
Weightshift training is provided by Flying
Flexwings at the Algarve Airsports centre using the Pegasus
Quantum 912 range of aircraft. The Pegasus Quantum is a tandem
dual seat, flexible wing, weightshift controlled microlight.
This aircraft has proved itself to be one of the most popular
weightshift aircraft in the world today, being used by the majority
of schools in the UK.


It
is a fun aircraft to fly where you actually feel part of the
aircraft and the flying environment. Often described as the
motorcycle of the sky, it is very manouverable with an unequalled
open cockpit view of the world below.

It
is extremely forgiving, having mild stall characteristics normally
associated with lower performance craft, yet still producing
fast cruise speeds and very high climb rates.
The
main structure of the rolling chassis (trike) is made from aluminium
alloy tube. Rigid composite seats are fitted, which locate onto
a tubular seat frame. The rear undercarriage comprises
of steel alloy tubes with elastomer suspension incorporated
into aluminium alloy struts. The nosewheel undercarriage
is steerable and incorporates footrests with throttle and brake
controls. The ‘hang glider‘ type wing is made from aluminium
alloy tubing and polyester (sailcloth) fabric with the aerofoil
section defined by pre-formed aluminium and composite ribs.
The
trike is fitted with a rear mounted Rotax 912, 80 hp engine,
reduction drive and pusher propeller. This 4-stroke, 4 cylinder
horizontally opposed engine has dual spark ignition, magneto,
dry sump lubrication and electric starter system. The cylinder
heads are liquid cooled and the barrels are ram-air-cooled.
It uses normal unleaded petrol but can operate on aviation gasoline
(AVGAS) also.
Specifications
& Performance
|
Empty
Weight
|
216.5
kg
|
|
Maximum
Take off Weight
|
409
kg
|
|
Minimum
Occupant Weight
|
55
kg
|
|
Maximum
Useable Fuel
|
47.4
litres (34 kg)
|
|
Maximum
Bank Angle
|
60
degrees
|
|
Maximum
Pitch Angle
|
45
degrees
|
|
Maximum
Flight Loads
|
+4
/ -0 g
|
|
Stall
@ MAUW
|
32
mph
|
|
Manoeuvring
Speed (VA)
|
59
mph
|
|
Maximum
Permissible Speed (Vne)
|
90
mph
|
|
Minimum
Sink Rate @ 40 mph
|
400
feet per min
|
|
Best
glide ratio @ 40 mph still air
|
7.92:1
|
|
Take
off distance to 50 feet at MAUW
|
130
metres
|
|
Maximum
rate of climb @ 45 mph (MAUW)
|
1000
feet per min
|
|
Landing
distance from 50 feet
|
190
metres
|
|
Fuel
Consumption @ 409 kg MAUW & 60mph
|
12
litres per hour
|
|
Maximum
Continuous Power
|
5600
rpm
|