N368AS
Registered owner: EXECUTIVE AIRSHARE LLC, KS (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| EXECUTIVE FLIGHT SERVICES, LLC (E07A) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
FOUND CRACK ON LH AND RH NOSE OMEGA BEAM FORWARD SUPPORT BRACKET
LH WINDSHIELD CRACKED IN CLIMB AT FL 270
LH WINDSHIELD CRACKED IN CLIMB AT FL 270
ON TAXI OUT. ECS 2 FAIL CAS. ECS DISPLAY SHOWED RED X ON ECS VALVE 2.
BLEED 1 OVER PSI, FOLLOWED BY BLEED1 FAIL IN FLIGHT
EMERGENCY LIGHTS STAYS ON IN ARM POSITION OR FLASHES ON/OFF IN ARM AND ON. REPLACED BATTERY PACK.
EMERGENCY LIGHTS STAYS ON IN ARM POSITION OR FLASHES ON/OFF IN ARM AND ON. REPLACED BATTERY PACK.
CRACKED RT PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION IAW SERVICE LETTER 505-36-0003. REPLACED WITH OVERHAULED UNIT.
CRACKED RH PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION IAW SERVICE LETTER 505-36-0003. REPLACED WITH OVERHAULED UNIT.
BLEED 1/2 FAIL. IAW SIL505-36-0003 INSPECTED ENGINE PRECOOLER AND FOUND INLET AIR DEFLECTOR BAFFLES BROKEN OFF AND LAYING ON TOP OF COOLER. REPLACED PRECOOLER ASSY.
BLEED 1/2 FAIL. PER SIL505-36-0003 INSPECTED ENGINE PRECOOLER AND FOUND INLET AIR DEFLECTOR BAFFLES BROKEN OFF AND LAYING ON TOP OF COOLER.
ENROUTE, CREW RECEIVED A NR 2 GENERATOR OFFLINE, WITH VIBRATION. ENGINE THROTTLED BACK TO IDLE. VIBRATION STILL PRESENT. CREW PERFORMED PRECAUTIONARY ENGINE SHUTDOWN IAW QUICK REFERENCE HANDBOOK AND DIVERTED. RT STARTER FOUND WITH BEARING DAMAGE.
CREW RECEIVED NUMERIOUS CAS MESSAGES FROM MULTIPLE SYSTEMS. PFD1 WENT INTO REVERSIONARY MODE. GEA 2 WAS DETERMINED TO HAVE GONE OFF LINE.
EMERGENCY LIGHTS STAYS ON IN ARM POSITION OR FLASHES ON/OFF IN ARM AND ON.
EMERGENCY LIGHTS STAYS ON IN ARM POSITION OR FLASHES ON/OFF IN ARM AND ON
AHRS1 FAIL, AP/FD FAIL, YAW DAMP FAIL. EMERGENCY DECLARED AND DECENT DUE TO CREW PERCEIVED AHRS2 FAIL THAT WOULD CAUSE VENTRAL RUDDER FAIL AND DUTCH ROLL TENDENCIES. AHRS1 RESTARTED AND ALL SYSTEMS RETURNED TO NORMAL. CMC EVALUATION AND FIM TASK FOR AHRS1 DETERMINED TO BE TRANSITORY.