|
Pegasus
Quantum 912 Weightshift(Flexwing) Microlight - 'The motorcycle
of the Sky'

The Pegasus Quantum is a tandem 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 aircraft
grade 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
|
Pioneer
P200 3 Axis Landplane

The
P200 is a low wing side-by-side seat, dual stick controlled monoplane.
This relatively new aircraft has been designed with the beginner
in mind, being very forgiving yet giving extremely lively performance
that leaves many conventional aircraft standing. The aircraft
has very light control forces normally only found in very advanced
more aerobatic type of aircraft. This makes for a more relaxed
and less strenuous flight even in very turbulent conditions.
The
main structure is made from wood with steel fittings and covered
with polyfibre fabric. It is one of the most advanced microlight
aircraft in the world today and can comfortably cruise at more
than 100 mph with a top speed of 140mph. Fitted with the extremely
reliable Rotax 912 engine developing 80 hp driving a tractor propeller.
This
4-stroke, 4 cylinder horizontally opposed engine has dual transistorised
magneto spark ignition, integrated AC generator, electric starter
and dry sump lubrication. It uses normal unleaded petrol but can
operate on aviation gasoline (AVGAS) also.

Specifications
& Performance
|
Powerplant
|
Rotax 912 UL – 80hp
|
|
Maximum Continuous Power
|
5600 rpm
|
|
Aircraft Empty Weight
|
260kg
|
|
MTOW
|
450 kg
|
|
Vso @ Maximum All Up Weight)
|
39 mph
|
|
Vne (Maximum Speed)
|
140 mph
|
|
Va
|
113 mph
|
|
Vfe
|
70 mph
|
|
Vy
|
70 mph
|
|
Vx
|
56 mph
|
|
Best Climb Rate @ MAUW
|
800 ft/min
|
|
Best glide ratio @ 70 mph
|
10:1
|
|
Minimum Sink Speed @ 60 mph
|
600ft/min
|
|
Short Field Landing Full Flap
|
56 mph
|
|
Short Field Takeoff 1st Stage Flap after 15 m
|
56 mph
|
|
Maximum Crosswind
|
16 mph
|
|
Fuel Capacity
|
54 ltrs (4ltrs Un-useable)
|
|
Fuel Consumption @ 450 kg AUW & 85mph
|
12 ltrs per hour
|
|
Max Load
|
+4 –2 G
|
|
Max Bank
|
60 degrees
|
X-Air
3 Axis Landplane

The
X Air is a high wing side-by-side seat, dual stick controlled
monoplane. This popular aircraft has been designed with the beginner
in mind, being very forgiving yet giving very lively performance
especially when it comes to operating from short unprepared fields.
Experience has shown that students who learn on this aircraft
find conversion to other aircraft much easier. This is due
firstly to the requirement to use the rudder pedals in order to
fly the aircraft more precisely, and secondly, the light control
forces normally only found in more advanced type aircraft.
This makes for a more relaxed and less strenuous flight even in
turbulent conditions.
The
main structure is made from aluminium alloy tube with steel fittings
and covered with polyester (sailcloth) fabric. The aerofoil section
is defined by the use of pre-formed aluminium ribs. The undercarriage
has an independent sprung shock absorbing system on each of the
large wheel assemblies. The fuselage keel member is fitted with
a Rotax 912, 80 hp engine, reduction drive and tractor 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
|
243
kg
|
|
Maximum
Take off Weight
|
450
kg
|
|
Minimum
Occupant Weight
|
55
kg
|
|
Maximum
Useable Fuel
|
48
litres
|
|
Maximum
Bank Angle
|
60
degrees
|
|
Maximum
Pitch Angle
|
30º
down 45º Up
|
|
Maximum
Flight Loads
|
+4
/ -2 g
|
|
Stall
@ MAUW
|
30
mph
|
|
Manoeuvring
Speed (VA)
|
75
mph
|
|
Maximum
Permissible Speed (Vne)
|
95
mph
|
|
Minimum
Sink Rate @ 38 mph
|
400
feet per min.
|
|
Best
glide ratio @ 40 mph still air
|
6.7:1
|
|
Take
off distance to 50 feet at MAUW
|
269
metres
|
|
Maximum
rate of climb @ 45 mph (MAUW)
|
625
feet per min.
|
|
Landing
distance from 50 feet @ MAUW
|
230
metres
|
|
Maximum
Continuous Power
|
5600
rpm
|
|
Fuel
Consumption @ 375 kg AUW & 50mph
|
10
ltrs per hour
|
|