# N76073: 1974 Mcdonnell-Douglas DC-10-30, registration cancelled 2002-03-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 29, 2002 - Status when cancelled: Sale reported - 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: 46940 - Year built: 1974 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 27, 1993 - Last registry action: January 17, 2002 - Mode S code: AA44F1 - Location: [Austin, TX](https://openairdocs.org/faa-place/TX/Austin) - Owner type: Individual - Owner's area on the map: 30.4538° N, 97.6867° W: Placed by OpenAirDocs at the center of ZIP code 78728, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N76073 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=76073 - Page: https://openairdocs.org/deregistered/N76073-2002-03-29 From the FAA registry file of November 7, 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 (16) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9901132](https://openairdocs.org/sdr/CALA9901132), Sep 5, 1999: STIFFENER. CORRODED. INSPECTION FOUND STIFFENER CORRODED IN AFT CARGO COMPARTMENT AT STA 2007. REPAIRED IAW ECRA 531-01069. - [SDR CALA9901117](https://openairdocs.org/sdr/CALA9901117), Sep 1, 1999: WEB. CRACKED. INSPECTION FOUND A 5 INCH CRACK AT FORWARD WEB OF NR 2 PYLON AFTER REMOVING VERTICAL FIN. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-31-01. - [SDR CALA9901116](https://openairdocs.org/sdr/CALA9901116), Sep 1, 1999: RIB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RIB AT LT INNER CAVITY OF TAIL CONE. THE RIB WAS TRIMMED OUT AND THE AREA WAS REINFORCED WITH AN ANGLE REPAIR IAW SRM 53-00-0 - [SDR CALA9901115](https://openairdocs.org/sdr/CALA9901115), Sep 1, 1999: SPAR. SHEARED. INSPECTION FOUND THE TAIL CONE WORK PLATFORM SPAR SHEARED IN SEVERAL PLACES. THE SHEARED AREAS WERE TRIMMED OUT AND REINFORCED WITH DOUBLERS IAW SRM 53-00-01, F - [SDR CALA9901114](https://openairdocs.org/sdr/CALA9901114), Sep 1, 1999: SUPPORT. CORRODED. INSPECTION FOUND LT LAV FLOOR SUPPORT CORRODED AT ZONE 290, STA 1871. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01. - [SDR CALA9801378](https://openairdocs.org/sdr/CALA9801378), Jul 30, 1998: SKIN. CRACKED. INSPECTION FOUND AN 8 INCH CRACK ON LEFT WING LEADING EDGE SKIN AT WING STA XOS 906.00. REPAIRED IAW ECRA 5731-01009. - [SDR CALA9801149](https://openairdocs.org/sdr/CALA9801149), Jun 20, 1998: FUSE. BLOWN. INSPECTION FOUND EMERGENCY LIGHT IN ZONE-D ON RT SIDE, SEATS 37KL-45KL INOPERATIVE. A BLOWN FUSE FOR BATTERY PACK WAS FOUND. THE FUSE WAS REPLACED AND OPERATION - [SDR CALA9801130](https://openairdocs.org/sdr/CALA9801130), Jun 18, 1998: BATTERY PACK. DISCHARGED. INSPECTION FOUND EMERGENCY LIGHTS IN LEFT AFT ZONE INOPERATIVE. THE BATTERY AND BATTERY CHARGER WERE REMOVED AND REPLACED. - [SDR CALA9801068](https://openairdocs.org/sdr/CALA9801068), Jun 12, 1998: BALLAST. FAILED. SMOKE STARTED COMING FROM OVERHEAD ABOVE ROW 44L JUST PRIOR TO LANDING. HALON WAS APPLIED AND THE SMOKE CEASED. MAINTENANCE FOUND SIDEWALL BALLAST AT ROW 44L BU - [SDR CALA9701120](https://openairdocs.org/sdr/CALA9701120), Jul 20, 1997: BULKHEAD WEB. CRACKED. INSPECTION FOUND A 17 INCH CRACK ON PRESSURE BULKHEAD WEB AT STA 1521 BETWEEN Z= 74 AND 80. FILLER, DOUBLER, AND A FINGER DOUBLER WERE FABRICATED AND INSTALLED - [SDR CALA9701042](https://openairdocs.org/sdr/CALA9701042), Jul 3, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 440, BETWEEN BL 0 AND LBL 28. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-35-01. - [SDR CALA9701041](https://openairdocs.org/sdr/CALA9701041), Jul 3, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 460, LBL 28. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-35-01. - [SDR CAL950394](https://openairdocs.org/sdr/CAL950394), May 11, 1995: FRAME. CORRODED. KUL - INSPECTION FOUND CORROSION ON FRAME CAPS AT STATION 1701 AND 1721 BETWEEN LONGERONS 50L AND 50R. THE FRAME CAPS WERE REPAIRED IAW ECRA 5310-03101. (W) - [SDR CAL950395](https://openairdocs.org/sdr/CAL950395), Apr 30, 1995: CORNER. CORRODED. KUL - INSPECTION FOUND CORROSION ON THE FORWARD CARGO DOOR CUTOUT FORWARD LOWER CORNER. THE FORWARD CARGO DOOR CUTOUT FORWARD LOWER CORNER WAS REPAIRED IAW ECRA - [SDR CAL950396](https://openairdocs.org/sdr/CAL950396), Apr 19, 1995: ACTUATOR BOLT. SHEARED. KUL - THE RT MLG RETRACT ACTUATOR ATTACH FITTING UPPER FORWARD BOLT WAS FOUND SHEARED. THE BOLT WAS REPLACED PER STANDARD PRACTICE CHAPTER 20 OF THE MAINTENANCE - [SDR CAL950080](https://openairdocs.org/sdr/CAL950080), Jan 30, 1995: FIRE LOOP. INOPERATIVE. HNL - FLT 0906 - THE NR 1 ENGINE FIRE WARNING 'B' LOOP LIGHT BEGAN TO FLICKER ON AND OFF AND EVENTUALLY ILLUMINATED STEADILY WHILE ON DESCENT INTO HNL. THE NR 1 ## Other aircraft with N76073 - [Cancelled 1986-04-09](https://openairdocs.org/deregistered/N76073-1986-04-09): Cessna 172N, S/N 17268113. Owner: [Henricks Dean E & Katherine M](https://openairdocs.org/faa-owner/HENRICKS%20DEAN%20E%20%26%20KATHERINE%20M), [Carmichael, CA](https://openairdocs.org/faa-place/CA/Carmichael) - [Cancelled 1949-05-17](https://openairdocs.org/deregistered/N76073-1949-05-17): Cessna 140, S/N 10467. Owner: [Isaacs Eugene Loeb](https://openairdocs.org/faa-owner/ISAACS%20EUGENE%20LOEB) --- 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.