# N14062: 1973 Mcdonnell-Douglas DC-10-30, registration cancelled 2003-06-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 11, 2003 - Status when cancelled: Triennial form not returned - 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: 47863 - Year built: 1973 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 8, 1984 - Certificate issued: June 28, 1990 - Last registry action: October 15, 2002 - Mode S code: A0A5F5 - Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14062 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14062 - Page: https://openairdocs.org/deregistered/N14062-2003-06-11 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 (53, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0100244](https://openairdocs.org/sdr/CALA0100244), Mar 22, 2001: SUPPORT. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN LT HORIZONTAL STABILIZER SECONDARY PIVOT SUPPORT. THE PIVOT SUPPORT WAS REPLACED IAW EA 5310-03417 AND ECRA 5310-04118. - [SDR CALA0100238](https://openairdocs.org/sdr/CALA0100238), Mar 19, 2001: SKIN. CORRODED. INSPECTION FOUND FUSELAGE BELLY SKIN CORRODED AT STA 1364. THE CORRODED AREA OF SKIN WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-40-00, FIGURE 20. - [SDR CALA0100237](https://openairdocs.org/sdr/CALA0100237), Mar 19, 2001: BOLT. SHEARED. INSPECTION FOUND BOLT SHEARED IN RT WING FORWARD SPAR TO FUSELAGE ATTACH ANGLE. THE BOLT WAS REPLACED IAW SRM 51-38-01. - [SDR CALA0100236](https://openairdocs.org/sdr/CALA0100236), Mar 19, 2001: BEAM. CORRODED. INSPECTION FOUND GALLEY G1A-G5 RT SUPPORT BEAM CORRODED. A NEW SUPPORT BEAM WAS INSTALLED IAW SRM 51-35-00. - [SDR CALA0100235](https://openairdocs.org/sdr/CALA0100235), Mar 18, 2001: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT STA 1139, LONGERON 51L. THE CORRODED SECTION OF FRAME WAS REMOVED AND A NEW SECTION WAS INSTALLED. - [SDR CALA0100217](https://openairdocs.org/sdr/CALA0100217), Mar 11, 2001: FLOORBEAM. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM AT STA 1298, RT, APPROXIMATELY TEN INCHES FROM EXTERNAL SKIN JOINT. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE - [SDR CALA0100210](https://openairdocs.org/sdr/CALA0100210), Mar 6, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND GALLEY G6 O/B FLOOR SUPPORT BEAM CORRODED AT STA Y = 1902-2007, X = 48R. THE FLOOR SUPPORT BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW - [SDR CALA0100209](https://openairdocs.org/sdr/CALA0100209), Mar 6, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND GALLEY G7 I/B FLOOR SUPPORT BEAM CORRODED AT STA Y = 1887-2007, X = 24L. THE FLOOR SUPPORT BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW - [SDR CALA0100208](https://openairdocs.org/sdr/CALA0100208), Mar 6, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND GALLEY G7 O/B FLOOR SUPPORT BEAM CORRODED AT STA Y = 1902-2007, X = 48L. THE FLOOR SUPPORT BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW - [SDR CALA0000083](https://openairdocs.org/sdr/CALA0000083), Jan 26, 2000: SKIN. CORRODED. INSPECTION FOUND LOWER FUSELAGE SKIN CORRODED WITH A PULLED RIVET AT STA 1761 BETWEEN STRINGER 45R AND 47R. REPAIRED IAW SRM 51-71-00. - [SDR CALA0000079](https://openairdocs.org/sdr/CALA0000079), Jan 25, 2000: DOOR SILL. CORRODED. INSPECTION FOUND FORWARD CARGO DOOR JAMB LOWER AFT CORNER DOOR SILL CORRODED. THE DOOR SILL WAS REPAIRED IAW SRM 53-70-00. - [SDR CALA9900120](https://openairdocs.org/sdr/CALA9900120), Feb 8, 1999: SUPPORT. CORRODED. INSPECTION FOUND THE RT MLG CYLINDER SUPPORT FRAME CORRODED IN ATTACHMENT BOLT HOLES. REPAIRED IAW ECRA 5743-01013. - [SDR CALA9800218](https://openairdocs.org/sdr/CALA9800218), Feb 12, 1998: ACTUATOR. LEAKING. THE NLG WAS VERY SLOW TO EXTEND AND INDICATE DOWN WHEN GEAR WAS LOWERED DURING TEST FLIGHT WHILE AIRCRAFT WAS IN D-CHECK AT MAN. MAINTENANCE FOUND THE NLG DOWNL - [SDR CALA9800193](https://openairdocs.org/sdr/CALA9800193), Feb 5, 1998: FRAME. CORRODED. INSPECTION FOUND CORROSION IN FRAME AND INTERCOSTALS IN AVIONICS BAY AT STA 450 BETWEEN STRINGER 44 AND 64L. THE AREA WAS REPAIRED IAW SRM 53-30-00. - [SDR CALA9800192](https://openairdocs.org/sdr/CALA9800192), Feb 5, 1998: STIFFENER. CORRODED. INSPECTION FOUND CORROSION AT LOWER LT CORNER OF DOOR IN AVIONICS COMPT AT REAR PRESSURE BULKHEAD STA 475, LT HORIZONTAL AND VERTICAL BEHIND GUSSET PLATE. THE A - [SDR CALA9800184](https://openairdocs.org/sdr/CALA9800184), Feb 4, 1998: LONGERON. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN LONGERON AT STA 1129, STRINGER 36R. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-10-00. - [SDR CALA9800176](https://openairdocs.org/sdr/CALA9800176), Feb 3, 1998: LONGERON. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN LONGERON AT STA 1129, STRINGER 36L. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-00-00. - [SDR CALA9800131](https://openairdocs.org/sdr/CALA9800131), Jan 28, 1998: BULKHEAD. FRETTED. INSPECTION FOUND, FRETTING ON CLG AFT PRESSURE BULKHEAD AT STA 1521. A REPAIR WAS ACCOMPLISHED IAW DOUGLAS DRAWING 90-53-1022. - [SDR CALA9800107](https://openairdocs.org/sdr/CALA9800107), Jan 26, 1998: ANGLE. CRACKED. INSPECTION FOUND A 1.2 INCH CRACK IN RT LOWER VERTICAL STABILIZER DRAG ANGLE AT FORWARD CENTER SPAR POSITION. THE ANGLE WAS REPAIRED IAW SRM 53-20-00, FIGURE 3. - [SDR CALA9701708](https://openairdocs.org/sdr/CALA9701708), Dec 1, 1997: FRAME. CRACKED. THE A/C LOST NR 3 HYDRAULIC SYSTEM AND GEAR UNSAFE LIGHT ILLUMINATED WHILE INBOUND TO EWR. THE A/C WAS TAKEN OUT OF SERVICE FOR T/S. INITIAL FINDINGS REVEALED T - [SDR CALA9701278](https://openairdocs.org/sdr/CALA9701278), Aug 28, 1997: BLADE. FAILED. NR 3 ENG MADE A LOUD BANG WITH EGT RISING TO 800 DEGREES AND N1 DROPPING TO 80 PERCENT WHILE EN ROUTE. THE ENGINE POWER WAS REDUCED TO IDLE AND OIL QUANTITY BEG - [SDR CALA9700731](https://openairdocs.org/sdr/CALA9700731), May 7, 1997: SKIN. DAMAGED. INSPECTION FOUND IMPACT DAMAGE TO SKIN AT STA 1901 TO 1921, STRINGER 7R AND SHEAR TIE HAD A 1.5 AND 1 INCH CRACK AT STA 1921 BETWEEN STRINGER 7R AND 8R. THE SKI - [SDR CALA9700730](https://openairdocs.org/sdr/CALA9700730), May 7, 1997: SKIN. DAMAGED. INSPECTION FOUND IMPACT DAMAGE TO FUSELAGE SKIN AT STA 1900 TO 1921 BETWEEN STRINGERS 7L AND 8L. THE SKIN WAS REPAIRED IAW SRM 53-20-00, FIGURE 6. - [SDR CALA9700743](https://openairdocs.org/sdr/CALA9700743), May 6, 1997: TEE SECTION. CORRODED. INSPECTION FOUND T-SECTION CORRODED AT STA 1986, LONGERONS 50R AND 51R. THE T-SECTION WAS REPLACED IAW SRM 53-10-00. - [SDR CALA9700742](https://openairdocs.org/sdr/CALA9700742), May 6, 1997: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL CORRODED AT STA 1975, LONGERON 47R AND 48R. THE INTERCOSTAL WAS REPLACED IAW SRM 53-10-00. - [SDR CALA9700752](https://openairdocs.org/sdr/CALA9700752), May 3, 1997: BEAM. CORRODED. INSPECTION FOUND SUPPORT BEAM CORRODED AT STA 1834 TO 1879, LAV F, X= -33. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-00. - [SDR CALA9700751](https://openairdocs.org/sdr/CALA9700751), May 3, 1997: BEAM. CORRODED. INSPECTION FOUND LATERAL SUPPORT BEAMS CORRODED AT STA 1879, X= +38 TO +53 AND X= -38 TO -53. THE SUPPORT BEAMS WERE REPLACED IAW SRM 53-22-00. - [SDR CALA9700750](https://openairdocs.org/sdr/CALA9700750), May 3, 1997: BEAM. CORRODED. INSPECTION FOUND SUPPORT BEAM CORRODED AT STA 1834 TO 1879, LAV E. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-00. - [SDR CALA9700749](https://openairdocs.org/sdr/CALA9700749), May 3, 1997: BEAM. CORRODED. INSPECTION FOUND INBOARD SUPPORT BEAM AND LATERAL SUPPORT BEAM CORRODED AT STA 1841 TO 1887, LAV F. THE SUPPORT BEAMS WERE REMOVED AND REPLACED IAW SRM 53-22-00 - [SDR CALA9700748](https://openairdocs.org/sdr/CALA9700748), May 3, 1997: BEAM. CORRODED. INSPECTION FOUND SUPPORT BEAMS CORRODED AT STA 1879, X = 4 TO 33 AND X = -4 TO -33. THE SUPPORT BEAMS WERE REPLACED IAW SRM 53-22-00. - [SDR CALA9700747](https://openairdocs.org/sdr/CALA9700747), May 3, 1997: BEAM. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT BEAM CORRODED AT STA 1899, X = 0 TO +20. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-00. - [SDR CALA9700745](https://openairdocs.org/sdr/CALA9700745), May 3, 1997: BEAM. CORRODED. INSPECTION FOUND LT GALLEY SUPPORT BEAM CORRODED AT STA 1879 TO 2007, X = 24. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-00. - [SDR CALA9700746](https://openairdocs.org/sdr/CALA9700746), May 1, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT L-1 DOOR, STA 395 TO 433. THE FLOORBEAM WAS REPLACED IAW SRM 53-27-00. - [SDR CALA9700744](https://openairdocs.org/sdr/CALA9700744), May 1, 1997: BEAM. CORRODED. INSPECTION FOUND LONGITUDINAL SUPPORT BEAM CORRODED AT LAV G, STA 1913 TO 2007. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-0. - [SDR CALA9700297](https://openairdocs.org/sdr/CALA9700297), Mar 2, 1997: PROX SWITCH. INOPERATIVE. WHEN GEAR WAS EXTENDED FOR LANDING, THERE WERE NO GREEN LIGHTS INDICATED ON FORWARD PANEL OR SECOND OFFICER'S PANEL. THE GEAR WAS CYCLED AND INDICATIONS WERE NO - [SDR CALA9700287](https://openairdocs.org/sdr/CALA9700287), Feb 27, 1997: HYD LINE. CHAFED. THE NR 1 HYDRAULIC SYSTEM FLUID QUANTITY AND PRESSURE DROPPED TO ZERO WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTEN - [SDR CALA9601793](https://openairdocs.org/sdr/CALA9601793), Dec 15, 1996: HYD LINE. RUPTURED. THE AIRCRAFT LOST NR 1 HYDRAULIC SYSTEM FLUID AFTER FLAP RETRACTION DEPARTING MAD. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO MAD WHERE IT LANDED WITHOUT - [SDR CALA9601489](https://openairdocs.org/sdr/CALA9601489), Oct 19, 1996: WAT SEP BAGS. DIRTY. THE FLIGHT ATTENDANTS REPORTED AN ODOR OF ELECTRICAL SMOKE WHILE ON APPROACH. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT FO - [SDR CAL960407](https://openairdocs.org/sdr/CAL960407), Mar 8, 1996: SKIN. DAMAGED. KUL - INSPECTION FOUND IMPACT DAMAGE AT LOWER AFT SECTION OF FORWARD CARGO DOOR CUT-OUT. THE AREA WAS REPAIRED IAW ECRA 5330-02370. (X) - [SDR CAL960405](https://openairdocs.org/sdr/CAL960405), Mar 4, 1996: ANGLE. CRACKED. KUL - INSPECTION FOUND TWO 1 INCH CRACKS IN ANGLE AT STA XCW 14 LT AND XCW 14 RT, BS 2123. A REPAIR WAS CARRIED OUT PER SRM 53-00-01, PAGE 7. (X) - [SDR CAL960404](https://openairdocs.org/sdr/CAL960404), Mar 4, 1996: SKIN. CRACKED. KUL - INSPECTION FOUND A DENT AND 1.25 INCH CRACK IN THE TOP SKIN OF THE LT HORIZONTAL STABILIZER INBOARD PANEL. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW S - [SDR CAL960406](https://openairdocs.org/sdr/CAL960406), Feb 29, 1996: FRAME. DAMAGED. KUL - INSPECTION FOUND A .50 INCH DIAMETER HOLE IN FRAME, STA 1841, ABOVE CENTER CARGO FLOOR AREA ON LT SIDE. THE FRAME WAS REPAIRED IAW ECRA 5310-03243. (X) - [SDR CAL960408](https://openairdocs.org/sdr/CAL960408), Feb 25, 1996: SPAR CAP. CRACKED. KUL - INSPECTION FOUND A 6 INCH CRACK JUST ABOVE RADIUS ON FORWARD SIDE OF RT WING AFT LOWER SPAR CAP AT STA 1043. THE SPAR CAP WAS REPAIRED IAW ECRA 5710-01720 - [SDR CAL960158](https://openairdocs.org/sdr/CAL960158), Feb 18, 1996: VALVE. LEAKING. FLT NR 10 - EWR - THE NR 1 HYDRAULIC SYSTEM BEGAN TO LOSE FLUID WHILE EN ROUTE FROM IAH TO ORY. THE QUANTITY DROPPED STEADILY. THE AIRCRAFT WAS DIVERTED TO EWR - [SDR CAL951068](https://openairdocs.org/sdr/CAL951068), Nov 27, 1995: HYD PUMP. CASE CRACKED. FLT NR 0005 - IAH - THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT ILLUMINATED AND THE NR 3 HYDRAULIC QUANTITY AND PRESSURE DECREASED TO ZERO IN FLIGHT. THE EMERGENC - [SDR CAL950941](https://openairdocs.org/sdr/CAL950941), Oct 19, 1995: EEL PIN. LOOSE. LAX - FLT NR 0063 - ROWS 19-33, INCLUDING OVERWING EMERGENCY LIGHTS COME ON WHEN POWER IS SHUTOFF. FOUND PIN 'V' DISARMED, PUSHED PIN BACK IN AT CONNECTOR. (M) - [SDR CAL950919](https://openairdocs.org/sdr/CAL950919), Oct 13, 1995: TRAILING EDGE. MISSING. FLT NR 0011 - ORY - A WALK AROUND INSPECTION, FOUND RIGHT INBOARD ELEVATOR TRAILING EDGE STRIP MISSING (APPROXIMATELY 24 INCHES). A PERMANENT REPAIR WAS PERFORM - [SDR CAL950600](https://openairdocs.org/sdr/CAL950600), Jul 15, 1995: EEL BATTERY. DISCHARGED. FLT NR 0012 - LAX - THE EMERGENCY LIGHTS WOULD NOT TEST DURING A PREFLIGHT CHECK. MAINTENANCE FOUND THE L-1 DOOR AND LEFT OVERWING BATTERY PACKS INOPERATIVE. TH - [SDR CAL950599](https://openairdocs.org/sdr/CAL950599), Jul 15, 1995: EEL BATTERY. DISCHARGED. FLT NR 0012 - LAX - THE EMERGENCY LIGHTS WOULD NOT TEST DURING A PREFLIGHT CHECK. MAINTENANCE FOUND THE L-1 DOOR AND LEFT OVERWING BATTERY PACKS INOPERATIVE. TH - [SDR CAL950598](https://openairdocs.org/sdr/CAL950598), Jul 15, 1995: EEL BATT CHARGER. INOPERATIVE. FLT NR 0012 - LAX - THE EMERGENCY LIGHTS WOULD NOT TEST DURING A PREFLIGHT CHECK. MAINTENANCE FOUND THE L-1 DOOR AND LEFT OVERWING BATTERY PACKS INOPERATIVE. TH All 53: https://openairdocs.org/deregistered/N14062-2003-06-11/reports.md ## 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 19971201040539I](https://openairdocs.org/incident/19971201040539I), Dec 1, 1997: Doug DC1030 (N14062), Newark, NJ, Minor damage. Left main gear retract cylinder boss fa iled allowing cylinder to sever hydraulic lines. Landed without incident - [Incident 19881231067289I](https://openairdocs.org/incident/19881231067289I), Dec 31, 1988: Doug DC1030 (N14062), Honolulu, HI. Crew window became unseated on takeoff roll. Aborted and stopped on runway. Found window seal loose. Replaced seal. ## Other aircraft with N14062 - [Cancelled 1975-10-20](https://openairdocs.org/deregistered/N14062-1975-10-20): Piper PA-18-150, S/N 18-8988. Exported to Australia. Owner: [T & D Air Inc](https://openairdocs.org/faa-owner/T%20%26%20D%20AIR%20INC), [Bloomington, IN](https://openairdocs.org/faa-place/IN/Bloomington) - [Cancelled 1955-10-20](https://openairdocs.org/deregistered/N14062-1955-10-20): Waco YKC, S/N 3987, built 1934. Owner: [Loudermilk Albert Russell](https://openairdocs.org/faa-owner/LOUDERMILK%20ALBERT%20RUSSELL), [Chicago12, IL](https://openairdocs.org/faa-place/IL/Chicago12) --- 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.