# N14063: 1973 Mcdonnell-Douglas DC-10-30, registration cancelled 2013-06-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 11, 2013
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Mcdonnell-Douglas DC-10-30](https://openairdocs.org/model/mcdonnell-douglas-dc-10-30) (registry code 3023501)
- Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 47864
- Year built: 1973
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 13, 1984
- Certificate issued: July 18, 2002
- Last registry action: July 15, 2008
- Mode S code: A0A5F6
- 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/N14063
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14063
- Page: https://openairdocs.org/deregistered/N14063-2013-06-11

From the FAA registry file of October 31, 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 (64, newest 50)

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

- [SDR CALA0100162](https://openairdocs.org/sdr/CALA0100162), Feb 24, 2001: SPOILER. DELAMINATED. INSPECTION FOUND LT WING SPOILER NR 2 DELAMINATED WITH LOWER SKIN CORRODED. THE NR 2 LT SPOILER WAS REMOVED AND REPLACED IAW MM 27-60-01.
- [SDR CALA0100161](https://openairdocs.org/sdr/CALA0100161), Feb 24, 2001: SKIN. CRACKED. INSPECTION FOUND A 1.2 INCH CRACK IN APU DOOR SKIN. A NEW DOOR WAS INSTALLED IAW DRAWING AHL7008 AND SRM 51-31-01.
- [SDR CALA0100160](https://openairdocs.org/sdr/CALA0100160), Feb 24, 2001: SPOILER. DELAMINATED. INSPECTION FOUND RT WING SPOILER PANELS NR 3, 4, & 5 DELAMINATED ON UPPER SURFACE. THE SPOILERS WERE REMOVED AND REPLACED IAW MM 27-60-01.
- [SDR CALA0100159](https://openairdocs.org/sdr/CALA0100159), Feb 24, 2001: SPOILER. DELAMINATED. INSPECTION FOUND RT WING NR 1 AND 2 SPOILER PANELS DELAMINATED ON UPPER SURFACE. THE NR 1 AND 2 SPOILERS WERE REMOVED AND REPLACED IAW MM 27-60-01.
- [SDR CALA0100157](https://openairdocs.org/sdr/CALA0100157), Feb 23, 2001: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN CENTER CARGO LT ANGLE AT STA 1721. THE ANGLE WAS REPLACED IAW SRM 51-31-01.
- [SDR CALA0001998](https://openairdocs.org/sdr/CALA0001998), Dec 26, 2000: BATTERY PACK. INOPERATIVE. THE EMERGENCY LIGHT TEST FUNCTION WOULD NOT GIVE A VALID TEST. THE L-2 DOOR EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-01. OPERATIONAL C
- [SDR CALA0000420](https://openairdocs.org/sdr/CALA0000420), Apr 6, 2000: SPAR. CRACKED. INSPECTION FOUND A 1.3 INCH CRACK IN LT HORIZONTAL STABILIZER REAR SPAR CAP AFT BARREL NUT BORE. THE LT HORIZONTAL STABILIZER UPPER AFT SPAR CAP SECTION WAS REP
- [SDR CALA0000327](https://openairdocs.org/sdr/CALA0000327), Mar 22, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT BEAM CORRODED AT STA 420, X=28L. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-70-00, FIGURE 13.
- [SDR CALA9900419](https://openairdocs.org/sdr/CALA9900419), Apr 16, 1999: CHANNEL. DAMAGED. INSPECTION FOUND DAMAGED CHANNEL SECTION IN CENTER CARGO BAY AT STA 1801-1841. THE CHANNEL WAS REPLACED WITH A NEW CHANNEL IAW MM 25-52-01.
- [SDR CALA9900415](https://openairdocs.org/sdr/CALA9900415), Apr 15, 1999: SILL. CORRODED. INSPECTION FOUND CENTER CARGO BAY DOOR SILL LOWER AFT FRAME AND LOWER FORWARD FRAME CORRODED. THE LOWER AFT AND LOWER FORWARD FRAMES WERE REPAIRED IAW SRM 53-50
- [SDR CALA9900414](https://openairdocs.org/sdr/CALA9900414), Apr 15, 1999: BEAM. CORRODED. INSPECTION FOUND SUPPORT BEAM CORRODED AT CENTER CARGO BAY CENTER ROLLER CHANNEL ADJOINING BULK CARGO AREA. THE SUPPORT BEAM WAS REMOVED AND REPLACED IAW SRM 53
- [SDR CALA9900413](https://openairdocs.org/sdr/CALA9900413), Apr 15, 1999: BRACKET. CRACKED. INSPECTION FOUND TAIL CONE CENTER RT, UPPER RT, AND UPPER LT SPIGOT MOUNTING BRACKETS CRACKED. EACH BRACKET HAD A 3 INCH CRACK. THE BRACKETS WERE REPAIRED IAW S
- [SDR CALA9900408](https://openairdocs.org/sdr/CALA9900408), Apr 14, 1999: BOLT. SHEARED. INSPECTION FOUND LT MLG BAY TRAPEZOIDAL FRAME UPPER FLANGE BOLT SHEARED. THE BOLT, NUT AND WASHERS WERE REPLACED IAW MM 20-20-01.
- [SDR CALA9900404](https://openairdocs.org/sdr/CALA9900404), Apr 14, 1999: SILL. CORRODED. INSPECTION FOUND THE FORWARD CARGO BAY FORWARD LOWER DOOR SILL CORRODED IN FORWARD CORNER. THE DOOR SILL WAS REPAIRED IAW SRM 53-50-00, FIGURE 9.
- [SDR CALA9900388](https://openairdocs.org/sdr/CALA9900388), Apr 12, 1999: RIB. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK RT WING LEADING EDGE DOUBLER AND SUPPORT RIB AT STA XORS 795. THE LEADING EDGE DOUBLER AND SUPPORT RIB WERE REPAIRED IAW SRM 5
- [SDR CALA9900360](https://openairdocs.org/sdr/CALA9900360), Apr 6, 1999: DOOR. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN Z SECTION AT FORWARD CORNER OF LT MLG DOOR. THE DOOR WAS REPAIRED IAW SRM 52-10-00, FIGURE 15.
- [SDR CALA9900359](https://openairdocs.org/sdr/CALA9900359), Apr 6, 1999: ANGLE. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN LT AND RT DRAG ANGLES BELOW NR 2 ENGINE AT THIRD BANJO FITTING. THE CRACKS WERE STOP DRILLED AND REPAIR ANGLES WERE INSTALLED
- [SDR CALA9900193](https://openairdocs.org/sdr/CALA9900193), Feb 25, 1999: WIRE. SHORTED. INSPECTION FOUND THE EMERGENCY AISLE PATH LIGHTING AT SEAT ROWS 29/36KL INOPERATIVE. A POWER WIRE WAS FOUND DAMAGED AND SHORTED UNDER SEAT 36L CAUSING POWER SUP
- [SDR CALA9801957](https://openairdocs.org/sdr/CALA9801957), Oct 14, 1998: WIRE. BROKEN. ROW 33 AND 34 L AND K EMERGENCY LIGHTS INOP. RESECURED BROKEN WIRE FOR EMERGENCY LIGHTS.
- [SDR CALA9801855](https://openairdocs.org/sdr/CALA9801855), Sep 20, 1998: DUCT. RUPTURED. THE NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED WHILE EN ROUTE. BOTH FIRE BOTTLES WERE DISCHARGED, BUT THE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT WAS DIVERTED 
- [SDR CALA9800645](https://openairdocs.org/sdr/CALA9800645), Apr 8, 1998: SUPPORT. CORRODED. INSPECTION FOUND CORROSION ON FLOOR OMEGA SUPPORT AT STA 455, RBL 45. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53
- [SDR CALA9800644](https://openairdocs.org/sdr/CALA9800644), Apr 7, 1998: JAMB. CORRODED. INSPECTION FOUND CORROSION ON ENTRY LOWER AFT CARGO JAMB BOX AT STA 1964 BETWEEN STRINGER 40-46. THE CORRODED AREAS WERE REMOVED. A STRAP, DOUBLERS, PLUG, ANGLE
- [SDR CALA9800636](https://openairdocs.org/sdr/CALA9800636), Apr 7, 1998: AIR BOTTLE. LOW PRESSURE. INSPECTION FOUND R-1 DOOR AIR BOTTLE PRESSURE LOW. THE AIR BOTTLE WAS FILLED IAW MM 52-11-06.
- [SDR CALA9800635](https://openairdocs.org/sdr/CALA9800635), Apr 7, 1998: AIR BOTTLE. LOW PRESSURE. INSPECTION FOUND L-2 DOOR AIR BOTTLE PRESSURE LOW. THE AIR BOTTLE WAS FILLED IAW MM 52-12-06.
- [SDR CALA9800634](https://openairdocs.org/sdr/CALA9800634), Apr 7, 1998: AIR BOTTLE. LOW PRESSURE. INSPECTION FOUND L-3 DOOR AIR BOTTLE PRESSURE LOW. THE AIR BOTTLE WAS FILLED IAW MM 52-12-06.
- [SDR CALA9800629](https://openairdocs.org/sdr/CALA9800629), Apr 6, 1998: CHARGER. INOPERATIVE. INSPECTION FOUND ZONE-A EMERGENCY LIGHT BATTERY PACK INOPERATIVE. THE EMERGENCY LIGHT CHARGER WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.
- [SDR CALA9800605](https://openairdocs.org/sdr/CALA9800605), Mar 30, 1998: RIBS. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN THREE RIBS OF NR 1 LT SLAT. THE CRACKED RIBS WERE REMOVED. NEW RIBS WERE FABRICATED AND INSTALLED IAW SRM 57-55-01 FIGURE 2 5
- [SDR CALA9800577](https://openairdocs.org/sdr/CALA9800577), Mar 22, 1998: BRACKET. CORRODED. INSPECTION FOUND NR 2 PYLON UPPER PYLON TRAILING EDGE ATTACH BRACKET CORRODED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-32-02, 51-38-01, FIGURE 13, 51-2
- [SDR CALA9800491](https://openairdocs.org/sdr/CALA9800491), Mar 18, 1998: JAMB. CORRODED. INSPECTION FOUND LOWER AFT CARGO DOOR JAMB CORRODED BETWEEN STA 1921 AND 1942. THE CORRODED AREA WAS REMOVED. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM
- [SDR CALA9800490](https://openairdocs.org/sdr/CALA9800490), Mar 18, 1998: T-PROFILE. CRACKED. INSPECTION FOUND SEVERAL 1 CRACKS IN INBOARD AND OUTBOARD ATTACH FLANGES OF RT HORIZONTAL STABILIZER NR 3 LEADING EDGE T-PROFILE. THE STRAP AND T-PROFILE WERE R
- [SDR CALA9800489](https://openairdocs.org/sdr/CALA9800489), Mar 18, 1998: MOUNT. CRACKED. INSPECTION FOUND TAILCONE UPPER SECTION RT WORK PLATFORM FORWARD MOUNT RIVETS LOOSE AND CRACKED. THE MOUNT WAS REMOVED AND A NEW MOUNT WAS FABRICATED AND INSTAL
- [SDR CALA9800488](https://openairdocs.org/sdr/CALA9800488), Mar 18, 1998: FLOOR POST. BROKEN. INSPECTION FOUND CABIN FLOOR POST BROKEN IN FORWARD CARGO AREA AT STA 1100. THE AREA WAS TRIMMED AND BLENDED OUT. A REPAIR CHANNEL, ANGLE, AND FILLER WERE FABRI
- [SDR CALA9800487](https://openairdocs.org/sdr/CALA9800487), Mar 18, 1998: FLOOR WEB. CRACKED. INSPECTION FOUND A 5 INCH CRACK ON FORWARD CARGO LOWER FLANGE OF FLOOR WEB AT STA 879 LBL 50. THE FLANGE WAS TRIMMED AND BLENDED OUT AND THE AREA WAS REWORKED. 
- [SDR CALA9800485](https://openairdocs.org/sdr/CALA9800485), Mar 17, 1998: FLOORBEAM. BROKEN. INSPECTION FOUND INTERIOR UPPER LOBE CABIN FLOORBEAM BROKEN AT STA 1275, RBL 103. THE FLOORBEAM WAS REPAIRED IAW ECRA 5320-01511 AND ENGINEERING ORDER MF MAN D1
- [SDR CALA9800484](https://openairdocs.org/sdr/CALA9800484), Mar 17, 1998: FLOORBEAM. BROKEN. INSPECTION FOUND INTERIOR UPPER LOBE CABIN FLOORBEAM BROKEN AT STA 1293, RBL 103. THE FLOORBEAM WAS REPAIRED IAW ECRA 5320-01511 AND ENGINEERING ORDER MF MAN D1
- [SDR CALA9800481](https://openairdocs.org/sdr/CALA9800481), Mar 17, 1998: STRINGER. CORRODED. INSPECTION FOUND STRINGER 52 CORRODED IN CENTER CARGO AREA AT STA 1581-1601. THE STRINGER WAS REMOVED. A NEW PART WAS INSTALLED IAW SRM 51-21-01.
- [SDR CALA9800480](https://openairdocs.org/sdr/CALA9800480), Mar 17, 1998: LONGERON. CORRODED. INSPECTION FOUND LONGERON 48L CORRODED IN CENTER CARGO AREA AT STA 1521-1541. THE CORRODED AREA WAS CLEANED AND BLENDED OUT. A NEW ANGLE WAS FABRICATED, THE ARE
- [SDR CALA9800479](https://openairdocs.org/sdr/CALA9800479), Mar 17, 1998: FLANGE. CORRODED. INSPECTION FOUND LOWER FLANGE IN CENTER CARGO AREA CORRODED AT STA 1821, STRINGER 51. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT, REWORKED, AND REINFORCED WI
- [SDR CALA9800478](https://openairdocs.org/sdr/CALA9800478), Mar 17, 1998: FLANGE. CORRODED. INSPECTION FOUND LOWER FLANGE IN CENTER CARGO AREA CORRODED AT STA 1741, STRINGER 48. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT. A NEW CHORD WAS FABRICATED 
- [SDR CALA9800477](https://openairdocs.org/sdr/CALA9800477), Mar 17, 1998: FLANGE. CORRODED. INSPECTION FOUND LOWER FLANGE IN CENTER CARGO AREA CORRODED AT STA 1761, STRINGER 48. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT. A NEW CHORD WAS FABRICATED 
- [SDR CALA9800476](https://openairdocs.org/sdr/CALA9800476), Mar 17, 1998: CHORD. CORRODED. INSPECTION FOUND LOWER CHORD IN CENTER CARGO AREA CORRODED AT STA 1761, STRINGER 51 TO 47L. THE CORRODED AREA WAS REMOVED. A NEW PART AND SHEAR CLIP WERE FABRIC
- [SDR CALA9800475](https://openairdocs.org/sdr/CALA9800475), Mar 17, 1998: CHORD. CORRODED. INSPECTION FOUND LOWER CHORD IN CENTER CARGO AREA CORRODED AT STA 1781, STRINGER 51. THE CORRODED AREA WAS REMOVED AND THE AREA WAS REWORKED. A NEW PART WAS INS
- [SDR CALA9800474](https://openairdocs.org/sdr/CALA9800474), Mar 17, 1998: FLANGE. CORRODED. INSPECTION FOUND LOWER FLANGE IN CENTER CARGO AREA CORRODED AT STA 1781, STRINGER 47-48R. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT. A NEW CHORD WAS FABRICA
- [SDR CALA9800462](https://openairdocs.org/sdr/CALA9800462), Mar 15, 1998: VENT BOX. CORRODED. INSPECTION FOUND CORROSION ON VENT BOX AT STA 1480 AT ATTACHMENT TO LONGERON 27R. CORRODED TRUSS WAS REMOVED. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51
- [SDR CALA9800461](https://openairdocs.org/sdr/CALA9800461), Mar 15, 1998: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 455, LBL 60. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-12-15,
- [SDR CALA9800460](https://openairdocs.org/sdr/CALA9800460), Mar 15, 1998: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 492, RBL 30. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-12-15,
- [SDR CALA9800459](https://openairdocs.org/sdr/CALA9800459), Mar 15, 1998: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK ON FAIRING SUPPORT ANGLE AT STA 1421, STRINGER 32R. THE SUPPORT ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW 
- [SDR CALA9800458](https://openairdocs.org/sdr/CALA9800458), Mar 15, 1998: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK ON FAIRING SUPPORT ANGLE AT STA 1381, STRINGER 32R. THE SUPPORT ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW 
- [SDR CALA9800457](https://openairdocs.org/sdr/CALA9800457), Mar 15, 1998: SUPPORT. CORRODED. INTERIOR UPPER LOBE CABIN UNDER FLOOR LAV/GALLEY CORROSION ON FLOOR SUPPORT BETWEEN STA 824 AND 879, RBL 73. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT 
- [SDR CALA9800456](https://openairdocs.org/sdr/CALA9800456), Mar 15, 1998: FLOOR TRACK. CORRODED. INTERIOR UPPER LOBE CABIN UNDER FLOOR LAV/GALLEY CORROSION ON FLOOR TRACK AT STA 840, RBL 27. THE FLOOR TRACK WAS REMOVED, A NEW TRACK WAS INSTALLED IAW SRM 53-

All 64: https://openairdocs.org/deregistered/N14063-2013-06-11/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA98WA088](https://openairdocs.org/ntsb/DCA98WA088), Sep 20, 1998: McDonnell Douglas DC-10-30 (N14063), Shannon, Ireland, incident, minor damage

## FAA accident and incident reports (3)

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 20010322009639I](https://openairdocs.org/incident/20010322009639I), Mar 22, 2001: Doug DC1030 (N14063), Houston, TX, Minor damage. (-23)Taxiing to runway 15L on WA while making the left turn from WA to wc, the left main gear departed the hard surface onto the grassy area adjacent to the…
- [Incident 19920804041819I](https://openairdocs.org/incident/19920804041819I), Aug 4, 1992: Doug DC1030 (N14063), Honolulu, HI. NR1 engine experienced compressor stall after departure. Dumped fuel. Returned. Found progressive compressor damage
- [Incident 19871112077979I](https://openairdocs.org/incident/19871112077979I), Nov 12, 1987: Doug DC1030 (N14063), Honolulu, HI, Minor damage. Number 2 engine left core cowl separated on takeoff due to improper installation. Created runway hazard.

## Other aircraft with N14063

- [Cancelled 1973-04-09](https://openairdocs.org/deregistered/N14063-1973-04-09): Piper PA-23-250, S/N 27-4671. Exported to United Kingdom. Owner: [Airspeed International Sales Inc](https://openairdocs.org/faa-owner/AIRSPEED%20INTERNATIONAL%20SALES%20INC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale)

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