N620AS
Registered owner: HGH AVIATION LLC, DE (owner ≠ operator)
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, 2010-04-18 – 2016-03-25.
Part: COMPUTER — FAILED (COCKPIT) · airframe 3,682 hrs · 2,987 cycles
WHILE AT CRUISE, CREW RECEIVED A GEA1 FAIL CAS MSG ALONG WITH NUMEROUS ASSOCIATED SYS FAULT CAS MSGS. DECLARED AN EMER & ELECTED TO DIVERT. GEA71 WAS REPLACED & ALL FAULTS CLEARED. ACFT WAS RETURNED TO SERVICE. SEVERAL OF THE KEY SYSTEMS EFFECTED WERE, NOSE GEAR DOWN INDICATION, AUTO PRESSURIZATION & N R 1 BLEED VLV.
Part: ENGINE — CONTAMINATED (ZONE 400) · airframe 3,549 hrs · 2,843 cycles
ON TAKEOFF, CREW NOTED SLIGHT SMOKE IN CABIN & SMELL OF BURNING OIL. RETURNED WITHOUT INCIDENT. THIS WAS FIRST FLIGHT AFTER OVERHAULED ENGS WERE INSTALLED. OPENED BLEED SYS & USED BORESCOPE TO INSPECTED ENG & BLEED SYS UP TO THE PRESS AFT PRESS BULKHEAD. NO INDICATION OF OIL IN THE BLEED SYS INCLUDING ENG CORE & ENG BLEED PORTS. PERFORMED ENG RUNS & OIL CONSUMPTION RUN IAW INSTRUCTIONS FROM MFG. DETERMINED CAUSE OF SMOKE & SMELL WERE FROM RESIDUAL OIL IN ENG CORE FROM OVERHAUL. ACFT WAS RETURNED TO SERVICE.
Part: SCREW — LOOSE (WINDSHIELD) · airframe 3,380 hrs · 2,679 cycles
FOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1/2 TURN LOOSE ON 15% OF SCREWS.
Part: PITOT TUBE — DELAMINATED (PITOT/STATIC SYS) · airframe 427 hrs · 285 cycles
ON POST FLIGHT INSPECTION IT WAS NOTICED THAT THE INSIDE OF THE RT PITOT TUBE WAS PEELING (DELAMINATED). NEW PITOT TUBE WAS INSTALLED BEFORE FLIGHT.