Thatcher CX4

The CX4 is a low wing, single-seat aircraft designed to be simple to build and safe to fly. The name of the plane, CX4, is taken from an old radio show featuring Hop Harrigan, whose plane was called CX4.

The aircraft is all metal, 6061-T6 aluminium, except the cowling. It has hydraulic disc toe brakes and a heater and ventilation system for all season flying. The aircraft can be built with an optional 3 gal aux fuel tank. The CX4’s standard specified powerplant is a Volkswagen air cooled engine. The design load factor is 3.8 g, with an ultimate load of 5.7 g

The CX4 first flew in 2004. At the end of 2010, there were eighteen flying CX4s in the United States and South Africa. Parts and kits are currently supplied by Peter Beck.

Gallery

Powerplant: 1 × Volkswagen
Length: 18 ft 3 in (5.56 m)
Wingspan: 24 ft (7.3 m)
Height: 4 ft 8 in (1.42 m)
Wing area: 48 sq ft (4.5 sq.m)
Empty weight: 520 lb (236 kg)
Gross weight: 850 lb (386 kg)
Cruise speed: 109 kn; 201 km/h (125 mph)
Stall speed: 35 kph 64 km/h (40 mph)
Never exceed speed: 135 kn; 249 km/h (155 mph)
Service ceiling: 10,000 ft (3,000 m)
Rate of climb: 825 ft/min (4.19 m/s)
Crew: 1

Thalman T-4

Thalman T-4 N53389

In 1949, Harry formed Thalman Aircraft Inc. at Salt Lake City. In the same year, he designed the Talman T-4 which, flew in 1951. The 1953 Thalman T-4 was a four-pace mid-wing cabin monoplane of all-wood geodetic construction. The T-4 followed the same wooden geodetic construction employed by Harry J. Thalman and William Earl Player when they helped form Plxweve Aircraft. (Construction techniques followed those of Thalman’s Oregonian mentor, George Yates – bending strips of cedar around heated former moulds.) In general construction technique, the T-3 and T-4 were similar – the T-3 being fabric-covered, the T-4 having a fibreglass covering.

Designed by Harry J. Thalman, the one built, N53389, had manually retracting undercarriage. Initially powered by a 135hp Lycoming O-290, it was later converted to T-tail with a 170hp O-340.

Convinced that serial wooden geodetic construction would be less expensive than by-then conventional metal construction, Thalman spent the next decade trying to get the T-4 into production. At one point, Thalman approached the Cache Chamber of Commerce in Utah for start-up funds of $50,000 (and a suitable workspace) to launch T-4 production – presumably near Logan, UT. The Chamber passed.

By 1960, Thalman Aircraft Corp. was doing business as Thalman Industries (sometimes given as Thalman Aircraft Industries). However, the firm was now planning to relocate to Roseburg, OR – 900 miles to the west. Roseburg businessman Lynn Andreas had become president and it was Andreas who was announcing the construction of a new factory on 5 acres of leased land at the Roseburg municipal airport. Early reports said that site ground preparation work had begun and that a “plywood plane” would be built. Harry Thalman is quoted, saying that his aircraft will sell for less than $14,000.

By 1963, Harry Thalman was working as a mechanic for Kelsey-Ellis Air Service at Salt Lake City Airport. The T-4 was in storage (and possibly disassembled by then) but Harry was still flying the T-3B. On 15 March 1963, Harry was doing flying cross-country when he flew into a blinding snowstorm. Harry Thalman died instantly when he crashed his T-3B monoplane in a gully outside of Grantsville, UT.

Engine: 135hp Lycoming O-290, later 170 hp Lycoming O-340
Wingspan: 40 ft 2.5 in
Length: 21 ft 6 in
Height: 6 ft 0 in
Empty weight: 1050 lb
MTOW: 2000 lb
Useful load: 1050 lb
Max speed: 175 mph
Cruise: 155 mph
Stall: 45 mph
Range: 700 mi
Seats: 4
Undercarriage: manual retractable

Thalman T-3

Thalman T-3B NX28374

The 1941 T-3B was a single-place cabin monoplane of fabric-covered wood geodetic construction by Harry J. Thalman. One was built, registered NX28374.

The T-3B was a revised airframe with a T-tail and spats fitted to main wheels.

Engine: Velie M-5, 55hp
Wingspan: 41’0″
Max speed: 130 mph
Cruise: 120 mph
Stall: 38 mph
Seats: 1

Thalman-T-3B

Thalman, Harry J

Harry J. Thalman: born 25 March 1911 at Challis, Idaho, USA.

George Yates of Beaverton, Oregon had been the mentor of Harry J. Thalman’s designs, Yates had been wooden geodetic construction pioneer, Thalman made several trips from Salt Lake City to Beaverton to learn about geodetic construction techniques from from Yates.

Thalman and Player were joined by a third geodetic aircraft builder – John Greenleaf of Portland, OR, to form the Plxweve Aircraft Company in 1940. Greenleaf then arranged financing through Ralph Hemphill of Los Angeles. As a result, the Plxweve Aircraft Co. became a division of another Hemphill-controlled firm – Aero Industries Technical Institute, Incorporated (Aero ITI). Ralph Hemphill became President of the Plexweve division but refused further investment. The money was run through quickly and much legal wrangling ensued.

The T-3 had first flown in 1941

At some point, the partners went their separate ways. In 1949, Harry formed Thalman Aircraft Inc. at Salt Lake City. In the same year, he designed the Talman T-4 which, flew in 1951.

By 1957 Thalman Aircraft Corp. had relocated to Mount Pleasant, UT, with plans to establish T-4 production there. In a letter to Flying Magazine (March 1957, pages 6 & 8), Mount Pleasant resident Rex C. Staker writes that the production T-4 was to be offered with 150-, 170-, or 180 hp engines. According to Aerofiles, Thalman Aircraft also took over a concept from Van Nuys-based ATS (Aircraft Technical Services Inc., Floyd E. Snow) in 1959. That ATS design was described as a 4-place mid-winged cabin monoplane (“reportedly 50 percent complete”).Thalman Aircraft then began reworking this laminar-flow winged design as a “twin-engine development”.

By 1960, Thalman Aircraft Corp. was doing business as Thalman Industries (sometimes given as Thalman Aircraft Industries). However, the firm was now planning to relocate to Roseburg, OR – 900 miles to the west. Roseburg businessman Lynn Andreas had become president and it was Andreas who was announcing the construction of a new factory on 5 acres of leased land at the Roseburg municipal airport. Early reports said that site ground preparation work had begun and that a “plywood plane” would be built. Harry Thalman is quoted, saying that his aircraft will sell for less than $14,000.

According to local media reports, the production type’s structure – under its fiberglass shell – would be an aluminum honeycomb. That jives with an article in Sport Aviation August 1961 – Geodetic Aircraft Structure by Keith D. Powell, EAA. On page 22, Powell writes that Thalman was “now working on another midwing featuring a plastic bonded honeycomb sandwich airframe.” Reportedly, circa 1958, Harry began losing interest in geodetic structures. Lynn Andreas was also president of the Oregon Red Cedar Co.

Contemporary reports say that Thalman was “working on a fifth model which will include a number of modifications, such as a more powerful motor, sweptback tail assembly, and electrically-operated landing gear and flaps.” These all sound like sensible updated for a production variant. But the The News-Review report says that an “all-hydraulic retractable landing gear” was to equip the production type. Needless to say, that Roseburg factory never materialized. In the early ’60s, some airport was holding the parked Thalman T-4 until storage fees in the order of $800 were paid.

By 1963, Harry Thalman was working as a mechanic for Kelsey-Ellis Air Service at Salt Lake City Airport. The T-4 was in storage (and possibly disassembled by then) but Harry was still flying the T-3B. On 15 March 1963, Harry was doing flying cross-country when he flew into a blinding snowstorm. Harry Thalman died instantly when he crashed his T-3B monoplane in a gully outside of Grantsville, UT.

Harry J. Thalman: died 15 March 1963.

Thalhofer Bronco

Single seat single engined high wing mono¬plane with conventional three axis control. Wing has unswept leading and trailing edges, and constant chord; conventional tail. Pitch control by elevator on tail; yaw control by fin mounted rudder; roll control by half span ailerons; control inputs through stick for pitch/roll and pedals for yaw. Wing braced from below by struts; wing profile Worth¬mann FX63 137; double surface. Undercar¬riage has three wheels in tricycle formation with additional tailskid; suspension on all wheels. Push right go right nose¬wheel steering connected to yaw control. No brakes. Aluminium tube framework, without pod. Engine mounted below wing driving pusher propeller.

An important manufactur¬er of hang gliders, producing around 300 of these aircraft per year, Thalhofer produced its first microlight in 1976. Two prototypes of the Bronco were built and flew for the first time at the end of March 1983. Production got under way in 1983, after the certification of the model.

Length overall 18.7ft, 5.70m
Wing span 28.5 ft, 8.70 m
Constant chord 3.9 ft, 1.20 m
Sweepback 0 deg
Tailplane span 5.2ft, 1.60 m
Total wing area 114 sq.ft, 10.6 sq.m
Total aileron area 6.9 sq.ft, 0. 64 sq.m
Total fin and rudder area 16.4 sq.ft, 1.52 sq.m
Total tailplane and elevator area 17.2 sq.ft, 1.60 sq.m
Wing aspect ratio 7.1/1
Wheel track 5.9 ft, 1.80 m
Engine: Konig SC430, 25hp at 4200rpm
Propeller diameter 55 inch, 1.40 m
Belt reduction, ratio 1.8/1
Max static thrust 132 lb, 60 kg
Power per unit area 0.22 hp/sq.ft, 2.4 hp/sq.m
Fuel capacity 5.3 US gal, 4.4 Imp gal, 20.0 litre
Empty weight 221 lb, 100 kg
Max take off weight 486 lb, 220 kg
Payload 265 lb, 120 kg
Max wing loading 4.24 lb/sq.ft, 20.7 kg/sq.m
Max power loading 19.4 lb/hp, 8.8 kg/hp
Load factors; +6.0, 3.0 ultimate
Max cruising speed 59 mph, 95 kph
Economic cruising speed 40mph, 65kph
Stalling speed 24mph, 40 kph
Max climb rate at sea level 400 ft/min, 2.0 m/s
Take off distance 165 ft, 50 m
Land¬ing distance 100 ft, 30 m

Thaden T-1 / Argonaut

Thaden T-1 NX3902

The 1928 Thaden T-1, or Argonaut, (ATC 2-29) was designed by Herbert von Thaden, registered NX3902, and first flew on 15 January 1928, piloted by George R Pond. The only one built crash-landed on 30 March 1933 in Chitkina AK., was recovered in 1988 and restored by an EAA group.

Engine: P&W Wasp A, 400-420hp
Wingspan: 53’0″
Length: 35’3″
Useful load: 2200 lb
Max speed: 135 mph
Cruise speed: 105 mph
Stall: 52 mph
Seats: 6-8

Thaden Metal Aircraft Co

1928: (Herbert von) Thaden Metal Aircraft Co,
Oakland Airport
USA
and
San Francisco CA
USA

1928:
1625 Island Ave,
Pittsburgh PA.
USA

Pittsburgh Metal Airplane Co Formed in 1929 to take over the San Francisco-based Thaden Metal Aircraft Company, which had built the Thaden T-4 four-seat all-metal monoplane, powered by a Wright Whirlwind engine.