N621AX
Registered owner: BC AIRCRAFT LEASING LLC, NM (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
14 reports on file, 2008-07-27 – 2011-02-06.
Part: MEC — DEFECTIVE (NR 3 ENGINE) · airframe 67,487 hrs · 11,371 cycles
AFTER 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. R & R OF NR 3 MAIN ENG CONTROL & FUEL PUMP SEE LOG PAGE 116780, ALSO CHANNEL NR 3 ENG CIT SENSOR 116779, ALSO ACCOMPLISHED WORTAN 11-0076 BOROSCOPE OF ENG IAW 72-00 AND HAD NO FINDINGS. ALSO ACCOMPLISHED WORTAN 11-0077 INSP OF CLIP DETECTORS WITH NO FINDINGS & VISUAL OF ENG & 8TH STAGE CK VALVE. RAN ENG AFTER MEC & FUEL PUMP R & R IAW JRH. OPS CK GOOD.
Earlier reports · 2008–2010 · 13 reports
2010
Part: FLOOR SUPPORT — CORRODED (BS 495-515) · corrosion level 2 · airframe 65,741 hrs · 11,005 cycles
CORROSION 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 B1CB30MYRK4X.
Part: INTERCOSTAL — DAMAGED (BS 1900-1921) · corrosion level 2 · airframe 65,741 hrs · 11,005 cycles
CORROSION 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 BACR30MY6X3 B/N 5836050 IAW SRM.
Part: ANGLE — CORRODED (BS 1099) · corrosion level 2 · airframe 65,741 hrs · 11,005 cycles
CORROSION 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.
Part: ANGLE — CORRODED (BS 1781) · corrosion level 2 · airframe 65,741 hrs · 11,005 cycles
CORROSION 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.
Part: FLOORBEAM — CORRODED (BS 2007) · corrosion level 2 · airframe 65,741 hrs · 11,005 cycles
BS 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 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 SRM VOL II 51-33-01 PAGE 34. BACB30MYGKGX.)
Part: FLOORBEAM — CORRODED (BS 2007) · corrosion level 2 · airframe 65,741 hrs · 11,005 cycles
BS 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 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 SRM VOL II 51-33-01 PAGE 34. BACB30MYGKGX.)
Part: FLOORBEAM — CORRODED (BS 2007) · corrosion level 2 · airframe 65,741 hrs · 11,005 cycles
BS 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 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 SRM VOL II 51-33-01 PAGE 34. BACB30MYGKGX.)
Part: FLOORBEAM — CORRODED (BS 2007) · corrosion level 2 · airframe 65,741 hrs · 11,005 cycles
BS 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 SRM VOL II, 51-33-01, PAGE 34, BACB30MYGKGX.
Part: FLOOR SUPPORT — CORRODED (BS 1700-1781) · corrosion level 2 · airframe 65,741 hrs · 11,005 cycles
CORROSION 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.
Part: FLOORBEAM — CORRODED (BS 1741) · corrosion level 2 · airframe 65,741 hrs · 11,005 cycles
CORROSION 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.
Part: FLOORBEAM — CORRODED (BS 1741) · corrosion level 2 · airframe 65,741 hrs · 11,005 cycles
CORROSION 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.
Part: FLOORBEAM — CORRODED (BS 1741) · corrosion level 2 · airframe 65,741 hrs · 11,005 cycles
CORROSION 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.
2008
Part: MANIFOLD — MALFUNCTIONED
LOST NR 3 AND SYSTEM WITH EVEN OFF LIGHT. R & R NR 3 SYSTEM FILTER MANIFOLD. IAW MM 29-10