N408FX
Registered owner: FLEXJET LLC, OH (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Flexjet, LLC (J7SA) | Certificate holder | — | Matched by certificate designator |
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.
5 reports on file, 2018-02-12 – 2020-11-12.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 3,434 hrs · 2,254 cycles
DISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REMOVED AND REPLACED EMERGENCY BATTERY 2, IAW EMBRAER LEGACY 450/50 AMM 33-51-01. OPERATIONAL CHECK GOOD.
Part: FAIRING — ERODED (VERTICAL STAB)
V-STAB TIP FAIRING IS SHOWING SIGNS OF EROSION AND PAINT PEELING. REMOVED AND REPLACED THE VERTICAL STABILIZER - AFT UPPER FAIRING AS REQUIRED.
Part: FAIRING — DAMAGED (VERTICAL STAB)
V-STAB TIP FAIRING IS SHOWING SIGNS OF EROSION AND PAINT PEELING. THIS SDR TO BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.
Part: ENGINE — POWER LOSS (NR 1) · airframe 1,462 hrs · 971 cycles
DURING DESCENT, AT APPROX. 11,000 MSL, THE NR 2 ENGINE FAILED N1 ROLLED BACK TO APPROXIMATELY 40 PERCENT BEFORE AUTO RELIGHT. THE FAIL MESSAGE WAS PRESENT IN THE IN THE NR 2 N1 GAUGE AFTER NR 2 RELIGHT, IT RAN WITHOUT EXCEEDING ANY TEMP OR SPEED PARAMETERS UNTIL SHUTDOWN WAS CONCLUDED AT CHOCK IN. THE AIRCRAFT LANDED WITHOUT INCIDENT. COMPLIED WITH OMS, FDR, AND FADEC DOWNLOADS. RAPID THROTTLE MOVEMENT PRECEDED THE EVENT. COMPLIED WITH OMS, FDR, AND FADEC DOWNLOADS. RAPID THROTTLE MOVEMENT PRECEDED THE EVENT. C/W WITH DETAILED LIST PROVIDED BY HONEYWELL AND EMBRAER AFTER ANALYZING THE DOWNLOADS. NO FAULTS FOUND. PERFORMED MULTIPLE SATISFACTORY HIGH POWER RUNS AND SATISFACTORY LEAK CHECK. SAME CREW CND THE FAULT ON THE MVF. MVF SUCCESSFUL.
Part: CONTROL UNIT — MALFUNCTIONED (BRAKES) · airframe 1,395 hrs · 923 cycles
INFLIGHT, RECEIVED A CYAN BRAKE RT & LT FAULT EICAS MESSAGE. ON LANDING ROLL & TAXI, THE BRAKES WERE LESS EFFECTIVE THAN USUAL. AIRCRAFT LANDED AND TAXIED WITHOUT INCIDENT. R & R BRAKE CONTROL UNIT. OPS CHECKED GOOD.