N600AS
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
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.
6 reports on file, 2010-12-05 – 2020-02-15.
Part: ACTUATOR — FAILED (TE FLAPS) · airframe 4,241 hrs · 3,788 cycles
FLAP CAS FAIL IN FLIGHT ON APPROACH. RAN CHECKLIST. EMERGENCY DECLARED.
Part: SUPPORT BRACKET — CRACKED (CABIN DOOR) · airframe 4,016 hrs · 3,572 cycles
DURING INSPECTION. AFT MAIN CABIN DOOR SUPPORT BRACKET FOUND CRACKED ON FWD SIDE. THIS BRACKET SUPPORTS THE DOOR OPEN ATTACHEMENT ROD AND DOOR EXTENSION SYSTEM.
Part: ACTUATOR — INOPERATIVE (RT WING TE FLAP) · airframe 2,844 hrs · 2,477 cycles
FLAP FAIL DURING APPROACH. THE RT FLAP ACTUATOR FOUND INOPERATIVE.
Part: CONTROL UNIT — INOPERATIVE (BRAKE) · airframe 2,490 hrs · 2,155 cycles
ON TAXI OUT TO TAKEOFF, CREW HAD A BRAKE FAILURE. ACFT DEPARTED TAXI WAY & STOPPED WHEN THE RT GEAR SANK INTO THE DIRT. ACFT WAS RECOVERED & INSPECTED FOR DAMAGE. NO DAMAGED NOTED BUT DETERMINED THAT BRAKE CONTROL UNIT FAILED. INSTALLED REPAIRED BRAKE CONTROL UNIT & RETURNED THE ACFT TO SERVICE.
Part: SCREW — LOOSE (WINDSHIELD) · airframe 2,181 hrs · 1,871 cycles
FOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1 TURN LOOSE ON 100% OF SCREWS.
Part: STARTER GEN — VIBRATION (ZONE 400) · airframe 992 hrs · 785 cycles
CREW EXPERIENCED A VIBRATION IN CRUISE FLIGHT. WITHIN SEVERAL MINUTES A NR2 GEN OFF BUS CAS WAS ILLUMINATED. STARTER/GEN WAS REPLACED AND ACFT WAS RETURNED TO SERVICE.