Airdale Airdale

The Airdale is the production version of John Larsen’s “Pursang”. John took his original Avid MkIV “Hauler” and highly modified it to suit the 4 cycle, 4 cylinder horizontally opposed 100hp Subaru EA81 auto engine. Engine options now include Continental and Rotax.
Modifications to the original Avid included:
-Fuselage stretched by 16″ to give better ground handling and CG flexibility.
-Two piece, easy to install, 74″ wide track aluminum landing gear.
-Re-raked windshield.
-Simplified control system which incorporated differential flaperon controls.
-Redesign of cockpit structure to remove tubes from behind seats giving easier access to a larger baggage area (55 gal. drum size).
-Individual, fully adjustable, easy to remove tilt and slide seats.
-Belly structure in footwell area modified to give extra leg and head room.
-Double tailspring for better resilience to rough terrain landings.
-Wider cockpit and doors to accommodate larger pilot and passenger.
-Redesigned cowling to accommodate greater range of engines.
-Modifications to Avid wing to increase Gross Weight capability to 1400 lb.
-Full stress analysis to comply with JAR regulations at 1400 lb. Maximum Takeoff Weight.

Engine: Subaru EA-81, 100 hp
Hp range: 65-125
Cruise: 108 mph
Stall: 48 mph
Range: 860 sm
ROC: 900 fpm
To dist: 800 ft
Ldg dist: 400 ft
Fuel cap: 28 USG
Empty wt: 730 lb
Gross wt: 1400 lb
Length: 18.8 ft
Wingspan: 31 ft
Wing area: 132 sq.ft
Cockpit width: 43 in
Seats: 2
Landing gear: tail or nose wheel

Aircraft ULM Magellan

A high wing single seater with wooden wings and a spaceframe fuselage, the Magellan can take engines between 30 and 50 hp.

Engine: Rotax 503, 52 hp
Wing span: 9.3 m
Wing area: 12 sq.m
Empty weight: 150 kg
Fuel capacity: 45 lt
Seats: 1
Max speed: 200 kph
Cruise speed: 120 kph
Minimum speed: 60 kph
Climb rate: 5 m/s
Fuel consumption: 12 lt/hr
Price (1998): 145 000 Fttc
Kit price (1998): 95 000 Fttc

Aircraft Rasukan UCL Maja

A 2004 ultralight, the UCL is a two place single-engine, high wing airplane of conventional configuration consisting of a composite fuselage and wood wings. It is equipped with a fixed tricycle landing gear. +4g/-2g

Stall: 35 kt / 40 mph / 65 kmh
Cruise: 65 kt / 75 mph / 120 kmh
VNE: 86 kt / 99 mph / 160 kmh
Empty Weight: 252 kg / 556 lbs
MTOW Weight: 475 kg / 1047 lbs
Climb Ratio: 800 ft/min / 4.0 m/s
Glide Ratio: 10:1
Take-off distance (50ft obstacle): 490 ft / 150 m
Landing distance (50ft obstacle): 590 ft / 180 m

Aircraft Manufacturing & Design Patriot 150

The Patriot 150 aircraft is only being supplied as a factory-built S-LSA aircraft, and is not available in kit form.

Engine: Continental O-200, 100 hp
Wing Span: 32 ft. 10 in / 10 m
Wing Chord: 48 inches / 1.23 m
Wing Area: 132 sq. ft / 12.25 m.sq
Length: 20 ft. 6 in / 6.3 m
Gross Weight: 1,310 lbs / 595 kg
Empty Weight: 785 lb / 356 kg
Useful Load: 525 lb / 240 kg
Fuel Capacity: 24 US Gallons (2 x 12) 90 litres
Load Limits: +6 G / -3 G
VNE (Never Exceed Speed): 143 mph / 230 km/h
Cruise Speed (75%): 124 mph / 200 km/h
Stall Speed: 41 mph / 66 km/h
Stall Speed, no flaps: 46 mph / 74 km/h
Rate of Climb: 1,100 fpm / 5.6 m/s
Range (no reserve): 500 sm / 800 km
Endurance: 5 hours 5 hours
Service Ceiling: 12,000+ ft / 3,660 m
Take-Off Roll: 400 ft / 122 m
Landing Roll: 500 ft / 150 m
Cabin Height: 45 inches / 1.13 m
Cabin Width: 46 inches / 1.16 m
Landing Gear: tricycle, steerable nosewheel
Landing Gear Width: 78 inches 2.0 m
Seats: 2 side by side