N3618 - 2014 MOSQUITO XET
Aircraft Summary
General
Year
2014
Manufacturer
MOSQUITO
Model
XET
Registration #
N3618
Serial Number
MXE1231F13B
FlightRules
VFR
Condition
New
Total Time
1.0
Number of Seats
1
Description
Brand new, factory built, never flown by anyone but the factory. Complete and ready to go, still at factory.
This is the ultimate experience in performance, technology and pure "wow" factor. With a top speed over 100 mph and rated climb rate of 1200 feet per minute this performer will satisfy the most demanding pilot and turn heads and gather crowds wherever you travel. There is nothing like the pure power and sound of the turbine propelling your helicopter into performance parameters all others will envy.
MANUFACTURERS SPECIFICATIONS
- Length: Airframe 16 ft / Overall 20 ft
- Width: 72 inch
- Height: 84 inch
- Main Rotor Diameter: 19 ft 6 inch
- Tail Rotor Diameter: 40 inch
- Empty Weight: 433 lb
- Gross Weight: 820 lb
- Useful Load: 240 lb
- Fuel Capacity: 20 gallon
- Engine: Solar T62-2A1
- Engine Power: HP 90 hp
- Battery/Starter: 12 VDC
- Alternator: 180 watt
PERFORMANCE
- Maximum Speed: 100+ mph
- Cruise Speed: 80 mph
- Climb Rate (est): 1200 fpm
- Flight Time: 2.2 hr
- Range: 160 miles
- Fuel Consumption: 8.5 gal/hour
- Main Rotor RPM: 590
- Tail Rotor RPM: 2700
- Hover in Ground Effect: 9000 ft
- Hover Out of Ground Effect: 7000 ft
Build turbine helicopter time for around $50 per hour!! This is legally recognized as a turbine helicopter!!
Only a private fixed wing license is required to fly the Mosquito XET in the US. No helicopter license is needed.
Airframe
Airframe Notes
The Mosquito XE airframe is a unibody construction made entirely of high quality fiberglass in a vinylester matrix.
Body and structure are the same to minimize weight and maximize structural efficiency.
Engine
Engine Notes
Engine:
90 hp (67 kW) Solar T62-2A1 turbine.
The Solar T62 Titan is an American gas-turbine engine used mainly as a helicopter Auxiliary Power Unit, ground power generator or helicopter power-plant.
General characteristics
- Type: Turboshaft
- Length: 33.41 in (84.86 cm)
- Diameter: 21.375 in (54.293 cm)
- Dry weight: 142 lb (64 kg) lb
Components
- Compressor: Centrifugal Impeller
- Combustors: Annular reverse flow with six burners
- Turbine: Radial inflow impeller
- Fuel type: JP-4 / JP-5 / JP-8
- Oil system: Wet sump
Performance
- Maximum power output: 60 to 150 hp (45 to 112 kW
Power Train:
The primary reduction is bolted directly to the engine. A centrifugal clutch on the engine crankshaft permits startup of the engine without the load of the rotor.
XET Engine Power is transmitted from the clutch to the driven pulley of the reduction through an HTD cog belt, one of the highest power to weight ratio power transmission methods available. The driven pulley houses the sprage clutch which permits the rotor to overspeed the engine during autorotation. Power is transmitted to a splitter gear box at the front of the tail boom through flex couplings and a floating drive shaft. The gear box sends power to the tail rotor through a drive shaft housed in the tail boom. Another floating drive shaft then transmits power to the secondary reduction at the top of the mast which drives the main rotor through a second high capacity HTD cog belt.
Props
Prop Notes
The main rotor is a semi-rigid configuration. Main rotor blades consist of an aluminum spar bonded to a wrapped aluminum sheet skin. Foam plugs at both ends prevent interior contamination and pumping losses. The tail rotor is also of a semi-rigid configuration with aluminum skin wrapped around a tube and foam plugs at either end. A 45 degree drag hinge is utilized to maintain tail rotor alignment.
Avionics
Avionics/Radios
Stratomaster Enigma Glass Panel EFIS / EMS / NAVIGATOR / GPS
Additional Equipment
Additional Equipment
The control system is unique to the Mosquito. Main rotor control is achieved from the floor mounted joystick and collective through a control mixer in the base of the main mast, then through push tubes in the mast up to the base of the swash plate. The swash plate is contained within the mast and is supported by a push tube located in the rotor shaft. Control rods on either side of the push tube transmit inputs through the rotor shaft to the control lever on top of the rotor shaft and then down to the blade pitch horns through pitch links.The tail rotor is controlled by the foot pedals through a push pull cable to an actuating lever on the tail rotor shaft.
- Collective friction lock
- Ground handling wheels
- Vertical fin
- Strobe
- Aux fuel tank
- VHF comm and transponder antennas and wiring (ready for radios)
- New David Clark K10 helmet with headset
Exterior
Year Painted
2013
Interior
Year Interior
2013
Recommended For You
View All(Recommended For You)Aircraft.com does not own the rights to the images displayed on this site. We do not have information regarding the original seller or source of these images unless explicitly stated.


