Micco SP26

Micco has gotten FAA approval for its SP26 two-seat taildragger, a re-engined version of the company’s SP20. Both airplanes are modern versions of the Meyers 145, designed in the 1940s.
The price in 1999 was US$199,500. The SP-26A sold for $329,000

Micco SP26
Engine: Lycoming IO-540-T4B5, 260 hp@2700@SL
TBO: 2000 hr
Fuel type: 100/100LL
Propeller: Hartzell CS/78 in
Landing gear type: Conv./Retr.
Max ramp weight: 2850 lb
Gross weight: 2850 lb
Landing weight: 2680 lb
Empty weight, std: 2040 lb
Useful load, std: 810 lb
Payload, full std. fuel: 402 lb
Usable fuel, std: 68 USG
Oil capacity: 8 qts
Wingspan: 30 ft. 4 in
Overall length: 24 ft. 1 in
Height: 6 ft. 6in
Wing area:156.6 sq. ft
Wing loading: 18.2 lbs./sq. ft
Power loading: 10.9 lbs./hp
Wheel base: 10 ft. 4 in.
Wheel size: 6.00 x 6 in
Seating capacity: 2
Cabin width: 43 in
Cabin height: 39 in
Baggage capacity: 100 lb /14 cu.ft
G-limits: +6/-3
Cruise speed 75% power @ 6,500 ft.: 155 kt
Max range (w/ reserve) 75% power: 800 nm
Max range (w/ reserve) 55% power: 1040 nm
Stall speed (gear, flaps up): 55 kt
Stall speed (gear, flaps down): 49 kt
Best rate of climb (SL): 1500 fpm
Service ceiling: 18,000 ft
Takeoff ground roll: 800 ft
Takeoff over 50-ft. obstacle: 1100 ft
Landing ground roll: 700 ft
Landing over 50-ft. obstacle: 2000 ft

Micco SP26A
Engine: Lycoming IO-540-T4B5, 260 hp@2700rpm@SL
TBO: 2000 hr
Fuel type: 100/100LL
Propeller type: Hartzell 3-blade, 78 in
Landing gear type: Conv./Retr
Max ramp weight: 2850 lb
Gross weight: 2850 lb
Landing weight: 2850 lb
Empty weight, std: 2040 lb
Useful load: 810 lb
Useful fuel: 96 USG
Payload: 402 lb
Oil capacity: 12 qts
Wingspan: 30 ft. 4 in
Overall length: 24 ft. 1 in
Height: 6 ft. 6 in
Wing area: 156 sq. ft
Wing Loading: 15.6 lbs./sq.ft
Power loading: 10.9 lbs./hp
Seating capacity: 2
Cabin width: 43 in
Cabin height: 39 in
Baggage capacity: 100 lb
Cruise speed 75% power: 155 kt
Fuel consumption 75% power: 14.3 USG/hr
Fuel consumption 65% power:12.4 USG/hr
Max range 75% power: 800 nm
Max range 55% power: 1040 nm
Vso: 49 kt
Best rate of climb, SL: 1500 fpm
Service ceiling: 14,000 ft
Takeoff ground roll: 800 ft
Takeoff over 50 ft. obstacle: 1100 ft
Landing ground roll: 700 ft
Landing over 50 ft. obstacle: 1600 ft

Micco SP20

A modern versions of the Meyers 145, designed in the 1940s.

1999 SP20
Engine: Lycoming IO-360-C1E6, 200 hp
TBO: 2000 hr
Propeller: Const. spd.
Landing gear type: Conv./Retr.
Gross weight: 2600 lb
Empty weight, std: 1800 lb
Useful load, std: 800 lb
Fuel capacity: 73 USG
Wingspan: 30 ft. 4 in
Overall length: 24 ft. 1 in
Height: 6 ft. 6 in
Wing area:156.6 sq. ft
Seating capacity: 2
Cabin width: 43 in
Cabin height: 39 in
Baggage capacity: 100 lb
Cruise speed 75% power: 140 kt
Cruise speed 65% power: 133 kt
Max range (w/ reserve) 75% power: 800 nm
Max range (w/ reserve) 65% power: 920 nm
Fuel consumption 75% power: 10.5 USgph
Fuel consumption 65% power: 9.1 USgph
Stall speed (gear, flaps down): 43 kt
Best rate of climb: 950 fpm
Service ceiling: 12,000 ft
Takeoff ground roll: 600 ft
Landing ground roll: 700 ft

Miami Aircraft MM-200 Miami Maid / MM-201 Miami Maid

MM-200

The five-seat amphibian monoplane MM-200 Miami Maid appeared in 1928 or 1929 with a 230 hp Menasco-Salmson B-2 radial engine pusher mounted on top of the wing, and registered NC619. The design combined an all-wood Fokker cantilevered wing with the wooden hull of a Curtiss F boat.

A second aircraft, the MM-201 registered NC178N, was modified in 1930 for installation of a 300 hp Wright R-975 Whirlwind engine.

MM-200
Engine: Menasco-Salmson B-2, 230 hp
Wingspan: 44 ft
Length: 33 ft
Useful load: 1250 lb
Top speed: 120 mph
Cruise speed: 100 mph
Range at cruise: 500 mi

Meyers Orbit Air

1990

David Meyers began development of a single seat ring design called Orbit Air in 1988 and obtained a patent for it in 1991. Orbit Air began as an unpowered craft in 1990 as it was tested by being towed down the runway to evaluate the wing’s stability and lift. Various follow-on testing programs have resulted in five configuration changes.

Changes included fitting a 40 hp Kawasaki 440 engine with a three blade, 62 inch propeller in both tractor and pusher positions. The down angled ring wing has also been moved to an up-tilt position, the cockpit area was reworked, and the tail surfaces and landing gear were redesigned.

1994

The primary structure is a 6061-T6 aluminium structure, but the wing and control surfaces are Stits PolyFiber covered wood. The wing employs leading and trailing edge spars that are 1.125 inch in diameter with 30 built-up quarter inch fir and mahogany plywood ribs. It is canted upward 15 degrees with a 12 foot span and a maximum chord of four foot 5 inches (in the 1995 configuration). Wing area is 100 sq.ft. Ailerons of five foot span and 9 inch chord are fitted within the wing just forward of the propeller.

Version 5

An elevator is installed in the trailing edge of the wing under a 4.5 foot rudder. The seat is a weight shift type.

Version 5

Orbit Air is 21 feet long and 7 feet high. Flight tests were only short hops to 100 ft altitude down a 3100 ft runway. Meyers claims that the airplane will take-off at 40 mph, cruise at a maximum 55 mph, and stall at 30-35 mph. Development and testing were continuing.

Meyers Little Toot

George W. Meyer was already a well known craftsman and model airplane builder prior to his full size project. He started the Little Toot by drawing it in ½ inch to the foot scaled drawings and proceeded to build a metal, 1/24 scale model of his dreams. The model duplicated what he wanted in the full size airplane including a scale metal engine. Many of the building processes were refined in the small model, prior to starting the full size project in 1952.

The full size airplane performed perfectly on the first flight with only a slight adjustment to the rudder trim tab. The first flight was flown on February 2, 1957 in Corpus Christi, Texas. The pilot for the test flight was a great lady pilot by the name of Pauline Glasson.

All the test hours were flown off and the plane came through with flying colours. The plane was fully aerobatic, and had no bad habits in stall or spin type maneuvers. George originally intended for the Toot to be a one of a kind airplane, but the requests for plans soon overwhelmed that decision so he began to produce plans with all of the modifications incorporated into them that he had made during the project.

The Little Toot took the top award from Mechanic Illustrated for “Outstanding Achievement in a Homebuilt Aircraft” at the 1957 EAA convention in Milwaukee. “Little Toot” also won the Paul H. Poberezny Award two years in a row. Year 1999 and 2000.

The single seat fuselage is an all-metal structure with metal-covered steel tube construction from rear of cockpit forward, and metal monocoque rear of tubular fuselage cockpit forward section. Plans also provide you with an alternate full Tube and Fabric fuselage construction.

It features all wood wings, two 1″ thick spar structure with fabric covering, and NACA 2212 wing section, 8 degrees sweepback on the top wing, and 2.5 degrees of dihedral on lower wing. There is 2 degrees incidence on both upper and lower wings. Braced biplane type with Cabane and I-struts. Fabric covered all metal full-length ailerons on lower wings only. No Flaps. Little Toot has a structure stressed to 10- and 10+ G’s

The original was fitted with a Continental 90-hp engine, but power plant options include 4-cylinder engines of up to 200 hp, or six cylinders up to 250 hp. The Little Toot has an eight-degree sweepback on the upper wing. The straight lower wing carries fabric covered, metal, almost full-span ailerons that give the ship an unusually high roll rate. Fiberglass engine cowlings are now available. A baggage compartment is located behind the pilot seat.

There are two tail type options. A cantilever all aluminum structure, or a tubular 4130 chrome-moly steel, fabric covered. Both have a trim tab in the port elevator. The main gear is fixed cantilever spring steel from Cessna 140/120, or new aluminum gear with integrated brake line, and a steerable tailwheel.

Jan 65

Wing span (both): 19 ft in
Fuselage length: 16 ft 6 in
Total height: 7 ft
Weight empty: 914 lb
Gross weight: 1320 lb
Max wing loading: 10 lb/sq foot
Max power loading: 13.7 lb/sq foot
Fuselage fuel tank: 19 USG
Opt. wing fuel tanks: 18 USG
Total fuel capacity: 37 USG
Roll rate: 120 deg/sec
Vne: 200 Mph
V2min (min takeoff speed): 65 mph
VFTO (Final takeoff speed): 70 mph
VC (most efficient cruising speed): 125 mph
VD (design diving speed): 200 mph
VDF (demonstrated flight diving speed): 160 to 180 mph in aerobatic configuration
VFC (Max speed for stability characteristics): 90 mph
VH (Max speed in level flight at max power): 138 mph
VLOF (Lift-off speed): 55-60 mph
VMC (Minimum control speed in flight): 48 mph
Vmcg (Minimum control speed on the ground): 40 mph
VMO (Maximum operating limit speed): 180 mph
VNO (Maximum structural cruising speed): 138 mph
VR (Rotation speed): 60 mph
VRef (Landing reference speed): 70 mph
VSO (Power off stall speed): 48 mph
VY (Best rate of climb): 100 mph
Max speed at sea level 125 hp: 135 mph
Max speed at sea level 150 hp: 150 mph
Max speed at sea level 180 hp: 165 mph
Normal cruising speed 125 hp: 125 mph
Normal cruising speed 150 hp: 135 mph
Normal cruising speed 180 hp: 145 mph
Max rate of climb 125 hp: 1600 fpm
Max rate of climb 150 hp: 2000 fpm
Max rate of climb 180 hp: 2150 fpm
Range (Standard with wing tanks)125 hp: 260 sm
Range (Standard with wing tanks)150 hp: 240 sm
Range (Standard with wing tanks)180 hp: 220 sm

Meyers MAC 125 / MAC 145

MAC 145

Postwar production included MAC 125 and MAC 145 two-seat cabin monoplanes with Continental engines.

The MAC 145, introduced in 1948, is a higher-powered development of the MAC 125-C, the first post-war design of Meyers Aircraft Company. The MAC 145 differs in having a 145 hp Continental C145-2H engine.

Both were side-by-side two-seat cabin monoplane of all metal construction. A small series of MAC 145 were built.

The MAC 125 and MAC 145 developed into the Micco SP 20 and SP 26.

MAX 125
Engine: 125 hp Continental C125
Seats: 2

MAC 145
Engine: 145 hp Continental C145-2H
Wingspan: 30 ft
Wing area: 149 sq.ft
Length: 21 ft 4 in
Height: 8 ft 6 in
Empty weight: 1135 lb
Loaded weight: 1735 lb
Max speed: 166 mph
Cruise: 145 mph
ROC: 950 fpm
Service ceiling: 18,000 ft
Range: 600 mi
Seats: 2