTERY PACK. DISCHARGED. THE EMERGENCY LIGHT SYSTEM IN A ZONE FAILED AFTER SIX MINUTES. THE BATTERY PACKS WERE REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00. - [SDR CALA9802007](https://openairdocs.org/sdr/CALA9802007), Nov 1, 1998: FLOORBEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM AT STA 1275, RBL 104. REPAIRED IAW ECRA 5316-01000. - [SDR CALA9701595](https://openairdocs.org/sdr/CALA9701595), Nov 5, 1997: THRUST REVERSER. CRACKED. INSPECTION FOUND A CRACK ON INNER SKIN ADJACENT TO OPEN CLOSE ACTUATOR OF #2 ENGINE C DUCT RH. THE #2 ENGINE R/H THRUST REVERSER WAS REPLACED IAW MM 78-32-11. - [SDR CALA9701594](https://openairdocs.org/sdr/CALA9701594), Nov 5, 1997: THRUST REVERSER. DELAMINATED. INSPECTION FOUND #2 ENGINE L/H THRUST REVERSER UPPER AFT SIDEWALL DELAMINATED. THE #2 ENGINE L/H THRUST REVERSER WAS REPLACED IAW MM 78-32-11. - [SDR CALA9701593](https://openairdocs.org/sdr/CALA9701593), Nov 5, 1997: EXHAUST NOZZLE. CRACKED. INSPECTION FOUND A 5 CRACK IN #2 ENGINE EXHAUST NOZZLE. THE #2 ENGINE EXHAUST NOZZLE WAS REPLACED IAW MM 78-11-08. - [SDR CALA9701525](https://openairdocs.org/sdr/CALA9701525), Oct 30, 1997: FASTENERS. SHEARED. INSPECTION FOUND SIX FASTENER HEADS SHEARED AT LOWER AFT FACE OF NR 4 BANJO FITTING, NR 2 PYLON. THE FASTENERS WERE REMOVED AND REPLACED WITH NEW FASTENERS IAW - [SDR CALA9701524](https://openairdocs.org/sdr/CALA9701524), Oct 30, 1997: BULKHEAD. HOLE. INSPECTION FOUND A .5625 DIAMETER HOLE IN AFT PRESSURE BULKHEAD BETWEEN FLOOR SUPPORT BEAM AND LONGERON 41L AT STA 2007. REPAIRED IAW SRM 53-40-00. - [SDR CALA9701512](https://openairdocs.org/sdr/CALA9701512), Oct 28, 1997: ANGLE. CORRODED. INSPECTION FOUND FLOORBEAM HORIZONTAL ATTACHMENT ANGLE CORRODED AT THIRD FLOORBEAM RT FROM O/B SIDE, STA 2007, AFT CARGO LAV AREA. THE AREA WAS REPAIRED IAW SRM ## Other aircraft with N12064 - [Registered now](https://openairdocs.org/aircraft/N12064): Cessna 172S, S/N 172S9839, built 2005 - [Cancelled 1933-06-17](https://openairdocs.org/deregistered/N12064-1933-06-17): Melvin C Harcourt HARCOURT MEAD R R I, S/N G-399. Owner: [Melvin Carl Harcourt](https://openairdocs.org/faa-owner/MELVIN%20CARL%20HARCOURT), [Tinley Park, IL](https://openairdocs.org/faa-place/IL/Tinley%20Park) --- 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.