- Registered owner
- Isaacson Andrew C
- Location
- Medical Lake, WA
- Owner type
- Individual
- Serial number
- 002
- Type
- Rotorcraft
- Engine
- Electric
- Certificate issued
- April 3, 2015
- Expires
- April 30, 2028
- Mode S code
- A6EBAC
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 0
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N545NAMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Andrew C Isaacson A ISAACSON X-8 aircraft
FAA incident reports
No FAA accident or incident reports matched to N545NAMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Andrew C Isaacson A ISAACSON X-8 aircraft
Service difficulty reports
No reports matched to N545NAGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Andrew C Isaacson A ISAACSON X-8 aircraft
Reports on N545NA not matched to an aircraft · 5
They name N545NA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 02082901Pump · failedCrew called with Left Engine Driven Hyd. pump overheat and later with Left Hyd. Qty. loss. Aircraft returned to LAS, an uneventful landing was accomplished. Further investigation revealed that the #1 Engine E.D.P. had suffered mechanical failure, causing loss SDR 02051701Transmitter · fluctuatesRight Engine fuel flow fluctuation on climbout. An uneventful flight occured. Upon return to LAS, removed and replaced fuel flow transmitter. Ops check good as per M/M 73-31-01SDR 2001F00166Connector · disconnectedFOUND FLOOR ESCAPE PATH LIGHTING LENS MISSING AT ROW 12 AND AT ROW 25, LIGHT INOPERATIVE. AT ROW 12 REPLACED LENS, P/N 81000-22701. AT ROW 25 RECONNECTED CONNECTOR SYSTEM, OPERATIONAL CHECK GOOD. (M)
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.