N362AS
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
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.
12 reports on file, 2018-02-08 – 2022-05-21.
Part: STAND OFF — BENT (ZONE 100) · airframe 4,020 hrs · 2,654 cycles
VISUAL INSPECTION REVEALS FOULING CONDITION EXISTS WHEN STEERING DAMPER IN FRONT OF PILOTS RUDDER PEDALS DURING OVERSTEERING EXTENDS FAR ENOUGH TO STRIKE AND EVENTUALLY CATCH AND BEND WIRING BRACKET AND CLAMP INBOARD AND FOUL THE WIRE BUNDLE.
Part: SHUTOFF VALVE — FAILED (ZONE 400) · airframe 3,340 hrs · 2,229 cycles
BLEED 2 OVERPRESSURE FOLLOWED BY BLEED 2 FAIL
Part: STARTER GEN — FAILED (ZONE 400) · airframe 2,742 hrs · 1,827 cycles
GEN 1 OFF BUS. POWERED DOWN, RESTARTED AND RECEIVED ENG CTRL FAULT
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 2,050 hrs · 1,389 cycles
EMERGENCY LIGHTS STAYS ON IN ARM POSITION OR FLASHES ON/OFF IN ARM AND ON. REPLACED BATTERY PACK.
Part: TRIM SYSTEM — MALFUNCTIONED · airframe 1,550 hrs · 1,071 cycles
DESCENDING THROUGH APPROXIMATELY 10,000â CREW RECEIVED A AP ROLL MISTRIM. CREW CORRECTED THE TRIM BASED ON THE ARROW IN THE TRIM WINDOW OF THE MFD AND SHORTLY THERE AFTER CREW RECEIVED YAW MISTRIM CAS. THESE TRIM CAS MESSAGES BECAME MORE IN MORE FREQUENT OVER A SHORT PERIOD OF TIME UNTIL THEY WERE GOING OFF ALMOST REPEATEDLY. CREW DISCONNECT THE AP AND HAND FLY THE AIRCRAFT. THIS RESULTED IN ALMOST A DUTCH ROLL TENDENCY TO THE LEFT AND A PITCH DOWN MOTION WITH MOMENTARY LOSS OF CONTROL OF THE AIRCRAFT. SHORTLY THERE AFTER CREW RECEIVED A FUEL IMBALANCE CAS. AS CREW EXPERIMENTED WITH SLIGHT/MOMENTARY ADJUSTMENTS TO PITCH, ROLL, AND YAW TRIMS, ALL AXIS WERE MET WITH VERY ABRUPT AND AGGRESSIVE CHANGES. BECAUSE OF THIS CREW OPTED TO DECLARE AN EMERGENCY AND DIVERTED.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 1,286 hrs · 869 cycles
EMERGENCY LIGHTS STAYS ON IN ARM POSITION OR FLASHES ON/OFF IN ARM AND ON. REPLACED BATTERY PACK.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 1,286 hrs · 869 cycles
EMERGENCY LIGHTS STAYS ON IN ARM POSITION OR FLASHES ON/OFF IN ARM AND ON. REPLACED BATTERY PACK.
Part: BRAKE — WARNING MESSAGE (EMERGENCY BRAKE) · airframe 976 hrs · 655 cycles
ON FIRST LANDING AFTER EMERGENCY PARKING BRAKE VALVE WAS CHANGED. CREW RECEIVED A PARK BRAKE SET WARNING AND CAS MESSAGES DURING LANDING ROLL OUT WHEN READY AIRCRAFT TOE BRAKES WAS APPLIED
Part: VALVE — LEAKING (EMERGENCY BRAKE) · airframe 975 hrs · 654 cycles
DURING PREFLIGHT CHECK. EMERGENCY BRAKE PRESSURE FOUND TO BE ZERO. PERFORMED A PRESSURE RECHARGE PROCEDURE. WITH PARK BRAKE SET THE EMERGENCY BRAKE PRESSURE CONTINUED TO BLEED DOWN. WITH PARK BRAKE RELEASED THE EMERGENCY BRAKE PRESSURE DECREASED RAPIDLY. REPLACED THE EMERGENCY PARKING BRAKE VALVE.
Part: BAFFLE — BROKEN (PRECOOLER) · airframe 850 hrs · 577 cycles
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.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 810 hrs · 555 cycles
EMERGENCY LIGHTS STAYS ON IN ARM POSITION OR FLASHES ON/OFF IN ARM AND ON
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 810 hrs · 555 cycles
EMERGENCY LIGHTS STAYS ON IN ARM POSITION OR FLASHES ON/OFF IN ARM AND ON.