# N19072: 1972 Mcdonnell-Douglas DC-10-30, registration cancelled 2002-10-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 23, 2002 - Status when cancelled: Valid registration - 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: 46576 - Year built: 1972 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 29, 1986 - Certificate issued: July 18, 2002 - Last registry action: July 18, 2002 - Mode S code: A16B93 - 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/N19072 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=19072 - Page: https://openairdocs.org/deregistered/N19072-2002-10-23 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 (19) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9901363](https://openairdocs.org/sdr/CALA9901363), Oct 8, 1999: SUPPORT. CRACKED. PYLON NUMBER ONE SUPPORT PANELS 437DR/437ML CRACKED (0.5). REPLACED SUPPORT PER SRM 51-31-01. - [SDR CALA9901362](https://openairdocs.org/sdr/CALA9901362), Oct 8, 1999: ANGLE. CRACKED. RIGHT WING OUTBOARD FLAP OUTBOARD FAIRING RIGHT SIDE ANGLE IS CRACKED (0.5). REPLACED ANGLE PER SRM 51-33-01. - [SDR CALA9901361](https://openairdocs.org/sdr/CALA9901361), Oct 8, 1999: SKIN. CRACKED. LEFT WING LEADING EDGE INTERNAL SKIN CRACKED (4) AT STA XORS562. FABRICATED AND INSTALLED DOUBLER PER SRM 57-10-00 AND DWG ARB 3954. - [SDR CALA9901336](https://openairdocs.org/sdr/CALA9901336), Oct 6, 1999: SKIN. CRACKED. INSPECTION FOUND A 2.5 INCH CRACK IN LT FORWARD NLG DOOR SKIN. THE AREA WAS REPAIRED IAW SRM 52-00-01. - [SDR CALA9901119](https://openairdocs.org/sdr/CALA9901119), Sep 1, 1999: WIRE. DAMAGED. INSPECTION FOUND EMERGENCY LIGHT INOPERATIVE AT SEATS 29AB TO 35AB. MAINTENANCE REPAIRED DAMAGED WIRES AT SEAT 32AB IAW WDM 33-53-03 AND OPERATION CHECKED GOOD. - [SDR CALA9900761](https://openairdocs.org/sdr/CALA9900761), Jun 30, 1999: BATTERY. DISCHARGED. THE EMERGENCY LIGHTS WOULD NOT TEST. THE BATTERY PACK AND CHARGER AT DOOR 3L WERE REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-01, PAGE 201. - [SDR CALA9900710](https://openairdocs.org/sdr/CALA9900710), Jun 18, 1999: FUEL LINE. BROKEN. THE NR 3 ENGINE FLAMED OUT DUE TO LOSS OF FUEL FLOW WHILE EN ROUTE FROM GUM TO HNL. ALL OTHER ENGINE PARAMETERS WERE IN NORMAL RANGE AT TIME OF FAILURE. THE AIR - [SDR CALA9900206](https://openairdocs.org/sdr/CALA9900206), Mar 3, 1999: SLIDE. LOW PRESSURE. THE R-3 DOOR EMERGENCY SLIDE LOW PRESSURE INDICATOR LIGHT WAS FOUND ILLUMINATED DURING A PRE-DEPARTURE CHECK. THE R-3 DOOR EMERGENCY SLIDE WAS REMOVED AND REPLA - [SDR CALA9802086](https://openairdocs.org/sdr/CALA9802086), Nov 20, 1998: BATTERY PACK. DISCHARGED. INSPECTION FOUND FIRST CLASS AREA EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. - [SDR CALA9801601](https://openairdocs.org/sdr/CALA9801601), Aug 31, 1998: SKIN. CRACKED. INSPECTION FOUND A 1 CRACK IN SKIN OF RT HORIZONTAL STABILIZER LEADING EDGE ON SECOND SECTION NEAR THE LOWER EXTERNAL CORNER. THE AREA WAS REPAIRED IAW ECRA 551 - [SDR CALA9801559](https://openairdocs.org/sdr/CALA9801559), Aug 26, 1998: SKIN. CRACKED. INSPECTION FOUND A 1.5 CRACK IN LT WING LEADING EDGE SKIN AT STA XORS 683. THE SKIN WAS REPAIRED IAW SRM 57-10-00, FIGURE 49 AND FIGURE 68, SHEET 10. - [SDR CALA9801173](https://openairdocs.org/sdr/CALA9801173), Jun 27, 1998: HYD LINE. RUPTURED. THE LANDING GEAR HANDLE WOULD NOT RAISE TO THE UP POSITION AFTER TAKEOFF. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO HNL WHERE IT LANDED WITHOUT INCIDENT. - [SDR CALA9800653](https://openairdocs.org/sdr/CALA9800653), Apr 8, 1998: FRAME. BROKEN. THE AIRCRAFT LOST NR 3 HYDRAULIC SYSTEM FLUID WHILE EN ROUTE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. INITIAL FINDINGS REVEALED THE L - [SDR CALA9701340](https://openairdocs.org/sdr/CALA9701340), Aug 20, 1997: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN STA 1964 TO 1973, LONGERON 47L TO 48L. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-00-01 AND 51-35-0 - [SDR CALA9701339](https://openairdocs.org/sdr/CALA9701339), Jul 31, 1997: DOUBLER. CORRODED. INSPECTION FOUND FINGER DOUBLER CORRODED BETWEEN STA 1700 AND 1720, LONGERON 51. THE FINGER DOUBLER WAS REMOVED, A NEW FINGER DOUBLER WAS FABRICATED AND INSTALL - [SDR CALA9601875](https://openairdocs.org/sdr/CALA9601875), Dec 24, 1996: HYD PUMP. CRACKED. THE A/C LOST NR 2 SYSTEM HYDRAULIC FLUID WHILE ENROUTE FROM HNL TO GUM. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF BOTH LT AND RT PUMP PRESSURE LOW LIGHT - [SDR CALA9601859](https://openairdocs.org/sdr/CALA9601859), Dec 20, 1996: DECODER. FAILED. THE SECOND OFFICER WAS NOTIFIED THAT THE READING LIGHTS IN MIDDLE SECTION OF COACH WERE INOPERATIVE WHILE IN FLIGHT. THE CIRCUIT BREAKER FOR THE READING LIGHTS - [SDR CAL960277](https://openairdocs.org/sdr/CAL960277), Feb 29, 1996: HYD PUMP. LEAKING. FLT NR 6 - LAX - THE NR 2 ENG TEMP HIGH LIGHT ILLUMINATED AND WAS FOLLOWED SHORTLY AFTERWARDS BY THE LOSS OF NR 2 HYDRAULIC QUANTITY. BOTH PUMPS WERE SHUTOFF AN - [SDR CAL960276](https://openairdocs.org/sdr/CAL960276), Feb 29, 1996: HYD PUMP. LEAKING. FLT NR 6 - LAX - THE NR 2 ENG TEMP HIGH LIGHT ILLUMINATED AND WAS FOLLOWED SHORTLY AFTERWARDS BY THE LOSS OF NR 2 HYDRAULIC QUANTITY. BOTH PUMPS WERE SHUTOFF AN ## FAA accident and incident reports (2) 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 19940326025629I](https://openairdocs.org/incident/19940326025629I), Mar 26, 1994: Doug DC1030 (N19072), Denver, CO. ILS system failure on approach to Denver, diverted to Colorado springs. Replaced ILS control panel. - [Incident 19870131006549I](https://openairdocs.org/incident/19870131006549I), Jan 31, 1987: Doug DC1030 (N19072), Honolulu, HI. First officer became ill en route. Flight engineer changed positions with ill crewmember. Suspect flu. ## Other aircraft with N19072 - [Cancelled 1975-09-08](https://openairdocs.org/deregistered/N19072-1975-09-08): Cessna 150L, S/N 15074143, built 1972. Exported to Canada. Owner: [Salem Aviation Inc](https://openairdocs.org/faa-owner/SALEM%20AVIATION%20INC), [Salem, OR](https://openairdocs.org/faa-place/OR/Salem) --- 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.