# N83071: 1982 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: 48293 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 2, 1992 - Certificate issued: June 3, 1992 - Last registry action: May 15, 2001 - Mode S code: AB5BC1 - Owner when cancelled: [Polaris Holding Company](https://openairdocs.org/faa-owner/POLARIS%20HOLDING%20COMPANY) - Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford) - Owner type: Corporation - Owner's area on the map: 41.0534° N, 73.5387° W: Placed by OpenAirDocs: center of Stamford, CT, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N83071 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=83071 - Page: https://openairdocs.org/deregistered/N83071-2003-06-11 From the FAA registry file of October 28, 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 (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9900638](https://openairdocs.org/sdr/CALA9900638), Jun 4, 1999: SUPPORT. CORRODED. INSPECTION FOUND LT AND RT MLG A FRAME SUPPORT BEAM BOLT HOLES CORRODED. THE SUPPORT BEAM WAS REPAIRED IAW SRM 57-20-00, PAGE 104. - [SDR CALA9900630](https://openairdocs.org/sdr/CALA9900630), Jun 3, 1999: MOUNTING. CORRODED. INSPECTION FOUND MOUNTING PLATE ASSEMBLY CORRODED AT STA 1876-1886 FROM POSITION X = 0.02L TO X = 0.10L. THE MOUNTING PLATE WAS REMOVED AND A NEW PLATE WAS INST - [SDR CALA9900611](https://openairdocs.org/sdr/CALA9900611), Jun 2, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND LT SEAT TRACK CORRODED FROM STA 1866 TO 1856 AT POSITION X = 0.74L. THE SECTION OF SEAT TRACK WAS REPAIRED IAW SRM 53-70-00, FIGURE 6. - [SDR CALA9900610](https://openairdocs.org/sdr/CALA9900610), Jun 2, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1903 FROM POSITION X = 0.25L TO X = 0.25R. THE FLOOR SUPPORT BEAM WAS REPLACED IAW 53-16-00, FIGURE - [SDR CALA9900607](https://openairdocs.org/sdr/CALA9900607), Jun 1, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND RT SEAT TRACK CORRODED FROM STA 1876-1866 AT POSITION X = 0.60R AND X = 0.60L. THE SEAT TRACK SECTIONS WERE REPAIRED IAW SRM 53-70-00, FIGURE 6 - [SDR CALA9900606](https://openairdocs.org/sdr/CALA9900606), Jun 1, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND RT SEAT TRACK CORRODED FROM STA 1866 TO 1856 AT POSITION X = 0.74R. THE CORRODED SECTION FOR SEAT TRACK WAS REPLACED IAW SRM 53-70-00, FIGURE 6 - [SDR CALA9900605](https://openairdocs.org/sdr/CALA9900605), Jun 1, 1999: BULKHEAD TEE. CORRODED. INSPECTION FOUND T-SECTION ON FORWARD FACE OF REAR PRESSURE BULKHEAD AT STA 2007 FROM POSITION X = 0.55L TO X = 0.65L CORRODED. THE CORRODED SECTION WAS REMOVED - [SDR CALA9900604](https://openairdocs.org/sdr/CALA9900604), Jun 1, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.27R TO X = 0.33R AND POSITION X = 0.38R TO X = 0.56R. THE FLOORBEAM CAPPING - [SDR CALA9900603](https://openairdocs.org/sdr/CALA9900603), Jun 1, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X =0.04R TO X = 0.22R. THE FLOORBEAM CAPPING SECTION WAS REPLACED IAW SRM 53-16-00 - [SDR CALA9900602](https://openairdocs.org/sdr/CALA9900602), Jun 1, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.60R TO X = 0.90R AND POSITION X = 0.60L TO X = 0.90L. THE FLOORBEAM CAPPING - [SDR CALA9900601](https://openairdocs.org/sdr/CALA9900601), Jun 1, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.04L TO X = 0.22L. THE FLOORBEAM CAPPING SECTION WAS REPLACED IAW SRM 53-16-0 - [SDR CALA9900600](https://openairdocs.org/sdr/CALA9900600), Jun 1, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.27L TO X = 0.38L. THE FLOORBEAM CAPPING SECTION WAS REPLACED IAW SRM 53-16-0 - [SDR CALA9900599](https://openairdocs.org/sdr/CALA9900599), Jun 1, 1999: BEAM. CORRODED. INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 2007 TO 1893 AT POSITION X = 0.60L AND X = 0.60R. THE CORRODED BEAM SECTIONS WERE REPLACED IA - [SDR CALA9900598](https://openairdocs.org/sdr/CALA9900598), Jun 1, 1999: BEAM. CORRODED. INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 2007 TO 1876 AT POSITION X = 0.25R AND X = 0.25L. THE CORRODED SECTIONS OF BEAM WERE REPLACED - [SDR CALA9900597](https://openairdocs.org/sdr/CALA9900597), Jun 1, 1999: BEAM. CORRODED. INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 1996 TO 1903 AT POSITION X = 0.20R AND X = 0.20L. THE CORRODED BEAM SECTIONS WERE REPLACED IA - [SDR CALA9900596](https://openairdocs.org/sdr/CALA9900596), Jun 1, 1999: BEAM. CORRODED. INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1986 FROM POSITION X = 0.60R TO 0.90R. THE CORRODED SECTION OF BEAM WAS REPLACED IAW SRM 53-16-00, F - [SDR CALA9900595](https://openairdocs.org/sdr/CALA9900595), Jun 1, 1999: BEAM. CORRODED. INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1986 FROM POSITION X = 0.27R TO X = 0.53R. THE BEAM SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10 - [SDR CALA9900594](https://openairdocs.org/sdr/CALA9900594), Jun 1, 1999: BEAM. CORRODED. INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1866, POSITION X = 0.03L TO X = 0.28L AND POSITION X = 0.03R TO X = 0.28R. THE BEAM SECTIONS WERE RE - [SDR CALA9900593](https://openairdocs.org/sdr/CALA9900593), Jun 1, 1999: BEAM. CORRODED. INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 1887 TO 1839 AT POSITION X = 0.03L AND X + 0.03R. THE BEAM SECTIONS WERE REPLACED IAW SRM 53- - [SDR CALA9900592](https://openairdocs.org/sdr/CALA9900592), Jun 1, 1999: BEAM. CORRODED. INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 1876 TO 1810 AT POSITION X = 0.36L AND X = 0.36R. THE BEAM SECTIONS WERE REPLACED IAW SRM 53- - [SDR CALA9800882](https://openairdocs.org/sdr/CALA9800882), May 18, 1998: LIGHT. INOPERATIVE. INSPECTION FOUND THE EMERGENCY FLOODLIGHT AT LAV B INOPERATIVE. THE FLOODLIGHT WAS REPLACED IAW MM 33-50-00. - [SDR CALA9800881](https://openairdocs.org/sdr/CALA9800881), May 18, 1998: BATTERIES. DISCHARGED. INSPECTION FOUND AFT MEGAPHONE INOPERATIVE. THE MEGAPHONE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD IAW MM 25-60-00. - [SDR CALA9800880](https://openairdocs.org/sdr/CALA9800880), May 17, 1998: ANGLE. CRACKED. INSPECTION FOUND A 1 CRACK IN ANGLE AT LT WHEEL WELL REAR SPAR, WS 118. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51- - [SDR CALA9800234](https://openairdocs.org/sdr/CALA9800234), Feb 14, 1998: TRIM MOTOR. CRACKED. THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT ILLUMINATED WHILE EN ROUTE TO EWR. APPROPRIATE CHECKLISTS WERE FOLLOWED AND BOTH PUMPS WERE SHUTOFF. THE HYDRAULIC FLU - [SDR CALA9800175](https://openairdocs.org/sdr/CALA9800175), Feb 2, 1998: SKIN. DENTED. INSPECTION FOUND A 2 X 3 DENT IN LT INBOARD LEADING EDGE SLAT WITH SIX POPPED RIVETS AT STA XIS 240.844. REPAIRED IAW ECRA 5750-02897 AND PLACED ON DIP TO REPLA - [SDR CALA9700809](https://openairdocs.org/sdr/CALA9700809), Jun 2, 1997: FIRE LOOP. CHAFED. THE NR 2 ENGINE FIRE WARNING LIGHT FOR B-LOOP (A LOOP WAS ON PLACARD) ILLUMINATED TEN MINUTES AFTER TAKEOFF. THE NR 2 ENGINE WAS SHUT DOWN, BOTH FIRE BOTTLES WE - [SDR CALA9700669](https://openairdocs.org/sdr/CALA9700669), Apr 8, 1997: SUPPORT. CORRODED. INSPECTION FOUND CORROSION ON FLOOR SUPPORTS AT STA 1875, LBL 30 AND RBL 30. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 53-16-01 AND 51-35-01. - [SDR CALA9700668](https://openairdocs.org/sdr/CALA9700668), Apr 8, 1997: SUPPORT. CORRODED. INSPECTION FOUND CORROSION ON FLOOR SUPPORTS AT STA 1887, RBL 24-80, LBL 20-80, AND LBL 3- RBL 3. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 53-16-01 AND 51-35-01 - [SDR CALA9700667](https://openairdocs.org/sdr/CALA9700667), Apr 8, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1880-2007, LBL 24 AND RBL 24. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 53-16-01 AND 51-33-01. - [SDR CALA9700670](https://openairdocs.org/sdr/CALA9700670), Apr 7, 1997: INTERCOSTAL. CORRODED. INSPECTION FOUND CENTER CARGO INTERCOSTAL CORRODED BETWEEN STA 1720-1740, STRINGER 51-52R. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-00-01. - [SDR CAL951081](https://openairdocs.org/sdr/CAL951081), Dec 3, 1995: BEARING. FAILED. FLT NR 28 - LGW - THE NR 2 ENGINE WAS SHUT DOWN FOR LOSS OF OIL WHILE EN ROUTE TO LGW. THE ENGINE WAS SHUT DOWN WITH POSITIVE OIL PRESSURE AND THE AIRCRAFT LAND - [SDR CAL950879](https://openairdocs.org/sdr/CAL950879), Oct 3, 1995: EEL BATT CHRGER. INOPERATIVE. EWR - FLT 0012 - WHEN THE EMERGENCY LIGHT SWITCH WAS PLACED ON AFTER ARRIVING IN EWR, THE FORWARD FIRST CLASS AREA AND AFT COACH SECTION TRACK LIGHTING WOULD NO - [SDR CAL950878](https://openairdocs.org/sdr/CAL950878), Oct 3, 1995: EEL BATT CHARGER. INOPERATIVE. EWR - FLT 0012 - WHEN THE EMERGENCY LIGHT SWITCH WAS PLACED ON AFTER ARRIVING IN EWR, THE FORWARD FIRST CLASS AREA AND AFT COACH SECTION TRACK LIGHTING WOULD NO ## Other aircraft with N83071 - [Cancelled 1989-07-19](https://openairdocs.org/deregistered/N83071-1989-07-19): Piper PA-28-161, S/N 288316015. N-number assigned, not yet registered - [Cancelled 1981-03-25](https://openairdocs.org/deregistered/N83071-1981-03-25): Piper PA-32R-301, S/N 32R-8013067. Exported to Chile. Owner: [Piper Aircraft Corp](https://openairdocs.org/faa-owner/PIPER%20AIRCRAFT%20CORP), [Lock Haven, PA](https://openairdocs.org/faa-place/PA/Lock%20Haven) - [Cancelled 1966-03-17](https://openairdocs.org/deregistered/N83071-1966-03-17): Aeronca 7AC, S/N 7AC-1727. Owner: [Jerry Batt](https://openairdocs.org/faa-owner/JERRY%20BATT), [Fort Wayne, IN](https://openairdocs.org/faa-place/IN/Fort%20Wayne) --- 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.