The World's First
Lancair  ES-P  Pressurized

"What a Columbia 400 Wants To Be When It Grows Up!"

N301ES
For full specifications in PDF, click here
For more information  - call or email Robert Simon
Phone:  614-214-9087
Email:  lancair-esp@ustek.com

Mt. St. Helens WA                                                                                 Lake Powell AZ 
Lancair:  A Real "Room With A View" 
 

Lancair Command Center

Kitplanes Magazine Feature October 2008

Oshkosh 2008 Outstanding Workmanship Award

                Composition:        Graphite fiber composite, autoclaved components
                Configuration:      Fixed gear, 4 person w/pressurized cargo
                Engine & Prop:     TSIO550 @ 400 hp, MT 4-blade feathering
                Aspiration:           Twin-turbocharged with 3 intercoolers
                Ignition:               One EI by LightSpeed Engineering plus one mag
                Fuel:                     100 LL, 100 std./116 max. US gal, (580/673 lb) useable
                Electric:                24v, three alternators, dual batteries, dual buss
                Comfort:               Pressurized, A/C, reclining heated seats
                Weights:                MTOW 3900lb,  MLW 3800lb,  empty 2540lb
                                            Useful load 1360lb,  useful load std. fuel 780lb
                                            (4 adults plus 100lb baggage)
                Performance:         Cruise RoP        260 kt (300 mph)+
                                            Cruise LoP         235 kt (270 mph)+
                Ceiling                  FL280 (28,000 feet)
                Range                   1,350 nm (1,550 sm)

Avionics:         
Panel by Avionics Systems, Chelton 3-screen Flight System, Garmin GNS480, SL30, and GTX327, L3 Stormscope, Ryan/Avidyne TCAD, WSI 300 weather, PSE intercom /Sirius radio, TruTrak Sorcerer AP, Grand Rapids EIS, full standby instruments, AOA (angle of attack), Bose headsets,  CO monitor, TechFibre met/graphite ground planes.  

Other:
Leading edge and prop de-ice by RDD Enterprises/Kelly Aerospace, dual heated pitot, dual oil pumps with micromesh filtration and chip detector, oil & cylinder pre-heaters, panel controlled Mountain High O2, XeVision HID landing lights with pulse, Precise Flight speed brakes, insurance by AIG. 

Finish: Graphics by Scheme Designers, paint by Sturgis Aviation

                    
De-ice: Therm-X hot wing & prop de-ice by RDD Enterprises: www.rddent.com

Interior: GSK Enterprises: gskenterprises@msn.com

Leisurely flight from
Redmond Oregon to Wichita Kansas
1,140nm VFR at 17,500ft:

157kt IAS or
210kt TAS
burning 17gph (LoP)
calculates as
235kt TAS at FL250