2005 LANCAIR IV-P

General Specs (cont.)

Total Time:873

Engine 1 Time:873 SNEW

Prop 1 Time:0 SNEW

Condition:Used

Flight Rules:BTH

# of Seats:4

Additional Classifications

Experimental / Homebuilt

Detailed Description

-TSIO-550 turbocharged engine
-Inspected and flight tested at Straight Flight KAPA
-located in Montana
-Engine IRAN Straight Flight KAPA July 2025
-Mags overhauled
-door latches overhauled
-New Hartzell Scimitar propeller
-hull pressure tested 4.6 psi delta
-both Turbochargers Zero SOH Main Turbo Visalia CA Dec 2025
-Complete flight test verification July-Sept 2025
-Airframe & engine 1018TT,
-New Pistons & Rings & honed cylinders
-Fresh Annual Condition inspection July 2025
-Recent interior, paint, panel upgrade
-Regular Oil Analysis
-TKS anti-ice system (prop, wings, tail)
-Tanis PreHeat system Installed
-406 ELT. Next battery 2027
-Latest nose gear drag link and inspection
-new Hartzell HC-H3YF-1RF 3-blade metal scimitar propeller
-Transponder/altimeter & pitot static checks July 2025
-G3X Dual 10-inch screen
-GTX 45R Transponder
-G5 backup ADAHRS ADI/HSI
-GTN 650
-GMC 507, GDU 460, GDU 465, GEA 24, GSU 25
-GMU 11, GSA 28(2), GTR 20, GAD 29, GAP 26, GAD 27
-GMA 245R
-Air Conditioning, electric compressor
-Many other features, call for specifications
-252 KTAS FL220

Avionics / Equipment

G3X with Dual GDU

Airframe

TKS deice system