- Registered owner
- Bc Aircraft Leasing LLC
- Location
- Albuquerque, NM
- Owner type
- LLC
- Serial number
- 48319
- Type
- Fixed wing multi engine
- Engine
- Turbo-jet
- Certificate issued
- December 2, 2013
- Expires
- December 31, 2029
- Mode S code
- A81A0A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 240
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1973 | 2 |
|---|---|
| 1974 | 8 |
| 1975 | 14 |
| 1976 | 8 |
| 1977 | 2 |
| 1978 | 10 |
| 1979 | 5 |
| 1980 | 8 |
| 1981 | 5 |
| 1982 | 1 |
| 1983 | 2 |
| 1984 | 6 |
| 1985 | 7 |
| 1986 | 4 |
| 1987 | 7 |
| 1988 | 7 |
| 1989 | 5 |
| 1990 | 6 |
| 1991 | 3 |
| 1992 | 9 |
| 1993 | 7 |
| 1994 | 14 |
| 1995 | 9 |
| 1996 | 11 |
| 1997 | 4 |
| 1998 | 2 |
| 1999 | 5 |
| 2000 | 8 |
| 2001 | 9 |
| 2002 | 6 |
| 2003 | 11 |
| 2004 | 8 |
| 2005 | 6 |
| 2006 | 6 |
| 2007 | 7 |
| 2008 | 4 |
| 2009 | 3 |
| 2010 | 6 |
| 2011 | 3 |
| 2012 | 1 |
| 2013 | 1 |
| 2014 | 1 |
| 2015 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2020 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 2 |
| 2025 | 1 |
| 2026 | 2 |
Airframe · Mcdonnell-Douglas DC-10-30
AD 2026-13-15NavigationAD 2026-13-02NavigationAD 2025-23-53Nacelles/pylonsEmergency ADInformation bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N621AXMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Mcdonnell-Douglas DC-10-30 aircraft
FAA incident reports
No FAA accident or incident reports matched to N621AXMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Mcdonnell-Douglas DC-10-30 aircraft
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CNMA20110001Mec · defectiveAFTER 1+ 25 INTO FLT. NOTICED NR 3 ENG N 2 FLUX BETWEEN 95-87 PERCENT N 2 ALSO NOTICE CONSIDERABLE VIBRATION NR 3 FUEL LEVER. AFTER NR 3 THROTTLE TO IDLE NOTICED NR 3 ENG FF/ EGT/ N2 ALSO FLUX. PERFORMED ENG FAILURE/ SHUTDOWN IN FLT. CKLIST IAW QRH 4-1-2-7. SDR CNMA20100020Floor Support · corrodedCORROSION ON FLOOR PANEL SUPPORT BS 485-515 RBL 55-60. DAMAGED FLOOR SUPPORT WAS REMOVED. NEW FLOOR SUPPORT PN OAI-53-0002 WAS FABRICATED AND INSTALLED USING FASTENERS BOCR1SCEGDG B/N 517060 B/N 828982 IAW SRM VOL 2, 51-35-01, PAGE 1 AND 51-33-01 PAGE 34 B1CBSDR CNMA20100023Intercostal · damagedCORROSION ON INTERCOSTAL BS 1900-1921 STR 43R. DAMAGED INTERCOSTAL AND ADJACENT ANGLE WERE REMOVED. NEW INTERCOSTAL AND ANGLE PN OAI53-004/005 WERE FABRICATED AND INSTALLED IAW ES0 53-03 AND DWC VCA7012 USING FASTENERS BACRI5CE606 B/N 5828382 AND BACR30MY6X3SDR CNMA20100022Angle · corrodedCORROSION ON NUT PLATE ANGLE BS 1099 LBL 41. REMOVED ANGLE AND NEW PN AOA7GG7-23 INSTALLED WITH NEW ANCHOR NUTS AND RIVETS IAW SRM VOL 2 51-31-01. PN BACB30NWGK3 B/N 5836738.SDR CNMA20100021Angle · corrodedCORROSION ON ANGLE C/T AFT CARGO TANK WALL BS 1781 4 PLACES RBL 30, RBL 36, LBL 30, LBL 36. DAMAGED ANGLE REMOVED, NEW FABRICATED PN OAI-53-00-11 IAW DWG AFA7548-21 & GMM 4.45 AND INSTALLED WITH FASTNERS IAW SRM VOL 2 51-31-01.SDR CNMA20100018Floorbeam · corrodedBS 2007, LBL 20-28 CORROSION ON M/D FLOOR SUPPORT TEE CHORD. ALL OPEN HOLES WERE NDT INSPECTED - NO CRACKS OR CORROSION WERE FOUND. THIS SECTION OF CHORD WAS INCLUDED IN THE REPAIR OF NRC -387. SEE NRC 387. (NONRO 387 CORRODED SECTION OF CHORD WAS TRIMMED OUSDR CNMA20100017Floorbeam · corrodedBS 2007, LBL 53-68 CORROSION ON FLOOR SUPPORT TEE CHORD. ALL OPEN HOLES NDT INSPECTED - NO CRACKS OR CORROSION FOUND. THIS SECTION WAS INCLUDED IN THE REPAIR OF NRC 387. NRC 387. (NONRO 387, CORRODED SECTION OF CHORD WAS TRIMMED OUT. NEW SECTION FABRICATED FRSDR CNMA20100016Floorbeam · corrodedBS 2007 LBL 77 CORROSION ON TEE CHORD FLOOR SUPPORT. ALL OPEN HOLES WERE NDT INSPECTED - NO CRACKS OR CORROSION FOUND. THIS SECTION OF CHORD WAS INCLUDED IN THE REPAIR OF NRC-387. SEE NRC 387. (NONRO 387, CORRODED SECTION OF CHORD WAS TRIMMED OUT. NEW SECTISDR CNMA20100015Floorbeam · corrodedBS 2007, LBL16 CORROSION ON THE TEE CHORD FLOOR STRUCTURE. CORRODED SECTION OF CHORD WAS TRIMMED OUT. NEW SECTION FABRICATED FROM THE TEE PN NJC6040-175 WAS INSTALLED WITH SPLICES PN N621AX-NRC387-1/-2 IAW SRM VOL I 53-40-00, FIG 16 AND USING FASTENERS IAW SSDR CNMA20100014Floor Support · corrodedCORROSION ON CTR CARGO LWR PANEL SUPPORT BS 1700-1781 BL-0.3, DAMAGED AREAS TRIMMED OUT. AREAS REINFORCED WITH DOUBLERS PN N621AX-NRC361-1 (QTY X3) FABRICATED AND INSTALLED IAW SRM VOL 1 53-00-01, FIG 8 USING FASTENERS IAW SRM VOL 2, 51-35-01, PAGE 1.SDR CNMA20100013Floorbeam · corrodedCORROSION ON CTR CARGO LWR PANEL SUPPORT BS 1741 LBL 16. DAMAGED SUPPORT REMOVED NEW FABRICATED PN OAI-53-0008 IAW SRM DWG AD0145-30 & OMNI GMM 4.45 AND INSTALLED WITH FASTNERS IAW SRM VOL 2 51-35-01, PAGE 1.SDR CNMA20100012Floorbeam · corrodedCORROSION ON CTR CARGO LWR PANEL SUPPORT BS 1741 RBL 16. DAMAGED SUPPORT REMOVED NEW FABRICATED PN OAI-53-0007 IAW SRM DWG AD00145 OMNI GMM 4.45 AND INSTALLED WITH FASTNERS IAW SRM VOL 2 51-35-01, PAGE 1.SDR CNMA20100011Floorbeam · corrodedCORROSION ON CTR CARGO LWR PANEL SUPPORT BS 1741 RBL 12-14. DAMAGED SUPPORT REMOVED NEW FABRICATED PN OAI-53-0009 IAW DWG AD00145 & OMNI GMM 4-45 AND INSTALLED WITH FASTNERS IAW SRM VOL 2 51-35-01, PAGE 1.SDR CNMA20080006Manifold · malfunctionedLOST NR 3 AND SYSTEM WITH EVEN OFF LIGHT. R & R NR 3 SYSTEM FILTER MANIFOLD. IAW MM 29-10
STCs that may be installed · 382
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Mcdonnell-Douglas DC-10-30
STC ST00272ATInstallation of an Airshow 210 enter- tainment system.STC ST00952LAInstallation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles.STC SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)