# N14079: 1973 Mcdonnell-Douglas DC-10-30, registration cancelled 2012-06-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 14, 2012 - Status when cancelled: Registration pending, canceled - 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: 46927 - Year built: 1973 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 19, 1997 - Last registry action: November 17, 2003 - Mode S code: A0A61F - Location: [Houston, TX](https://openairdocs.org/faa-place/TX/Houston) - Owner type: Individual - Owner's area on the map: 29.7568° N, 95.3657° W: Placed by OpenAirDocs at the center of ZIP code 77002, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14079 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14079 - Page: https://openairdocs.org/deregistered/N14079-2012-06-14 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 CALA0001683](https://openairdocs.org/sdr/CALA0001683), Nov 3, 2000: SKIN. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN RT HORIZONTAL STABILIZER UPPER AFT O/B SKIN. THE RT UPPER AFT O/B SKIN PANEL WAS REPAIRED IAW ECRA 5511-01035. - [SDR CALA0001681](https://openairdocs.org/sdr/CALA0001681), Nov 1, 2000: FITTING. CORRODED. INSPECTION FOUND LAV E O/B SUPPORT BEAM CORRODED AT AFT ATTACHMENT FITTING, STA Y = 1831-1887, X = 31L. A NEW SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND S - [SDR CALA0001657](https://openairdocs.org/sdr/CALA0001657), Oct 26, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND LAV F I/B SUPPORT BEAM CORRODED. A NEW BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01. - [SDR CALA0001656](https://openairdocs.org/sdr/CALA0001656), Oct 26, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND LAV E I/B SUPPORT BEAM CORRODED AT STA. Y = 1831-1887, X = 5L. A NEW SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01. - [SDR CALA0001655](https://openairdocs.org/sdr/CALA0001655), Oct 26, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND GALLEY G-2 SUPPORT BEAM CORRODED AROUND FORWARD ATTACHMENT BOLT HOLE AT STA Y = 392-412, X = 8R. A REPAIR WAS INSTALLED IAW GMM 10-900-01 AND 5 - [SDR CALA0001654](https://openairdocs.org/sdr/CALA0001654), Oct 26, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND GALLEY G-2 FLOOR SUPPORT CHANNEL SECTION CORRODED AT STA Y = 392-459, X = 40R. A NEW FLOOR SUPPORT CHANNEL SECTION WAS INSTALLED IAW GMM 10-900 - [SDR CALA0001653](https://openairdocs.org/sdr/CALA0001653), Oct 26, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND LONGITUDINAL SUPPORT BEAM AFT OF GALLEY G-1 CORRODED AT STA Y = 412-487, X = 24L. A NEW SECTION OF SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 - [SDR CALA0001652](https://openairdocs.org/sdr/CALA0001652), Oct 26, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND GALLEY G-6 O/B SUPPORT BEAM CORRODED AT FORWARD END. A NEW SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01. - [SDR CALA0001651](https://openairdocs.org/sdr/CALA0001651), Oct 26, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND GALLEY G-1 SUPPORT BEAM CORRODED AT STA Y = 392-422, X = 20L. A REPAIR WAS PERFORMED IAW GMM 10-900-01 AND SRM 53-11-1. - [SDR CALA0001650](https://openairdocs.org/sdr/CALA0001650), Oct 26, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND LAV F O/B SUPPORT BEAM CORRODED AT Y = 1831-1887, X = 31R. THE FLOOR SUPPORT BEAM WAS REPLACED IAW SRM 53-16-01. - [SDR CALA0001641](https://openairdocs.org/sdr/CALA0001641), Oct 24, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT BEAM J SECTION AT BASE OF FLIGHT DECK STEP CORRODED AT STA Y = 392, X = 20L-20R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AN - [SDR CALA0001640](https://openairdocs.org/sdr/CALA0001640), Oct 23, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT BEAM CAPPING STRIP FORWARD OF GALLEY 6 AND 7 CORRODED AT STA Y = 1914, X = 17L-17R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 - [SDR CALA0001639](https://openairdocs.org/sdr/CALA0001639), Oct 23, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT BEAM FWD OF LAV H CORRODED AT STA Y = 1914, X = 44L-66L. A NEW SUPPORT SECTION WAS INSTALLED IAW SRM 53-16-01 AND GMM 10-900-01. - [SDR CALA0001628](https://openairdocs.org/sdr/CALA0001628), Oct 23, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT BEAM CAPPING STRIP AFT OF LAVS E AND F AT STA Y = 1887, X = 5R-24R CORRODED. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SR - [SDR CALA0001627](https://openairdocs.org/sdr/CALA0001627), Oct 23, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT BEAM CAPPING STRIPS AFT OF LAVS E & F AT STA Y = 1887, X = 28L-32L AND X = 38L-58L CORRODED. NEW SECTIONS WERE INSTALLED IAW GMM - [SDR CALA0001626](https://openairdocs.org/sdr/CALA0001626), Oct 23, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT BEAM CAPPING SECTIONS AFT OF LAVS E & F AT STA Y = 1887, X = 5L-24L AND X = 27R-53R CORRODED. NEW SECTIONS WERE INSTALLED IAW GMM - [SDR CALA0001625](https://openairdocs.org/sdr/CALA0001625), Oct 23, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT BEAM J SECTION CORRODED AT STA Y = 421, X = 24L-24R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01. - [SDR CALA0001624](https://openairdocs.org/sdr/CALA0001624), Oct 23, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND GALLEY G3 LATERAL FLOORBEAM J SECTION CORRODED AT STA Y = 459, X = 18L-24R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01. - [SDR CALA0001623](https://openairdocs.org/sdr/CALA0001623), Oct 23, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT LAVS E & F, STA Y = 1887, X = 38R-58R. A REPAIR WAS ACCOMPLISHED BY INSTALLING A NEW J SECTION IAW GMM 10-900-01 AND - [SDR CALA0001622](https://openairdocs.org/sdr/CALA0001622), Oct 22, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND LATERAL FLOORBEAM CORRODED AT STA Y = 459, X = 38R-41R. A SPLICE REPAIR WAS PERFORMED IAW SRM 53-30-00. - [SDR CALA0000146](https://openairdocs.org/sdr/CALA0000146), Feb 12, 2000: FUSE. FAILED. THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM HNL. THE A/C WAS RETURNED TO HNL WHERE IT LANDED W/O INCIDENT. MX FOUND THE MLG INTERLOCK CYLINDER RETRACT - [SDR CALA9901499](https://openairdocs.org/sdr/CALA9901499), Nov 16, 1999: SAFETY WIRE. OUT OF POSITION. CREW RECEIVED RED GEAR WARNING LIGHTS WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. A GO-AROUND WAS PERFORMED AND GEAR WAS EXTENDED MANUALLY. ALL GEAR LIGHTS WERE - [SDR CALA9901480](https://openairdocs.org/sdr/CALA9901480), Nov 9, 1999: ANGLE. CRACKED. INSPECTION FOUND NR 1 ENGINE INTAKE EXTERNAL SIDE AFT SUPPORT ANGLES(2) CRACKED. THE CRACKS WERE 1 LONG. THE SUPPORT ANGLES WERE REPLACED IAW SRM 51-30-00. - [SDR CALA9901479](https://openairdocs.org/sdr/CALA9901479), Nov 9, 1999: ANGLE. CRACKED. INSPECTION FOUND A 3 CRACK IN RT WING FIXED L/E SUPPORT ANGLE AT STA XOS 414.125. A NEW ANGLE WAS INSTALLED IAW SRM 51-31-01. - [SDR CALA9901478](https://openairdocs.org/sdr/CALA9901478), Nov 8, 1999: SKIN. CRACKED. INSPECTION FOUND RT WING LEADING EDGE LOWER SKIN CRACKED AT STA XORS 455 AND STA XORS 506. BOTH CRACKS WERE 1 LONG. REPAIRS WERE INSTALLED IAW DRAWING ARB2933-4 - [SDR CALA9901444](https://openairdocs.org/sdr/CALA9901444), Oct 28, 1999: STRIP. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 SLAT O/B STRIP. PERFORMED REPAIR IAW SRM 57-10-00. - [SDR CALA9901434](https://openairdocs.org/sdr/CALA9901434), Oct 25, 1999: SKIN. CRACKED. INSPECTION FOUND A 0.9 INCH CRACK IN RT WING LEADING EDGE SKIN AT XORS 783. A REPAIR WAS INSTALLED IAW SRM 57-10-00, FIGURE 68. - [SDR CALA9900509](https://openairdocs.org/sdr/CALA9900509), May 10, 1999: ROD. DISCONNECTED. UNABLE TO ARM L3 DOOR AT DEPARTURE. FOUND ROD AT LOCKING MECHANISM OUT OF PLACE. REINSTALLED ROD AND TIGHTENED HARDWARE. - [SDR 98ZZZX4012](https://openairdocs.org/sdr/98ZZZX4012), Sep 24, 1998: FAN FRAME. CRACKED. THE NR 1 ENGINE REVERSER SEAL SUPPORT RING, LEFT, WAS FOUND CRACKED AT ALL FIVE FORWARD ATTACH POINTS. THE FLANGE SECTIONS HAD BROKEN COMPLETELY AWAY FROM THE T - [SDR CALA9801671](https://openairdocs.org/sdr/CALA9801671), Sep 9, 1998: HYD LINE. PUNCTURED. THE NR 2 HYDRAULIC SYSTEM QUANTITY AND PRESSURE WAS LOST ON APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HOLE IN HYDRAULIC PRESSUR - [SDR CALA9801456](https://openairdocs.org/sdr/CALA9801456), Aug 16, 1998: SMOKE DETECTOR. INOPERATIVE. THE AFT CARGO FIRE WARNING LIGHT AND SMOKE DETECTOR LIGHT ILLUMINATED WHILE ENROUTE. EMERGENCY PROCEDURES WERE COMPLIED WITH AND THE LIGHTS EXTINGUISHED. BOTH C ## Other aircraft with N14079 - [Cancelled 1934-10-06](https://openairdocs.org/deregistered/N14079-1934-10-06): Waco YKC, S/N 4200, built 1934. Owner: [Kemmerer Mahlon S](https://openairdocs.org/faa-owner/KEMMERER%20MAHLON%20S), [Short Hills, NJ](https://openairdocs.org/faa-place/NJ/Short%20Hills) --- 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.