Aircraft > Turboprop > Lancair > N750BH: Lancair PROPJET
Flight Rules: IFR Based at: KRDM Total Time: 512.8 Number of Seats: 4 The Lancair Propjet is a four-seat, pressurized, composite aircraft powered by a 751-shp Walter M601E turboprop engine. The aircraft is based on the successful Lancair kit-plane, the Lancair IV-P. Like its piston-powered predecessor, the Propjet is noted for its performance, with a typical cruise speed of 325 knots at 24,000 feet and a climb performance of 4,000 feet per minute. General Specs: - 4 passengers, Wingspan 30 ft 3 in, Gross Weight 3,800 lbs, Fuel Capacity 145 gal. Performance Specs: - Cruise 370 mph, Range 1,216 nm, Climb rate 4,000 fpm(gross), Take Off Roll 1,200 ft, Landing Roll 1,400 ft.
Avionics Notes: Dual Garmin G3X EFIS Garmin G3X Autopilot with GMC 507 Control Head GTN 750 NAV/COM/GPS GTX 45R Transponder GTR 20 COM 2 G5 Backup AI ADSB Compliant
Airframe Notes: Extensive maintenance performed in January 2023 CAV TKS Systems (Airframe and Propeller) Updated Garmin Avionics Flight Line A/C System HID Taxi and Landing Lights 35 Gallon Aux Fuel Tank MOD 145 Gallon Fuel Systems Modifications: CAV TKS Systems Belly Tank Modified to be AUX fuel tank TKS tank removable in baggage compartment with external fill port Emergency Blow Down Gear System (no hand pump)
Engine Notes: Walter M601E 751-SHP IRAN performed 2/17/2020 AFTT 503.1 HRS 9.37 hrs since IRAN (Overhaul) Overhaul 2,000 hrs, 2,250 cycles or 8 years whichever comes first Propeller Notes: AVIA V508E/84/A TKS De-ice New AVIA Propeller installed 10/7/2020 AFTT 503.1 hrs 9.37 hrs TSN Overhaul 2,500 hrs or 72 months whichever comes first
Exterior Notes: Aircraft Re-Painted 3/24/2015 Interior Notes: 10/26/2015 Interior Headliner Replaced