1995 LANCAIR 360
Aircraft Summary
General
Year
1995
Manufacturer
LANCAIR
Model
360
Condition
New
FlightRules
VFR
Based at
Switzerland
Total Time
0
Number of Seats
2
Description
Lancair 360 MKII (Large Tail) project
Specifications subject to verification by purchaser
Airframe
Airframe Notes
Experimental Kit Built Lancair 360 MKII (Large Tail)
o 90% Completed
o All new parts
o Can use AVGAS & MOGAS
o Construction under supervision of Swiss autorities
o Wing & tail load test performed
Material costs as of today (No Labour): USD 122,000 (all costs documented)
o Martin Hollman Tail Flutter modification
o R&G Epoxy laminating system approved for aerospace applications
o Rhino 9700 Fuel Tank Sealer (double treatment)
o Cabin heating system
o All Aeroquip 666 hoses
o 2x Infinity stick grip
o No vacuum system
Weight: As of today: 473.89 Kg
Estimated Weight for completion: 47.33 Kg
Total Estimated Empty Weight: 521.22 Kg
MTOW (Maximum Takoff Weight) Utility 4.4G: 764 Kg
MTOW Normal Category 3.8G (UFAC 1995): 794 Kg
Engine
Engine 1 Hot Section Time
0
Engine Notes
Lycoming YIO-360-M1A-EXP New (2011)
sn: EL-35544-51E
o Factory engine preservation & annual boroscope check
o Vetterman Exaust system
Props
Prop Notes
MTV-12-B / 175-59b (3 bladed, constant speed, composite) New (2011)
MTV spinner P281
Avionics
Avionics/Radios
Dynon EMS D120
AV-Map GPS
2x AV-30 Uavionix
AOA
o COM & Transponder to be defined (all wiring done)
o 2x USB charger
o RG400 coax cable
Additional Equipment
Additional Equipment
Lancair options
hydraulically activated Gear doors
Outback Gear
Canopy latch system
RT rudder
Fuel capacity 200L
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