NCFAKB
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
5 reports on file, 2023-02-22 – 2024-04-01.
Part: LONGERON — CRACKED (ZONE 400) · airframe 42,789 hrs · 88,369 cycles
RH ENGINE NACELLE OUTBOARD LOWER LONGERON CRACKED.
Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,337 hrs · 87,085 cycles
LH SIDE FRAME AT FS218 CORRODED BEYOND MANUAL LIMITS.
Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,337 hrs · 87,085 cycles
RH SIDE FRAME AT FS219 CORRODED BEYOND MANUAL LIMITS.
Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,002 hrs · 86,094 cycles
SUPPLEMENT REPORT TO CONTROL NUMBER 2023F00064. PLEASE CHANGE CONTROL NUMBER FROM 2023F00064 TO OPERATOR UNIQUE CONTROL NUMBER S9BA20230001. ALL OTHER INFORMATION IS THE SAME. RH SIDE FUSELAGE SKIN (.050) CORRODED (.023) DEEP BEYOND SRM LIMITS (.006) AT FS131-FS132 AT TOP OF WINDOW CUTOUT.
Part: STRUCTURE — CORRODED (ZONE 200) · airframe 42,002 hrs · 86,094 cycles
RH SIDE FUSELAGE SKIN (.050 THICK) CORRODED (.023 DEEP) BEYOND SRM LIMITS (.006) AT FS131-FS132 AT TOP OF WINDOW CUTOUT.