N54EA
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.
4 reports on file, 2019-11-06 – 2022-05-17.
Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,507 hrs · 27,988 cycles
R/H FS 280 BEAM WEB IS CORRODED. REMOVED AND INSTALLED LH FS 280 WEB IAW EO C550/700-53MA-009
Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,507 hrs · 27,988 cycles
R/H FS 280 BEAM WEB IS CORRODED. REMOVED AND INSTALLED RH FS 280 WEB IAW EO C550/700-53MA-009
Part: BEAM — CRACKED (FUSELAGE) · airframe 29,411 hrs · 27,367 cycles
CENTER POST BEAM HAS A CRACK FOLLOWING THE BEND RADIUS. BEAM LOCATED AT FS202.75.
Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 29,411 hrs · 27,367 cycles
DENT ON FORWARD FUSLEAGE BEYOND ALLOWABLE LIMITS LOCATED BETWEEN FS280 TO FS295 AND STR24R TO STR25R.