Merlin E-Z Flyer

EZ Flyer

The two-place ultralight trainer EZ-Flyer was designed by Canadian Wayne Winters, using a lot of the Merlin’s wing and tail structure.

The LSA EZ-Flyer II has a chromoly steel tube fuselage structure. It is a predominantly triangulated structure. The engine is pusher mounted behind the wing and on top of the steel fuselage cage. It can handle all the bigger Rotax engines and Merlin indicates that the 80-hp Rotax 912 four-stroke engine.

It is a 4130 chromoly steel construct that is painted at the factory prior to shipping. The wing has an aluminum “D” cell, is Ceconite covered and strut braced, but sports a large wingtip “fence” at the end that was removed from factory ships for testing. The ailerons are not quite full-span but are hinged in a frise-type setup with no differential. There are no flaps, and the wing is a constant chord assembly.

The rudder tri-gear has a set of very heavy spring steel gear legs and 18 inch tundra tires. The EZ-Flyer II is 21 feet long, 6 feet high, and has a span of 30 feet. The wing has 165 sq. ft. of wing area, a 10 US gal fuel capacity, and is stressed to +4 and -2 Gs. With the standard Rotax 503, the 465-lb EZ-Flyer II has a max gross weight of 1000 lbs, leaving more than a 500 lbs payload.

The empty EZ-Flyer has a tendency to sit on its tail with the nose sticking skyward.

Dual controls come in the form of a long J-neck control stick, rudder pedals, and a single-lever braking system to the left of the pilot seat. The throttle is also on the left and is made prominent on the prototype by a small golf-ball-shaped handle that sits atop the lever. The front seat offers minimal protection from the elements with a small windscreen that does keep the worst of the breeze out of your face.

There is some notable down thrust evident in full-power operations that will require initiating a positive rotation until you get to a much higher than normal light-off speeds. Lift-off at about 35 mph and 350 feet.

Engine: Rotax 582, 65 hp
Max speed: 100mph
Cruise speed: 70 mph
Stall: 30 mph
ROC:700 fpm
Takeoff distance: 90 ft.
Landing dist: 150 ft
Fuel cap: 9 USG
Empty weight: 483 lb
Gross weight: 1050 lbs
Height: 6 ft
Length: 21 ft
Wing span: 26 ft
Wing area: 137 sq.ft.
Seats: 2
Undercarriage: tricycle

Blue Yonder EZ Flyer
Engine: Rotax 503, 52 hp
HP range: 50-74.
Speed max: 100 mph
Cruise: 65 mph.
Stall: 30 mph
ROC: 650 fpm.
Take-off dist: 90 ft
Landing dist: 150 ft.
Fuel cap: 9 USG
Weight empty: 469 lbs.
Gross: 1050 lbs
Height: 6 ft.
Length: 21 ft
Wing span: 26 ft.
Wing area: 137 sq.ft
Seats: 2 tandem.
Landing gear: nose wheel.

Blue Yonder EZ Flyer
Engine: Rotax 582, 65 hp
HP range: 50-130.
Cruise: 70 mph.
Stall: 35 mph
ROC: 700 fpm.
Take-off dist: 100 ft
Landing dist: 175 ft.
Fuel cap: 24 USG
Weight empty: 535 lbs.
Gross: 1300 lbs
Length: 21 ft
Wing span: 31 ft.
Wing area: 176 sq.ft
Seats: 2 tandem.
Landing gear: nose wheel.

Merlin Explorer

A four seat kit aircraft. Kit deliveries were planned for Spring 1996.

Engine: Lycoming IO-360, 180 hp
HP range: 180-250
Est. Speed max: 135 mph
Cruise: 115 mph
Stall: 35 mph
ROC: 1500 fpm
Take-off dist: 400 ft
Landing dist: 400 ft
Fuel cap: 72 USG
Weight empty: 1480 lb
Gross: 3000 lb
Wing span: 39 ft
Wing area: 210 sq.ft
Seats: 4
Landing gear: tail wheel

Merlin Aircraft Inc

Made kits available to construct the Merlin GT-582 two-seat monoplane, originally developed in Canada as the Macair Merlin.

1996: 509 Airport Rd, Muskegon, MI 49441, USA.
The company closed due to financial difficulty.
The designs were being produced by Blue Yonder Aviation, Inc., and one is also available from AeroComp Inc.

Merkel Mark II

This two-seat aerobatic biplane is stressed to a +6G and -3G limit, and +9G to -4.5G ultimate. It was first flown in 1973, and its designer, Edwin Merkel, planned to produce the biplane in a two-seater trainer version and a single-place competition model. The Mark II is completely covered with a light alloy skin outside, and underneath the fuselage is welded steel tube while the wings feature a single-spar tor¬sional structure. Other extras include an antiservo tab, ground-adjustable trim tab and optional cockpit canopy.

Gross Wt. 1540 lb
Empty Wt. 1200 lb
Fuel capacity 18 USG
Wingspan 25’6”
Length 22’9”
Engine 220-hp Franklin
Top speed 206 mph
Cruise mph 160
Stall 55 mph
Climb rate 2500 fpm
Takeoff run 300 ft
Landing roll 300 ft
Range 250 miles

Meridionali-Aerfer Spa

Meridionali-Aerfer Spa succeeded Societa Aninima Industrie Aeronautiche Romeo, which had been formed in 1934 to absorb Officine Ferroviarie Meridionali’s aviation activities. Became part of Societa Italiana Ernesto Breda group. Developed Ro.37 two-seat reconnaissance biplane which served October 1936 with Italian Aviacion Legionaria during Spanish Civil War and equipped Italian Air Force reconnaissance units during Second World War. Also used operationally were Ro.43 two-seat, single-float catapult seaplane and single-seat fighter version, Ro.44.